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AIRFRAME MAINTENANCE RECORDS Log No. Ai rc ra ft Reg istrati 0 n No. --.Lt,---,! 1L.: 2 =---.,1./.'-L J ---'C......,'7'------ _ Serial No.£L«:C / Mfg. _ Model _ Serial No. _ Propeller Mfg. L1J.K-tzti! Hub Design No. Blade Design No. J#-' 1-13' yr-/ t2F Model ':::-7t Cf3 () P"/< Serial No. L )C53Z& _ . Hub Serial No. Blade Serial "-7""'l_L-L--L ;!LtZ 76 -7 J< i-/Z7 _ _ Propeller Mfg. _ Model. _ Serial No. _ Hub Design No. _ Hub Serial No. _ Blade Design No. _ Blade Serial No's. _ (All applicable information must be filled in) www.adlog.com PO BOX 1359/ SOUTHOLD, NY 11971-0965 (631) 765-9375 1-800-235-6444 FAX: (631) 765-9359 01979 AeroTech Publlcallons Inc.

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AIRFRAME MAINTENANCE RECORDS

Log No. ----J/f~-

Ai rcraft Reg istrati 0 n No. --.Lt,---,!1L.:2=---.,1./.'-LJ---'C......,'7'------ _

Serial No.£L«:C / ~ine Mfg. _ Model _ Serial No. _

Propeller Mfg. L1J.K-tzti! Hub Design No.

Blade Design No.

J#-' ~ 1-13' yr-/ t2F Model ':::-7t Cf3 ()P"/< Serial No. L )C53Z&

_

.

Hub Serial No.

Blade Serial NO'S.--'-J(~~----"("'--,"-7""'l_L-L--L ;!LtZ 76 -7 J< i-/Z7 7(~

_

_

Propeller Mfg. _ Model. _ Serial No. _

Hub Design No. _ Hub Serial No. _

Blade Design No. _ Blade Serial No's. _

(All applicable information must be filled in)

www.adlog.com PO BOX 1359/ SOUTHOLD, NY 11971-0965

(631) 765-9375 1-800-235-6444

FAX: (631) 765-9359 01979 AeroTech Publlcallons Inc.

- ---- - - - --- -- - - - -- - - --

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DESCRIPTION OF WORK PERFORMED­SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK

William Tinney Jr. 2781132 ATP •Complied with SB-07-002 Section 1-Pilot Action

~r7 J­

~COLUMBIA

The standby altimeter Aerosonic PIN 15035-01102 SIN 176247 The Gannin GDC 74A data computer SIN 47807983 systems were tested as required by FAR 91.411, and were found to comply with FAR part 43

Appendix E. A static system leak test has been perfonned, and was found to comply with FAR 23.1325

(;--tL ~ Authorized Signature for Columbia Aircraft Mfg. • -- - - _._--- - - --- - -- --- -- -- - ­

COLUMBIA

This aircraft was manufactured under FAA Production Certificate 719NM to Type Certificate Data Sheet A00003SE Revision 19. The following items were incorporated at the time of manufacture: Teledyne Continental TSIO-550C(11) Engine serial number 802881 Oregon Aero seats; STC SA01597SE; Production flight testing has been completed pursuant to

Document QC900004 Revision B. A check of Airworthiness Directives complied with using Bi-Weekly 2007- 16. A Standard Airworthiness Certificate is applied for on this date.

........ ~ ~ Q.-s@~l Columbia Aircraft Mfg.

I I ~.

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Au&/10kv.~ ~..;} ~Ol

NC Model LC41-550FG

Registration # N 1241"G

Serial Number 41777

I FIND THAT THE ABOVE AIRCRAFT MEETS THE REQUIREMENTS FOR THE CERTIFICATE REQUESTED AND HAVE ISSUED A STANDARD AIRWORTHINESS CERTIFICATE, (FAA FORM 8100-2),

DATED AUG 110 12007 .

THE NEXT It.SPECTION IS DUE August 2008.

Signeda~~ Aaron Kathman ODARF636210NM

I

~

---­ -

N1241G Hobbs: 32.1

«~ ~~. IINlAIi{ Date: September 21, Columbia LC41-550vUL", ........ 111 SIN: 41777~ COLUMBIA AIRCRAFr MANUFACTURING CORPORATION

22550 NELSON ROAD, BEND, DR 97701

Replaced GCU-476, pin 011-01237-00, sin 30005114 with new, same pin, sin 30005164. Op; check good. All work done per Garmin G I000 and Columbia 4maintenance manuals,

~a~f- = en Andersen AP48286663

2007 FG

00

3IA - ­ --­

MAKE: Columbia MODEL: LC41-550FG SIN: 41777 REG. NO: N1241G

Airplane Company of Salinas, Inc.

1585 Moffett Street Salinas, Ca 93905

DATE: 1/31/2008 NC TSN: 42.6 HOBBS: 42.6

WORK ORDER: 117HJ1-2008 Phone: 831-753-1077

Airframe Entries

COMPLIED WITH ANNUAL INSPECTION PER COLUMBIA 400 MODEL LC41-550FG INSTRUCTIONS FOR CONTINUED AIRWORTHINESS AND REQUIRED MAINTENANCE CHECK LIST

8 INDUCTION AIR FILTER ELEMENTREPLACEMENT DUE EACH 100 HOURS OR ANNUALLY DUEAT 100 HOURS OR 07/2008.

9 PERFORMED AD SEARCH ON AVENTEXT LIBRARY 2008-01,

11 SB-07-011 N/A BY TURBO SER NO. AD 2007-16-10 N/A BY TURBO SER. NO.

13 COMPLIED WITH AD 2007-07-06 PREVENT JAMMING IN THE AILERON AND ELEVATOR CONTROL SYSTEMS - REPETITIVE INSPECTION

14 TIGHTEN LENS COVER ON LEFT STROBE LIGHT ASSEMBLY.

DRESSED AND TOUCHED UP PAINT ON PROPELLER BLADES AS NEEDED.c~ 17

CLEAN AND DETAIL AS NECESSARY."18

I CERIFY THAT THIS AIRCRAFT WAS INSPECTED IN AC~~51'ITH ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AN AIRWORTHY CONDITION.

DATE: 1/31/2008 SIGNED:1 •.~/..'D/.~"-~ Work Order: 1171-01-2008

David Reek, IA 470720725 Printed by EBis 3 (datcomedia.com)

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r------:----+------r----------------IW-'

Athffn~ ~ Turltoprop Man_Iement, Inc.

970 Ben Epps Drive' Athens, Georgia 30605 • 706-546-7969

AIRFRAME LOG ENTRY

ACFT: N1241G MFG: CESSNA HOBBS: 136.9 DOM: BRGHT FWD MIN: LC41-SS0FG TACH: NIA DATE: 07-16-08 SIN: 41777 AFTT: 136.9

1. CONNECTED EXTERNAL POWER, POWERED UP SYSTEM. VERIFIED NO ATITTUDE AND NO HEADING DISPLAY. VERIFIED AUX PAGE 6-GRS1 REPORTS FAILURE, AND GMU1 REPORTS FAILURE. POWERED DOWN, OPENED LEFT WING PANEL, VERIFIED WIRING TO GMU, WIRING GOOD. REMOVED CENTER FWD PEDESTAL ASSY, REMOVED AHRS UNIT GRS77, FOUND PIN AND SIN REQUIRES CESSNA 5B-07-013C lAW GARMIN SB 073S. REPLACEMENT PART ORDERED. INSTALLED NEW AHRS, CONNECTED AND CLOSED FWD CENTER CONSOLE. POWERED UP AIRCRAFT AND AVIONICS, OPS CHECK GOOD.

2. REMOVED CENTER FWD CONSOLE PANEL, REMOVED CO DETECTOR, INSTALLED NEW PIN 4S2-201­006. REINSTALLED CONSOLE PANEL.

3. OPENED BAG BAY, OPENED AVIONICS PANEL, DISCONNECTED COM 1 CONNECTION. VERIFIED CONNECTOR, VERIFIED SHIELDING AND VERIFIED RESISTANCE TO COM 1. CABLE GOOD, CLOSED AVIONICS PANEL AND CLOSED BAG BAY.

4. 5B-07-017 AVIDYNE GLARESHIELD NIA DUE TO G1000 AIRCRAFT.

Page 1 of 2

Turltoprop Man.,_ment, Inc. 970 Ben Epps Drive * Athens, Georgia 30605 * 706-546-7969

AIRFRAME LOG ENTRY

ACFT: N1241G MFG: CESSNA HOBBS: 136.9 DOM: BRGHT FWD MIN: LC41-SS0FG TACH: NIA DATE: 07-16-08 SIN: 41777 AFTT: 136.9

5. REMOVED DOOR TREADS, BOTH DOOR POST PANELS AND OVERHEAD PANEL, INSTALLED ROSEN SUN VISOR lAW STC #101838SE AND ROSEN INSTALLATION INSTRUCTIONS. REINSTALLED DOOR TREADS, DOOR SIDE POST PANELS AND OVERHEAD PANEL, All. ASSOCIATED SYSTEMS OPS CHECKED GOOD.

6. POWERED UP SYSTEM, LOADED SOFTWARE AND CONFIGURATION FILES FOR GMU1 AND GRS1. REBOOTED AND PERFORMED OPERATIONAL TEST lAW GARMIN GlOOO FOR C400 MM Wn-H NO DISCREPANCIES NOTED.

7. SERVICED 02 SYSTEM FROM 400 PSI TO 1800 PSI.

,. .

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Athffn~

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AERO INDUSTRIES, INC 5745 HUNTSMAN RD. RICHMOND INTL AIRPORT

VA. , 23250 -2411

COMPLIED WITH THE FOLLOWING IN ACCORDANCE WITH CESSNA COLUMBIA 400 AMM UNLESS OTHERWISE NOTED: PRELIMINARY INSPECTION PER AERO INDUSTRIES, INC. FORM 005. COMPLIED WITH PAINT AND BODY WORK ON TOP AND BOTTOM COWLINGS IN ACCORDANCE WITH CESSNA 400 AMM CHAPTER 51-70-00.REPAIRED NOSE AND MAIN WHEEL PANTS IN ACCORDANCE WITH CHAPTER 51 TO ELIMINATE PAINT CHIPS. REPAIRED CARBON FIBER BAFFLE/FAIRING ACROSS FRONT OF ENGINE INSIDE COWLING IN ACCORDANCE WITH CHAPTER 51-70-00. INSTALLED EXTENDED PROTECTIVE PAINT KIT AND PROTECTIVE PAINT RUBBER BOOT KIT PER KIT INSTRUCTIONS. REPAIRED NOSE AND MLG VERTICAL FAIRINGS TO REMOVE CHIPS IN PAINT IN ACCORDANCE WITH CHAPTER 51-70-00. REPAIRED LH AND RH WING SURFACES TO REPAIR PAINT CHIPS AND SCRATCHES AROUND WALKWAY AREAS IN ACCORDANCE WITH CHAPTER 51-70-00. REPAIRED PAINT CHIPS ON RH DOOR LEDGE, LOWER SIDE PER CHAPTER 51-70-00. REPAIRED FILLER CRACKS UNDER WING AT FUSELAGE ON LH AND RH SIDES PER CHAPTER 51-70-00. ALL PAINTING AND POLISHING ACCOMPLISHED IN ACCORDANCE WITH CESSNA 400 AMM CHAPTER 51 TO MATCH PAINT SCHEME OF FACTORY PAINT JOB. COMPLIED WITH FINAL INSPECTION FOR WORK ACCOMPLISHED UNDER THIS WORK ORDER. AIRCRAFT TOTAL TIME: 149.3 HOURS

DESCRIBED ABOVE WAS INSPECTED AND REPAIRED IN ACCORDANCE WITH CURRENT

RESPECT TO THE WORK PERFORMED, THE AIRCRAFT IS APPROVED FOR RETURN TO SERVICE. DETAILS OF THIS INSPECTION AND/OR REPAIR ARE ON FILE AT

FACILITY UNDER WORK ORDER No. 50:z.61.

~~CRSCERTIFICATE No: BIER466C

CHIEF INSPECTOR

"­970 Ben Epps Drive' Athens, Georgia 30605' 706-546-7969

N1241G MFG: CESSNA HOBBS: 152.5 BRGHTFWD MIN: LC41-550FG TACH: N/A 9-23-08 SIN: 41777 AFTT: 152.5

ADJUSTED RIGHT FLAP OUTBOARD PUSH-PULL TUBE ROD END, TIGHTENED JAM NUTS AND COTTER PINNED FINAL DRIVE NUT.

ALL WORK PERFORMED IN I~CCORDANCE WITH CURRENT FEDERAL AVIATION REGULATIONS AND

MANUFACTURER'S MAINTENA~NUALS. THE AIRFRAME IDENTIFIED ABOVE HAS BEEN INSPECTED, WAS

DETERMINED T07IN AIRWORT ~mO~D IS AP~~RETURN TO SERVICE.

" ~ ~ /~ ,;1 .M~ 'l'_ '/0­~ </ Samuel . Humbles AP240113770lA ­

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IENTER IN : AIRFRAME RECORD I

THE MAINTENANCE TECHNICAL DATA AND FAA REGULATIONS AND WITH

THIS REPAIR

SIGNATURE:

-Athen.s ~ Turboprop Man-.ement. Inc.

AIRFRAME LOG ENTRY

ACFT: DOM: DATE:

1.

DATE - 19 SEPT 2008 MAKE - CESSNA M/N - LC41-550FG S/N- 41777 REG. # N 1 241 G

TIME - 149.3

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Athen~

Turboprop

TACH OR RECORDING DESCRIPTION OF WORK PERFORMED­

METER SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK TIME

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AtanaMement. Inc. 970 Ben Epps Drive" Athens, Georgia 30605 * 706-546-7969

AIRFRAME lOG ENTRY

ACFr: N12'11G MFG: CESSNA HOBBS: 177.7 DOM: BRGI·rr FWD MIN: LC41-550FG TACH: NIA DATE: 10-13-08 SIN: 41777 AFTT: 177.7

1. REMOVED PROP SPINNER AND TOP ENGINE COWL, REMOVED ALL 3 PROP DEICE BOOTS AND ALL OLD ADHESIVE, PREPPED ALL SURFACES AND INSTALLED NEW PROP DEICE BOOTS AND RESTRAINER STRAPS lAW Sr'lR TECHNOLOGIES REPORT #97-33-013, EDGE SEALED ALL PROP DEICE BOOTS. RElNSTAl.lED PROP SPINNER.

2. REMOVED AND REPLACED #1 AND #3 CHT PROBES WITH NEW. OPS CHECK GOOD. 3. JACKED AIRCRAFT, REf"10VED TOP AND BOTTOM ENGINE COWLS FOR STRUT REPLACEMENT AND CHT/EGT

REPLACEMENTS. REMOVED NOSE WHEEL ASSY, REMOVED NOSE STRUT AND REPLACED WITH NEW PIN LA71325000RA SIN SL030, SHIMMY DAf"lPENING AND SELF-CENTERING CHECKED GOOD. RElNSTAl.lED NOSE WHEEL ASSY AND COWLS AND DOWN JACKED AIRCRAFT. ALL WORK DONE lAW CESSNA 300 MM.

4. REMOVED AND REPLACED #3 AND #5 EGT PROBES WITH NEW. OPS CHECK GOOD.

REGULATIONS AND

;~~~~ INSPECTED, WAS

Page 1 of 1

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Athens ~ Turboprop

Manasement. 'nc. 970 Ben Epps Drive' Athens, G]orgia 30605 • 706.546.7969

AIRFRAME lOG ENTRY

ACFT: N1241G MFG: (ESSNA HOBBS: 179.1 DOM: BRGHT FWD MIN: L.C41-550FG TACH: NIA DATE: 10-17-08 SIN: 41777 AFTT: 179.1

1. JACKED AIRCRAFT, REMOVED 'OP AND BOlTOM ENGINE COWLS, REMOVED NOSE WHEEL AND FORK ASSY, CLEANED ALL PARTS OF LEAKED HYDRAUUC OIL, REMOVED NOSE STRUT PIN LA71325000RA SIN SL030 AND INSTALLED NEW PIN LA71325000RA SIN SL037 lAW CESSNA 400 MM 32-30-00. REINSTALLED ENGINE COWLS AND NOSEWHEEL AND FORK ASSY. OOWNJACKED AIRCRAFT.

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TOTAL TACH OR TIME RECORDING DESCRIPTION OF WORK PERFORMED-­DATE

IN METER SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK SERVICE TIME

TOTAL brought forward from previous page

Athen$

Turboprop

Mana••ment, Inc. 970 Ben Epps Drive * Athens, Georgia 30605 * 706·546..7969

AIRFRAME LOG ENTRY

ACFT: N1241G MFG: CESSNA HOBBS: 202.7 DOM: 2007 MIN: LC41-550FG TACH: N/A DATE: 02-03-09 SIN: 41777 AFTT: 202.7

1. COMPLIED WITH ANNUAL INSPECTION lAW CESSNA 400 MM AND FAR 43 APPENDIX D. 2. COMPLIED WITH 5B-08-34-05 (G1000 SOFTWARE UPGRADE) lAW INSTRUCTIONS PROVIDED

AND GARMIN G1000 LINE MM FOR -rHE CESSNA 350/400. OP CHECK GOOD. 3. COMPLIED WITH 5B-08-32-01 (GEAR LEG CHAFING) BY JACKING AIRCRAFT, REMOVING WHEEL

AND AXLE ASSEMBLES. REMOVED MLG LEG FAIRINGS. COMPLIED WITH INSTRUCTIONS PROVIDED BY CESSNA SB-08-32-01. REINSTALLED LEFT FAIRINGS, WHEEL, AND AXLE ASSEMBLIES AND WHEEL FAIRINGS. ALL WORK DONE lAW SB-08-32-01 AND CESSNA 400 MM.

4. REMOVED AND REPLACED NOSE STRUT ASSEMBLY WITH NEW DUE TO SHIMMYING OF WHEEL. 5. TIGHTENED ROSEN VISOR lAW ROSEN VISOR SERVICE INSTRUCTIONS. 6. REMOVED PROP DE-ICE BOOT RESTRAINER STRAP AND OLD ADHESIVE. INSTALLED NEW

RESTRAINER STRAP lAW SMR TECHNOLOGIES INSTALLATION MANUAL #97-33-013. 7. ADJUSTED MANIFOLD PRESSURE lAW TCM TSIO-550 MM AND SET UP FUEL lAW TCM SID #97-3E. 8. REMOVED ELECTRICAL CONTROL UNIT AND INSTALLED NEW UNIT. POWERED ON SYSTEM, OPS

CHECK GOOD. 9. C-RAY AVIONICS COMPLIED WITH FAR 91.411 (ALTIMETER) AND FAR 91.413 (TRANSPONDER)

CHECKS. SEE AVIONICS LOGS. Page 1 of'1

Turboprop Ma_t.lnc.

970 Ben Epps Drive' Athens, Georgia 30605 • 706-546-7969

AIRFRAME LOG ENTRY

ACFT: N1241G MFG: CESSNA HOBBS: 202.7 DOM: 2007 MIN: LC41-550FG TACH: N/A DATE: 02-03-09 SIN: 41777 AFTT: 202.7

10. REMOVED ELT, INSPECTED AND TESTED lAW FAR 91.207{D) WITH NO DISCREPANCIES NOTED. REINSTALLED. BATTERY NEXT DUE JULY 2012.

11. REMOVED INDUCTION AIR FILTER ELEMENT AND REPLACED WITH NEW lAW CESSNA 400 MM. 12. COMPLIED WITH AD 2007-07-06 (LINEAR BEARING INSP) lAW INSTRUCTIONS PROVIDED BY

CESSNA 5B-07-002C WITH NO DEFECTS NOTED. 13. COMPLIED WrrH 5B-07-005 (MLG BUSHING INSP) BY VISUAL INSPECTION OF LANDING GEAR

BUSHINGS WITH NO DEFECTS NOTED. ALL WORK DONE lAW INSTRUCTIONS PROVIDED AND CESSNA 400 MM.

14. COMPLIED WITH 5B-07-011B (KELLY AEROSPACE TURBOCHARGERS). NOT APPLICABLE BY SIN. 15. COMPLIED WITH 5B-07-012 (GARMIN SERVICE ALERT)- NOT APPLICABLE DUE TO SOFTWARE

LEVEL 0530.05. 16. COMPLIED WITH 5B-07-014 (VFR ONLY)- NOT APPLICABLE DUE TO AHRS MOD LEVEl/SERIAL

NUMBER. 17. COMPLIED WITH 5B-07-016A (SOFTWARE UPGRADE PON). VERIFIED BY SOFTWARE LEVEL

0530.05.

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METERIN SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK SERVICE TIME

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Athens

Turboprop

Manalement, Inc. 970 Ben Epps Drive * Athens, Georgia 30605 * 706.546-7969

AIRFRAME LOG ENTRY

ACFT: N1241G MFG: CESSNA HOBBS: 202.7 DOM: 2007 MIN: LC41-550FG TACH: N/A DATE: 02-03-09 SIN: 41777 AFTT: 202.7

18. COMPUED WITH 58-07-018 (ACCESS PANEL PCW), VERIFIED PANEL INSTALLATION BY VISUAL INSPECTION.

19. TIGHTENED PITOT UNE CONNECTION lAW CESSt.JA 400 MM. COMPUED WITH PART 43 APPENDIX E. LEAK CHECKED WITH NO DISCREPANCIES NOTED.

20. REMOVED RIGHT MLG WHEEL FAIRINGS, REMOVED AND DISASSEMBLED KIGHT MLG WHEEL ASSY. BUILT UP NEW RIGHT MLG WHEEL ASSY WITH NEW TIRE TUBE AN.:> NEW TIRE. REPACKED BEARINGS AND INSTALLED RIGHT MLG WHEEL ASSY. INSTAllED RIGtiT MLG WHEEL FAIRINGS. ALL WORK DONE lAW CESSNA 400 MM AND CLEVELAND MM.

21. REMOVED LEFT MLG WHEEL FAIRINGS, REMOVED AND DlSASSEMBl£l) LEFT MLG WHEEL ASSY. BUILT UP NEW LEFT MLG WHEEL ASSY WITH NEW TIRE TUBE AND NEW TIRE. REPACKED BEARINGS AND INSTALLED LEFT MLG WHEEL ASSY. INSTAllED LEFT MI.G WHEEL FAIRINGS. ALL WORK DONE lAW CESSNA 400 MM AND CLEVELAND MM.

22. REMOVED, CLEANED, AND INSPECTED NOSE WHEEL BEARINGS WITH NO DISCREPANCIES NOTED. BALANCED NOSE WHEEL, REPACKED AND INSTALLED BEARINGS. ALL WORK OONE lAW CESSNA 400 MM.

Page 3 of 4

-----------------------------.j

Athft'$

Turboprop Mamllement. Inc.

970 Ben Epps Drive' Athens, Georgia 30605 • 706-546-7969 AIRFRAME LOG ENTRY

ACFT: N1241G MFG: CESSNA HOBBS: 202.7 DOM: 2007 MIN: LC41-550FG TACH: N/A DATE: 02-03-09 SIN: 41777 AFTT: 202.7

23. BLED BRAKES lAW CESSNA 400 MM. 24. JACKED AIRCRAFT, REMOVED NOSE WHEEL FAIRING AND BOTH MLG WHEEL FAIRINGS. FOUND RH

MLG WHEEL ASSY WITH BROKEN BOLT AND WARPED WHEEL ASSEMBlY. RESEARCHED AIRCRAFT LOGS AND NO TIRE HAS BEEN CHANGED ON AIRCRAFT SINCE PURCHASED NEW FROM CESSNA. DIAGNOSED PROBLEM TO WHEEL ASSY CAUSING VIBRATION AT WHEEL HALVES. ASSEMBLY REQUIRES REPLACEMENT.

25. REMOVED ALL BRAKE LININGS AND REPLACED WITH NEW lAW CESSNA 400 MM. 26. REMOVED GFID TOWER, REMOVED CUMATE CONTROL HEAD. INSTALLED NEW CUMATE CONTROL

HEAD AND REINSTALLED GFID TOWER. OPS CHECKED GOOD.

AVIATION REGULATIONS AND VE BEEN INSPECTED, WAS

~~JRP-$Rf SERVICE.

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" L&M AIRCRAFT INC. ROME, GA 30165

. N1241G Columbia LC41-550-FG SiN 41777 August 28,2009 Tach 230.9f Removed Rudder and inspected hing~ckets in accordance with AD 2009-09-09 and Cessna SB09-27-0l. No cracks at this time. %~ Mitchell Todd Bone /' /" "/"': A&P 255653270 ( ~

At".". ~ Turboprop Mana.."..,..t. Inc.

970 Ben Epps Drive' Athens, Georgia 30605' 706-546-7969

AIRFRAME LOG ENTRY

ACFT: N1241G MFG: CESSNA HOBBS: 211.2 DOM: 2007 MIN: LC41-SS0FG TACH: N/A DATE: 03-21-09 SIN: 41777 AFTT: 211.2

1. REMOVED ENGINE UPPER AND LOWER COWLINGS AND REMOVED NOSE WHEEL ASSY. CHECKED BALANCE OF NOSE WHEEL WITH NO DEFECfS NOTED. REMOVED STRUT FAIRING AND NOSE STRUT. INSTALLED NEW STRUT PjN LA7132S000 REV. A SjN lSA200jRSLOOS. REINSTALLED NOSE WHEEL ASSY TO STRUT PER CESSNA MM. RECOWLED ENGINE UPPER AND LOWER COWLINGS.

ALL WORK PERFORMED IN ACCORDANCE WITH CURRENT FEDERAL AVIATION REGULATIONS AND MANUFACTURER'S MAl NANCE MANUALS. THE AIRFRAME IDENTIFIED ABOVE HAS BEEN INSPECfED, WAS DETERMINED TO BE RWORTHY CO ." ~ AND I OVED F TO SERVICE.

samuel R. Humbles AP240113770IA

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At".". ~ Turboprop Man....,nent. Inc.

970 Ben Epps Drive' Athens, Georgia 30605' 706-546-7969

AIRFRAME LOG ENTRY

ACFT: N1241G MFG: CESSNA HOBBS: 216.1 DOM: 2007 MIN: LC41-550FG TACH: N/A DATE: 04-01-09 SIN: 41777 AFTT: 216.1

1. REMOVED ENGINE UPPER AND LOWER COWLINGS AND REMOVED NOSE WHEEL ASSY. CHECKED BALANCE OF NOSE WHEEL WITH NO DEFECfS NOTED. REMOVED STRUT FAIRING AND NOSE STRUT. INSTALLED NEW STRUT PjN LA7132S000 REV_A SjN-RSL016TM SO# 2346973. REINSTALLED NOSE WHEEL ASSY TO STRUT PER CESSNA MM AND SL-06-004. RECOWLED ENGINE UPPER AND LOWER COWLS. OPS CHECK GOOD.

2. REMOVED RH INNER DOOR PANEL TO FREE UP DOOR LATCH ASSY. REMOVED RH DOOR INNER LOCK ASSY. INSTALLED PjN S22-XA LATCH ASSY. OPERATIONAL CHECK PERFORMED SATISFACfORY. ALL WORK DONE lAW CESSNA MM.

ALL WORK PERFORMED IN ACCORDANCE WITH CURRENT FEDERAL AVIATION REGULATIONS AND MANUFACTURER'S MAINTENANCE MANUALS. THE AIRFRAME IDENTIFIED ABOVE HAS BEEN INSPECTED, WAS DETERMINED TO N AIRWORTHY~]P10N AN S APPROVED FO RETURN TO SERVICE.

~d-e/lr ~q# samuel R. Humbles AP2401l377OI

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1

L&M AIRCRAFT INC. ROME, GA 30165

N1241G Columbia LC41-550-FG SiN 41777 August 28,2009 Tach 230.9

Removed Rudder and inspected hinge brackets in accordance with AD 2009-09-09 and Cessna SB09-27-01.

No cracks at this time. /J~~ Mitchell Todd Bone /J/l/h A&P 255653270

=~~.---L~_~---l .. _---~

" . 2601 Cessna Lane Kennesaw, GA 30144 770-427-4954 "~P ~ LOG 10# 12108 03-December-2009 WO# 9532 ., N1241G SIN 41777 COLUMBIA LC41-550FG

Pg 1/1

Pg 1/1

I III ... .' 2601 Cessna Lane Kennesaw, GA 30144 770-427-4954".-P~ LOG 10# 12302 01-March·2010 WO# 10057 ., N1241G SIN 41777 COLUMBIA LC41-550FGIIDIIII AC TT 251.7 HOBBS 251.7

*** AIRFRAME LOG ENTRY ***

ANNUAL INSPECTION COMPLETED. THE FOLLOWING AD'S WERE COMPLIED WITH DURING THIS ANNUAL: AD 2009-09-09 p/C/W AS PER S/B 09-27-01R2 AD 2007-07-06R1 BY INSPECTION AS PER S/B 07-002D NO DEFECTS NOTED ­NEXT DUE MARCH 2011, AD 2009-24-52E N/A NO LIFTER CHANGES DURING TIMES INDICATED~ AD 2007-26-09 N/AALL BLADES START WITH "K". REPLACED THE FOLLOWING: RIGHT BRAKE SHIM P/N 068-0110u AND LEFT NAV LAMP P/N A508-28v. C/W S/B 07-002D. SERVICED OXYGEN. SERVICED NOSE STRUT. RETORQUED LEFT OUTBOARD FLAP BRACKET. CHECKED HEAT SYSTEM AIR FLOW - COULD NOT DUPLICATE WRITE-UP - GOOD FLOW FROM DEFROST AND FLOOR VENTS. SERVICED TIRES. LUBRICATED AIRCRAFT. SERVICED BATTERY. COMPLETED REQUIRED AD'S. INSPECTED ELT S/N 04301 IN ACCORDANCE WITH FAR 91.207D (d1)(d2)(d3)(d4). REPACKED WHEEL BEARINGS. BLED BRAKES. VISUALLY INSPECTED BRAKES AND LININGS. C/W S/B 09-53-01 BY INSPECTION AND INSTALLATION OF LEFT AND RIGHT GUSSETS P/N 2810303-7 & P/N 2810303-8. REPLACED NAV LAMP ASSY P/N 2828102-9. C/wS/B 09-21-01 BY ROUTING HOSES AWAY FROM EXHUAST - SERVICED AIRCONDITION SYSTEM WITH R34 FREON. C/WS/B 09-34-02 BY INSPECTION COCKPIT REFERENCE GUIDE P/N 190-00567-01REV - PRESENT. c/w S/B 10-34-01 BY UPLOADING GARMIN 1000 TO 534.13 - ALL CHECKS NORMAL - P/N 190-0056-03 REV A - PRESENT. C/W S/B09-34-10 BY INSPECTION - NO INTERFERENCE BETWEEN KNOBS. I CERTIFY THAT THIS AIRCRAFT AND/OR ENGINE HAS BEEN INSPECTED IN ACCORDANCE WITH A/AN ANNUAL INSPECTION AND DETERMINED TO BE IN AIRWORTHY CONDITION.

MAINTENANCE RELEASE. THIS AIRCRAFT, AIRFRAME, AIRCRAFT ENGINE, OR APPLIANCE IDENTIFIED ABOVE WAS REPAIRED AND INSPECTED IN ACCORDANCE WITH CURRENT MAINTENANCE RULES OF THE FEDERAL AVIATION REGULATIONS AND IS APPROVED FOR RETURN TO SERVICE FOR WORK PERFORMED UNDER WO#10057 AT REPAIR STATION DK7R795J. PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THIS REPAIR STATION.

sig

*** AIRFRAME LOG ENTRY ***

C/W S/B 09-27-01R2 BY INSTALLING KIT MK400-27-01 - AD 2009-of-09 C/W AS PER S/B 09-27-01R2.

MAINTENANCE RELEASE. THIS AIRCRAFT, AIRFRAME, AIRCRAFT ENGINE, OR APPLIANCE IDENTIFIED ABOVE WAS REPAIRED AND INSPECTED IN ACCORDANCE WITH CURRENT MAINTENANCE RULES OF THE FEDERAL AVIATION REGULATIONS AND IS APPROVED FOR RETURN TO SERVICE FOR WORK PERFORMED UNDER WO#9532 AT REPAIR STATION DK7R795J. PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT T IS REPAIR STATION.

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2601 Cessna Lane Kennesaw, GA 30144 770-427-4954 LOG 10# 12377 02-April-2010 WO# 14152

Pg 1/1N1241G SIN 41777 COLUMBIA LC41-550FG HOBBS 272.5

*** AIRFRAME LOG ENTRY ***

RIGHT CABIN DOOR WILL NOT LOCK - REPLACED LOCK ASSEMBLY piN 522-XA. REPLACED LEFT AFT NAV LAMP piNLB57332003-1-A DUE TO BROKEN CERAMIC HOLDER.

MAINTENANCE RELEASE. THIS AIRCRAFT, AIRFRAME, AIRCRAFT ENGINE, OR APPLIANCE IDENTIFIED ABOVE WAS REPAIRED AND INSPECTED IN ACCORDANCE WITH CURRENT MAINTENANCE RULES OF THE FEDERAL AVIATION REGULATIONS AND IS APPROVED FOR RETURN TO SERVICE FOR WORK PERFORMED UNDEE WO#10126 AT REPAIR STATION DK7R795J. PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THIS REPAIR STATION.

;rlt~f.;~TION' INC

2601 Cessna Lane Kennesaw, GA 30144 770-427-4954 LOG 10# 12542 26-May-2010 WO# 10216

Pg 1/1p~"~ - N1241G SIN 41777 COLUMBIA LC41-550FG AC TT 278.3 HOBBS 278.3

• *** AIRFRAME LOG ENTRY ***

REPLACED RIGHT NAV LAMP pIN A7512-24. REPAIRED PILOTS DOOR SEAL.

MAINTENANCE RELEASE. THIS AIRCRAFT, AIRFRAME, AIRCRAFT ENGINE, OR APPLIANCE IDENTIFIED ABOVE WAS REPAIRED AND INSPECTED IN ACCORDANCE WITH CURRENT MAINTENANCE RULES OF THE FEDERAL AVIATION REGULATIONS AND IS APPROVED FOR RETURN TO SERVICE FOR WORK PERFORMED UNDER wo#10216 AT REPAIR STATION DK7R795J. PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THIS REPAIR STATION.

l--j---1L---+------------------------I

2601 Cessna Lane Kennesaw, GA 30144 770-427-4954 LOG 10# 12730 19-July-2010 WO# 10262 N1241G SIN 41777 COLUMBIA LC41-550FG AC TT 280.3 HOBBS 280.3

p~"~ IIIIIIII

Pg 1/1

'r*;, AIRFRAME LOG ENTRY *,,;,

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-~-

-~AthMS

Turboprop Man_Bement, Inc. -970 Ben Epps Drive· Athens, Georgia 30605 • 706·546-7969

AIRFRAME LOG ENTRY -ACFT: N1241G MFG: CESSNA HOBBS: 286.0

DaM: 2007 MIN: LC41-550FG TACH: N/A DATE: 08-27-10 SIN: 41777 AFTT: 286.0

1. COMPUED WITH ANNUAL/l00 HOUR INSPECTION lAW CESSNA 400 M/M AND FAR 43 APPENDIX D. ­

2. COMPLIED WITH 5Bl0-32-01 (NOSE STRUT SHIM AND FASTENER HOLE INSPEffiON) BY INSPEffiON OF FASTENER HOLES WITH NO DISCREPANOES NOTED, INSPECTION OF NOSE ­STRUT AND STRUT SOCKET GAP WHICH WAS FOUND TO BE OUT OF TOLERANCE, AND INSTALLATION OF SHIM BETWEEN STRUT AND STRUT SOCKET. ALL WORK ACCOMPLISHED IAW -SB10-32-01 INSTRUCTIONS AND CESSNA 400 M/M.

3. FOUND 5Bl0-81-01 N/A DUE TO TURBOCHARGER PART NUMBERS AND SERIAL NUMBERS. -4. COMPLIED WITH 5Bl0-78-01 (ENGINE EXHAUST SYSTEM TURBOCHARGER TRANSmON

INSPECTION) BY VISUAL INSPECTION OF l/H AND RfH ENGINE EXHAUST TURBO TRANSmONS FOR CRACKS WITH NO DISCREPANCIES NOTED. ALL WORK ACCOMPUSHED IAW SBlO-78-01 ­INSTRUCTIONS AND TCM 5Bl0-l.

-

-Page 1 of6

-

Turboprop

ManaBement. Inc. 970 Ben Epps Drive * Athens, Georgia 30605 • 70~546-7969

AIRFRAME LOG ENTRY

ACFT: DaM: DATE:

N1241G 2007 08-27-10

MFG: MIN: SIN:

CESSNA LC41-550FG 41777

HOBBS: TACH: AFTT:

286.0 N/A 286.0

5. COMPLIED WITH 5Bl0-71-01 (ENGINE CRANKCASE INSPECTION) BY INSPECTING SUSPECT AREA FOR CRACKS WITH NO DISCREPANCIES NOTED. REMOVED AlC COMPRESSOR, STARTER, AND AlC COMPRESSOR BRACKET. REPLACED AlC COMPRESSOR BRACKET wrrn NEW STYLE BRACKET, TORQUED IT TO SPECS. REINSTALLED STARTER USING NEW O-RING AND REINSTALLED AlC COMPRESSOR. ALL WORK ACCOMPLISHED lAW INSTRUCTIONS PROVIDED IN TCM 5B09-4A AND SBlO-71-01.

6. COMPLIED WITH 5Bl0-28-01 (GASCOLATOR AND FUEL MANIFOLD VALVE INSPECTION) BY REMOVING GASCOLATOR BOWL, GASCOLATOR SCREEN, AND FUEL MANIFOLD VALVE. DISASSEMBLED FUEL MANIFOLD VALVE. INSPECTED GASCOLATOR SCREEN AND FUEL MANIFOLD VALVE SCREEN FOR FIBER OR LINT-TYPE FOREIGN DEBRIS wrrn NO DISCREPANCIES NOTED. REASSEMBLED FUEL MANIFOLD VALVE AND INSTALLED GASCOLATOR SCREEN, GASCOLATOR BOWL, AND FUEL MANIFOLD VALVE. ALL WORK ACCOMPLISHED IAW SB10-28-01 INSTRUCTIONS AND CESSNA 400 M/M.

Page 2 of 6

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Turboprop Man_Ie.".nt, Inc.

970 Ben Epps Drive' Athens, Georgia 30605 • 706-546-7969 AIRFRAME LOG ENTRY

ACFT: N1241G MFG: CESSNA HOBBS: 286.0 DOM: 2007 MIN: LC41-550FG TACH: N/A DATE: 08-27-10 SIN: 41777 AFTT: 286.0

7. COMPUED WITH 5810-55-01 (HORIZONTAL STABILIZER TUBE INSPECTlON) BY REMOVING ELEVATORS, RUDDER, AND HORIZONTAL STABILIZERS. INSPECTED HORIZONTAL STABILIZER TUBES WITH NO DISCREPANCIES NOTED. REINSTALLED HORIZONTAL STABILIZERS, RUDDER, AND ELEVATORS. OPS CHECKED ELEVATORS AND RUDDER, OPS CHECKED GOOD. ALL WORK ACCOMPUSHED lAW CESSNA 400 MIM AND SBlO-55-01 INSTRUCTlONS.

8. COMPLIED WITH 5809-71-02 (ENGINE OIL COOLER WINTERIZATION MODIFICATION) BY INSTALLATION OF OIL COOLER WINTERIZATION SYSTEM. ALL WORK ACCOMPLISHED lAW SB09­71-02 INS1RUCTlONSAND INS1RUCTlONS PROVIDED IN MK400-71-01.

9. COMPUED WITH 5810-11-01 (P.O.H. REVISIONS) BY INSTALLATION OF TEMPORARY REVISION IN THE P.O.H. lAW SB10-11-01 INSTRUCTlONS.

10. COMPLIED WITH A02007-07-06 (LINEAR BEARING) lAW INSTRUCTlONS PROVIDED IN 58-07­0020 (LINEAR BEARING INSPECTlON). VISUALLY INSPECTED ALL LINEAR BEARINGS. AILERON UNEAR BEARINGS DAMAGED DUE TO IMPROPER LUBRICATION. REPLACEMENT OF LINEAR BEARINGS WITH NEW STYLE BEARINGS REQUIRED.

Page 30f6

Ath~s ~ Turboprop

Manaaeme-nt. Inc. 970 Ben Epps Drive" Athens, Georgia 30605" 706.546-7969

AIRFRAME LOG ENTRY

ACFT: N1241G MFG: CESSNA HOBBS: 286.0 DOM: 2007 MIN: LC41-550FG TACH: N/A DATE: 08-27-10 SIN: 41777 AFTT: 286.0

11. REMOVED L./H AND R/H SPEEDBRAKES AND LOGIC CONTROL BOX. CONNECTED SPEEDBRAKES TO ALC BOX WITHOUT USING AIRCRAFT HARNESS WITH R/H SPEEDBRAKE WORKING INTERMmENTLY. NO ALC BOX AVAILABLE FOR -2 SPEEDBRAKES. UPDATED AND INSTALLED NEW PIN 300S0003-4 SPEEDBRAKES (L./H SIN 985395, R/H SIN 985396) AND NEW LOGIC BOX PIN 010S0302-1 SIN ALC2264. OPS CHECKED GOOD.

12. CLEANED LEADING EDGE OF WINGS AND REPLACED ALL TURBULATOR TRIANGLES WHERE MISSING OR LOOSE.

13. REMOVED LEFT AILERON PUSH-PULL ROD, REMOVED LEFT AILERON UNEAR BEARING, INSTALLED NEW STYLE LINEAR BEARING PIN LA57272600 AND BRACKET PIN 2861104-1, REINSTALLED LEFT AILERON PUSH-PULL ROD IN WING. ALL WORK ACCOMPUSHED lAW CESSNA 400 MIM WITH REFERENCE TO IPC. RIGHT AILERON LINEAR BEARING DAMAGED AND CONTAMINATED DUE TO IMPROPER LUBRICATION. REMOVED RIGHT AILERON PUSH-PULL ROD IN WING, REMOVED LINEAR BEARING, INSTALLED NEW STYLE LINEAR BEARING PIN LA57272600 AND BRACKET PIN 2861104-1, REINSTALLED RIGHT AILERON PUSH-PULL ROD. ALL WORK ACCOMPLISHED lAW CESSNA 400 MIM WITH REFERENCE TO IPC.

Page 4 of6

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Athen5 ~ Turboprop Management, Inc.

970 Ben Epps Drive' Athens, Georgia 30605' 706-546-7969

AIRFRAME LOG ENTRY

ACFT: N1241G MFG: CESSNA HOBBS: 286.0 DOM: 2007 MIN: LC41-550FG TACH: N/A DATE: 08-27-10 SIN: 41777 AFTT: 286.0

14. REMOVED EXTERIOR PANEL AROUND l/H STEP, PUSHED UGHT ASSEMBLY OUT, AND FOUND A BROKEN WIRE. RECONNECTED BROKEN WIRE TOGETHER WITH BtJTT SPUCE. OPS CHECK FAILED. TROUBLESHOT AND FOUND FUSE BLOWN. REPLACED BLOWN FUSE WITH NEW AND REPLACED STEP UGHT. OPS CHECK GOOD. REINSTALLED UGHT ASSEMBLY AND EXTERIOR PANEL AROUND l/H STEP. ALL WORK ACCOMPUSHED lAW CESSNA 400 M/M.

15. REMOVED AND REPLACED INDUCTION AIR FILTER WITH NEW IAW CESSNA 400 M/M. 16. REMOVED PANEL (BRACKET) OVER AlC EVAPORATOR AND REINSTAllED IN THE CORRECT WAY

lAW CESSNA 400 M/M. 17. REMOVED R/H INBOARD MLG FAIRING AND PREPPED AND REPAIRED, PRIMED AND PAINTED.

REINSTALLED R/H INBOARD MLG FAIRING AFTER PAINTING IAW CESSNA 400 M/M. 18. REMOVED NOSE WHEEL ASSEMBLY AND REMOVED NOSE FAIRING. FAIRING AND PREPPED AND

REPAIRED, PRIMED AND PAINTED. REINSTALLED R/H FAIRING AFTER PAINTING IAW CESSNA 400 M/M.

Page 5 of 6

r----=-:±======±-===d=====-=_--=--=--==-=~.=_====~~~===I _

Turboprop

Management. Inc. 970 Ben Epps Drive"* Athens, Georgia 30605 * 706-546--7969

AIRFRAME LOG ENTRY

ACFT: N1241G MFG: CESSNA HOBBS: 286.0 DOM: 2007 MIN: LC41-550FG TACH: N/A DATE: 08-27-10 SIN: 41777 AFTT: 286.0

19. REMOVED THE THREE FAILED STATIC WICKS AND REPLACED WITH NEW IAW CESSNA 400 M/M. 20. REMOVED AND REPLACED AlC BELT WITH NEW AND TENSIONED IAW CESSNA 400 M/M. 21. REMOVED RIGHT MAIN AXLE FOOT TO F.O.M. (REMOVAL OF l/H OIL PUSH-PULL ROD).

REINSTALLED RIGHT MAIN AXLE FOOT lAW CESSNA 400 M/M. BLED RIGHT BRAKE, OP CHECKED GOOD.

ALL WORK PERFORMED IN ACCORDANCE WIlli CURRENT FEDERAL AVIATION REGULATIONS AND MANUFACTURER'S MAINTENANCE MANUALS. THE AIRFRAME IDENTIFIED ABOVE HAS BEEN INSPECTED, WAS DETERMINED TO BE IN AI ORTHY COND ON AND IS APPROVED FOR RETURN 0 SERVICE.

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11-15-10 N1241G TACH: 315.5 TI: 3155

Complied with AD 2007-07-07 R2 (linear bearings) by inspection and S810-34-02 (Synthetic Vision) by SVT enablennent. Installed new right TIT probe. This aircraft, airframe, aircraft engine, propeller or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Administration and is approved for return to service. Pertinent details of the repair are

on file at this 1(?':Jer/fder 18167.

. ed: """~- Rite-Way AVlalion, Inc nature of authorized representative Repair Station YWYR832L

7814 Eagle Lane, Spring, TX 77379

I I

MAKE: Columbia Aircraft DATE: 211612011Houston Aviation Center, LLC MODEL: LC41-550FG AlC TSN: ­SIN: 41777 12888 Hwy 6 S Ste 113 HOBBS: 322.8 REG. NO: N1241G ~ Sugar Land, TX 77498 USA WORK ORDER: Phone: 281-494-5800 -1804-02-2011

Airframe Entries -Resealed RH brake caliper with (2) new 0- rings Pin MS28775-222. Bled brakes and serviced with hydraulic fluid Pin MIL-H-5606. Operational check satisfactory.... Lubricated induction alternate air cable. Operational check satisfactory.... Installed new TIT probe Pin 86245, SIN 1052 Operational check satisfactory. ­

Maintenance Release -

The aircraft andlor component(s) on N1241 G was repaired andlor inspected in accordance with current requirements of the Federal Aviation Regulations and was found Airworthy for return to service. Pertinent details of the repair are on file at Houston Aviation Center, LLC under Work Order No. 1804-02-2011. ­

DATE: 2116/2011 SIGNED: Work Order: 1804-02-2011 11M; n·~ Pustejovsky, N, A&P: 3194~57 rf

Printed by EBis 3 (datcomedia.com) I ­

MAKE: Columbia Aircraft Houston Aviation Center, LLC DATE: 1213012011MODEL: LC41-550FG AlC TSN: 364.1 ­SIN: 41777 12888 Hwy6 S Sle 113 HOBBS: 364.1 ~ REG. NO: N1241G Sugar Land, TX 77498 USA WORK ORDER: Phone: 281-494-5800 -2233-12-2011

I

Airframe Entries -

Serviced and inslalled (2) new Concord balteries Pin RG 24-10, (LH) SIN 40461806, (RH) SIN 40461807 Operational check satisfactory.

-Maintenance Release

The aircraft andlor component(s) on N1241 Gwas repaired andlor inspected in accordance with currenl requirements of the Federal Aviation Regulations -and was found Airworthy for return to service. Pertinent details of the repair are on file at Houston Aviation Center, LLC under Work Order No. 2233-12-2011.

-• DATE: 12130/2011 SIGNED: 1tid. 1fJ· ,~. Work Order: 2233-12-2011

Pustejovsky, N, A&P: 3194257 V Printed by EBis 3 (datcomedia.com) -

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DATE: 9/1312011MAKE: Columbia Aircraft Houston Aviation Center, LLC NC TSN: 392.9 MODEL: LC41-550FG

12888 Hwy 6 S Sle 113 HOBBS: 392.9 REG. NO: N1241G SIN: 41777

Sugar Land, TX 77498 USA WORK ORDER: Phone: 281-494-5800 2043-07-2011

Airframe Entries

Completed an Annual Inspection this date Ref Cessna Model LC41-55FG MM 5-20. Installed new engine induclion air finer Pin BA345E. ELTwas inspected by Solapp Avionics, Inc. CRS No OSJR598L under W/O 18654. Reinstalled 406 ELT. Baltery expiration date July 2012. Checked AD's thru BW 2011-17. AD 201 0-26-53 & AD 2010-26-54 Wing Skin to Spar Integrity are NIA by SIN.... CW AD 2007-07-os R1 Aileron and elevator bearing inspection by inspecting aileron and elevator linear bearings per Cessna SB-07-0020. No discrepancies noted. Next due: 0812014.... CW AD 2011-03-04 Rudder hinge bracket inspection by inspecting rudder hinge bracket hardware for proper thread engagement lAW Cessna SB-27-03 R3. Proper hingelbracket hardware thread engagement is present this date. Note: Kit Pin MK400-27-o1 was installed 12lO3l2OO9. No further action is required.... Installed new oil cooler damper cable. Pin 05-13172. Operational check satisfactory.... Installed new strobeIposiIion light switch assy. Pin 281 8203-8. Performed operational check and found satisfactory.... Placarded Propeller heat inop and will schedute repair work when R&D Propeller can accommodate.... Installed spacer Pin 2841104-15 on RH wheel fairing.... Installed new LH brake caliper insuIaIor Pin 06B-Q11oo.... I certify that this Airframe has been inspected in accordance with an Annual Inspection and was determined to be in Ainoorthy condition.

Maintenance Release

The aircraft andlor component(s) on N1241G was repaired andlor inspected in accordance with lUT9I1I requirements of the Federal Aviation Regulations and was found Airworthy for relurn 10 service. Pertinent details of the repair are on file at Houston Aviation Center, LLC under Wor1< Order No. 2043-07-2011.

DATE: 9/13/2011 SIGNED: Wort< Order: 2043-07-2011

Fouad Hussain, A&P: 3204861 IA Printed by EBis 3 (datcomedia.com)

DATE: 111112011 MAKE: Columbia Aircraft Houston Aviation Center, LLC NC TSN: 352.7 MODEL: LC41-550FG HOBBS: 352.7 ~•.'. 12888 HWI6 S Ste 113 SIN: 41777 ~ Sugar Land, TX 77498REG. NO: N1241G

Phone: 281-494-5800 WORK ORDER: 2142-10-2011

Airframe Entries . 5DR343X Removed propeller Pin HC-H3YF-1RF, SIN LX337B for installation of deice boots Pin 102196 by R&D Propeller seMce, Inc. CRS No. R under W/O 13216. Reinstalled propeller, operatIonal check satIsfactory.

Maintenance Release . . . ccordan<:e with lUT9I1I reqo.*emenIs of the Federal Aviation Regulations

The aircraft andlor component!s) on N1241 G was r~pa"ed andlor Inspected In a fil at Houst Aviation Center LLC under Work Order No. and was found Airworthy for return to service. Pertinent details of the repair are on eon,

2142-10-2011.

Wort< Order: 2142-10-2011 DATE: 11/1/2011 SIGNED: ~~

Printed by EBis 3 (datcomedia.com) Pustejovsky, N, IA: 3194257

MAKE: Columbia Aircraft MODEL: LC41-550FG SIN: 41777 REG. NO: N1241G

Houston Aviation Center, LLC DATE: 511112012 NC TSN: 392.9

12888 Hwy 6 S Ste 113 HOBBS: 392.9 Sugar Land, TX 77498 USA

WORK ORDER: Phone: 281-494-5800 2426-05-2012

Airframe Entries

Installed new door seal pump Pin C117H-13. Operational check satisfactory.

Maintenance Release

The aircraft andlor component(s) on N1241G was repaired andlor inspected 1'1 accordance with current requirements of the Federal Aviation Regulations and was found Airworthy for return to service. Pertinent details of the repair are on file at Houston Aviation Center. LLC under Wor1< Order No 2426-05-2012. . .

DATE: 5/11/2012 Wort< Order: 2426-05-2012

Printed by EBis 3 (datcomedia.com)

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MAKE: Columbia Aircraft Houston Aviation Center, LLC DATE: 10/2412012MODEL: LC41-550FG NC TSN: 411.2SIN: 41777 12688 Hwy 6 S Ste 113 HOBBS: 411.2 ~ REG. NO: N1241G Sugar Land, TX 77498 USA WORK ORDER: Phone: 281-494-5800 2593-c8-2012

Airframe Entries

Completed an Annual Inspection this date Ref Cessna Model LC41-55FG MM 5-20. Installed new engine induction air filter Pin BA345E. ELTwas inspected by Solapp Avionics, Inc. CRS No OSJR598L under WIO 19452. Reinstalled 406 ELT. Battery expiration date Oct. 2019. Checked AD's thru BW 2012-21 .... CW AD 2007-c7-c6 R1 Aileron and elevalor bearing inspection by inspecting aileron and elevator linear bearings per Cessna SB-c7-C02D. No discrepancies noted. Next due: 1012013.... Installed new engine induction alternate air cable Pin A7oo·Black. Function check satisfactory.... I certify this Airframe has been inspected in accordance with a Annual Inspection and was determined to be in Airworthy condition.

Maintenance Release

The aircraft andlor component(s) on N1241 G was repaired ancIJor inspected in accordance with current requirements of the Federal Aviation Regulations and was found Airworthy for relum to service. Pertinent details of the repair are on file at Houston Aviation Center, LLC under Work Order No. 2593-08-2012.

,DATE: 10/24/2012 SIGNED: Work Order: 2593-08-2012'"J--II-/) -

Fouad Hussain, A&P: 3204861 IA Printed by EBis 3 (datcomedia.com)

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