aircraft description - aso · " deral aviali ~n i\jmi nistr~tl on and is approve d fo r return...
TRANSCRIPT
AIRCRAFT DESCRIPTION
4oj l AC TURER BEECH AIRCRAFT COSp MODEl_-----tr~gtL5~H~------------
i II I NUMBER CI pound j II REGISTRATION NUMBER I v --d77 i1 i I n lED OWNER ___________________________________--l
m ET ADDRESS -----------------------------------J
I Y STATE ZIP __________________________________~
HA TOR ________________________________________~
REET ADDRESS ___________________________________-J
( ITY STATE ZIP ___________________________________~
( ISTERED OWNER -------------------------------------l
STREET ADDRESS ___________________________________~
_ CI TY STATE ZIP _________________________________--
illERATOR _____________
___ STREET ADDRESS ________________________________~
Inspection t Sta us
D [Check one]
FAR 91169 ANNUAl100 HOUR
D FAR 9171 PROGRESSIVE
D FAR 91217 SUBPART D
D FAR 13560 A LeO
D OTHER
DATEENTERED _____________
CITY STATE
MAINTENANCE RESPONSIBILITY
ALTIMETER amp STATIC SYSTEM CHECKS FAR91170
RECHECK APPROVED BY DA TE MANUFACTURER MODEL SERIAL NO LOCATION MAX ALT REQUIRED AGENCY CERT NO
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ALTIMETER amp STATIC SYSTEM CHECKS FAR91170
APPROVED BY AGENCY CER T NO
RADIO amp ELECTRONIC CHECKS TOTAL EQUIPMENT TYPE OF ERROR OR NE XT CHECK CHECKED BY
DATE TIME CHECKED CHECK RESUl TS DUE SIGNATURE - CERT NO
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RADIO amp ELECTRONIC CHECKS
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TYPE OF NE XT C HECK
DATE TOTAL EQUIPMENT ERROR OR CHECKED BY TIME C HECKED CHECK RESULTS DUE i SIGNATURE - CERT NO
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r1 IIts ) 7 This aircrafi and o r camp nent identified a bove I
w~ rapJlrp d and il lspect cJ ill accorual1ce with c~ ~a~ lt~i u ll~ ~ ~
(drre n jprj ~ra i iJ ir r( ~ r1 I in -I W~ I n airvI)rthy ( return to ~er IU P rtlqrnl deld ii
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s1middot ~ I r i r AVJOnlC ~Cf I Ce S Int eflH-l ti onaL I n
4317 Maher Street Laredo Texas 78041 (956) 72S-8898
CRS S78R1SIN Date shJIO N jO L-ff1
AlC po 3 31
FAR 91413 SIN eli -111
1 certify that the ATC xansponder test and inspection required by FAR 91413 have been perforrned on 512~f to The II1tergrated system test and Inspection was preformed on 51-lt ( IV _
I Transponder Model ( rx -3 -~7 SIN g5 ZO-)
2_ Transponder Model ___-tshy_____ SIN =
I
SS _-0 50 Ii Work Order No 1LD ASI-14
Avionics Se~i~es T~te~-on l Inc 4317 Maher Street Laredo Texas 78041
(956) 725-8898 CRS S78R151N
Date sh-lUo N3Q314 AIC poundgt 3 It
fAR94 SIN (G-(III
I certify that the altimeter and reporting equipment test and inspections required by FAR 91411 have been performed_ The left altimeter PIN fLU - (7---6shy SIN i-r5pound 00 was tested to 2 5 _ODO feet on 50--110 _The right altimeter P(N__~~-_____ SIN -7 - was tested to -t - feet on______ The static system was tested on 51) 0 Tile automatic pressure reporting system was tested on 5)4110
Work Order No )1 til Signature ----d Date 5 Jut() ASlLt - - shy- shy-shy
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RADIO amp ELECTRONIC CHECKS DATE TOTAL
TIME EQUIPMENT
CHECKED TYPE OF CHECK
ERROR OR RESUL TS
N- 3034 4 EM 118
CHECKED BY SIGNATURE - CERT NO
3-3 - 90
T or~ue d all wing bolts as per Beech Man ua l See work order 14171 for deta i ls
I ( o~
MAINTENANCE RECORD FAR439
DATE OF COMPLETION
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AIRCRAFT TIME IN SERVICE
2-29-93
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NO WORK PERFORMED RETURNED TO SERVI( I
MAINTENANCE RECORD FAR439
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AIRCRAFT TIME IN SERVICE
DATE OF COMPLETION
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AIRCRAFT TIME IN SERVICE
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MAINTENANCE RECORD FAR439
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MAINTENANCE RECORD FAR439
DATE OF I OM PLETION
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MAINTENANCE RECORD
) SERVICfULTIMATE ENGINES INC b
Mena Arkansas 71953 501394-5422
52603 W O 96167october 24 1996 Tach Time Date C E- 1111Reg N30344 Ae sn
On this date the following items were accomplished
1 RampR fue l cap 0 ring s pn MS29513-338 2ea 2 RampR uplock block springs pn 1 00942C0020-31 2ea
3 RampR cabin door seal
4 I
--L---~~----L-~~c--___
ULTIMATE E N GINES P O Box B O~)
Mcn a Ark ansa s ( I 50 1 - 394 -542
PETER J LO BELLO AP7354 The aircraft engine or appliance identified and inspected in accordance with curren Federal Aviation Administration and is ap service Pert inent detai ls of Ihe repair are
Dale c 7~[ - l or p y--~-
Signed -I- ~-lto- A zgt-l JU- shy
Jl TIMATE ENGINES ~ R S YCTR973K
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NOhAT E OF AIRCRAFT TIME DESCRIPTION OF WORK PERFORMED I MPLE TION IN SERVICE OR APPROVED OAT A USED WORK PERFORMEDRETURNED TO SE IlVI I
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
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1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
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CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
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INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
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DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
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11
INSPECTION RECORD FAR4311-91217
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JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
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1
II
INSPECTION RECORD r- r- -IIl n
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JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
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The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
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Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
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I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
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Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
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I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
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Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
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MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
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INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
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ALTIMETER amp STATIC SYSTEM CHECKS FAR91170
RECHECK APPROVED BY DA TE MANUFACTURER MODEL SERIAL NO LOCATION MAX ALT REQUIRED AGENCY CERT NO
Tsss i Rc~lred By
RH Air
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ALTIMETER amp STATIC SYSTEM CHECKS FAR91170
APPROVED BY AGENCY CER T NO
RADIO amp ELECTRONIC CHECKS TOTAL EQUIPMENT TYPE OF ERROR OR NE XT CHECK CHECKED BY
DATE TIME CHECKED CHECK RESUl TS DUE SIGNATURE - CERT NO
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RADIO amp ELECTRONIC CHECKS
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TYPE OF NE XT C HECK
DATE TOTAL EQUIPMENT ERROR OR CHECKED BY TIME C HECKED CHECK RESULTS DUE i SIGNATURE - CERT NO
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I N Iigt tltJ rl) c (= 5 t( Erh AkJv ~ jKJ5 JJ A lAND p tlt I rJ(- i-ltFc 66 I ) ( fJ I~J r ltv TPrn ~ Se I (J gt j) Ale D (u r ~ r3 ~I- -r J -3 ) 1-0 l2 vlS
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r1 IIts ) 7 This aircrafi and o r camp nent identified a bove I
w~ rapJlrp d and il lspect cJ ill accorual1ce with c~ ~a~ lt~i u ll~ ~ ~
(drre n jprj ~ra i iJ ir r( ~ r1 I in -I W~ I n airvI)rthy ( return to ~er IU P rtlqrnl deld ii
c ~lrnalur~middot jf AUtilOnOJ( lMvltIuJI
of I h p rr-n ai nn fi legt th - - LA AI IJNl l ~ INC I (h3(JR 2 4Y
I 422S ~HUCI YEAgt - BATON OUGE LA 7080~
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4317 Maher Street Laredo Texas 78041 (956) 72S-8898
CRS S78R1SIN Date shJIO N jO L-ff1
AlC po 3 31
FAR 91413 SIN eli -111
1 certify that the ATC xansponder test and inspection required by FAR 91413 have been perforrned on 512~f to The II1tergrated system test and Inspection was preformed on 51-lt ( IV _
I Transponder Model ( rx -3 -~7 SIN g5 ZO-)
2_ Transponder Model ___-tshy_____ SIN =
I
SS _-0 50 Ii Work Order No 1LD ASI-14
Avionics Se~i~es T~te~-on l Inc 4317 Maher Street Laredo Texas 78041
(956) 725-8898 CRS S78R151N
Date sh-lUo N3Q314 AIC poundgt 3 It
fAR94 SIN (G-(III
I certify that the altimeter and reporting equipment test and inspections required by FAR 91411 have been performed_ The left altimeter PIN fLU - (7---6shy SIN i-r5pound 00 was tested to 2 5 _ODO feet on 50--110 _The right altimeter P(N__~~-_____ SIN -7 - was tested to -t - feet on______ The static system was tested on 51) 0 Tile automatic pressure reporting system was tested on 5)4110
Work Order No )1 til Signature ----d Date 5 Jut() ASlLt - - shy- shy-shy
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RADIO amp ELECTRONIC CHECKS DATE TOTAL
TIME EQUIPMENT
CHECKED TYPE OF CHECK
ERROR OR RESUL TS
N- 3034 4 EM 118
CHECKED BY SIGNATURE - CERT NO
3-3 - 90
T or~ue d all wing bolts as per Beech Man ua l See work order 14171 for deta i ls
I ( o~
MAINTENANCE RECORD FAR439
DATE OF COMPLETION
l shy S - 9~
AIRCRAFT TIME IN SERVICE
2-29-93
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NO WORK PERFORMED RETURNED TO SERVI( I
MAINTENANCE RECORD FAR439
3shy
AIRCRAFT TIME IN SERVICE
DATE OF COMPLETION
r-shy
AIRCRAFT TIME IN SERVICE
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MAINTENANCE RECORD FAR439
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MAINTENANCE RECORD FAR439
DATE OF I OM PLETION
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MAINTENANCE RECORD
) SERVICfULTIMATE ENGINES INC b
Mena Arkansas 71953 501394-5422
52603 W O 96167october 24 1996 Tach Time Date C E- 1111Reg N30344 Ae sn
On this date the following items were accomplished
1 RampR fue l cap 0 ring s pn MS29513-338 2ea 2 RampR uplock block springs pn 1 00942C0020-31 2ea
3 RampR cabin door seal
4 I
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ULTIMATE E N GINES P O Box B O~)
Mcn a Ark ansa s ( I 50 1 - 394 -542
PETER J LO BELLO AP7354 The aircraft engine or appliance identified and inspected in accordance with curren Federal Aviation Administration and is ap service Pert inent detai ls of Ihe repair are
Dale c 7~[ - l or p y--~-
Signed -I- ~-lto- A zgt-l JU- shy
Jl TIMATE ENGINES ~ R S YCTR973K
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NOhAT E OF AIRCRAFT TIME DESCRIPTION OF WORK PERFORMED I MPLE TION IN SERVICE OR APPROVED OAT A USED WORK PERFORMEDRETURNED TO SE IlVI I
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
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1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
l~ I3d-shy
CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
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INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
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11
INSPECTION RECORD FAR4311-91217
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JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
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1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
ALTIMETER amp STATIC SYSTEM CHECKS FAR91170
APPROVED BY AGENCY CER T NO
RADIO amp ELECTRONIC CHECKS TOTAL EQUIPMENT TYPE OF ERROR OR NE XT CHECK CHECKED BY
DATE TIME CHECKED CHECK RESUl TS DUE SIGNATURE - CERT NO
I
i
J
RADIO amp ELECTRONIC CHECKS
shy
TYPE OF NE XT C HECK
DATE TOTAL EQUIPMENT ERROR OR CHECKED BY TIME C HECKED CHECK RESULTS DUE i SIGNATURE - CERT NO
~ ~ ) RI I IJjq heuro(n b e ) P 11 oflt I h ~ IA f1 ( (I 1 V JOO cr fJS ltK6lt) lt
f I J J
1ol-D-tV ~ TII) JA L Te) J Cc gt tV~ u (vII (~N 0 --eN5TALi-ei)I
P Non~ h Srppoundlt 1Y13 Po P P Iltct I ~ ch C--fO--Sc-vs reI Ch W~
r C4 1 J LI f Ac ullt e 5 fNsT(2fC- ilt) ~ c A c jII] laquoJ - II~~9A l I
I N Iigt tltJ rl) c (= 5 t( Erh AkJv ~ jKJ5 JJ A lAND p tlt I rJ(- i-ltFc 66 I ) ( fJ I~J r ltv TPrn ~ Se I (J gt j) Ale D (u r ~ r3 ~I- -r J -3 ) 1-0 l2 vlS
~ I- I I
1-6 ~ j)(PiIJt-S I
J ~l middotl I
~ 1 + D n )1 ~~
r1 IIts ) 7 This aircrafi and o r camp nent identified a bove I
w~ rapJlrp d and il lspect cJ ill accorual1ce with c~ ~a~ lt~i u ll~ ~ ~
(drre n jprj ~ra i iJ ir r( ~ r1 I in -I W~ I n airvI)rthy ( return to ~er IU P rtlqrnl deld ii
c ~lrnalur~middot jf AUtilOnOJ( lMvltIuJI
of I h p rr-n ai nn fi legt th - - LA AI IJNl l ~ INC I (h3(JR 2 4Y
I 422S ~HUCI YEAgt - BATON OUGE LA 7080~
~
bull
4
1
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s1middot ~ I r i r AVJOnlC ~Cf I Ce S Int eflH-l ti onaL I n
4317 Maher Street Laredo Texas 78041 (956) 72S-8898
CRS S78R1SIN Date shJIO N jO L-ff1
AlC po 3 31
FAR 91413 SIN eli -111
1 certify that the ATC xansponder test and inspection required by FAR 91413 have been perforrned on 512~f to The II1tergrated system test and Inspection was preformed on 51-lt ( IV _
I Transponder Model ( rx -3 -~7 SIN g5 ZO-)
2_ Transponder Model ___-tshy_____ SIN =
I
SS _-0 50 Ii Work Order No 1LD ASI-14
Avionics Se~i~es T~te~-on l Inc 4317 Maher Street Laredo Texas 78041
(956) 725-8898 CRS S78R151N
Date sh-lUo N3Q314 AIC poundgt 3 It
fAR94 SIN (G-(III
I certify that the altimeter and reporting equipment test and inspections required by FAR 91411 have been performed_ The left altimeter PIN fLU - (7---6shy SIN i-r5pound 00 was tested to 2 5 _ODO feet on 50--110 _The right altimeter P(N__~~-_____ SIN -7 - was tested to -t - feet on______ The static system was tested on 51) 0 Tile automatic pressure reporting system was tested on 5)4110
Work Order No )1 til Signature ----d Date 5 Jut() ASlLt - - shy- shy-shy
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RADIO amp ELECTRONIC CHECKS DATE TOTAL
TIME EQUIPMENT
CHECKED TYPE OF CHECK
ERROR OR RESUL TS
N- 3034 4 EM 118
CHECKED BY SIGNATURE - CERT NO
3-3 - 90
T or~ue d all wing bolts as per Beech Man ua l See work order 14171 for deta i ls
I ( o~
MAINTENANCE RECORD FAR439
DATE OF COMPLETION
l shy S - 9~
AIRCRAFT TIME IN SERVICE
2-29-93
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NO WORK PERFORMED RETURNED TO SERVI( I
MAINTENANCE RECORD FAR439
3shy
AIRCRAFT TIME IN SERVICE
DATE OF COMPLETION
r-shy
AIRCRAFT TIME IN SERVICE
-r~
MAINTENANCE RECORD FAR439
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MAINTENANCE RECORD FAR439
DATE OF I OM PLETION
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MAINTENANCE RECORD
) SERVICfULTIMATE ENGINES INC b
Mena Arkansas 71953 501394-5422
52603 W O 96167october 24 1996 Tach Time Date C E- 1111Reg N30344 Ae sn
On this date the following items were accomplished
1 RampR fue l cap 0 ring s pn MS29513-338 2ea 2 RampR uplock block springs pn 1 00942C0020-31 2ea
3 RampR cabin door seal
4 I
--L---~~----L-~~c--___
ULTIMATE E N GINES P O Box B O~)
Mcn a Ark ansa s ( I 50 1 - 394 -542
PETER J LO BELLO AP7354 The aircraft engine or appliance identified and inspected in accordance with curren Federal Aviation Administration and is ap service Pert inent detai ls of Ihe repair are
Dale c 7~[ - l or p y--~-
Signed -I- ~-lto- A zgt-l JU- shy
Jl TIMATE ENGINES ~ R S YCTR973K
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NOhAT E OF AIRCRAFT TIME DESCRIPTION OF WORK PERFORMED I MPLE TION IN SERVICE OR APPROVED OAT A USED WORK PERFORMEDRETURNED TO SE IlVI I
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
---- shy
1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
l~ I3d-shy
CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
ifYr1 r~JnK
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f- shy
INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
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INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
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RADIO amp ELECTRONIC CHECKS TOTAL EQUIPMENT TYPE OF ERROR OR NE XT CHECK CHECKED BY
DATE TIME CHECKED CHECK RESUl TS DUE SIGNATURE - CERT NO
I
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RADIO amp ELECTRONIC CHECKS
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TYPE OF NE XT C HECK
DATE TOTAL EQUIPMENT ERROR OR CHECKED BY TIME C HECKED CHECK RESULTS DUE i SIGNATURE - CERT NO
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I N Iigt tltJ rl) c (= 5 t( Erh AkJv ~ jKJ5 JJ A lAND p tlt I rJ(- i-ltFc 66 I ) ( fJ I~J r ltv TPrn ~ Se I (J gt j) Ale D (u r ~ r3 ~I- -r J -3 ) 1-0 l2 vlS
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r1 IIts ) 7 This aircrafi and o r camp nent identified a bove I
w~ rapJlrp d and il lspect cJ ill accorual1ce with c~ ~a~ lt~i u ll~ ~ ~
(drre n jprj ~ra i iJ ir r( ~ r1 I in -I W~ I n airvI)rthy ( return to ~er IU P rtlqrnl deld ii
c ~lrnalur~middot jf AUtilOnOJ( lMvltIuJI
of I h p rr-n ai nn fi legt th - - LA AI IJNl l ~ INC I (h3(JR 2 4Y
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4317 Maher Street Laredo Texas 78041 (956) 72S-8898
CRS S78R1SIN Date shJIO N jO L-ff1
AlC po 3 31
FAR 91413 SIN eli -111
1 certify that the ATC xansponder test and inspection required by FAR 91413 have been perforrned on 512~f to The II1tergrated system test and Inspection was preformed on 51-lt ( IV _
I Transponder Model ( rx -3 -~7 SIN g5 ZO-)
2_ Transponder Model ___-tshy_____ SIN =
I
SS _-0 50 Ii Work Order No 1LD ASI-14
Avionics Se~i~es T~te~-on l Inc 4317 Maher Street Laredo Texas 78041
(956) 725-8898 CRS S78R151N
Date sh-lUo N3Q314 AIC poundgt 3 It
fAR94 SIN (G-(III
I certify that the altimeter and reporting equipment test and inspections required by FAR 91411 have been performed_ The left altimeter PIN fLU - (7---6shy SIN i-r5pound 00 was tested to 2 5 _ODO feet on 50--110 _The right altimeter P(N__~~-_____ SIN -7 - was tested to -t - feet on______ The static system was tested on 51) 0 Tile automatic pressure reporting system was tested on 5)4110
Work Order No )1 til Signature ----d Date 5 Jut() ASlLt - - shy- shy-shy
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RADIO amp ELECTRONIC CHECKS DATE TOTAL
TIME EQUIPMENT
CHECKED TYPE OF CHECK
ERROR OR RESUL TS
N- 3034 4 EM 118
CHECKED BY SIGNATURE - CERT NO
3-3 - 90
T or~ue d all wing bolts as per Beech Man ua l See work order 14171 for deta i ls
I ( o~
MAINTENANCE RECORD FAR439
DATE OF COMPLETION
l shy S - 9~
AIRCRAFT TIME IN SERVICE
2-29-93
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NO WORK PERFORMED RETURNED TO SERVI( I
MAINTENANCE RECORD FAR439
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AIRCRAFT TIME IN SERVICE
DATE OF COMPLETION
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AIRCRAFT TIME IN SERVICE
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MAINTENANCE RECORD FAR439
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MAINTENANCE RECORD FAR439
DATE OF I OM PLETION
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MAINTENANCE RECORD
) SERVICfULTIMATE ENGINES INC b
Mena Arkansas 71953 501394-5422
52603 W O 96167october 24 1996 Tach Time Date C E- 1111Reg N30344 Ae sn
On this date the following items were accomplished
1 RampR fue l cap 0 ring s pn MS29513-338 2ea 2 RampR uplock block springs pn 1 00942C0020-31 2ea
3 RampR cabin door seal
4 I
--L---~~----L-~~c--___
ULTIMATE E N GINES P O Box B O~)
Mcn a Ark ansa s ( I 50 1 - 394 -542
PETER J LO BELLO AP7354 The aircraft engine or appliance identified and inspected in accordance with curren Federal Aviation Administration and is ap service Pert inent detai ls of Ihe repair are
Dale c 7~[ - l or p y--~-
Signed -I- ~-lto- A zgt-l JU- shy
Jl TIMATE ENGINES ~ R S YCTR973K
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NOhAT E OF AIRCRAFT TIME DESCRIPTION OF WORK PERFORMED I MPLE TION IN SERVICE OR APPROVED OAT A USED WORK PERFORMEDRETURNED TO SE IlVI I
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
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1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
l~ I3d-shy
CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
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INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
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RADIO amp ELECTRONIC CHECKS
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TYPE OF NE XT C HECK
DATE TOTAL EQUIPMENT ERROR OR CHECKED BY TIME C HECKED CHECK RESULTS DUE i SIGNATURE - CERT NO
~ ~ ) RI I IJjq heuro(n b e ) P 11 oflt I h ~ IA f1 ( (I 1 V JOO cr fJS ltK6lt) lt
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1ol-D-tV ~ TII) JA L Te) J Cc gt tV~ u (vII (~N 0 --eN5TALi-ei)I
P Non~ h Srppoundlt 1Y13 Po P P Iltct I ~ ch C--fO--Sc-vs reI Ch W~
r C4 1 J LI f Ac ullt e 5 fNsT(2fC- ilt) ~ c A c jII] laquoJ - II~~9A l I
I N Iigt tltJ rl) c (= 5 t( Erh AkJv ~ jKJ5 JJ A lAND p tlt I rJ(- i-ltFc 66 I ) ( fJ I~J r ltv TPrn ~ Se I (J gt j) Ale D (u r ~ r3 ~I- -r J -3 ) 1-0 l2 vlS
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r1 IIts ) 7 This aircrafi and o r camp nent identified a bove I
w~ rapJlrp d and il lspect cJ ill accorual1ce with c~ ~a~ lt~i u ll~ ~ ~
(drre n jprj ~ra i iJ ir r( ~ r1 I in -I W~ I n airvI)rthy ( return to ~er IU P rtlqrnl deld ii
c ~lrnalur~middot jf AUtilOnOJ( lMvltIuJI
of I h p rr-n ai nn fi legt th - - LA AI IJNl l ~ INC I (h3(JR 2 4Y
I 422S ~HUCI YEAgt - BATON OUGE LA 7080~
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4317 Maher Street Laredo Texas 78041 (956) 72S-8898
CRS S78R1SIN Date shJIO N jO L-ff1
AlC po 3 31
FAR 91413 SIN eli -111
1 certify that the ATC xansponder test and inspection required by FAR 91413 have been perforrned on 512~f to The II1tergrated system test and Inspection was preformed on 51-lt ( IV _
I Transponder Model ( rx -3 -~7 SIN g5 ZO-)
2_ Transponder Model ___-tshy_____ SIN =
I
SS _-0 50 Ii Work Order No 1LD ASI-14
Avionics Se~i~es T~te~-on l Inc 4317 Maher Street Laredo Texas 78041
(956) 725-8898 CRS S78R151N
Date sh-lUo N3Q314 AIC poundgt 3 It
fAR94 SIN (G-(III
I certify that the altimeter and reporting equipment test and inspections required by FAR 91411 have been performed_ The left altimeter PIN fLU - (7---6shy SIN i-r5pound 00 was tested to 2 5 _ODO feet on 50--110 _The right altimeter P(N__~~-_____ SIN -7 - was tested to -t - feet on______ The static system was tested on 51) 0 Tile automatic pressure reporting system was tested on 5)4110
Work Order No )1 til Signature ----d Date 5 Jut() ASlLt - - shy- shy-shy
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RADIO amp ELECTRONIC CHECKS DATE TOTAL
TIME EQUIPMENT
CHECKED TYPE OF CHECK
ERROR OR RESUL TS
N- 3034 4 EM 118
CHECKED BY SIGNATURE - CERT NO
3-3 - 90
T or~ue d all wing bolts as per Beech Man ua l See work order 14171 for deta i ls
I ( o~
MAINTENANCE RECORD FAR439
DATE OF COMPLETION
l shy S - 9~
AIRCRAFT TIME IN SERVICE
2-29-93
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NO WORK PERFORMED RETURNED TO SERVI( I
MAINTENANCE RECORD FAR439
3shy
AIRCRAFT TIME IN SERVICE
DATE OF COMPLETION
r-shy
AIRCRAFT TIME IN SERVICE
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MAINTENANCE RECORD FAR439
c~~shy~~ -r = -zc C Ir
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MAINTENANCE RECORD FAR439
DATE OF I OM PLETION
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MAINTENANCE RECORD
) SERVICfULTIMATE ENGINES INC b
Mena Arkansas 71953 501394-5422
52603 W O 96167october 24 1996 Tach Time Date C E- 1111Reg N30344 Ae sn
On this date the following items were accomplished
1 RampR fue l cap 0 ring s pn MS29513-338 2ea 2 RampR uplock block springs pn 1 00942C0020-31 2ea
3 RampR cabin door seal
4 I
--L---~~----L-~~c--___
ULTIMATE E N GINES P O Box B O~)
Mcn a Ark ansa s ( I 50 1 - 394 -542
PETER J LO BELLO AP7354 The aircraft engine or appliance identified and inspected in accordance with curren Federal Aviation Administration and is ap service Pert inent detai ls of Ihe repair are
Dale c 7~[ - l or p y--~-
Signed -I- ~-lto- A zgt-l JU- shy
Jl TIMATE ENGINES ~ R S YCTR973K
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NOhAT E OF AIRCRAFT TIME DESCRIPTION OF WORK PERFORMED I MPLE TION IN SERVICE OR APPROVED OAT A USED WORK PERFORMEDRETURNED TO SE IlVI I
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
---- shy
1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
l~ I3d-shy
CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
ifYr1 r~JnK
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t-shy
r-- shy
f- shy
INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
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4317 Maher Street Laredo Texas 78041 (956) 72S-8898
CRS S78R1SIN Date shJIO N jO L-ff1
AlC po 3 31
FAR 91413 SIN eli -111
1 certify that the ATC xansponder test and inspection required by FAR 91413 have been perforrned on 512~f to The II1tergrated system test and Inspection was preformed on 51-lt ( IV _
I Transponder Model ( rx -3 -~7 SIN g5 ZO-)
2_ Transponder Model ___-tshy_____ SIN =
I
SS _-0 50 Ii Work Order No 1LD ASI-14
Avionics Se~i~es T~te~-on l Inc 4317 Maher Street Laredo Texas 78041
(956) 725-8898 CRS S78R151N
Date sh-lUo N3Q314 AIC poundgt 3 It
fAR94 SIN (G-(III
I certify that the altimeter and reporting equipment test and inspections required by FAR 91411 have been performed_ The left altimeter PIN fLU - (7---6shy SIN i-r5pound 00 was tested to 2 5 _ODO feet on 50--110 _The right altimeter P(N__~~-_____ SIN -7 - was tested to -t - feet on______ The static system was tested on 51) 0 Tile automatic pressure reporting system was tested on 5)4110
Work Order No )1 til Signature ----d Date 5 Jut() ASlLt - - shy- shy-shy
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RADIO amp ELECTRONIC CHECKS DATE TOTAL
TIME EQUIPMENT
CHECKED TYPE OF CHECK
ERROR OR RESUL TS
N- 3034 4 EM 118
CHECKED BY SIGNATURE - CERT NO
3-3 - 90
T or~ue d all wing bolts as per Beech Man ua l See work order 14171 for deta i ls
I ( o~
MAINTENANCE RECORD FAR439
DATE OF COMPLETION
l shy S - 9~
AIRCRAFT TIME IN SERVICE
2-29-93
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NO WORK PERFORMED RETURNED TO SERVI( I
MAINTENANCE RECORD FAR439
3shy
AIRCRAFT TIME IN SERVICE
DATE OF COMPLETION
r-shy
AIRCRAFT TIME IN SERVICE
-r~
MAINTENANCE RECORD FAR439
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MAINTENANCE RECORD FAR439
DATE OF I OM PLETION
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MAINTENANCE RECORD
) SERVICfULTIMATE ENGINES INC b
Mena Arkansas 71953 501394-5422
52603 W O 96167october 24 1996 Tach Time Date C E- 1111Reg N30344 Ae sn
On this date the following items were accomplished
1 RampR fue l cap 0 ring s pn MS29513-338 2ea 2 RampR uplock block springs pn 1 00942C0020-31 2ea
3 RampR cabin door seal
4 I
--L---~~----L-~~c--___
ULTIMATE E N GINES P O Box B O~)
Mcn a Ark ansa s ( I 50 1 - 394 -542
PETER J LO BELLO AP7354 The aircraft engine or appliance identified and inspected in accordance with curren Federal Aviation Administration and is ap service Pert inent detai ls of Ihe repair are
Dale c 7~[ - l or p y--~-
Signed -I- ~-lto- A zgt-l JU- shy
Jl TIMATE ENGINES ~ R S YCTR973K
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NOhAT E OF AIRCRAFT TIME DESCRIPTION OF WORK PERFORMED I MPLE TION IN SERVICE OR APPROVED OAT A USED WORK PERFORMEDRETURNED TO SE IlVI I
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
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1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
l~ I3d-shy
CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
ifYr1 r~JnK
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INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
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- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
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MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
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RADIO amp ELECTRONIC CHECKS DATE TOTAL
TIME EQUIPMENT
CHECKED TYPE OF CHECK
ERROR OR RESUL TS
N- 3034 4 EM 118
CHECKED BY SIGNATURE - CERT NO
3-3 - 90
T or~ue d all wing bolts as per Beech Man ua l See work order 14171 for deta i ls
I ( o~
MAINTENANCE RECORD FAR439
DATE OF COMPLETION
l shy S - 9~
AIRCRAFT TIME IN SERVICE
2-29-93
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NO WORK PERFORMED RETURNED TO SERVI( I
MAINTENANCE RECORD FAR439
3shy
AIRCRAFT TIME IN SERVICE
DATE OF COMPLETION
r-shy
AIRCRAFT TIME IN SERVICE
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MAINTENANCE RECORD FAR439
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MAINTENANCE RECORD FAR439
DATE OF I OM PLETION
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MAINTENANCE RECORD
) SERVICfULTIMATE ENGINES INC b
Mena Arkansas 71953 501394-5422
52603 W O 96167october 24 1996 Tach Time Date C E- 1111Reg N30344 Ae sn
On this date the following items were accomplished
1 RampR fue l cap 0 ring s pn MS29513-338 2ea 2 RampR uplock block springs pn 1 00942C0020-31 2ea
3 RampR cabin door seal
4 I
--L---~~----L-~~c--___
ULTIMATE E N GINES P O Box B O~)
Mcn a Ark ansa s ( I 50 1 - 394 -542
PETER J LO BELLO AP7354 The aircraft engine or appliance identified and inspected in accordance with curren Federal Aviation Administration and is ap service Pert inent detai ls of Ihe repair are
Dale c 7~[ - l or p y--~-
Signed -I- ~-lto- A zgt-l JU- shy
Jl TIMATE ENGINES ~ R S YCTR973K
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NOhAT E OF AIRCRAFT TIME DESCRIPTION OF WORK PERFORMED I MPLE TION IN SERVICE OR APPROVED OAT A USED WORK PERFORMEDRETURNED TO SE IlVI I
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
---- shy
1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
l~ I3d-shy
CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
ifYr1 r~JnK
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f- shy
INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
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L r ~ ( - J L ~lS -~
MAINTENANCE RECORD FAR439
DATE OF COMPLETION
l shy S - 9~
AIRCRAFT TIME IN SERVICE
2-29-93
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NO WORK PERFORMED RETURNED TO SERVI( I
MAINTENANCE RECORD FAR439
3shy
AIRCRAFT TIME IN SERVICE
DATE OF COMPLETION
r-shy
AIRCRAFT TIME IN SERVICE
-r~
MAINTENANCE RECORD FAR439
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MAINTENANCE RECORD FAR439
DATE OF I OM PLETION
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MAINTENANCE RECORD
) SERVICfULTIMATE ENGINES INC b
Mena Arkansas 71953 501394-5422
52603 W O 96167october 24 1996 Tach Time Date C E- 1111Reg N30344 Ae sn
On this date the following items were accomplished
1 RampR fue l cap 0 ring s pn MS29513-338 2ea 2 RampR uplock block springs pn 1 00942C0020-31 2ea
3 RampR cabin door seal
4 I
--L---~~----L-~~c--___
ULTIMATE E N GINES P O Box B O~)
Mcn a Ark ansa s ( I 50 1 - 394 -542
PETER J LO BELLO AP7354 The aircraft engine or appliance identified and inspected in accordance with curren Federal Aviation Administration and is ap service Pert inent detai ls of Ihe repair are
Dale c 7~[ - l or p y--~-
Signed -I- ~-lto- A zgt-l JU- shy
Jl TIMATE ENGINES ~ R S YCTR973K
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NOhAT E OF AIRCRAFT TIME DESCRIPTION OF WORK PERFORMED I MPLE TION IN SERVICE OR APPROVED OAT A USED WORK PERFORMEDRETURNED TO SE IlVI I
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
---- shy
1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
l~ I3d-shy
CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
ifYr1 r~JnK
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INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
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1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
2-29-93
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NO WORK PERFORMED RETURNED TO SERVI( I
MAINTENANCE RECORD FAR439
3shy
AIRCRAFT TIME IN SERVICE
DATE OF COMPLETION
r-shy
AIRCRAFT TIME IN SERVICE
-r~
MAINTENANCE RECORD FAR439
c~~shy~~ -r = -zc C Ir
shy I ~tt=~ Lqd ~~~ -r
----------+shy
~ ( I cz ==~----shy ~
c-------
MAINTENANCE RECORD FAR439
DATE OF I OM PLETION
[
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-
a
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0
MAINTENANCE RECORD
) SERVICfULTIMATE ENGINES INC b
Mena Arkansas 71953 501394-5422
52603 W O 96167october 24 1996 Tach Time Date C E- 1111Reg N30344 Ae sn
On this date the following items were accomplished
1 RampR fue l cap 0 ring s pn MS29513-338 2ea 2 RampR uplock block springs pn 1 00942C0020-31 2ea
3 RampR cabin door seal
4 I
--L---~~----L-~~c--___
ULTIMATE E N GINES P O Box B O~)
Mcn a Ark ansa s ( I 50 1 - 394 -542
PETER J LO BELLO AP7354 The aircraft engine or appliance identified and inspected in accordance with curren Federal Aviation Administration and is ap service Pert inent detai ls of Ihe repair are
Dale c 7~[ - l or p y--~-
Signed -I- ~-lto- A zgt-l JU- shy
Jl TIMATE ENGINES ~ R S YCTR973K
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NOhAT E OF AIRCRAFT TIME DESCRIPTION OF WORK PERFORMED I MPLE TION IN SERVICE OR APPROVED OAT A USED WORK PERFORMEDRETURNED TO SE IlVI I
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
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1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
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CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
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INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
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11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
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1
II
INSPECTION RECORD r- r- -IIl n
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JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
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Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
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~~ un fil e at thi S agf1 cy WOI 22766
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
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MAINTENANCE RECORD FAR439
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AIRCRAFT TIME IN SERVICE
DATE OF COMPLETION
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AIRCRAFT TIME IN SERVICE
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MAINTENANCE RECORD FAR439
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DATE OF I OM PLETION
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MAINTENANCE RECORD
) SERVICfULTIMATE ENGINES INC b
Mena Arkansas 71953 501394-5422
52603 W O 96167october 24 1996 Tach Time Date C E- 1111Reg N30344 Ae sn
On this date the following items were accomplished
1 RampR fue l cap 0 ring s pn MS29513-338 2ea 2 RampR uplock block springs pn 1 00942C0020-31 2ea
3 RampR cabin door seal
4 I
--L---~~----L-~~c--___
ULTIMATE E N GINES P O Box B O~)
Mcn a Ark ansa s ( I 50 1 - 394 -542
PETER J LO BELLO AP7354 The aircraft engine or appliance identified and inspected in accordance with curren Federal Aviation Administration and is ap service Pert inent detai ls of Ihe repair are
Dale c 7~[ - l or p y--~-
Signed -I- ~-lto- A zgt-l JU- shy
Jl TIMATE ENGINES ~ R S YCTR973K
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NOhAT E OF AIRCRAFT TIME DESCRIPTION OF WORK PERFORMED I MPLE TION IN SERVICE OR APPROVED OAT A USED WORK PERFORMEDRETURNED TO SE IlVI I
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
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1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
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CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
ifYr1 r~JnK
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INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
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11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
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1
II
INSPECTION RECORD r- r- -IIl n
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JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
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- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
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MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
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DATE OF COMPLETION
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AIRCRAFT TIME IN SERVICE
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MAINTENANCE RECORD FAR439
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MAINTENANCE RECORD FAR439
DATE OF I OM PLETION
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MAINTENANCE RECORD
) SERVICfULTIMATE ENGINES INC b
Mena Arkansas 71953 501394-5422
52603 W O 96167october 24 1996 Tach Time Date C E- 1111Reg N30344 Ae sn
On this date the following items were accomplished
1 RampR fue l cap 0 ring s pn MS29513-338 2ea 2 RampR uplock block springs pn 1 00942C0020-31 2ea
3 RampR cabin door seal
4 I
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ULTIMATE E N GINES P O Box B O~)
Mcn a Ark ansa s ( I 50 1 - 394 -542
PETER J LO BELLO AP7354 The aircraft engine or appliance identified and inspected in accordance with curren Federal Aviation Administration and is ap service Pert inent detai ls of Ihe repair are
Dale c 7~[ - l or p y--~-
Signed -I- ~-lto- A zgt-l JU- shy
Jl TIMATE ENGINES ~ R S YCTR973K
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NOhAT E OF AIRCRAFT TIME DESCRIPTION OF WORK PERFORMED I MPLE TION IN SERVICE OR APPROVED OAT A USED WORK PERFORMEDRETURNED TO SE IlVI I
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
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1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
l~ I3d-shy
CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
ifYr1 r~JnK
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INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
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11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
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1
II
INSPECTION RECORD r- r- -IIl n
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JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
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Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
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INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
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MAINTENANCE RECORD FAR439
DATE OF I OM PLETION
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MAINTENANCE RECORD
) SERVICfULTIMATE ENGINES INC b
Mena Arkansas 71953 501394-5422
52603 W O 96167october 24 1996 Tach Time Date C E- 1111Reg N30344 Ae sn
On this date the following items were accomplished
1 RampR fue l cap 0 ring s pn MS29513-338 2ea 2 RampR uplock block springs pn 1 00942C0020-31 2ea
3 RampR cabin door seal
4 I
--L---~~----L-~~c--___
ULTIMATE E N GINES P O Box B O~)
Mcn a Ark ansa s ( I 50 1 - 394 -542
PETER J LO BELLO AP7354 The aircraft engine or appliance identified and inspected in accordance with curren Federal Aviation Administration and is ap service Pert inent detai ls of Ihe repair are
Dale c 7~[ - l or p y--~-
Signed -I- ~-lto- A zgt-l JU- shy
Jl TIMATE ENGINES ~ R S YCTR973K
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NOhAT E OF AIRCRAFT TIME DESCRIPTION OF WORK PERFORMED I MPLE TION IN SERVICE OR APPROVED OAT A USED WORK PERFORMEDRETURNED TO SE IlVI I
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
---- shy
1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
l~ I3d-shy
CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
ifYr1 r~JnK
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INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
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1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
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J I I I ~ l f _ 0
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~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
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MAINTENANCE RECORD
) SERVICfULTIMATE ENGINES INC b
Mena Arkansas 71953 501394-5422
52603 W O 96167october 24 1996 Tach Time Date C E- 1111Reg N30344 Ae sn
On this date the following items were accomplished
1 RampR fue l cap 0 ring s pn MS29513-338 2ea 2 RampR uplock block springs pn 1 00942C0020-31 2ea
3 RampR cabin door seal
4 I
--L---~~----L-~~c--___
ULTIMATE E N GINES P O Box B O~)
Mcn a Ark ansa s ( I 50 1 - 394 -542
PETER J LO BELLO AP7354 The aircraft engine or appliance identified and inspected in accordance with curren Federal Aviation Administration and is ap service Pert inent detai ls of Ihe repair are
Dale c 7~[ - l or p y--~-
Signed -I- ~-lto- A zgt-l JU- shy
Jl TIMATE ENGINES ~ R S YCTR973K
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NOhAT E OF AIRCRAFT TIME DESCRIPTION OF WORK PERFORMED I MPLE TION IN SERVICE OR APPROVED OAT A USED WORK PERFORMEDRETURNED TO SE IlVI I
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
---- shy
1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
l~ I3d-shy
CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
ifYr1 r~JnK
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t-shy
r-- shy
f- shy
INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
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r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
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L r ~ ( - J L ~lS -~
MAINTENANCE RECORD FAR439
AGENCY amp CERTIFICATE NOhAT E OF AIRCRAFT TIME DESCRIPTION OF WORK PERFORMED I MPLE TION IN SERVICE OR APPROVED OAT A USED WORK PERFORMEDRETURNED TO SE IlVI I
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
---- shy
1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
l~ I3d-shy
CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
ifYr1 r~JnK
I
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f- shy
INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
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I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
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- -
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Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
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MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
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INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
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L r ~ ( - J L ~lS -~
MAINTENANCE RECORD
DATI ilL TiivJA TE ENGINES IIVCII COMPl
Mena Arkansas 5011394-5422 Oate July 2 1 1997 Tach 574 03 ACTT57 4 03
WO 97513 ETi 57403 PTT 574 03 Engine Data TCM 10 -520-B6 sin 578210 Aircrijft Data 1987 Beechcraft F33A SIN CE-1 11 N30344
On this date the following items were accomplished to
---- shy
1 Complied with Service Buletin 2305 by installing placard pin shy36-430057-1
2 Installed compass card 3 Tightened nose gear forward retract rod end bolts
~----- 4 Tightened nose gear aft retract rod end bolt 5 Replaced filters in gyro pressure system pi n BA 7112 DA9-14shy
5 1J4-7 _---- shy
6 Adjusted LH flap bumper -~
MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
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CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
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INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
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11
INSPECTION RECORD FAR4311-91217
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JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
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1
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INSPECTION RECORD r- r- -IIl n
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JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
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Date S--2 -err) Signed JJdt~ For
I I
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Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
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- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
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MAINTFNA(J Dl=rnDn
nA TE bull C1 MPLI
Performed a 100-hour inspection in accordance with Beechcraft A36 Inspection Guidelines (FAR 43 appendix D) Current status of Airworthiness Directives may be found in maintenance records I certify that this airframe has been inspected in accordance with a 1 OO-hour inspection and was determined to be in airworthy condition
~------ Anthony Butera AP429399101
I CERTIFY THAT THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AS PER THE BEECHCRAFT A36 INSPECTION GUIDELINES AND FAR PART 43 GUIDELINES ALL APPLICABLE ADS THRU 97shy14L WERE CHECKED FOR APPLICABILITY AND COMPLIANCE AND IS APPROVED
~TURN$VICE
l~ I3d-shy
CERTIFIED REPAIR STATION YCTR973 K
ULTIMATE ENGINES INC PO Gox 80
Mena Arkansas 71953 ~O 1-1 C)4-)4 2
PETER J LO BELLO AP735430361A
11 lt 1iL-1jj~t eng In e o r 2 1 middotjinncc identrfied above w as repau f lei inspected in ilccordltJ1 ce w ith current Reg ula tions of tl deral Avial i ~n Ijm i n ist r~t l o n and is approve d fo r retu rn l
SlIce Peni llc lll details 01 the rep air are on fil e at this rep
sta ti on under W0rllt Orde r No 17SI 3 ~)a te --A -~a iuned -GS ~ t JLTt ~MTI f NGIN _ INC
ifYr1 r~JnK
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INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
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II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
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--
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~~ un fil e at thi S agf1 cy WOI 22766
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
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J I I I ~ l f _ 0
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~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
INSPECTION RECORD FAR 4311 - 91217
IIH E AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
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--
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~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
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J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
INSPECTION RECORD FAR 4311 - 91217
--------------------------------------~K ~D~ ~L~IS~T~------------------------~~I~N~D~O~F~I~N~SP~E~C~T~IO~N~~S~T~ATU~S~amp IS~C~R=EP~A~N~C=YDATE SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
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~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
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J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
INSPECTION RECORD FAR 4311 - 91217
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
middot
DATE AIRCR AFT TIME
IN SER VICE
I l -CJ3I II~ LL 1-
INSPECTION RECORD FAR 4311 - 91217
INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
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I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
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INSPECTION RECORD FA R 4311 - 91217
KINO OF INSPECTION - ST A TUS amp DISCREPANCY LISTAIRCRAFT TIMEIlATE IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
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1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
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Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
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--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
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L r ~ ( - J L ~lS -~
I
INSPECTION RECORD FAR 4311 - 91217
SPECTION STATUS amp DISCREPANCY LISTAIRCRAFT TIMEDATE PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICEIN SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
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I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
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J I I I ~ l f _ 0
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L r ~ ( - J L ~lS -~
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME IN SE RVICE A IRCRA FT FOR SERVICE
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
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I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
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L r ~ ( - J L ~lS -~
INSPECTION RECORD FAR 4311 - 91217
AIR CRA FT TIME IN SERVICE
~
Ji llP iI-~ium5J - shy - fl ~ 110
11
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
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--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
INSPECTION RECORD FAR4311-91217
___ bullbullbull _____ __ bull _ bullbull _ n __r_~_ ~__ I
JETSUN AVIAnON CENTRE 5815 MITCHELL SIOUX ClTY IA 51110 CRS SG7R549J
N30344 TACI-j 6378 SNCE-IIII
Removed and reinstalled after repair KI-525A PIN 066-3046-00 SIN 23491 Removed Compass PAI-700 SN23352 and installed new PAI-700 SIN 29185A Compass sw ing prerormed and correction card installed on compass base
The aircrart and or component above was repaired and inspcctcd in accordance with current Fedclal Aviation Administration Regulations and is approved for return to servicc ~s ainvorthy pco-~nt dltfails of~c rwail arc on filc at this agency under
Workorder 150 Datedo -)3 97 Slgned W JUlti - cie~~~ lnspectorforJetsunAvl atlon Centre CRSII SG7R549J
1
~ I
1
II
INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
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INSPECTION RECORD r- r- -IIl n
-- - --shy
JETSUN A VIA nON CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
BEECH F-33A CE-II I 1 N30344
102897 WO 10357 TAC H
REMOVED ALCO R EGT SYSTEM PIN 460 13 SIN 179575 [N STALLED JPI INSTRUMENTS EDM 70 1 TEMPERATURE --shyMONITORING SYSTEM SIN 7820 INSTALLED TANIS HEATER PER INSTRUCTION MANUAL SEE 337 THIS DATE
fhe aircraft and or component above was repaired and inspected in accordance with current Federal Aviation Administration Regulations and is approved for -eturn to service as airworthy_ Pertinent details of the repair are on file at this agency under ---shywork order J ~ dated A0 l[ 1 7
Signed ~----y Inspector for Jetsun Aviation Centre CRS SG7R549J ~
For
I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
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INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
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I
INSPECTION RECORD I1 AR 43 11 ~ 91217
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
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--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
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- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
INSPECTION RECORD -F AR 43 11 - 91217
I II AIRCRAFT TIME
IN SERVICE KIND O F INSPEC TION - STATUS amp DISCREPANCY LIST
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING AIRCRAFT FOR SERVICE
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
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r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
INSPI (TION HI G( Uti-
JETSUN AVlATION ONTIHlt HI M 1I11 J1 j bullbullbull fHi II i bullbull I II I I I II I I I i II HI i
BEECH F-33A CE-llll N 30344
I I I I I I II II I 11 I I)ERF()I~M EIl NNII I I NS JlI 111111 I W 111 II I
DOOR IIAND)ES O( I WII AS III il H IN 11 II i l REQUIRED r~ 1-1 (1-1) U ( I IX l ll VIlli Ij l I IN III I I I Iil l I I I
WITH NEW PIN 5()()~ (IIC 11 l J N( 11) N II IN I I-f I I I ) I I I I CAJI06RI2S-S C II NFI) 11111 -i 111 l N I II 1 1 111 1 N I 11 11il l t il
~_ TEST fLOWN AND ()PS ( I middot11) N I) H II IN I 11 II)
-- [ r(lfify that this (lIi ull) ( III i l ttH Hili t ill f 1 1 ainvorthy condilu ))ulf 411 Ii ClI I t 1
Signed c 7 bull 11I1pmiddottlrul lUI 1 1
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
INSPECTION REC~~D FAR4311 1912dl
------------------------~
IETS1JN VIATION CENTRE SUX lA-FAA APPRO1 ) RG-PAIR STATION CRS SG7R549J VIJCE
Date 11-30-98 N30344 TACH 122596 SN CE-876
I Removed Flight Director KI256 pn060-00 17-00 sn 14479 Installed exchange overhaul Fl Director
pn060-00 17-00 sn I 1322 2 Removed anet re-installed after repair HSI KI525 sn23491
1
Signed ~ l h
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
~ altz I L oclh V AampP for Jetsun Aviation C tll (ItS II S( II jI1
IrolSPECTION RECORD - bull A~middot4311 - 91U7
JETSUN AVIATION CENTRE 58 5 MHCH ELL Sioll x ( Ily 11 III ( 1
12-4-98 UEECU F-33A N30344 SIN (1--11 II I I 1111 I
JACKED M C REMOVED BOTIl MAIN STRlJTS RESIAL ANIgt SEIII(F AN I 11 1 I I I I NEW MAIN GEAR TIRES AND NEW BRAKE LlNNINGS HESEAL BOTti IIIIA I 1 Ii ~ fl il l PLACARD ON FUEL CONTIOI PANEL-INSTALLED EXCIIANGt- III-AILH I~II Hi i II 1 ij i i INSTALLED ENG AFnm OVEHIIAlJL UY CENTHAL (VI NI-W ENC IVIO IIN I I Ni h i I II I II ~ j i I i ~ 1 LlNI~S PROP GOVEHNOH WAS OVERBlJLD UY MAXWIL1 AI( Slot(I( I
Thc aircraft lllld or componcnl above was repaired and insp (led ill aolll I 11 110 I I 1 01 HClIlati o ns and is applovcd for rctun to service as aiworthy Icrtitllllail I Ih 1101 I I ll i IH i work order ~ r~1 dated 1- LJ - rp--shy
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
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I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
-i
INSPECTION RECORD FAR 4311 - 91217
KIND 01 IN~II ( liON middot A TUmiddotc-S-camp--D-IScC-OR-Ep-A-Nc-C7Y-l--IST---------------jAIRCRAFT TIME IN SERVICE SIGNATURE - CERT NO OF 11 1l~()N AII1l0VING OR DISSAPPROVING AIRCRAFT FOR SERVICE
~JETSUN AVIATION CENTRE 15815 MITCHELL Sioux City IA 51110 CRS SG7R549J BEECH F-33A 12-21-98 SIN CE-1111 WO 10911
N30344 TACH 1264 REMOVED BATTERY AND REPLACED WITH A NEW ONE PIN G-242 DRAINED OIL AND
REFILLED WITH 12 QUARTS OF PHILLIPS XC20W50 REPLACED FILTER AND TOOK OIL SAMPLE FOR EVALUATION POST RUN SATISFACTORY
f-
The airerafl and or component above was repairell anll inspectell in aecorllance with current Fellual Aviation Allminislrolio Regulations and is approved for return to service as airworthy Pertincnt details of Ihe repair an on file at this agency Inlier work order _10911 lIated 12-21-98_
Signcll _DAN D CUMMINS AampP for Jetsun Aviation Centre CRS SG7R549J (~IJ~ JETSUN AVIATION CENTRE I 5815 MITCHELL SIOUX CITY IA 51110 CRS SG7R549J
N30344 Au 158396 luly 27 1999 Bcech FJ3A Ett 33996 Tso WOI 11193
SIN CE-IIII Pu 1583968255 SOH Hobbs 158396 ContincntalIO-520IlB Selial Numbcl 578210
Complicd with annual inspection in accordance with Beech inspection guide Installed GampD window kit (STC SA 3759NM) in accord lViii FAA sealed Gale R Calhoon Rep0l1 No I dated Dec 71987 337 tiled 3Jld weight and balance calculated and cntered into POll Icpiad nose wheel assy with new pIn 040-07705 Ins1alled new spilUler back plate fillet with new pIn B5254 Changed oil and lilter Oil sa lllpk takn and sent in for analysis Installed new CI-l48 109 filtcr and serviccd with 12 qts XlC 2050 oil Removed UH exbaust muiller and in stoll cd new Illumer pIn 701-4 Inspected and tested ELT lAW FAR 91207 Due Date Aug 2000 Verified that AD 99-05-13 EFD 4-19-99 was previollsly CW CW AD 95-04-03 EFD 4-7-95 by visual inspection next due tach of 2083 Inspected wings fuselage and t1il scctions Lubed all controls lacked alc Inspected and lubed gear Performcd retraction test
I cCI1ify that fltis (aircmft) (enginc) has bccn inspected in accolIIlUCC with an Annual inspection and was determincd to be ill ainvorthy conditionDatcd 7-27-1299 wOIk otder 11193
Signcd OM Dl Jt D~ Inspcctor fOJ JCtSWl Aviation Ccntrc CRS SG7R549J ~ i
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
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L r ~ ( - J L ~lS -~
~J1d can be referenced [or future li se in any inspections or maintenance 4 The Weight and [lalancc and Equi pment l ist have been updated to reflect th e changes 5 The above installation does not interfere with any other ex istin g equipment nor does it cause a current draw of over 80
rated aiL outpuL 6 A FAA approved Flight manual supplement Datcd~ has been installed into th e pilot operating handbook and placed into the aircraft The pil ots(1Vide for th e Ryan TCAD Model 8800 was placed inlo the aircrall papcrwork
7 FAAFor~ 337 Fil~S~ Signed do
CRS DDNR 793K 3501 Aviation Av Sioux falls SO 57104
1111
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KI DATE IN SERVICE SIGNATURE - CERT
Business Aviation r _ Airframe Log Joe Foss I-Ie ld
Sioux Falls SO Cessna
MAKEMODEL HOUR METER TOTAL TIME REGISTRATION SERIAl NUMBER
[lEECHCRAFT N30344 CE-ilil
MAINTENANCE RELEASE The aircraft andor component identified was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service Detail s on file at thi s agency WO20406 I Installed Ryan TCAD Mod 8800 Silver A t FS 630 Transponder Coupler A t FS55 0 KA60 Antenna A t FS 85 KA 60 antenna at FS 162 The System was installed in accordance manufacturers instructions and AC43 13- 1 a Chapters 5 I 1 15 and
AC43 13-2A Chapters 123 2 An Integrated System Chcck Was Preformed Following The Installation Per Far 9 1411 9 14 13 and Far 43 app e A ll systems check Good 3 The Following Installati on Manual was used for Installation of the RYAN TCAD 8800 series Rev 2 December 14 1998
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
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--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
~ - u1 111 cl1110 bull
INSPECTION RECORD FAR 4311 - 9Wll
K I NO OF INSPEC TlON - S T A TlIS amp=O-ISCCR-=E-=-PA--N-C=-Oy--l-IST=---AiRCRAFT TIME IN SERVICE SIGNATURE- euroEIH NO OF PERSON APPROVING Oil Ol 5SAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J v
2-17-00 mmCH F-33 SIN CE-ll11 18800 TT AIRFRAME 6360 SMO ENG
I N ~TALLED NEW MAIN TIRES LUBE HEARINGS INSTALLED NEW LANDING LIGHT CfW SLICK SIB S81-98 1 (1 0 I II INSgt ON BOTH 11AGS NEXT DUE AT 1136 1m ENG TIME
11 airclaft and 01 component abovc was repaired and inspcctcd ill aceoldance with cuncnt Fedcral Aviation Adminishation Ilqulatiolls antis apoundProvcd for 1stUnIJ0jcrvice as ailWOl1hy Pertinent dctails oftJlc rcpail arc olllilc at this agcncy undel Id onlelU_LDL DATEDoL-~~-O
11 1 ~) ~t lnspcctOl for JctSun Aviation Ccntre CRS SG7R549J
Airframe Log
MAKEMODE
BEECHfF33A
Busmess A vbition
HOURMEfER
TACHI9418
Joe Foss Field
Sioux Fal ls SD
TOTAL TlME
NA
eessna
30344
bull Removed and replced alternator with newly overhauled unit PN 462055RX SN NO 13736 Ops check normal MAINTENANCE RELEASE The aircraft andlor component identified was repaired and inspected in accordance with currer fi deral aviation reWllations and is approved for return to servlce Detalls on file at this a nc r ~fM~491
SIgned ~ - Adam Timat
CRS DDNR793K 3501 Aviation Av Sioux faDs SD 57104
---1
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
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--
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~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
NSf TnfIJn~~
INSPECTION RECORD
~___ 1F ~ ~ 43_ i1 -=-91217 --c___ _______
IAIRCRAFT TIME I -KIND O~ INSPU [IONmiddotmiddot STATUS amp DISCREPANCY LISTDA TE ~ ltlt=oOrlt= ~INA ~) IRF - CERT NO OF PE RSON APPIlQVi N( C~ DISSAPPROVING AIRCRAFT FOR SERVICE
N30344 ModelF-33A Date 8-11-00 SIN CE-1111 WO 2782
Tach 218k CflMETER CERTIFICATION ~ CERTIFIED THE FOLLOWING COMPONENTS TRANSPONDER SIN49969 Altimeter Transponder anti Alti tude Reporting
~ ENCODING ALTIMETER ~~pound- Equipment tested in com~iance with FAR 91 411 Date 6- II -e~ Signed t ltgt For FAR 91413 Part 43 Appendix E and Part 43Jetsun Aviation Centre CRSSG7R549J bull Appendix F Stalic System certified per FAR 231325Sioux City IA 51110
All systems meet reguire~~ Thi3 data filed with Work Order it z7 -lt at R~air Station
sect~~~ ~Jpound Date Signature
JETSUN AVIATION CENTRE 5815 MITCHELL SIOUX CITY IA 51111 CRS SG7R549J
8-10-00 BEECH F-33A N30344 SIN CE-I III 2187 IT AlC 943 SMO ENG
JACKED AlC LUB WHEEL BEARINGS AND LANDING GEAR CK FUEL SCREEN AND STRAINER NEW MAIN TIRES NEW BRAKE LININGS RESEALED NOSE STRUT AND SERVICE NEW ELT BAn-ERY AND CW WITH FAR-91-207 CRASH TEST ELT NEXT DUE DATE JULY 02 NEW INST AIR FILTER INSTALLED NEW STOP BUITON ON FUEL CONTROL LANEL CW AD95-04-0J SPAR CAImEY TilRU CW AD 72-22-01 LUB UP LOCK ROLLERS
certify that tllis aircraft has been iljspected ill accordance with A _ HR OR ANNUAL inspection and was detern~llt to b~~ondition Dated 8-10-00 WOo 11733 Signeda~( 4 ~ Inspector for JetSUIl Avialion Cenlre CRSII SG7R549J
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
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Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
INSPECTION RECORD FAR 4311 - 91217
AIRCRAFT TIME KINO OF INSPECTION - STA iu-s=--amp-cshymiddot OCO--ISCc=-R-=-EP=-A-N-CY-l--IS-T------------shy
IN SERVICE SIGNATURE - CERT NO OF PERSON APPROVING OR OISSAPPROVING AIRCRAFT FOR SERVICE
JETSUN AVIATION CENTRE I SUX lA-FAA APPROVED REPAIR STATION CRS SG7R549J
Date 08-12-00 N30344 TACH 218758 WO 2782SNCE-111
II) J Removed and reinstalled after repair horizon indo PIN 060-0017-00 SIN 11322 I
~~
I
- ~
r t~ ~ - -
Date S--2 -err) Signed JJdt~ For
I I
I
Jetsun Aviation Centre CRSSG7R549J I
Sioux City IA 51110
I -I
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
INSPECTIO~ RECORD FAR4311-91217
-------r-shy -------shy ----------K---N=shyD--=o-=-=-r-cN---SCP-=E-=C=-=TONshy 7ST=--ATUS amp DSCREPANCY LIST ~ DATE SGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING ARCRAFT FOR SERVICE
AIC-MAINTENANCE INC 30344 SIN CE-1111 Tach 238665 ate 4127101
Performed the follcming repairs on this aircraft lAW Beech F33A Maintenance Manual Chapter 51 (Structures) page 1 and AC 43 13-1B Chapter 4 Section 4 Replaced the following parts with OEMparts Grill PIN 002-410000-21 RH nose side skin PIN 002-410027-56 L1H side skin PIN 002-410027-55 RIH keel PIN 002-41 0019-2 L1H nose gear door PIN 35-410077-37 RIH door PIN 35-410077-36 L1H main gear door PIN 35-815055-212 nose gear retract rod PIN 35-825087-16 nose gear drag link (used selViceable) PIN 002-820016-37 right side skin angle PIN 002-410027-8 RIH stiffener PIN 002-410027-1 4 center keel plate PIN 002-410011-3 nose wheel track PIN 002-410015-1 Rerroved nose bug PIN 002-410010-3 and repaired as required Reinstalled using same rivet holes and diameter rivets Removed L1H flap repaired flap by replacing flap spar PIN 35-165050-68 and inboara end rib PIN 35-165050-74 flap skin PIN 35-165051-8 Etched aJodined primed and painted flap reinstalled on aircraft Continued on next page
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
INSPECTION RECORD FAR4311-91217
AIRCRAFT TIME11 1 TE IN SERVICE SIGNATURE - CE NG AIRCRAFT FOR SERVICE
AlC MAINTENANCE INC~ 30344 SIN CE-1111j Tach 238665
ate 412701 continued from previous page Painted nose section gear doors and RJH wing tip using the follolMng colors Blue DCC-Q 193728 Blaze Gold DCC-Q 29667 and Matterhorn White OCC-G 92573 Propeller was removed and overhauled by Propworks Propel ler Systems Inc Reinstalled this prop PIN 3AF32C406-C SIN861 853 ELT was inspected lAW FAA action ndice 81503 and was found to meet the requrements d FAR 91207(d) ELT battery due July 2002 AD compliance list updated thru 2001 -07 I certify this aircraft has been inspected lAW an annual inspection and was found to
bD 7rthy condition
~ Perry W ltXhsner AampP4688434861 A
h
I ~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
INSPECTION RECORD FAR 4311 - 91217
~
DATE
2 rr J c- O (
AIRCRAFT TIME IN SERVICE
KINO OF INSPECTION _STATUS P ntcro-o 1 krv I ICT bullbull
SIGNATURE - CERT NO OF PERSON APPROVING AIRCRAFT FOR SERVICE
- J ft-r lttC--
lqjJSo y oSl1 ~V~
Business A viltion Airframt Log Joe Foss Field
Sioux Fal ls SD
TOTAL TIME I REGTSTRATION
NlA N30344
bull Remo ved aJid replAced cngjne driven vac~wn p ump with new PIN 21 2CW SIN 26M369 ) Adjusted reg1llator Op check good ( se - - f (~H ~6J ~okJ IH~-~ ( ~4r() 4ltlt5ampamp-
bull RemovecJ and replaced 2 vacUlUTl air fi lters on engine driven system with new PN 1]1- 7 and bull PIN D9- 14-5
MAINTENANCE RELEASE Tbe ilircrail andor component identified WtlS repaired and inspected in accordance with current Ierleral aviallOTl regulations and is approved for re rUm to service Detaib
on fikat ~ris a~~yo~J
SIgned ~ ~t-----dam Timat
eRS tl UDNR793K 3)01 Aviation Ave Sioux Falb SD 57104
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
I
INSPECTION RECORD
Business Aviation ---- ---- --AirfraUJ~ Log Jo~ Foss Field
Sioux Falls ~D eessna REGISTRATION I SERIAL NUMBER
N3 0344 CEmiddot] J 11
Replaced tanding Gear Motor with OH unit PIN 58-3800090-1 SfN 4962 Ops checked good See FAA Form 8130-3 dated 5-2 1-01 (Western Sky [ndustries)
bull Replaced Altemator out sensor with new PIN 36-380000-3 SIN 80239920 Ops checked good See FAi Form 8130-3 dated 6- 12-01 (Raytheon)
bull Lubed heater control cable Ops checked good MAINTENANCE RELEASE The aircra ft andlor component identified was repaired in ( accordance with current federal aviali()n regulations and is approved for retUnl to -elyicc Details on file at this aeency W O M73middotB
Signed 6 -0laquo - Ken BJumenauer
CRS DDNR793K 3501 Aviation Av Sioux falls SD 57101
t
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
- --
I Ar 1 J
INSPECTION RECORD FAR 4311 - 91217
Business Aviation Airframe Lo S Joe Foss Field =f
Sioux Falls SD CesSna
II1AKEIMODEL TACH TOTAL TIME REGISTRATION SERIAL N UMBER
BEECHfF33A 285907 285907 N30344 CEmiddotllll
bull Replaced LH amp RH mall tires with new 700-6 6 ply Flight Custom II Also replaced both tubes with new Cleaned and repacked wheel bearings
MAINTENANCE RELEASE The aircraft andor component identified was repaired in accordance with current federal aviation regulations and is approved for retum to service Details on file at~~ency~wo M7443
Slgned~poundC~A~_OltOLlt-- =ct= Ken Blurnenauer
CRS DDNR793K 3501 Aviati on Av Sioux faIls SD 57104 i------ooI l
~ ~
~I I
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
-I
~
r ~-I Ir-
r ~l
I- shy
--
I
~~ un fil e at thi S agf1 cy WOI 22766
) Al rz7 5J
i
~ ~
I
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
- -
I
Business Aviation Airframe Lo g Joe Foss Field
Sioux Falls SD Cessna
MAKEIMODEL TACH TOTAL 11MB REGISTRATION SERIAL NUMBER 1--shyBEECHIF33A 28617 28617 N30344 CE-U l J
~--~--
bull Removed ManifoldFuel Flow Indicator PIN 36-380071-3 and installed OlH unit PIN 651035shyII 13 SiN 613489 (See InstrumentTech Corp FAA Fonn 8130-3 dated 2-13-01) Ground nul
-JY b middot1 ~~
MAINTENANCE RELEASE The aircraft andor component identified was repaired in I~ -- accordance llirith current federal aviation regulations and is approved for return to service
Details on ~ag~ M7446 SIgned ) J
t---- Chris Hoffinan ~ I CRS DDNR 793K 3501 Aviation Av Sioux falls SD 57104 f r-- shy
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~~ un fil e at thi S agf1 cy WOI 22766
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i
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- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
- bull
Business Aviation Airframe Log Joe Foss Field i--f
Sioux Falls SD Cessna ====rtI
bull Compiled with an Annual Inspection in accordance with FAR 43 Appendix D bull CiW AD 95-04-03(4-7-95) by visual and dye penelrant inspection of Wing Can)-Thm Spar No defects
noted Next due 345748
bull CW AD 2001-11-03(7-20-01) by replacement of Avionics Cooling Fan Cucuit Breaker with 1 Amp breaker PIN 7277-2-1 No further a1ion required
bull CIW ELT 12 month inspection lAW FAR 91 207(d) No defects noted Next inspection due 503 bull Installed new EL T Battery PIN BS2173 Negtot due 212004 bull Cleaned and repacked wheel bearings bull Installed new fuel cap o-rings with PIN MS29S13-338 bull Installed new Induction Air Filter PIN BA-7112 bull Installed (2)PIN D9-14-4 and (1 )PIN 114-7 Instrument Air Filters bull lnstaJled new Nose Tire PIN 301-016-420 (5 00-S 6PR) bull Installed new Brake Discs PIN 164-02S05 and new Brake Linings PIN 066-10500 LHlRH wheels bull Installed new Fuel Selector Stop PIN 36-9200S2-3 bull Installed new Nose Gear Retract Rod Boot PIN 36-820023-1 bull Performed Propeller Balance using Chadwick Helmuth Vibration Analyzer bull Ground run and test fligltt completed Satisfactoril) _ --tmiddot
( f) d) - jj - o rJo~~tt i 1 ~je fv j B1 J tlAIU~0 Ir ~ 1- 7 fr ~5 I certify t1wt this aircraft has teen inspected in accord~ce with an Annual inspection and has been detemJined to be in an airworthy condition Pertinent details of the inspection are on file at this repair station under WOM7628
amp A ( ~ shySigned ~~(i- ) I dlli~
Edward F DahlllOff CRS DDNR793K 3501 Aviation Av Sioux Falls SD 57104
DATE AI
--
MAKFlMODEL HOUR METER TOTAL TIME I REGISTRATION I SERIAL NUMBER
5-14-02 I BEECH F33A 295748 295748 N30344 CE-l111
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
Business Aviation Airframe Log Joe Foss Field
Sioux Falls SO Cesltgtna REGISTRATION SERIAL Nlltd lliRHOUR METER TOTALTIMFDATE ivIAKEltvlODELigtATE
N30344 CEllI I FDA
Removed King KA 39 Voltage Regulator frolll FS 20400 Northstar C-l remote conlin transc~iver from FS 20200 N)J1hstar Ml _ _ GPS receiver from FS 6300 King KR87 ADF Receiver from FS 6300 King KI 227 ADF Ind from FS 6700 King K4411 IW Antenna from FS 15900 Kin KI208 Nav IndConv from FS 6500 King KC 155 NavCom from FS 6l00i(iug Kfy 24 lIdio Panel from FS 6300 King KX 155 NavCom with Glideslope Receiver from FS 6300 King KN72 Nav Conve1or frolll FS 19300 King KT76A Transponder from FS 65 00 and King KDI 572 DME Ind from FS 6200 Instalkd Apollo SLl5 Audio Panel with Intercom SIN 6055134 at FS 65 00 Apollo MX20 Multifi1I1ction Display (MFD SIN (053947) at FS 6300 Apollo SI
7302 BEECHCRAFT
r 30 NavCom SIN 6054229 at FS 6300 Apollo DB30 011pound Interface at FS 6000 Sandia SAE5-35Altitude Data System at FS __ 6000 AmeriKing AK950 GPSlNav switching Annunciator at FS 6200 Apollo GX 60 GISCOlll SIN 6053825 at FS 65 00 and ) Garmin GTX327 Transponder at FS 6500 The GIS Nav and Multifunction Display system wer coupled togcther and display onmiddot both th~ MFD and an already ex isting HSI The Nav and GPS systems were also couple to an cxisting AutoPilot system lhe r-shyCorns and Navs utili zed existing Nav and Com antennas and the Switching Annullciator panel mowlted in plain view ofthe pilot 111is system does not cause any interference with any other aircraft equipment The abo ve modilications were made iJ accordance with the Manufactures installation manuals listed below Wiring All systems were wired to the Avionics Master electrical buss through th e manufactures recommended circuit breakers Operational Flight and Ground Checks lhe Garmin ground check and
~ flight adjustment procedures (Section 3) of the Gannin GTX 327 installation manual were satisfactorily completed Tlle Apollo ground check and flight adjustment procedures (Section 2) of the Apollo GX 60 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 28) of the Apollo MX20 installation manual were satisfactoril y completed 11e Apollo ground check and flight adjustment procedures (Section 29) ofthe Apollo SLl5 installation manual were sati sfactoril y completed The Apollo ground check and flight adjustment procedures (Section 28) of th e Apollo DB30 installation manual were satisfactorily completed The AmeriKin g ground check and flight adjustment procedures (Section24) of the AmeriKing AK950-2001 installation manual were satisfactorily completed 11e Sandia ground check and flight adjustment procedures (Section 37) of the Sandia SAE5-35 installation manual were satisfactorily completed lhe ~ystems operated in accordance with manufacturers specifications and did not interfere with the nonnal operation of the other equipment installed nor does the entire system cause a current draw exceeding 80 of the rated alternator output It has been determined that ~shythe nterelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of this aircraft Documents and ReferencesGarmin GTX327 Installation Manual PIN 190-00~87-02 Rev F dated November 2001 Sandia SAE5-35 All Data System Installtion Manual PIN 305186-00 rev I dated Sept 8 2000 AmeriKing In 1allation and Ops Manual Doc No IM-950 Apollo 0830 DME interface Installation Manual PIN 560-203l-00a dated May 2002 Apollo SLl5 Audio Panel Inatallation Manual PIN 560-0979-00 dated Dec 200 I Apollo MX20 MFD Installation Manual __ PIN 560-1025-04 dated July 2001 Apollo GX60 GPSComm Installation Manual PIN 560-0959-04 dated Feb2002 ) 111e manuals listed above will provide guidance for any continued airworthiness tests tilat may arise in tlle fulure he weight and r---
balanceequipment list has been updated 10 reflect the above installations and Form 337 filed with tl Ie FAA this date 7302 MAINTENANCE RELEASE 111e aircraft andor component identified were repairedin spected in accordance wilh CUTent f federal aviation regu lations and arc approved for return to service Details on fil e at this agency WO 22766
J ~A
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
INSPECTION RECORD n
BusinfSS Aitiop Aidimiddotam Log Joe Fo~ Iltle ld
Sioux Fal l SD
bull MA1JMODEL TACH TOTAL 11ME REGJSTRATION I SEPJA l NIIM I j l(
[ 6-26-02 BEECBF33A 2979 98 297998 N30311 CH II I
bull Installed Nose landing gem door roUer rehact kit PiN 3U-8005- 1 SIN 509 In-tul kd IA W 1 II inslmction dra ing Rigging and retraction test completed lAW Beech F3JA MM
bull C W annual inspecti on of upper tind lower will ~par caps rAW Beech SB 2538 Re I Nu uefecls noted Nexl due 6-03
l1AINTENANCF RtLEAS[ The 31IcraJ1 andior cOTIlj))nent identified was repaired in aC~Dldll lH)
vli th CllIrent federal a jation regu1ations and is approved li)r remrn to service Details on tilt J I 1111
agency WO t M77 ~ S d ~~ 1bull Igne _ _0 v Ck f J --=
Je Larser CRS Ii DDNR793K 3501 A viat io n Av Sioux falls SD 57104
I
1 Certify that the altimeter (5) alt reporting and 5tatic sY5tem tast required by FAR Po rt 91 411 have been performed The altimeter (s) were tested to
No1 c2~ 000 f~et en 4afe~ No 2 If feet0f1~a6~ InspeCtor ~M ( 00t8 Jj Busine-Aviotiori Avionics Deportm ht
WOil 764 Sioux FolIl SO Certi fied Repair StatiBR ~8 DDNlt793K
i usinas Aviation Avionics Department Sioux FoU SO Certified Repair Station No ODNR793K
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
-e I
INSPECTION RE~ORO F AR 4311 - 91217
NII 01 INgtlr C liON - ST ATU-S-amp-O-ISCREP-A-N7C-Y~l-IST=--------------shy
NC C)I 11 IION APPROVING OR OISSAPPROVING A IRCRA FT FOR SERVICE AIRCRAFT TIME
lA TE IN SERVICE
~ 16 c1lt
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
Repair
INSP~CHON RECoaQ FAR 4311 - 91217
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~
INSPFCTtON REcoao ~~~ v~ FAR 4311 - 91217
KIND OF INSPECTION S T A TU-S-amp-D-IS~C-R-EP-A-N-C-middotY-L-IS-l---
tD3
DATE IRECORDING ITODAYS TACH FLIGHT
19 __ TIME
SIGNATURE - CERT NO OF PERSON APPROVING OR DISSAPPROVING Illlt H I Ii I
TOTAL TIME IN SERVICE
Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility (See back pages for other specific entries)
utgt i lGshy
-=- ~
J I I I ~ l f _ 0
HI ~ )
~ _ 1 l 1 It J_l ) ~ i shy l Ol1shy
L r ~ ( - J L ~lS -~