uh-60a helicopter, utility 8023506 - gsa auctions · uh-60a helicopter, utility 8023506 1. aircraft...

NUMBERLOCATIONPIDENTRYORGANIZATION

8.7.DATE

6.REMARKS

4. 5.

UH-60A 8023506HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL

Report Date: of 12409-Mar-2016

L-3 RASM-E, FTCAMPBELL, KY 42223

OCM/ACE PERFORMED AT 4970.8 ACFT HRSBY TEAM MEMBER UU AND QQ

26-Sep-2012 1

COLUMBUS, OH 43217

FD441686

For use of this form, see DA PAM 738-751; the proponent agency is DCSLOGEDITION OF JAN 64 IS OBSOLETE

HISTORICAL RECORD FOR AIRCRAFTDA FORM 2408-15 E, OCT 91


8.7.DATE

6.REMARKS

4. 5.



1/159TH AVN REGT(FWD)

UH-60-04-ASAM-01 GLARE SHIELD LIGHTINGCIRCUIT BREAKER REPLACEMENT,COMPLIED WITH THIS DATE @ 3329 ACFTHRS. (WC4204)

27-Feb-2004 1

CAMP UDAIRI, KUWAIT

QC000000




8.7.DATE

6.REMARKS

4. 5.



1107TH AVCRADUH-60-04-ASAM-02 ONE TIME INSP OF LOOSET/R DRIVESHAFT FLANGE NUTS C/W (GR2952)

07-Apr-2004 1

CAMP ARIFJAN,KUWAIT

QC000000




8.7.DATE

6.REMARKS

4. 5.



1109 TASMGH-60-14-ASAM-03, ENGINE INLET BARRIERFILTER (EIBF) BRACKET REMOVAL.COMPLIED WITH.

30-Dec-2013 1

GROTON, CT 06340

JA580641




8.7.DATE

6.REMARKS

4. 5.



1109TH AVCRAD(TB 1-1520-237-20-261) ASAM UH-60-02-ASAM-11 AN/ARC 220 WIRING INSPECTION C/W @3069.3 ACFT HRS (MB4514)

02-Oct-2002 1

GROTON, CT

QC000000

1109TH AVCRADUH-60-03-SOF-01 UT INSP OF MAIN MODPLANETARY CARRIER ASSY C/W 3069.3(MR6538)

21-Nov-2002 1

GROTON, CT

QC000000

1109TH AVCRADAIRFRAME STRIPPED USING PMB. PAINTEDIAW CONTRACT # F34601-97-D-0423, CARC MIL-C-53039 (MR6538)

22-Nov-2002 1

GROTON, CT

QC000000

1109TH AVCRADUH-60-03-ASAM-02 TAIL ROTOR SERVORETIREMENT LIFE C/W 3069.3 ACFT HRS(MR6538)

30-Dec-2002 1

GROTON, CT

QC000000

1109TH AVCRADGEN-03-ASAM-01 SINGARS ARC-201 BATTERYBOX C/W 3069.3 ACFT HRS (MR6538)

31-Dec-2002 1

GROTON, CT

QC000000

1109TH AVCRADH-60-10-ASAM -06 (AUTO-IGNITION ANDTRANSIENT DROOP IMPROVEMENT MOD)COMPLIED WITH @ 4457.3 ACFT HRS.

10-Feb-2010 1

GROTON, CT

SS928944

1109TH AVCRADH-60-10-ASAM-04 (SAS LINKS) COMPLIEDWITH @ 4457.3 ACFT HRS.

12-Feb-2010 2

GROTON, CT

SS928944

1109TH AVCRADH-60-09-AMAM-07 (HALON HAND HELD FIREEXTINGUISHERS) COMPLIED WITH @ 4457.3ACFT HRS.

12-Feb-2010 1

GROTON, CT

SS928944

1109TH AVCRADTHE FOLLOWING AWRS APPLY TOWARDSTHIS AIRFRAME;AWR 1309 RV4 DTD 2DEC09OREGON SEAT CUSHIONS, AWR 1656 DTD30DEC09 PHOENIX DRIP PAN, AND AWR 1516RV2 DTD 8JUN09 EBC-406HM ELT

10-Mar-2010 4

GROTON, CT 06340

MB844514

1109TH AVCRADTAIL ROTOR CABLE TENSION SET @ 72DEGREES "F" L/H=145 LBS & R/H=146 LBS

10-Mar-2010 3

GROTON, CT 06340

MB844514

1109TH AVCRADTAIL BIAS COMPLETED;RED 4.478-5.118=.334BLK 4.286-4.615=.329YEL 4.884-5.217=.333BLU 4.294-4.621=.327

10-Mar-2010 2

GROTON, CT 06340

MB844514

1109TH AVCRADUH-60-10-AMAM-11 OIL SAMPLING SCHEDULECHANGES C/W @ 4457.3 ACFT HRS.

10-Mar-2010 1

GROTON, CT 06340

MB844514

1109TH AVCRADTail Rotor Bias Completed at 44665. A/ChoursRED: Initial = 4.758 Bias = 5.088 DIFF =0.330BLK: Initial = 4.182 Bias = 4.515 DIFF =0.333YEL: Initial = 4.827 Bias = 5.159 DIFF =0.332BLU: Initial = 4.205 Bias = 4.531 DIFF =0.326

08-Apr-2010 1

GROTON, CT 06340-5300

EM683732

1109TH AVCRADTHE FOLLOWING AWRS APPLY TOWARDSTHIS AIRFRAME;AWR 1309 RV4 DTD 2DEC09OREGON SEAT CUSHIONS, AWR 1656 DTD30DEC09 PHOENIX DRIP PAN, AND AWR 1516RV4 DTD 29 Mar 2010 EBC-406HM ELT

09-Apr-2010 3

GROTON, CT 06340

EM683732

1109TH AVCRADPMI 2 COMPLETED AT 4457.3 ACFT HRS, PMI 1WILL BE DUE AT 4817.3 ACFT HRS (EM3732)

09-Apr-2010 1

GROTON CT, 06340-5300

EM683732




8.7.DATE

6.REMARKS

4. 5.



1109TH TASMGCOMPLIED WITH H-60-13-AMAM-07 LOASDDEMAND SPINDLE (LDS) CABLE CLEARANCE.FOUND OK

26-Mar-2013 2

GROTON, CT 06340

KI646418

1109TH TASMGCOMPLIED WITH THE REQIUREMENTS OF H-60-13-ASAM-04, PLASTIC MEDIA BLAST (PMB)AND OXIDE FLAKE RESIDUE. FOUND OK

26-Mar-2013 1

GROTON, CT

KI646418

1109TH TASMGCOMPLIED WITH H-60-13-ASAM-05, BREEZEEASTERN VARIABLE SPEED ELECTRICRESCUE HOIST. NOT INSTALLED

12-Apr-2013 1

GROTON, CT

KI646418

1109TH TASMGH-60-13-SOF-01 (ATTITUDE HEADINGREFERENCE SET AHRS) COMPLIED WITH @5067.3 ACFT HRS.

31-May-2013 2

GROTON, CT

SS928944

1109TH TASMGDURING UNSCHEDULED MAINTENANCE ITWAS DISCOVERED THAT THE AIRFRAME HASHAD IN THE PAST MAJOR REPAIRSCOMPLETED AND WHEN RESEARCHEDTHERE IS NO RECORD OF THE REPAIR. THEREPAIRS IN THE CABIN CEILING AREA WEREDEPOT LEVEL AND AFTER FURTHERINSPECTION AND GUIDANCE FROM THEAMCOM LAR AND ENGINEERING AS WELL ASA RECENT ACE INSPECTION THE AIRCRAFT ISDEEMED FLIGHT WORTHY.

31-May-2013 1

GROTON, CT

SS928944

1109TH TASMGH-60-13-AMAM-01 (FLIGHT CONTROL RIGGINGPROCEDURES) COMPLIED WITH @ 5067.3ACFT HRS.

03-Jun-2013 2

GROTON, CT

SS928944

1109TH TASMGH-60-13-ASAM-03 (MAIN ROTOR SPINDLE ANTI-FLAP ASSEMBLIES) COMPLIED WITH @5067.3 ACFT HRS.

03-Jun-2013 1

GROTON, CT

SS928944

1109TH TASMGOCM/ACE PERFORMED AT 5067.3 ACFT HRSBY TEAM MEMBERS L9 + M3

13-Jun-2013 1

GROTON, CT

WS521003

1109TH TASMGMEC # F168046, The 1109th TASMG ofConnecticut is granted permission to useSikorsky AED approved airframe repair toolingspecifically: Sikorsky Enterprise tool kit 70210-02102-041T046 and the cabin heightmeasurement procedure to verify that the FlightDeck’s structural configuration has notchanged significantly due to an extraordinaryand extensive amount of undocumentedstructural repairs.which were discovered duringthe aircrafts induction process. THE RESULTSOF THE NON-DESTRUCTIVE INSPECTIONWERE TURNED IN TO ENGINEERING FORFURTHER GUIDANCE.

21-Jun-2013 1

GROTON, CT 06340

1109TH TASMGH-60-13-AMAM-11 (MAIN TRANSMISSIONFILTER BOWL ATTACHMENT HARDWAREREPLACEMENT) COMPLIED WITH @ 5067.3ACFT HRS.

02-Jul-2013 1

GROTON, CT 06340

SS928944




8.7.DATE

6.REMARKS

4. 5.



1109TH TASMGMEC F168434: Upon completion of the 48month flight control inspection unit had severdificulty Performing the aircraft rig.Upontroubleshooting/fault isolation of the aircraftLAR/Sikorsky FSR noted an extensive amountof sheetmetal repairs to the structure (20Total)and were inquiring if this had any effect.Upon further research it appeared that all therepairs were not documented anywhere. ACFTGRANTED PERMISSION TO REMAIN INSERVICE. 1. The 1109th TASMG, Connecticut isgranted permission to allow Aircraft 80- 23506to remain in service. 2. The Liaison EngineerBill Humes and the Aviation EngineeringDirectoratehas reviewed the request and it isauthorized to keep the aircraft in service aslong as the previous repairs are inspected andthey have been accomplished properly. Beloware the major structural components that werediscovered as repaired/replaced withoutdocumentation:1.) L/H 16.5 beam P/N: 70219-02133-045 2.) R/H 16.5 beam P/N: 70219-02133-046 3.) Sta 360 BL 16.5L to 16.5R (aft xmsnbeam) P/N: 70219-02132-042, was replaced andcurrently cracked 4.) Sta 379 beam P/N: 70211-02114-102 5.) Support-L/H BL 14 Sta 379-398P/N: 70212-02124-101 6.) Support- L/H BL 10.75Sta 379-398 P/N: 70212-02124-102 7.) Channel-L/H BL 5 Sta 361-379 P/N: 70212-02116-107 8.)Channel-R/H BL Sta 361-379 P/N: 70212-02116-108 9.) Web Sta 379-398 P/N: 70212-02113-10110.) Angle Sta 361-379 RH BL0 P/N: 70212-02123-103 11.) Angle Sta 361-379 LH BL0 P/N:70212-02123-109 12.) L/H 34.5 channel P/N:70212-02112-011 13.) R/H 34.5 channel P/N:70212-02112-012 14.) Skin Sta 360-399 L/H BL10 to R/H BL10 P/N: 70213-02101-105 15.) SkinSta 342-398 L/H BL 10 to BL 41 P/N: 70213-02101-145 16.) Entire R/H broom closet from Sta247-265 WL 208-260 17.) Web Sta 281 to 295 BL16.5L P/N: 70212-02113-126 18.) Web Sta 281 to295 BL 16.5R P/N: 70212-02113-127 19.) FormerSTA 189-200 P/N: 70201-01003-109 Cracked 20.)Frame splice STA 485 P/N: 70211-03009-041

09-Jul-2013 1

GROTON, CT 06340

SS928944

1109TH TASMGGEN-13-AMAM-04 (AN/APN-209 RADARALTIMETER SET COMPONENT TRACKING)COMPLIED WITH @5067.3 AIRCRAFT HOURS.

26-Jul-2013 1

GROTON, CT 06340

RB749359

1109TH TASMGH-60-13-AMAM-10 (LCF CHANGE 64REQUIREMENTS) COMPLIED WITH @ 5067.3ACFT HRS.

07-Aug-2013 2

GROTON, CT 06340

SS928944

1109TH TASMGH-60-13-ASAM-06 (PHASE MAINTENANCEINSPECTION PMI CHECKLIST CHANGE)COMPLIED WITH @ 5067.3 ACFT HRS.

07-Aug-2013 1

GROTON, CT 06340

SS928944

1109TH TASMGH-60-12-ASAM-02 (DRAG BEAMREPLACEMENT) COMPLIED WITH @ 5067.3ACFT HRS.

14-Aug-2013 2

GROTON, CT 06340

SS928944




8.7.DATE

6.REMARKS

4. 5.



1109TH TASMGH-60-12-ASAM-01 (TAIL ROTOR OUTPUTBEVEL GEAR NDI) COMPLIED WITH @ 5067.3ACFT HRS.

14-Aug-2013 1

GROTON, CT 06340

SS928944

1109TH TASMGH-60-13-ASAM-10 (WOODWARD HYDRO-MECHANICAL UNIT (HMU) P3 TUBE)COMPLIED WITH @ 5067.3 ACFT HRS.

19-Aug-2013 1

GROTON, CT 06340

SS928944

1109TH TASMGH-60-13-AMAM-15 (CRASHWORTHY EXTERNALFUEL SYSTEM (CEFS) RIGHT HAND FUELCELL COVER PLATE) COMPLIED WITH @5067.3 ACFT HOURS.

26-Sep-2013 1

GROTON, CT 06340

SS928944

1109TH TASMGH-60-14-SOF-01 (BREEZE EASTERN EXTERNALRESCUE HOIST INSTALLATION) COMPLIEDWITH @ 5067.3 ACFT HOURS.

31-Oct-2013 1

GROTON, CT 06340

SS928944

1109TH TASMGH-60-14-ASAM-02 (HEALTH MONITORINGSYSTEM (HUMS) ACCELEROMETERS)COMPLIED WITH @ 5067.3 ACFT HRS.

21-Nov-2013 1

GROTON, CT 06340

SS928944

1109TH TASMGMEC F175019, Extruded angle damaged beyondlimits on the forward upper right hand corner ofthe transmission mount area STA 327 BL 16.Authorization is granted to the 1109th TASMGto remove one or more Hi-Locs to blend outminor damage on the Extruded Angle, smoothdamaged area to amaximum depth not toexceed .040 inch deep.

26-Nov-2013 39

GROTON, CT 06340

SS928944

1109TH TASMGMEC F174258, Authorization granted for the1109th Connecticut TASMG to fabricate andinstall one Forward Sliding Pylon Bracket PartNumber 70219-04205-047, NSN: 01-378-1230,IAW SAC DWG 70219-04205, Item -121.

26-Nov-2013 38

GROTON, CT 06340

SS928944

1109TH TASMGMEC F172511, The 1109th TASMG is grantedauthorization to locally fabricate and install oneLeft Hand Side Center Engine Deck Drain Panel,Part Number 70219-42425-050 located atapproximately Station 341.0, WL 260.0, BL 40.0due to shortage in the US Army and OEMSupply System.

26-Nov-2013 37

GROTON, CT 06340

SS928944

1109TH TASMGMEC F172890, The 1109th TASMG is grantedpermission to replace the Tail Pylon PulleyBracket Part Number 70400-06680-046 due toelongated Pulley Bracket Bushing Holes.

26-Nov-2013 36

GROTON, CT 06340

SS928944

1109TH TASMGMEC F172075, The 1109th TASMG is grantedauthorization to locally fabricate and installPartNumbers 70211-02110-113 and 70211-02110-114Strap Assemblies.

26-Nov-2013 35

GROTON, CT 06340

SS928944

1109TH TASMGMEC F172012, The 1109th TASMG is grantedauthorization to locally fabricate and install PartNumbers 70219-03002-130/131 Fuel Line andPump Enclosure Installation for the AftFuselage make from .032, 7075- T6.Manufacturing is required due to the part is nolonger available as a localpurchase item and itis not in the Army Supply system.

26-Nov-2013 34

GROTON, CT 06340

SS928944




8.7.DATE

6.REMARKS

4. 5.



1109TH TASMGMEC F171591, During OCM multiple cracks anddamage were located behind #1 enginecowlinglatch receptacle. TASMG is requestingauthorization to manufacture replacement thispart using301 1/4 hard SS of equal thicknessusing original as a template. Authority isgranted to the 1109th Connecticut TASMG tofabricate and install a new strengthened part.

26-Nov-2013 33

GROTON, CT 06340

SS928944

1109TH TASMGMEC F171564, Authority is granted for the1109th TASMG to replace the Lower ForwardCo-Pilot’s Door Frame damaged section IAWUS Army Standard Sheet Metal Shop Practicesand the Sikorsky Engineering Drawing.

26-Nov-2013 32

GROTON, CT 06340

SS928944

1109TH TASMGMEC F171593, The 1109th TASMG is grantedauthorization to locally fabricate andinstallAluminum Doubler Straps due to ashortage in the US Army Supply System.Manufacture Two 70212-02137-114 Straps makefrom 7075-T6 material .032 thickness or two70212-02137-146 Straps make from 7075-T6material .050 thickness.

26-Nov-2013 31

GROTON, CT 06340

SS928944

1109TH TASMGMEC F171184, During OCM, CT TASMG FOUND4 EA #40 holes between STA 295-308 BL 34.5 inthe top of the eaded panel. The 1109th TASMGis granted authorization to Flush Plug Fourunused #40 holes and Two #10 holes asrequired. Use Standard Sheet Metal ShopPractices TM 1500-204-23-10.

26-Nov-2013 30

GROTON, CT 06340

SS928944

1109TH TASMGMEC F171571 B, Authorization is granted to the1109th TASMG to replace the Left Forward SideSection of the 34.5 Beam Assembly IAWSikorsky procedure AJM-BL34-1C. Repair Oneoversized oblong .325 x .345 hole in the CabinRoof Plating at Station 270 LBL 34.5 IAWSikorsky Drawing 70070-02112, and TM 1-1500-204-23-10.

26-Nov-2013 29

GROTON, CT 06340

SS928944

1109TH TASMGMEC F171026, The 1109th TASMG is grantedauthorization to locally fabricate One Clip 70450-01070-117. Fabricate by using the existing Clipas a template. Perform this work IAW TM-1500-204-23-10.

26-Nov-2013 28

GROTON, CT 06340

SS928944

1109TH TASMGMEC F171023, The 1109th TASMG is grantedauthorization to locally fabricate One Clip PartNumber 70450-01070-120. Fabricate by usingthe existing Clip as a template. Perform thiswork IAW TM-1500-204-23-10.

26-Nov-2013 27

GROTON, CT 06340

SS928944

1109TH TASMGMEC F171122, CT TASMG has discovered anunauthorized repair on the I/G/B mount fitting#2 cable conduit hole enlarged. Authorization isgranted to the 1109th TASMG to leave theIntermediate GearBox Mount Fitting #2 CableConduit as is.

26-Nov-2013 26

GROTON, CT 06340

SS928944




8.7.DATE

6.REMARKS

4. 5.



1109TH TASMGMEC F170979, The 1109th TASMG is grantedauthority to replace the Plug assembly on theIntermediate Gearbox Output Housing PartNumber 70357-06300-042. IAW DMWR 1- 1615-288. Removal is on Page 3-8, Paragraph 3-10.2.g, installation is on Page 3-100 Paragraph 3-14.3.d.

26-Nov-2013 25

GROTON, CT 06340

SS928944

1109TH TASMGMEC F171116, During OCM it was found thatdamage was caused from a previous repair. Ahole was drilled into STA L295 Beam WL 255which was not allowed. The edge distance tothe rivet is out of tolerance, center of rivet tocenter of hole is 17/64. Authorization is grantedto the 1109th TASMG to repair the Station L 295Beam located at WL 255. Install a double flushFreeze Plug for an extra holewhich was drilledfor sound proofing.

26-Nov-2013 24

GROTON, CT 06340

SS928944

1109TH TASMGMEC F170453, The 1109th TASMG is grantedauthorization to locally fabricate PaRt Number70211-02110-132 Angle out of 0.032, make from4130 MIL-S-18729 Alloy Steel. Make from thesame material, same thickness only. Use thedamaged part as a template, perform this workIAW TM 1-1500-204-23-10.

26-Nov-2013 23

GROTON, CT 06340

SS928944

1109TH TASMGMEC F170343, THE 1109TH TASMG ISGRANTED PERMISSION TO REPAIR A RIGHTSIDE TAIL ROTOR PYLON 3" CRACK ANDINSTALL A NEW DOUBLER IAW DMWR 1-1520-237-3 WP 0348 00. REPLACE P/N 70202-06051-162 STRAP IAW US ARMY STANDARD SHEETMETAL SHOP PRACTICES.

26-Nov-2013 22

GROTON, CT 06340

SS928944

1109TH TASMGMEC F170033, The 1109th TASMG is grantedauthorization to replace the Forward CargoHook Mount because it is gouged beyondrepairable limits.

26-Nov-2013 21

GROTON, CT 06340

SS928944

1109TH TASMGMEC F170034 A, The 1109th TASMGConnecticut is granted authorization to replacethe AFT Cargo Hook Fitting, Part Number 70219-0251-044.

26-Nov-2013 20

GROTON, CT 06340

SS928944

1109TH TASMGMEC F169628, The 1109th Connecticut TASMGand Sikorsky Technicians are grantedpermission to replace 2 Servo Rail Beams.Replace the Servo Rail Beams at locations RBL3.06 and LBL 10.70.

26-Nov-2013 19

GROTON, CT 06340

SS928944

1109TH TASMGMEC F169435, During OCM induction,mechanics discovered that the doubler at STA465-485 under the STA 470 T/R D/S mount wasinstalled and not documented along with theadditional stringer required at STA 465-485LBL7. The tail cone skin was already upgradedand did not require the doubler at STA STA 465-485 but was installed anyway. The 1109thTASMG is authorized to leave the Doublerinstallation at Flight Station 465-485 and theStringer located at Station 465-485, LBL7 inposition.

26-Nov-2013 18

GROTON, CT 06340

SS928944




8.7.DATE

6.REMARKS

4. 5.



1109TH TASMGMEC F169426, During OCM inductionmechanics discovered that the doubler at STA591 for the T/R D/S mount was installedimproperly. WP0377 call for thicker skined tailcones skins. The tail cone skin was alreadyupgraded and did not require the doubler atSTA 591 but was installed anyway. The 1109thTASMG is authorized to leave the Doublerinstallation at Flight Station 591 in position. TheTail Rotor Drive Shaft Mount repair isstructurally sound as is.

26-Nov-2013 17

GROTON, CT 06340

SS928944

1109TH TASMGMEC F169424, During OCM inductionmechanics discovered that the doubler at STA531 for the T/R D/S mount was installedimproperly. The tail cone skin was alreadyupgraded and did not require the doubler atSTA 531 but was installed anyway. The 1109thTASMG is authorized to leave the Doublerinstallation at Flight Station 531 in position. TheTail Rotor Drive Shaft Mount repair isstructurally sound as is, the Lima, modelthicker Tail cone skin does not require aDoubler.

26-Nov-2013 16

GROTON, CT 06340

SS928944

1109TH TASMGMEC F169455, The 1109th Connecticut TASMGis authorized to replace the damaged beyondrepair Station 363 Transmission Frame PartNumber 70219-02132-042/-043. Perform thiswork IAW OEM Procedure SSE-7021902132-01and US Army TM Series TM 1-1500-204-23-10.The aircraft is currently completelydepopulated, Jacked, Leveled and Shored.

26-Nov-2013 15

GROTON, CT 06340

SS928944

1109TH TASMGMEC F170046, The 1109th TASMG is grantedauthorization to repair Skin Section PartNumber 70213-02101-105 at STA 363, WL261 BL0. Fabricate by using 0.040, 7075- T6 material.Fabricate and replace Gusset Part Number70213-02101-126 from 0.040, 7075-T6 material.

26-Nov-2013 14

`GROTON, CT 06340

SS928944

1109TH TASMGMEC F169382, During OCM maintenanceinspections it was discovered that the 70213-02501-101belly skin from STA 330-343 BL5RWL200 is Oil canned. LAR provided the CTTASMG WP 0027 00/0033 00 and assisted theCT TASMG evaluate the oil canning. The 1109thTASMG is authorized to repair 70213-02501-101Belly Skin Section Flight Station 330-343, BL5R, WL 200 for a Oil Canning condition IAW,DMWR 1-1520-237-1 WP0261 00/ WP0262 00.

26-Nov-2013 13

GROTON, CT 06340

SS928944

1109TH TASMGMEC F169381, During OCM maintenanceinspections it was discovered that the 70213-02501-101belly skin from at STA 308 LBL 10 toRBL 10 was creased. LAR provided the CTTASMG WP 0027 00/0033 00 and assisted theCT TASMG evaluate the oil canning. The 1109thTASMG is authorized to repair all verified OilCanning conditions IAW, DMWR 1-1520-237-1WP0261 00/ WP0262 00.

26-Nov-2013 12

GROTON, CT 06340

SS928944




8.7.DATE

6.REMARKS

4. 5.



1109TH TASMGMEC F169806, During OCM maintenanceinspections it was discovered that the thedoubler strap on the belly at STA 295 LBL10 iscreased. The 1109th Connecticut TASMG isgranted permission to remove, fabricate andreplace one damaged doubler by using theexisting part as a template, performthis repairIAW TM 1-1500-204-23-10.

26-Nov-2013 11

GROTON, CT 06340

SS928944

1109TH TASMGMEC F169807, Authorization is granted to the1109th Connecticut TASMG to leave onepreexisting doubler repair located at Station295-326, Left Hand Side Exterior FuselagePlating as is.

26-Nov-2013 10

GROTON, CT 06340

SS928944

1109TH TASMGMEC F169409, Authorization is granted to the1109th TASMG to leave one small preexistingdoubler repair on the Left Hand Side Belly Skinlocated at Station 360 in place.

26-Nov-2013 9

GROTON, CT 06340

SS928944

1109TH TASMGMEC F169394, Authorization is granted to the1109th TASMG to leave a minor drill start STA379, WL267, LBL16 with a maximum depth of.030 as is.

26-Nov-2013 8

GROTON, CT 06340

SS928944

1109TH TASMGMEC F169392, The 1109th Connecticut TASMGis authorized to leave one Station 379 UPPERLeft Hand D Ring repair in place. The repair isstructurally sound as is.

26-Nov-2013 7

GROTON, CT 06340

SS928944

1109TH TASMGMEC F166883, The 1109th TASMG is authorizedto replace the Bearings and Bushings on theAft Longitudinal Servo Bellcrank Assembly70400-08102-045 (NSN 1680-01-158-9685)inaccordance with the procedures outlined inDMWR 1-1680-370. Paragraph 3-17Replacement of Spherical Bearing.

26-Nov-2013 6

GROTON, CT 06340

SS928944

1109TH TASMGMEC F175019, Authorization is granted to the1109th TASMG to remove one or more Hi-Locsto blend out minor damage on the ExtrudedAngle AT UPPER R/H CORNER OF XMSNMOUNT AREA STA 327, RBL16.

26-Nov-2013 5

GROTON, CT 06340

SS928944

1109TH TASMGMEC F171936, The 1109th Connecticut TASMGis authorized to use Adhesive EC1751 in placeof 9309.3 to re-bond the UH-60 Tail RotorConduit Assembly. This substitution ofadhesives is due to an unavailability of Hysol inthe US Army Supply System. Perform this workIAW Sikorsky Drawing 70400-00510 REV AD.

26-Nov-2013 4

GROTON, CT 06340

SS928944

1109TH TASMGMEC F169273, The Connecticut ARNG isgranted permission to replace the Right Handand Left Hand Beaded Panels on UH-60Aaircraft 80-23506.

26-Nov-2013 3

GROTON, CT 06340

SS928944

1109TH TASMGMEC F171571 B, Authorization is granted to the1109th TASMG to replace the Left Forward SideSection of the 34.5 Beam Assembly IAWSikorsky procedure AJM-BL34-1C. Repair Oneoversized oblong .325 x .345 hole in the CabinRoof Plating at Station 270 LBL 34.5 IAWSikorsky Drawing 70070-02112, and TM 1-1500-204-23-10.

26-Nov-2013 1

GROTON, CT 06340

SS928944




8.7.DATE

6.REMARKS

4. 5.



1109TH TASMGMEC F175905 THE 1109TH TASMG ISGRANTED AUTHORIZATION TO LOCALLY FABAND INSTALL A GUSSET ASSY

27-Nov-2013 2

GROTON, CT 06340

WS521003

1109TH TASMGMEC F175902 THE 1109TH TASMG ISGRANTED AUTHORIZATION TO LOCALLY FABAND REPLACE DOUBLER ASSY

27-Nov-2013 1

GROTON, CT 06340

WS521003

1109TH TASMGMEC F176385 THE 1109TH TASMG ISGRANTED AUTHORIZATION TO LOCALLY FABP/N 70219-04600-119

10-Dec-2013 1

GROTON, CT 06340

WS521003

1109TH TASMGMEC F176505 THE 1109TH TASMG ISGRANTED AUTHORIZATION TO REPAIR ASMALL 1/4 IN DENT ON THE HYD DECK

12-Dec-2013 1

GROTON, CT 06340

WS521003

1109TH TASMGH-60-14-AMAM-03 (DISCREPANT LATERALCONNECTING LINKS) COMPLIED WITH @5067.3 ACFT HRS.

24-Dec-2013 1

GROTON, CT 06340

SS928944

1109TH TASMGMEC F175902, During OCM 1109th found anarea on the cabin roof that is gouged. Thegouged area is approximately 1.00in length X0.030 in width. This has worn through the cabinroof plating adjacent to the AFT inboard foot ofroll trim servo, STA 253 WL270 BL1R.The1109th TASMG is granted authorization tolocally fabricate and replace the DoublerAssembly.

02-Jan-2014 3

GROTON, CT 06340

SS928944

1109TH TASMGMEC F176491, THE 1109TH TASMG ISGRANTED AUTHORIZATION TO LOCALLYFABRICATE ANE INSTALL ONE TRANSFERMODULE SHIM P/N: 70213-02101-135.

02-Jan-2014 1

GROTON, CT 06340

SS928944

1109TH TASMGMEC F177393 THE 1109TH TASMG ISGRANTED AUTHORIZATION TO FLUSH PLUGAN UNUSED PILOT HOLE AS REQ'D.

08-Jan-2014 2

GROTON, CT 06340

WS521003

1109TH TASMGMEC F177382 THE 1109TH TASMG ISGRANTED AUTHORIZATION TO FLUSH PLUGAN UNUSED PILOT HOLE AS REQ'D.

08-Jan-2014 1

GROTON, CT 06340

WS521003

1109TH TASMGIVHMU S/N: 01430 INSTALLED, CURRENTSOFTWARE 3019551-04-0305A.

13-Jan-2014 1

GROTON, CT 06340

SS928944

1109TH TASMGMEC F178423 THE 1109TH TASMG ISGRANTED AUTHORIZATION TO LOCALLYFABRICATE AND INSTALL PART NUMBER70361-03010-121 FORWARD OIL COOLERMOUNTING PLATE. IAW TM-1-1500-204-23-10AND SIKORSKY DRAWING.

31-Jan-2014 1

GROTON, CT 06340

JM743799

1109TH TASMGFLIGHT CONTROL RIGGING COMPLETED @5067.3 ACFT HRS

07-Feb-2014 2

GROTON, CT 06340

JF986581

1109TH TASMGTAIL ROTOR BIAS - RED A: 4.72, B: 5.08, DIFF:.354, BLADE FINAL: 3.0BLACK A: 4.04, B: 4.35, DIFF: .301, FINAL: 3.1YELLOW A: 4.81, B: 5.13, DIFF: .32, FINAL: 3.0BLUE A: 4.08< B: 4.39, DIFF: .289, FINAL: 3.1

07-Feb-2014 1

GROTON, CT 06340

JF986581

1109TH TASMGMWO 1-1520-237-50-99 COMPLETEINSTALLATION OF THE COMMON MISSILEWARNING SYSTEMS (CMWS)FIFTH SENSORINSTALLED AT 5067.3 A/C HOURS

12-Feb-2014 3

GROTON, CT 06340

JM743799




8.7.DATE

6.REMARKS

4. 5.



1109TH TASMGMWO 1-1520-237-50-93 COMPLETEINSTALLATION OF THE MODERNIZED (P3I)AN/AAR-57 IMPROVED COUNTERMEASUREDISPENSER SYSTEM (ICMD) COMMONMISSILE WARNING SYSTEM (CMWS)COMPLETED AT 5067.3 A/C HOURS

12-Feb-2014 2

GROTON, CT 06340

JM743799

1109TH TASMGMWO 1-1520-237-50-100COMPLETEINSTALLATION OF INTEGRATED VEHICLEHEALTH MANAGEMENT SYSTEM (IVHMS)COMPLETED AT 5067.2 A/C HOURS

12-Feb-2014 1

GROTON, CT 06340

JM743799

1109TH TASMGOCM INSPECTION (PMI 1 AND PMI 2)COMPLETED AT 5067.3 ACFT HOURS. NEXTPMI DUE IS PMI 1 DUE AT 5427.3 ACFT HOURS

20-Feb-2014 4

GROTON, CT 06340

JF986581

1109TH TASMGAWR 1494 R7 DATED 29JUN12 APPLIED FORINSTALLATION OF COMMON MISSILEWARNING SYSTEM (CMWS) 5TH SENSOR AKIT AT 5067.3 ACFT HRS.

20-Feb-2014 3

GROTON, CT 06340

JF986581

1109TH TASMGAWR 1425 R17 DATED 18SEP12 APPLIED FORINSTALLATION OF COMMON MISSILEWARNING SYSTEM (CMWS) AND PREPLANNED PRODUCT IMPROVEMENT (P3I) AT5067.3 ACFT HRS.

20-Feb-2014 2

GROTON, CT 06340

JF986581

1109TH TASMGAWR 1346 R21 DATED 24JAN14 APPLIED FORINSTALLATION OF INTEGRATED VEHICLEHEALTH MANAGEMENT SYSTEM (IVHMS) AT5067.3 ACFT HRS.

20-Feb-2014 1

GROTON, CT 06340

JF986581

1109TH TASMGH-60-14-AMAM-05 (ULLS-A(E) ALC LegitimateCode File (LFC) Change 65 Requirements)COMPLIED AT 5067.3 ACFT HRS

24-Feb-2014 1

GROTON, CT 06340

JF986581

1109TH TASMGH-60-14-AMAM-0 (AN/ASC 15COMM CONSOLECIRCUIT BREAKER PROTECTION) COMPLIEDAT 5075.9 ACFT HRS

04-Mar-2014 1

GROTON, CT 06340

WS521003

1109TH TASMGAIRWORTHINESS RELEASE (AWR) FOR UH/HH-60A/L AIRCRAFT EQUIPPED WITH THEATTITUDE HEADING REFERENCE SET (AHRS),SINGLE ATTITUDE HEADING REFERENCEUNIT (AHRU) AWR 1444 DTD 11JUL13 REV 6

12-Mar-2014 2

GROTON, CT 06340

JF986581

1109TH TASMGCWO 1-1520-237-20-2 INSTRUCTIONS FORREMOVAL OF THE # 1 (CO-PILOTS) AHRU ANDINSTALLATION OF NAVIGATIONAL SYSTEMS:CN-1314 (VG), TRU-2A/A (RG) ON H-60A/LAIRCRAFT COMPLETED AT 5087.4

12-Mar-2014 1

GROTON, CT 06340

JF986581

1109TH TASMGCOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-04 @ 5095 ACFT HRS ( M/R HUD EDDYCURRENT)

25-Mar-2014 1

GROTON, CT 06340

WS521003

1109TH TASMGCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-09 @ 5095 ACFT HRS (MAIN MODRECESSED WASHERS)

26-Mar-2014 1

GROTON, CT 06340

WS521003

1109TH TASMGCOMPLIED WITH REQUIREMENTS H-60-14-AMAM-10 (HONTEK COATED M/R BLADEREMOVAL) N/A THIS ACFT

08-Apr-2014 1

GROTON, CT 06340

WS521003

1109TH TASMGH-60-14-AMAM-14 INTERGRATED VEHICLEHEALTH MANAGEMENT (IVHMS), COMPLIEDWITH.

30-May-2014 1

GROTON, CT 06340

JA580641




8.7.DATE

6.REMARKS

4. 5.



1109TH TASMGH-60-14-SOF-03, DISCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS, COMPLIED WITH.

24-Jun-2014 1

GROTON, CT 06340

JA580641

1109TH TASMGCOMPLIED WITH H-60-14-ASAM-09 (IMPROVED ENGINE OUTPUT SHAFT) @ 5197.6ACFT HRS

01-Aug-2014 1

GROTON, CT 06340

JF986581

1109TH TASMGH-60-14-ASAM-10, MAIN TRANSMISSIONPLANETARY CARRIER ASSEMBLY, COMPLIEDWITH.

02-Sep-2014 1

GROTON, CT 06340

JA580641

1109TH TASMGH-60-15-AMAM-05 (ATTITUDE HEADINGREFERENCE SYSTEM (AHRS) EMERGENCYPROCEDURE) COMPLIED WITH @ 5355.6 ACFTHRS

12-Mar-2015 2

GROTON, CT 06340

LS800246

1109TH TASMGH-60-15-AMAM-06 (IDENTIFICATION OFAVIATION SURVIVABILITY EQUIPMENT)COMPLIED WITH @ 5355.6 ACFT HRS

12-Mar-2015 1

GROTON, CT 06340

LS800246

1109TH TASMGH-60-15-ASAM-03 (TROOP/GUNNER SEATENERGY ATTENUATORS COMPLIED WITH @5379.9 ACFT HRS

28-Jun-2015 1

GROTON, CT 06340

JF986581

1109TH TASMGH-60-15-AMAM-11 (MODE–S TRANSPONDERADDRESS REVIEW) COMPLIED WITH @ 5379.9ACFT HRS

06-Jul-2015 2

GROTON, CT 06340

JF002190

1109TH TASMGH-60-15-AMAM-10 (AV-DEC GASKETINSPECTION) COMPLIED WITH @ 5379.9 ACFTHRS.

06-Jul-2015 1

GROTON, CT 06340

JF986581

1109TH TASMGTAIL ROTOR CABLE TENSIONL/H - 148 @82.0°FR/H - 147 @ 82.0°F

03-Aug-2015 3

GROTON, CT 06340

DB829792

1109TH TASMGTAIL ROTOR BIASRED - DIM "A" 4.813, DIM "B"5.125, DIFF .312, FINAL 3.1BLK - DIM "A" 4.125,DIM "B" 4.438, DIFF .313, FINAL 3.1YEL - DIM"A" 4.875, DIM "B" 5.188, DIFF .313, FINAL3.1BLU - DIM "A" 4.125, DIM "B" 4.438, DIFF.313, FINAL 3.1

03-Aug-2015 2

GROTON, CT 06340

DB829792

1109TH TASMGMAIN ROTOR RIG COMPLETED @ 5379.9 ACFTHRS.

03-Aug-2015 1

GROTON, CT 06340

DB829792

1109TH TASMGH-60-15-AMAM-14 (LEGITIMATE CODE FILE(LCF) CHANGE 67 REQUIREMENTS) COMPLIEDWITH @ 5379.9 ACFT HRS.

31-Aug-2015 1

GROTON, CT 06340

DB829792

1109TH TASMGCOMPLIED WITH REQUIREMENTS OF H-60-15-SOF-02, FRIES RELEASE CABLE, @ 5379.9ACFT HOURS

28-Sep-2015 1

GROTON, CT 06340

DB829792

1109TH TASMGCOMLIED WITH REQUIREMENTS OF H-60-15-AMAM-18, MEDEVAC CAROUSEL, @ 5379.9ACFT HOURS

01-Oct-2015 1

GROTON, CT 06340

DB829792

1109TH TASMGCOMPLIED WITH REQUIREMENTS OF H-60-16-AMAM-01, EIBF FRAMES, @ 5379.9 ACFTHOURS

28-Oct-2015 1

GROTON, CT 06340

DB829792

1109TH TASMGCOMPLIED WITH REQUIREMENTS OF H-60-16-ASAM-01, INBOARD RETENTION PLATETORQUE CHECKS, @ 5379.9 ACFT HRS

16-Nov-2015 1

GROTON, CT 06340

DB829792




8.7.DATE

6.REMARKS

4. 5.



1109TH TASMGCOMPLIED WITH REQUIREMENTS OF H-60-16-AMAM-03, PERSONNEL LOCATOR SETREMOVAL @ 5379.9 ACFT HRS

01-Dec-2015 1

GROTON, CT 06340

DB829792




8.7.DATE

6.REMARKS

4. 5.



1109TH TASMG (M2SERVICES)

ACFT. STRIPPED WITH PLASTICMEDIA,REPAINTED WITH MIL-DTL-64159 IAWCONTRACT # W91ZRS-11-D-0001

04-Dec-2013 1

GROTON, CT 06340

GL544447




8.7.DATE

6.REMARKS

4. 5.



1-147TH AVIATIONBATTALION

A/C DEPLOYED TO SOUTHWEST ASIATHEATER OF OPERATIONS VIA SEATRANSPORT AT 3568.0 A/C HRS FOROPERATION BRIGHT STAR (XC8756)

06-Sep-2005 1

MMC ROZ, EGYPT

QC000000




8.7.DATE

6.REMARKS

4. 5.



1-147TH AVN BN TASKFORCE EAGLE

MULTIPLE INTERGRATED LASERENGAGEMENT SYSTEM/AIR TO GROUNDENGAGEMENT SYSTEM (MILES/ANGES)INSTALLED IAW AWR 1345 DTD 7 JUN 06 ONETIME PDD EMC CHECK COMPLETED AT 3029.5(WH1187)

18-Oct-2006 1

MANNHIEM GERMANY

QC000000


MULTIPLE INTERGRATED LASERENGAGEMENT SYSTEM/AIR TO GROUNDENGAGEMENT SYSTEM (MILES/ANGES) AWR1345 REMOVED FROM ACFT AT 3769.5(WH1187)

08-Nov-2006 1

HOHENFELS GERMANY

QC000000


ALL H-60 SERIES AIRCRAFT, REROUTING OFWHITE ENGINE/AIRFRAME HARNESSASSEMBLY, UH-60-07-ASAM-01 COMPLIEDWITH AT 3805.8 ACFT HRS (WH1187)

07-Dec-2006 1

CAMP BONDSTEEL APOAE 09340

QC000000


ALL H-60 SERIES AIRCRAFT, REVISION TO UH-60-07-ASAM-01,REROUTING OF WHITEENGINE/AIRFRAME HARNESS ASSEMBLY,UH-60-07-ASAM-02 COMPLIED WITH AT 3817.7ACFT HRS (WH1187)

20-Dec-2006 1


QC000000


ALL H-60 SERIES AIRCRAFT, YAW ANDCOLLECTIVE BOOST SERVOS ROLL PIN, UH-60-07-ASAM-03. COMPLIED WITH AT 3817.7ACFT HRS 29DEC06. VARIFIED BOTH ROLLPINS (WH1187)

29-Dec-2006 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



2CADSOF UH-60A-88-04 TB 55-1520-237-20-96 REVOF ONE TIME INSP OF T/R GEARBOX OUTPUTSHAFT C/W (JG0000)

16-Aug-1994 32

CORPC, TX

QC000000




8.7.DATE

6.REMARKS

4. 5.



326 MEDSOF UH60A BLACKHAWK AIRCRAFT INSPECTAND REPLAE WASHER AN960PD416L, NSN5310-00-184-9001 ON COLLECTIVE BIAS TUBEASSY P/N 70301-02107-043 NSN 5340-01-115-3905 IAW UH60A-83-10 TB 55-1520-237-20-44C/W. D LEE. (NO PID)

28-Oct-1983 2

FTCKY

QC000000

326 MEDSOF UH-60S BLACKHAWK AIRCRAFTREPETIVE INSPECTION FOR STABILATORAMPLIFIER IAW UH60A-83-09 TB 55-1520-237-20-43 C/W SSG LEE. (NO PID)

28-Oct-1983 1

FTCKY

QC000000

326 MEDSOF INSPECTION OF TAIL ROTOR SERVOASSEMBLY NSN 1650-125-5430 FOR BENTSERVO VALVE INPUT STEM IAW UH 60A-83-12TB 55-1520-237-20-46 C/W. D LEE (NO PID)

08-Nov-1983 1

FTCKY

QC000000

326 MEDSOF INSPECTION OF ACCESSORY MODULEOIL RETURN SCREEN NSN 1615-01-092-7883FOR CONTAMINATION WITH FIBEROUSMATERIAL IAW UH60A-83-11 TB 55-1520-23720-47 C/W. SSG LEE. (NO PID)

23-Nov-1983 1

FTCKY

QC000000

326 MEDSOF INSPECTION OF MAIN ROTOR SHAFT P/N70351-08131-044-015 NSN 1650-01-134-2508IAW TB 55-1520-237-50-01 UH60A-84-01 BYFACTORY TEAM C/W SSG C LEE. (NO PID)

29-Jan-1984 1

FTCKY

QC000000




8.7.DATE

6.REMARKS

4. 5.



326 MED BNSOF INSTALLATION OF ENGINE EXHAUSTDESWIRL DUCT PN 70700-30011-108 NSN 1560-01-100-8243 IAW TWX 202230ZJAN82 UH-60A-82-05 C/W LOUISE A. LEASER SGT TI CO D.(NO PID)

13-Apr-1982 1

FTCKY

QC000000

326 MED BNSOF TWX 291600ZAPR82 MAINT MANDATORYMSG RCS-CSGLD-1860ONE TIME INSP FOR UH-60A BLACKHAWK AIRCRAFT PILOT/COPILOTSEAT RUBBING BAR (UH60A-82-06) TB 55-1520-237-20-27 INSPECTION C/W. L.A. LEASER TI.(NO PID)

03-May-1982 1

FTCKY

QC000000

326 MED BNSOF MAINT MANDATORY MESSAGE021930ZJUL82 RCS-CSGLD-1860, ONE TIMEINSP FOR UH-60A BLACKHAWK ACFT GIMBALENGINE MOUNT ELASTOMERIC P/N 70361-08002-102 ON ACFT SN 80-23501 ANDSUBSEQUENT (UH-60-82-09) C/W. (NO PID)

09-Jul-1982 1

FTCKY

QC000000

326 MED BNSOF MESSAGE MAINTENANCE MANDATORY,RCS-CSGLD-1860, UH-60A HELICOPTER ECP-SA-H-60-0224 BOOST SERVOS, COLLECTIVEAND YAW, IMPROVED CRANK SPLINE (UH-60A-82-12) C/W (NO PID)

07-Aug-1982 2

FTCKY

QC000000

326 MED BNSOF MESSAGE MAINTENANCE MANDATORY,RCS-CSGLD-1860, ONE TIME INSP FOR UH-60ABLACKHAWK ACFT, MAIN ROTOR SERVOSCREWS (UH-60A-82-11) TB 55-1520-237-20-30.(NO PID)

07-Aug-1982 1

FTCKY

QC000000

326 MED BNSOF EMERGENCY TECHNICAL MESSAGE ONETIME INSPECTION FOR UH-60A-82-13) L.A.LEASER. (NO PID)

15-Aug-1982 1

FTCKY

QC000000

326 MED BNSOF MAINT MESSAGE, RCS-CSGLD-1860, ONETIME INSPECTION FOR UH-60A BLACKHAWKACFT TAIL ROTOR SERVO PN 70410-06520 ONACFT SN 77-22714 THRU 81-23570 (UH-60A-82-14) (TB 55-1520-237-20-31. L.A. LEASER (NOPID)

07-Sep-1982 1

FTCKY

QC000000

326 MED BNSOF MAINT MAND MESSAGE, ONE TIMEINSPECTION FOR UH-60A BLACKHAWK ACFTTAIL ROTOR SERVO PN 70410-06520 ON ACFTSN 77-22714 THRO 81-23570 (UH-60A-82-17)(TB 55-1520-237-20-31) L.A. LEASER (NO PID)

09-Sep-1982 1

FTCKY

QC000000

326 MED BNSOF ONE TIME INSPECTION FOR ALL UH-60AAIRCRAFT FLIGHT CONTROLS MIXER LIMITERBEARING IAW TWX UH-60A-82-16 (TB 55-1520-237-23-4) 222135ZSEP82 C/W L.A. LEASER.(NO PID)

22-Sep-1982 1

FTCKY

QC000000

326 MED BNSOF ONE TIME INSPECTION FOR UH-60ABLACKHAWK AIRCRAFT CARGO DOORTRACKS PPER PN 70217-02702-041/042 IAWTWX 211930ZDEC82 (UH-60A-82-22) TB 55-1520-237-20-37 C/W. S/C LEE. (NO PID)

22-Dec-1982 1

FTCKY

QC000000




8.7.DATE

6.REMARKS

4. 5.



326 MED BNSOF ONE TIME INSPECTION OF FLIGHTCONTROLS FOR UH-60A BLACKHAWK ACFT.DIRECTIONAL CONTROL LEVER ASSY PN70400-02623-041. NSN 1560-01-08306799 (UH-60A-83-02) (TB 55-1520-237-20-40 C/W. L.A.LEASER (NO PID)

28-Mar-1983 1

FTCKY

QC000000

326 MED BNSOF ONE TIME INSPECTION OF STABILATORASSY PN 70200-07050-043/044 (UH-60A-83-03)(TB 55-1520-237-20-41) N/A THIS SERIES OFACFT. L.A. LEASER (NO PID)

01-Apr-1983 1

FTCKY

QC000000

326 MED BNSOF ONE TIME INSP FOR UH60A BLACKHAWKAIRCRAFT INLET DUCT ASSEMBLY PN 70302-101000 AND ALIGNMENT PIN BRACKET 70209-04301-044/045 IAW UH-60A-83-04 TB 55-1520-237-30-01 C/W. C. LEE (NO PID)

11-Apr-1983 1

FTCKY

QC000000




8.7.DATE

6.REMARKS

4. 5.



A CO 5TH TRANS BNSOF UH-60-86-06 ONE TIME INSPECITON OFPRIMARY SERVOS AND CONTROL RODS C/WR TARO SSG TI A CO 5TH TRANS BN, FT.CAMPBELL, KY (RT0000)

22-Mar-1985 1

FT. CAMPBELL, KY

QC000000

A CO 5TH TRANS BNSOF UH-60-85-07 GENERAL INSPECTION OFTHE FLIGHT CONTROL SYSTEM C/W SSG HALIMENT TI A CO 5TH TRANS BN FT.CAMPBELL, KY (HA0000)

09-Apr-1985 1

FT. CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



AAFS # 2 OHARNGH-60-10-ASAM-07 STABILATOR HINGEFITTINGS COMPLIED WITH 20100421 @ 4474.8ACFT HRS.

21-Apr-2010 1

COLUMBUS, OH 43217

FD441686




8.7.DATE

6.REMARKS

4. 5.



AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FORUH/EH/HH-60A/L AIRCRAFT EQUIPPED WITHTHE ATTITUDE HEADING REFERENCE SET(AHRS), DUAL ATTITUDE HEADINGREFERENCE UNIT (AHRU) AWR 1529 DTD 07OCT 11 REV 2

07-Oct-2011 1

COLUMBUS, OH 43217

FD441686




8.7.DATE

6.REMARKS

4. 5.



AASF # 2 OHARNH-60-09-ASAM-08 ENGINE COWLING WEIGHTRESTRICTIONS C/W 22 APR 2009 @ 4319.5ACFT HRS.

04-May-2009 1

COLUMBUS, OH 43217-5918




8.7.DATE

6.REMARKS

4. 5.



AASF # 2 OHARNGAIRCRAFT RECIEVED FROM 1-174TH AVNMADISON, WI. HISTROCIAL RECORDSMISSING SOF AND ASAM MESSAGES. CALLEDUH-60 MESSAGE OFFICE AND WAS INFORMEDTHAT ALL MESSAGES HAVE BEEN COMPLIEDWITH. HISTORICAL INFORMATIOM MISSINGFROM JUL 1988 THRU AUG 1994.

27-Mar-2009 2

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRCRAFT ASSIGNED TO CO B 1-137TH, ACFTTRANSFERED FROM WI. ACFT HRS 4314.2

27-Mar-2009 1


FD441686

AASF # 2 OHARNGH-60-09-ASAM-07 FIRE EXTINGUISHER WIRING(BREAKAWAY THREAD), COMPLIED WITH20090406 @ 4315.4 ACFT HRS

06-Apr-2009 1


FD441686

AASF # 2 OHARNGH-60-09-ASAM-09 FIRE EXTINGUISHER WIRING(BREAKAWAY THREAD) ( REVISION TO H-60-09-ASAM-07) COMPLIED WITH 20090506 @4332.6ACFT HRS.

06-May-2009 1


FD441686

AASF # 2 OHARNGH-60-09-AMAM-04, CO-PIOLT SEATINTERFERENCE WITH ARMY AIRBORNECOMMAND AND CONTROL SYSTEM (A2C2S).COMPLIED WITH 20090903 @ 4413.5 ACFTHOURS.(A2C2S) NOT INSTALLED

24-Aug-2009 1


FD441686

AASF # 2 OHARNGH-60-09-AMAM-06 CARGO HOOK CARTRIDGEACTUATED DEVICE (CAD) LIFE REDUCTIONCOMPLIED WITH 20090903 @ 4413.5 ACFTHOURS.

25-Aug-2009 2


FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE FOR ALL UH-60A/L HELICOPTERS EQUIPPED WITH THEBATTELLE CAUTION ADVISORY PANEL (CAP)AWR 1455 DTD 23 OCT 09 REV 1

23-Oct-2009 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-10-ASAM-03 FIRE BOTTLE DISCHARGELINES AND NOZZLES COMP;IED WITH20091112 @ 4448.5 ACFT HRS.

10-Nov-2009 1


FD441686

AASF # 2 OHARNGH-60-10-AMAM-04 ASN-128D/C DOPPLERGLOBAL POSITIONING SYSTEM GPSNAVIGATION SET COMPLIED WITH 20091112 @4448.5 ACFT HRS.

12-Nov-2009 1


FD441686

AASF # 2 OHARNGH-60-10-ASAM-04 STABILITY AUGMENTATIONSYSTEM (SAS) LINKS. COMPLIED WITH20100212 @ 4457.3 ACFT HRS

18-Nov-2009 2


FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOR THEPHOENIX MODIFIED DRIP PAN ON UH/HH-60A/L HELICOPTERS AWR 1656 DTD 30 DEC09.

30-Dec-2009 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOR UH-60A AND EH-60A HELICOPTERS WITH MAINMODULE ASSEMBLIES (PART NUMBERS 70351-08100-075 AND 70351-08100-076) EQUIPPEDWITH NTHE IMPROVED PLANETARY CARRIERASSEMBLY, PART NUMBER 70351-08175-046AWR 1479 DTD 04 JAN 10 REV 1.

04-Jan-2010 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-10-AMAM-12 IMPROVED DRAG BEAMCOMPLIED WITH 29APR10 @ 4479.0

28-Apr-2010 1

COLUMBUS, OH 43217

FD441686




8.7.DATE

6.REMARKS

4. 5.



AASF # 2 OHARNGH-60-10-ASAM-12 T700 SERIES ENGINESCOMMON COMPONENT RETIREMENT CHANGETIMES C/W 20100803 @4567.0 ACFT HRS.

29-Jul-2010 3

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-11-AMAM-04 ALL H-60 AIRCRAFT: UNITLEVEL LOGISTICS SYSTEM-AVIATION(ENCHANCED) INTEGRATED MATERIELMANAGEMENT CENTER LEGITIMATE CODEFILE CHANGE 61 REQUIREMENTS COMPLIEDWITH 20110110 @ 4706.7 ACFT HRS.

25-Oct-2010 2

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-11-AMAM-03 ALL H-60A/L SERIESAIRCRAFT, OIL COOLER FAN AXIAL BEARINGCOMPLIED WITH 20101026 @ 4652.8 ACFTHRS. N/A THIS AIRCRAFT

25-Oct-2010 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOROPERATION OF UH/HH-60A/L/M AIRCRAFTWITH THE EBC-406HM EMERGENCY LOCATORTRANSMITTER (ELT) INSTALLED, AWR 1516DTD 29 OCT 10 REV 6.

29-Oct-2010 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOROPERATION OF UH-60A/L HELICOPTERS WITHTHE M-240H MACHINE GUN INSTALLED, AWR1120 R-8, 30 NOV 10.

30-Nov-2010 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-11-ASAM-04 ALL H-60 SERIES AIRCRAFT,AN/ARN153 TCN 500 TACAN RECEIVERBEARING ERROR, COMPLIED WITH 20201202.TACAN NOT INSTALLED

01-Dec-2010 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-11-ASAM-08 LINE OF SITE (LOS) /IDENTIFY FRIEND OR FOE (IFF) ANTENNA ANDINTEGRATED VEHICLE HEALTH ANDMONITORING SYSTEMS (IVHMS)ACCELEROMETER CONNECTORS SAFETYWIRE. COMPLIED WITH 20110204 @ 4724.9ACFT HRS.

03-Feb-2011 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-11-AMAM-06 MEDEVAC CAROUSELREFURBISHMENT COMPLIED WITH 20110207.N/A THIS AIRCRAFT

07-Feb-2011 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOR USEOF THE INTEGRATED PERFORMANCE ANDAIRCRAFT CONFIGURATION (IPAC)SOFTWARE FOR PERFORMANCE PEDICTIONFOR UH/HH-60A/L/M HELICOPTERS AWR 1513DTD 25 FEB 11 REV 1.

25-Feb-2011 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE FOR ALL UH/HH-60A/L/M HELICOPTERS EQUIPPED WITH THETITANIUM (1000997-001(S7020-12008-043) ORSTAINLESS STEEL RESCUE HOIST CABLE(GUARD) DEFLECTOR AWR 1566 DTD 18 MAR11 REV 2

18-Mar-2011 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOROPERATION OF AVIATOR'S NIGHT VISIONIMAGING SYSTEM (ANVIS) AN/AVS-6 SERIESNIGHT VISION GOGGLES (NVG) IN UH/HH-60A/L/M AIRCRAFT AWR 1750 DATED 25 MAR11.

25-Mar-2011 1

COLUMBUS, OH 43217

FD441686




8.7.DATE

6.REMARKS

4. 5.



AASF # 2 OHARNGH-60-11-ASAM-09 ALL H-60A/L SERIESAIRCRAFT, INTERNAL AUXILIARY FUELTRANSFER SYSTEMS (IAFTS), NOTINSTALLED IN THIS AIRCRAFT. COMPLIEDWITH 20110329.

28-Mar-2011 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOROPERATION OF GOODRICH 42305-3/-5INTERNAL RESUE HOIST (IRH) ON UH-60A/LHELICOPTERS AWR 1308 R-7 13APR 11

13-Apr-2011 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOR EH-60A AND UH/HH-60A/L/M HELICOPTERSEQUIPPED WITH OREGON AERO SEATCUSHIONS AWR1309 REV 6 22APR 2011

22-Apr-2011 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-11-AMAM-13 ALL H-60 SERIES AIRCRAFT,EXTERNAL HOIST MOUNT FITTING N/A THISACFT.

07-Jun-2011 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOROPERATION OF GOODRICH 42305-3/-5INTERNAL RESUE HOIST (IRH) ON UH-60A/LHELICOPTERS AWR 1308 DTD 17AUG11, REV8.

17-Aug-2011 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOR USEOF THE INTEGRATED PERFORMANCE ANDAIRCRAFT CONFIGURATION (IPAC)SOFTWARE FOR PERFORMANCE PEDICTIONFOR UH/HH-60A/L/M HELICOPTERS AWR 1513DTD 23 AUG 2011 REV 2.

23-Aug-2011 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FORIMMUNE AN/ARN-123 VOR/ILS RECEIVER INUH-60A/L AIRCRAFT, AWR 1787 DTD 26 AUG11.

26-Aug-2011 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOR USEOF THE INTEGRATED PERFORMANCE ANDAIRCRAFT CONFIGURATION (IPAC)SOFTWARE FOR PERFORMANCE PREDICTIONFOR UH/HH-60A/L/M HELICOPTERS AWR 1513DTD 26 OCT 11 REV 3

26-Oct-2011 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE FOR ALL UH-60A/L HELICOPTERS EQUIPPED WITH THEBATTELLE CAUTION ADVISORY PANEL (CAP)AWR 1455 DTD 10 NOV 11 REV 3

10-Nov-2011 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-12-ASAM-02 ALL H-60A/K/L SERIESAIRCRAFT, DRAG BEAM REPLACEMENTCOMPLIED WITH ######## @ ####># ACFTHRS.

05-Dec-2011 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOR UH-60A AND EH-60A HELICOPTERS WITH MAINMODULE ASSEMBLIES (PART NUMBERS 70351-08100-075 AND 70351-08100-076) EQUIPPEDWITH NTHE IMPROVED PLANETARY CARRIERASSEMBLY, PART NUMBER 70351-08175-046AWR 1479 DTD 13 JAN 12 REV 2.

13-Jan-2012 1

COLUMBUS, OH 43217

FD441686




8.7.DATE

6.REMARKS

4. 5.



AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOR EH-60A AND UH/HH-60A/L/M HELICOPTERSEQUIPPED WITH OREGON AERO SEATCUSHIONS AWR1309 DTD 10 FEB 12 REV 7

10-Feb-2012 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-12-ASAM-06 UPPER BULKHEAD FUELSYSTEM BREAKWAY VALVE AND FIREEXTINGUISHING SYSTEM DIEECTIONALVALVE, COMPLIED WITH 20120228 @ 4875.7ACFT HRS.

21-Feb-2012 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOROPERATION OF AVIATOR'S NIGHT VISIONIMAGING SYSTEM (ANVIS) AN/AVS-6 SERIESNIGHT VISION GOGGLES (NVG) IN UH/HH-60A/L/M AIRCRAFT AWR 1750 DTD 27 MAR 12REV 1.

27-Mar-2012 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOR USEOF THE INTEGRATED PERFORMANCE ANDAIRCRAFT CONFIGURATION (IPAC)SOFTWARE FOR PERFORMANCE PREDICTIONFOR UH/HH-60A/L/M HELICOPTERS AWR 1513DTD 02 JUL 2012 REV 4

02-Jul-2012 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-12-ASAM-07 ELECTRICAL WIRING CHAFECOMPLIED WITH 20120821 @ 4965.0

10-Jul-2012 2

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-12-AMAM-12 RESCINDED COMMONCOMPONENT REMOVAL DATES COMPLIEDWITH 20120710 @ 4951.7 ACFT HRS.

10-Jul-2012 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-12-ASAM-08 CARGO HOOK MANUALRELEASE SPRING ASSEMBLY COMPLIEDWITH 20120723 @ 4956.7 ACFT HRS.

18-Jul-2012 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FORGARMIN GPSMAP 696,496,495,396,296, OR 295ON US AMRY UH/HH-60A/L/M HELICOPTERSAWR 1466 DTD 22 AUG 12 REV 5.

22-Aug-2012 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-12-AMAM-15 TRIM ACTUATORSCOMPLIED WITH 20120906 @ ACFT HRS 4966.3

29-Aug-2012 2

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE FOR ALL UH-60A/L HELICOPTERS EQUIPPED WITH THEBATTELLE CAUTION ADVISORY PANEL (CAP)AWR 1455 DTD 18 SEP 12 R4.

18-Sep-2012 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOROPERATION OF UH/HH-60A/L/M AIRCRAFTWITH THE EBC-406HM EMERGENCY LOCATORTRANSMITTER (ELT) INSTALLED, AWR 1516DTD 11 OCT 2012 REV 7.

11-Oct-2012 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-13-AMAM-01 FLIGHT CONTROL RIGGINGPROCEDURES.COMPLIED WITH ######## @####.# ACFT HRS.

23-Oct-2012 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-13-AMAM-02 ATTITUDE HEADINGREFERENCE SYSTEM (AHRS) WIRINGHARNESS COMLIED WITH 20121114 @5020.4ACFT HOURS.

06-Nov-2012 1

COLUMBUS, OH 43217

FD441686




8.7.DATE

6.REMARKS

4. 5.



AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOR USEOF THE INTEGRATED PERFORMANCE ANDAIRCRAFT CONFIGURATION (IPAC)SOFTWARE FOR PERFORMANCE PREDICTIONFOR UH/HH-60A/L/M HELICOPTERS AWR 1513DTD 27 NOV 12 REV 5.

27-Nov-2012 4

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-13-AMAM-04 UNIT LEVEL LOGISTICSSYSTEM- AVIATION (ENHANCED) (ULLS-A(E)AMCOM LOGISTICS CENTER (ALC),LEGITIMATE CODE FILE (LCF) CHANGE 63REQUIREMENTS, COMPLIED WITH 20130114 @5058.0.

27-Nov-2012 3

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-13-AMAM-03 DIGITAL ENGINE CONTROLUNIT (DECU) / ELECTONIC DIGITAL ENGINECONTROL UNIT (EDECU) TURBINE GASTEMPERATURE (TGT) BIAS. COMPLIED WITH20121128 @ 5044.3 ACFT HRS.

27-Nov-2012 2

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGH-60-13-ASAM-01 ANTI-COLLISION LIGHTSPOWER SUPPLY COMPLIED WITH 20121128 @5044.3 ACFT HRS.

27-Nov-2012 1

COLUMBUS, OH 43217

FD441686

AASF # 2 OHARNGAIRWORTHINESS RELEASE (AWR) FOROPERATION OF UH-60A/L HELICOPTERS WITHTHE M-240H MACHINE GUN INSTALLED, AWR1120 DTD 30 NOV 12 REV 9.

30-Nov-2012 1

COLUMBUS, OH 43217

FD441686




8.7.DATE

6.REMARKS

4. 5.



AASF # 2 WIARNGH-60-08-ASAM-03 CHANGES TO CURRENTFUEL SYSTEM INTEGRITY CHECKS C/W(XO8975)

27-Dec-2007 1

MADISON WI 53704-2517

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF #1H-60-15-AMAM-02, IVHMS WIRINGMANAGEMENT, COMPLIED WITH

22-Oct-2014 1

BLDG 19-101ANNVILLE,PA 17003

RH542424




8.7.DATE

6.REMARKS

4. 5.



AASF #1 FTIGMAIN MOD FILTER BUTTON POPPED AT 5066AIRCRAFT HOURS. FILTERS REPLACED, MOCCOMPLETED WITH NO BUTTON POP.

28-Aug-2014 1


RH542424

AASF #1 FTIGH-60-15-SOF-01, OIL COOLER FAN AXIALBEARING, COMPLIED WITH

29-Oct-2014 1


RH542424




8.7.DATE

6.REMARKS

4. 5.



AASF #1 FTIG,H-60-14-ASAM-06, MIXER ASSEMBLY PARTTRACKING AND LUBRICATIONREQUIREMENTS, COMPLIED WITH

16-Apr-2014 1

FTIG

RH542424




8.7.DATE

6.REMARKS

4. 5.



AASF #2 OHARNGTAIL ROTOR BIAS COMPLETED @ 4965 ACFTHRS. RED DIM A 4.816 DIM B 5.149 = .333.YELLOW DIM A 4.156 DIM B 4.499 =.343, BLUEDIM A; 4.866, DIM B 5.196 = .330; BLACK DIM A4.212 DIM B 4.542 = .330.

21-Aug-2012 1

COLUMBUS, OH 43217

JB762128




8.7.DATE

6.REMARKS

4. 5.



AASF #2 WIARNGEMC TEST COMPLETED I/A/W AWR DTD 20MAR 90 FOR INSTALLATION OF ELT. (XR4264)

24-Mar-1995 2

1950 PEARSON ST.MADISON WI.

QC000000

AASF #2 WIARNGUH-60-98-ASAM-04/TB 1-1520-237-20-205LOOSE HUCK BOLTS ON OVERHAULEDPRIMARY SERVOS, COLL. & YAW BOOSTSERVOS, AND T/R SERVOS C/W. (DR4264)

17-Mar-1998 1

MADISON, WI 53704-2517

QC000000

AASF #2 WIARNGUH-60-98-ASAM-05/TB 1-1520-237-20-203 ALL H-60 ACFT WITH SWASHPLATE LINKSMANUFACTURED BY TEC CAGE CODE 65780,P/N 70400-08110-054/-061 C/W (XK1861)

07-May-1998 2


QC000000

AASF #2 WIARNGACFT RECORDS CONVERTED TO ULLS-A(XK1861)

07-May-1998 1


QC000000

AASF #2 WIARNGUH-60-99-ASAM-02/TB 1-1520-237-20-207 H-60HELICOPTERS WITH PROVISIONS TO INSTALLEXTERNAL HOIST AND ALL EXTERNALHOISTS MANUFACTURED BY BREESE C/W.(XR4264)

09-Nov-1998 2


QC000000

AASF #2 WIARNGUH-60-99-ASAM-01/TB 1-1520-237-20-208RESTORATION OF FULL SERVICE LIFE ONSWASHPLATE LINK MANUFACTURED BY TECC/W. (XR4264)

09-Nov-1998 1


QC000000

AASF #2 WIARNGEMC TEST COMPLETED FOR LOCALLYMANUFACTURED LOCKING DEVICE I/A/W AWRDTD 7 JAN 99. (XR4264)

04-Feb-1999 2

1950 PEARSON ST.MADISON WI

QC000000

AASF #2 WIARNGINSTALLATION OF LOCALLY MANUFACTUREDLOCKING DEVICE I/A/W AWR DTD 07 JAN 99.(XR4264)

04-Feb-1999 1


QC000000

AASF #2 WIARNGUH-60-99-ASAM-10/TB1-1520-237-20-213INSPECTION AND PREVENTIVE MAINTENANCEON THE NUMBER TWO CROSSFEEDBREAKAWAY VALVE C/W. (XK1861)

01-Oct-1999 1

MADISON WI. 53704-2517

QC000000

AASF #2 WIARNGAIRCRAFT DIGITAL ELECTRONIC CLOCKS P/NPDMME-367-3 INSTALLED IAW ECP-454REPLACING MECHANICAL CLOCKS P/N ABU-11/A AT PMS-2 AT 2466 ACFT HRS. (XK1861)

19-Nov-1999 2


QC000000

AASF #2 WIARNGTB 1-1520-237-20-167 INSPECTION ANDREPAIR OF STA 635 FRAME ASSEMBLY FORT/W STRUT CLEARANCE FOUND PREVIOUSLYCOMPLIED WITH AT PMS-2 AT 2466 ACFT HRS.(XK1861)

19-Nov-1999 1


QC000000

AASF #2 WIARNGUH-60-00-ASAM-02/TB 1-1520-237-20-216RELOCATION OF CYCLIC STICK WIREBUNDLES C/W AT 2466.0 ACFT HRS. (XR4264)

16-Dec-1999 1


QC000000

AASF #2 WIARNGEMC TEST COMPLETED I/A/W AWR DTD 17DEC99 FOR INSTALLATION OF ELT. (XR4264)

04-Jan-2000 2


QC000000

AASF #2 WIARNGAWR DTD 17 DEC 99 FOR THE INSTALLATIONOF ELT'S SUPERCEDES AWR DTD 20 MAR 90.(XR4264)

04-Jan-2000 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF #2 WIARNGPMS-2 COMPLETED AT 2466 ACFT HRS. NEXTDUE AT 2966 ACFT HRS. (XK1861)

06-Jan-2000 1


QC000000

AASF #2 WIARNGUH-60-00-ASAM-04/TB1-1520-237-20-218INSPECT TAIL LANDING GEAR ASSY. FORMISSING BEARING PINS C/W (XR4264)

24-Feb-2000 1


QC000000

AASF #2 WIARNGUH-60-00-ASAM-05/TB1-1520-237-20-219INSPECT FIRE EXTINGUISHER WIRING C/W.219C/W. (XR4264)

17-May-2000 1


QC000000

AASF #2 WIARNGEMC TEST COMPLETED FORCOMMUNICATION EAR PLUG I/A/W AWR DTD14 JUL 99. (XR4264)

18-Sep-2000 2


QC000000

AASF #2 WIARNGAWR DTD 14 JUL 99 FOR THECOMMUNICATION EAR PLUG INSTALLATIONAND TESTING C/W. (XR4264)

18-Sep-2000 1


QC000000

AASF #2 WIARNG100 HR EXTENSION GRANTED FORREPLACEMENT OF SERVO BEAM RAILS PERMEMO DTD 29 SEP 00. FROM AMCOM LARMR. GARRY DAVIS AT 2700.0 ACFT HRS.(XR4264)

03-Oct-2000 1


QC000000

AASF #2 WIARNGUH-60-01-07/08 TB 1-1520-237-20-232 INSP M/RFLIGHT CONTROL SELF LOCKING BOLTS C/W(XC8756)

14-Jun-2001 1

1950 PEARSON STMADISON, WI

QC000000

AASF #2 WIARNGSAND & DUST EROSION TAPE INSTALLED ONM/R & T/R BLADES FOR DEPLOYMENT TOKUWAIT AT 3095.5 ACFT HRS (XM2513)

10-Feb-2003 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF #2 WIARNG1/147TH AVN

SOF UH-60-01-01/TB 1-1520-237-20-225 INITIALAND RECURRING INSPECTION OF MLG DRAGBEAM ASSY'S AND REDUCTION OF TORQUEON JACKPAD NUT C/W AT 2724.3 ACFT HRS.(XK1861)

09-Nov-2000 1


QC000000

AASF #2 WIARNG1/147TH AVN

SOF UH-60-01-02/TB 1-1520-237-20-225/227INITIAL & RECURRING INSPECTION OF MLGDRAG BEAM ASSY'S AND REDUCTION OFTORQUE ON JACKPAD NUT. UPDATE C/W.(XR4264)

03-Jan-2001 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF #2 WIARNG 1-147TH AVN

SOF UH-60-04-03 CRASHWORTHY EXTERNALFUEL SYSTEM (CEFS) OPERATIONS. N/A THISAIRCRAFT, ESSS HARD-POINTS NOTINSTALLED (XK1861)

15-Jul-2004 1


QC000000


UH-60-04-ASAM-04 REVISION TO UH-60-04-03FUEL SYSTEM INTEGRITY CHECK. (ENTRYMADE IN LOGBOOK) (XK1861)

25-Aug-2004 2


QC000000


SOF UH-60-04-04 MAIN ROTOR HUB REWORK,COLLECTION OF HUB PART NUMBERS ANDTIME SINCE NEW INFORMATION C/W.(XK1861)

25-Aug-2004 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF #2 WIARNG.UH-60-97-ASAM-02/ TB 1-1520-237-20-184 ONETIME INSPECTION OF TAIL DRIVE FLEXCOUPLING CONNECTIONS C/W. (DR4264)

28-Oct-1996 1

MADISON, WI.53704-2517

QC000000

AASF #2 WIARNG.UH-60-97-ASAM-08/TB 1-1520-237-20-187 ALLH60 ACFT. WITH CONNECTING LINK ASSY.P/N70400-08155-056 MANUFACTURED BYPURDY MACHINE CO. C/W. (DR4264)

22-Jan-1997 3


QC000000

AASF #2 WIARNG.UH-60-97-ASAM-05/TB 1-1520-237-23-03 ONETIME INSP. FOR REMOVAL & REWORK OFCERTAIN VISCOUS DAMPER BRNG.SUPPORTASSYS. C/W. (DR4264)

22-Jan-1997 2


QC000000

AASF #2 WIARNG.GEN-97-ASAM-03 CHANGE OF PROCEDURESFOR LOADING THE CRYPTO KEYS INNAVSTAR AN/ASN-149 GPS RECEIVER C/W.(DR4264)

22-Jan-1997 1


QC000000

AASF #2 WIARNG.UH-60-97-ASAM-15/TB 1-1520-237-20-196 ONETIME INSP. FOR BEARING ROD END C/W.(JV1079)

11-Aug-1997 2


QC000000

AASF #2 WIARNG.UH-60-97-ASAM-14/TB 1-1520-237-20-195 ONETIME INSP. FOR BELLCRANK SUPPORT C/W(JV1079)

11-Aug-1997 1


QC000000

AASF #2 WIARNG.UH-60-97-ASAM-17/TB 1-1520-237-20-199 ONETIME INSP. FOR THE INTERNAL RESCUEHOIST BRKT. ASSY.C/W (DR4264)

20-Aug-1997 1


QC000000

AASF #2 WIARNG.UH-60-98-ASAM-02/TB 1-1520-237-20-197 ONETIME INSP. FOR SUSPECT PUSHRODSP/N70400-08155-050 & 51 C/W (RK1861)

04-Oct-1997 2


QC000000

AASF #2 WIARNG.UH-60-97-ASAM-19/TB 1-1520-237-20-204 ONETIME INSP. OF ANVIS / HUD POWER SUPPLYC/W. (DR4264)

04-Oct-1997 1


QC000000

AASF #2 WIARNG.UH-60-98-ASAM-03/TB 1-1520-237-20-203 ONETIME INSP. FOR SWASHPLATE LINK P/N 70400-08110-054 C/W (DR4264)

10-Nov-1997 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF #2, 1/147TH AVNUH-60-94-ASAM-12/TB 1-1520-237-50-156AUTHORIZATION OF UH-60L ACFT FOR 9000LB EXTERNAL LOAD AND MAXIMUMEXTERNAL LOAD OPERATIONS OF 23,000LBS. N/A THIS ACFT. (XK1861)

18-Nov-1994 6


QC000000

AASF #2, 1/147TH AVNUH-60-92-ASAM-15/TB 1-1520-237-50-145REVISION TO UH-60-93-ASAM-14 INSPECTIONOF ERFS EJECTOR RACKS. N/A THIS ACFT.(XK1861)

18-Nov-1994 5


QC000000

AASF #2, 1/147TH AVNUH-60-92-ASAM-14/TB 1-1520-237-50-145 H-60ACFT WITH ESSS & ERFS MISSION KITSINSTALLED. INSPECTION OF ERFS EJECTORRACKS. N/A THIS ACFT. (XK1861)

18-Nov-1994 4


QC000000

AASF #2, 1/147TH AVNUH-60-92-ASAM-13/TB 1-1520-237-50-148 H-60ACFT WITH ESSS & ERFS MISSION KITSINSTALLED. N/A THIS ACFT. (XK1861)

18-Nov-1994 3


QC000000

AASF #2, 1/147TH AVNUH-60-93-ASAM-12/TB 1-1520-237-20-143ABRUPT CHANGE IN M/R TRACK/VIBRATIONSPCW. (XK1861)

18-Nov-1994 2


QC000000

AASF #2, 1/147TH AVNACFT RECEIVED AT THIS STATION WITH1480.9 ACFT HRS FROM CCAD. (DR4264)

18-Nov-1994 1


QC000000

AASF #2, 1/147TH AVNUH-60-95-ASAM-04/TB 1-1520-237-20-160REDUCTION OF TORQUE OF PIVOT BOLTSC/W. (DR4264)

15-Dec-1994 1


QC000000

AASF #2, 1/147TH AVNUH-60-95-ASAM-05/TB 1-1520-237-20-163CHANGE IN RETIREMENT LIFE FOR P/N -50/-52/-54/-56 SERVO BEAM RAILS C/W. (XK1861)

04-Jan-1995 1


QC000000

AASF #2, 1/147TH AVNSOF UH-60-95-02/TB 1-1520-237-20-161CHANGE TO RETIREMENT LIFE M/R BLADECUFFS C/W. (DR4264)

03-Mar-1995 1


QC000000

AASF #2, 1/147TH AVNINSTALLATION OF ELT EBC-302 I/A/WAIRWORTHINESS RELEASE DATED 20 MAR 90C/W. (DR4264)

24-Mar-1995 1


QC000000

AASF #2, 1/147TH AVNUH-60-95-ASAM-06/TB 1-1520-237-20-168 ONETIME INSPECTION FOR CRACKED MAIN XMSNBEAMS AND IMPLEMENTATION OFREACURRING 100 HR INSPECTION C/W.(DR4264)

09-Aug-1995 1


QC000000

AASF #2, 1/147TH AVNUH-60-95-ASAM-07/TB 1-1520-237-20-164REPLACEMENT CRITERIA FORTROOP/GUNNER SEAT ATTENUATION WIRESC/W. (DR4264)

13-Aug-1995 1


QC000000

AASF #2, 1/147TH AVNUH-60-96-ASAM-01/TB 1-1520-237-20-170 ALLACFT WITH IMPROVED FLT CONTROLS,REPLACEMENT OF 70400-08159 SERIESBOLTS C/W, N/A THIS ACFT. (XK1861)

14-Oct-1995 1

MADISON,WI

QC000000

AASF #2, 1/147TH AVNSOF UH-60-96-01/TB 1-1520-237-20-172CHANGE IN RETIREMENT LIFE OF CERTAINFWD BELLCRANK SUPPORTS AND REMOVALOF SUSPECT S/N'S C/W. (XK1861)

08-Nov-1995 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF #2, 1/147TH AVNSOF UH-60-96-02/TB 1-1520-237-20-173 ONETIME INSPECTION FOR SUSPECT TAIL ROTORINBOARD PLATES C/W. (XK1861)

30-Nov-1995 1


QC000000

AASF #2, 1/147TH AVNUH-60-96-ASAM-03/TB 1-1520-237-20-171REVISION TO ONE TIME INSPECTION FORSUSPECT M/R SHAFT NUT BOLTS REQ'D BYUH-60-96-ASAM-02 C/W. (DR4264)

25-Jan-1996 2


QC000000

AASF #2, 1/147TH AVNUH-60-96-ASAM-02/TB 1-1520-237-20-171 ONETIME INSPECTION FOR SUSPECT M/R SHAFTNUT BOLTS C/W. (DR4264)

25-Jan-1996 1


QC000000

AASF #2, 1/147TH AVNUH-60-96-ASAM-04/TB 1-1520-237-20-176 ALLACFT WITH FAST ROPEINSERTION/EXTRACTION SYSTEM (FRIES)BAR MAXIMUN ALLOWABLE LOADREDUCTION C/W, N/A THIS ACFT. (XK1861)

26-Jan-1996 1

MADISON,WI

QC000000

AASF #2, 1/147TH AVNUH-60-96-ASAM-10/TB 1-1520-237-20-182 ALLH-60 SERIES ACFT, SPINDLE ASSY'S ANDELASTOMERIC BEARINGS C/W. (DR4264)

06-Oct-1996 1


QC000000

AASF #2, 1/147TH AVNSOF UH-60-98-01 RISK MANAGEMENT OF 230GALLON EXTERNAL TANKS FLIGHTOPERATIONS C/W, N/A THIS ACFT W/O ESSS.(XK1861)

27-Jan-1998 1

MADISON,WI

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF #2, OHARNGH-60-10-AMAM-10, REVISED USE OFAMOGS/OBOGS, COMPLIED WITH, N/A THISMDS, HH-60 ACFT ONLY.

26-Jan-2010 1


GG540327

AASF #2, OHARNGH-60-10-ASAM-06, ALL H-60A ACFT, AUTO-IGNITION AND TDI, COMPLIED WITH, N/A THISACFT, T700-GE-700 ENGINES INSTALLED.

09-Feb-2010 1


GG540327

AASF #2, OHARNGH-60-10-ASAM-08, APU & APU FIREWALL,COMPLIED WITH 18 MAY 2010 @ 4497.0 ACFTHRS.

17-May-2010 2

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-10-ASAM-08, ALL H-60A/L SERIESAIRCRAFT, APU & APU FIREWALL C/W18MAY2010 @ 4497.0 ACFT HRS.

17-May-2010 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-10-SOF-02, ALL H-60 SERIES AIRCRAFT,SPINDLE LUG NDI & RETIREMENT LIFECHANGES, COMPLIED WITH ON 22 JUN 2010 @4523.0 ACFT HRS.

18-Jun-2010 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-10-AMAM-16, CMWS SWITCH GUARD,COMPLIED WITH ON 24 JUN 10 @ 4524.0 ACFTHRS.

23-Jun-2010 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-10-ASAM-11, COMMOM COMPONENT RCTIMES UPDATE, COMPLIED WITH 29JUL10 @4567.0 ACFT HRS

15-Jul-2010 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGLEFT SIDE CABIN PLATING BELOW GUNNERSWINDOW (TORQUE BOX) REPAIRED IAW MECF112516.

29-Jul-2010 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-10-ASAM-15, IMPROVED ESSS FUELSYSTEM VENT ELBOW (TERMISTOR)COMPLIED WITH ON 11AUG2010 @4568.0ACFT HOURS.

10-Aug-2010 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-10-ASAM-16, RESCUE HOIST CABLE CUTHARNESS CONNECTOR COMPLIED WITH.

12-Sep-2010 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-11-AMAM-11, EH/HH/UH-60A/B/L/MSERIES AIRCRAFT, AIRWORTHINESSRELEASE STATUS UPDATE, COMPLIED WITH21 APR 2011 @ 4779.8 ACFT HRS.

18-Apr-2011 2

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-11-AMAM-09, ALL H-60/AH-64 SERIESAIRCRAFT, DA FORM 2408-19-3 ENGINECOMPONENT OPERATING HOUR RECORDCOMPLIED WITH 26 APR 2011 @ 4779.8 ACFTHRS.

18-Apr-2011 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-11-ASAM-13, ALL H-60A/L SERIESAIRCRAFT, ENGINE AIR INLET ANTI-ICING/MODULATING VALVE, COMPLIED WITH1 JUL 11, @ 4809.4 ACFT HRS.

29-Jun-2011 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-11-SOF-01, ALL H-60 SERIES AIRCRAFT,DISCREPANT SELF LOCKING DOUBLEHEXAGON NUTS, COMPLIED WITH 16 JUL 11.

07-Jul-2011 2

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNG H-60-11-ASAM-14, ALL H-60 SERIESAIRCRAFT, ENGINE COWLING REPAIRRESTRICTIONS, COMPLIED WITH 27 JUL 11@ 4809.4 ACFT HRS.

07-Jul-2011 1

COLUMBUS, OH 43217

GG540327




8.7.DATE

6.REMARKS

4. 5.



AASF #2, OHARNGH-60-11-AMAM-15, ALL EH/HH/UH-60A/LSERIES AIRCRAFT, INTEGRATED VEHICLEHEALTH MANAGEMENT SYSTEM (IVHMS)ACCELEROMETERS, COMPLIED WITH20110808 @ 4809.4 ACFT HRS. N/A THISAIRFRAME

11-Jul-2011 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGPMI 1 COMPLETED AT 4809.4 ACFT HRS, PMI 2WILL BE DUE AT 5169.4 ACFT HRS.

20-Aug-2011 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNG H-60-11-AMAM-17, ALL H-60 SERIESAIRCRAFT, TAIL ROTOR INBOARD /OUTBOARD RETENTION PLATE SHIMS,COMPLIED WITH 20120821 @ 4965.0 ACFTHRS.

19-Sep-2011 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-11-AMAM-19, AVIATION MAINTENANCEACTION MESSAGE (AMAM), MAINTENANCEMANDATORY, UNIT LEVEL LOGISTICSSYSTEM-AVIATION (ENHANCED)(ULLS-A(E))INTEGRATED MATERIEL MANAGEMENTCENTER (IMMC) LEGITIMATE CODE FILE (LCF)CHANGE 62 REQUIREMENTS, COMPLIED WITH20111114.

20-Sep-2011 2

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-11-AMAM-20, ALL UH-60A/L SERIESAIRCRAFT, AN/ASN-128D DOPPLER ANDAVIATION MISSION PLANNING SYSTEM(AMPS) SOFTWARE UPGRADE, COMPLIEDWITH 20110921 @ 4822.8 ACFT HRS.

20-Sep-2011 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-12-SOF-01, SAFETY OF FLIGHT (SOF),EMERGENCY, ALL H-60 SERIES AIRCRAFT,TAIL ROTOR INTERMEDIATE GEARBOXCOMPLIED WITH, 20111011 @ 4827.3 ACFTHRS.

08-Oct-2011 1

COLUMBUS, OH 43217

AASF #2, OHARNGH-60-12-SOF-02, SAFETY OF FLIGHT (SOF),TECHNICAL, REVISION TO H-60-12-SOF-01,ALL H-60 SERIES AIRCRAFT, TAIL ROTORINTERMEDIATE GEARBOX COMPLIED WITH,20111011 @ 4827.3 ACFT HRS.

11-Oct-2011 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-12-SOF-03, SAFETY OF FLIGHT (SOF),TECHNICAL, ALL H-60 SERIES AIRCRAFT, TAILROTOR INTERMEDIATE GEARBOX COMPLIEDWITH 20111016 @ 4829.7 ACFT HRS.

14-Oct-2011 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-12-ASAM-01, AVIATION SAFETY ACTIONMESSAGE (ASAM), MAINTENANCEMANDATORY, ALL H-60 SERIES AIRCRAFT,TAIL ROTOR OUTPUT BEVEL GEAR NON-DESTRUCTIVE INSPECTION COMPLIED WITHXXXX @ XXXX ACFT HRS.

17-Oct-2011 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-12-AMAM-03, AVIATION MAINTENANCEACTION MESSAGE (AMAM), MAINTENANCEMANDATORY, ALL H-60A/L SERIES AIRCRAFT,TRANSPONDER AND COMMON MISSILEWARNING SYSTEM INSTALLATION COMPLIEDWITH 20111103 @ 4840.1 ACFT HRS, N/A THISAIRCRAFT CMWS NOT INSTALLED.

31-Oct-2011 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGAirworthiness Release (A WR) for Operationofthe Goodrich 42305-3/-5 Internal Rescue Hoist(IRH) on UH-60AlL Helicopters (AWR 1308)

23-Dec-2011 1

COLUMBUS, OH 43217

GG540327




8.7.DATE

6.REMARKS

4. 5.



AASF #2, OHARNGAirworthiness Release (AWR) for UH/HH-60A/LHelicopters Equipped with the PhoenixModified Drip Pan (AWR 1656R1).

28-Dec-2011 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-12-SOF-04, EMERGENCY, ALL H-60SERIES AIRCRAFT, BREEZE EASTERNEXTERNAL RESCUE HOIST OPERATIONS, C/W20120221. N/A THIS ACFT, EXTERNAL HOISTPROVISIONS NOT INSTALLED.

22-Feb-2012 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-12-AMAM-09, MAINTENANCEMANDATORY, ALL H-60 SERIES AIRCRAFT,HYDRAULIC LINE CHAFE DUE TO MISSINGCLAMPS, COMPLIED WITH ON 20120522 @4925.7 ACFT HRS.

16-May-2012 1

COLUMBUS, OH 43217

GG540327

AASF #2, OHARNGH-60-13-AMAM-05 MAIN LANDING GEARWHEEL BRAKE ASSY. COMPLIED WITH ON20130117 @ 5058.0 ACFT HOURS

18-Jan-2013 1

COLUMBUS, OH 43217

JB762128




8.7.DATE

6.REMARKS

4. 5.



AASF #2, OHARNGH-60-11-ASAM-06, ALL H-60 SERIESAIRCRAFT, CYCLIC STICK STOP BOLTS,COMPLIED WITH 20110322 @ 4755.9 ACFTHRS.

21-Dec-2010 1

COLUMBUS, OH 43217

GG540327




8.7.DATE

6.REMARKS

4. 5.



AASF #2, WIARNG,1/147TH AVN

UH-60-00-ASAM-06/TB 1-1520-237-20-219REVISION TO UH-60-00-ASAM-05 INSPECTIONOF FIRE EXTINGUISHER WIRING C/W AT2603.1 ACFT HRS. (XK1861)

23-Jun-2000 1


QC000000


SOF UH-60-01-04/TB 1-1520-237-20-228REVISION TO SOF UH-60-98-01 RISKMANAGEMENT OF 230 GAL EXTERNAL TANKOPERATIONS, INSP FOR INSTALLATION OFFUEL MONITORING SYSTEM. N/A THIS ACFT,ESSS HARDPOINTS NOT INSTALLED AT 2776.6ACFT HRS. (XK1861)

09-Jan-2001 1


QC000000


PERMISSION GRANTED TO EXTEND PMS-2DUE TIME BY 10 HRS FROM 2966 TO 2976ACFT HRS TO FACILITATE FLIGHT FROMHOME STATION TO KILLEEN, TX FORCOMPLETION OF PMS-2 BY MR STEPHENDOREY OF AMCOM. ALSO EXTENDED BY 10HRS WERE REPLACEMENT OF FWDBELLCRANK SUPPORT P/N 70400-08116-048, 4M/R SPINDLE NUTS P/N 70102-08105-102, AND#1 VISCOUS DAMPER BEARING P/N 110KSZZ-401, (XK1861)

27-Nov-2001 1


QC000000


ACE PERFORMED AT 2985 ACFT HRS ATMADISON, WI BY P & D, PROJECT OLR FTLEWIS, WA. (XK1861)

30-May-2002 1


QC000000


SIGTRONIC TRANSCOM 2 PORTABLEBATTERY POWERED INTERCOM INSTALLEDAND EMC TEST COMPLETED IAW AWR 759DTD 05 JUN 02 AT 3097.1 ACFT HRS. (XK1861)

15-Feb-2003 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF #2/1-147TH AVNISAQ 135 DATED 13 APR 07 (PHOENIXMAODIFIED DRIP PAN) SUPERCEDES AWR 888R1 DATED 01SEP06 (XL5732)

02-Jul-2008 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF #2/1-147TH AVNBN

UH-60-05-ASAM-02 BLUE FORCE TRACKERINSTALLATION C/W AT 3425.7 ACFT HRS. BFTNOT INSTALLED ON THIS ACFT. (XK1861)

03-Mar-2005 1


QC000000


SOF UH-60-05-01 REACTIVAITON OF COCKPITAIRBAG SYSTEM (CABS) C/W AT 3447.0 ACFTHRS. CABS NOT INSTALLED ON THIS ACFT.(XK1861)

16-Mar-2005 1


QC000000


TFM-138B FREQUENCY MODULATED (FM)HIGH BAND RADIO INSTALLED IAW AWR 913DATED 01 AUG 2003. EMC TEST ORIGINALLYCOMPLETED ON ACFT 8123554 20 NOV 2003.(XK1861)

22-Mar-2005 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF #2/1-147TH AVN,WIARNG

DAVID CLARK INTERCOM SYSTEM WITHU3800 MASTER STATION, U3806 REMOTEHEADSETS, AND H3332 HEADSET/MICROPHONES INSTALLED IAW AWR 1227DATED 05 NOV 2004. EMC TEST ORIGINALLYCOMPLETED ON ACFT 8123554 17 NOV 2004.(XK1861)

22-Mar-2005 2


QC000000


UH-60-05-ASAM-04 TAIL LANDING GEAR YOKEASSEMBLY C/W (XK1861)

15-Apr-2005 3

MADISON WISCONSIN53704-2517

QC000000


UH-60-05-ASAM-03 AIRCREW RESTRAINTSYSTEM COMPATABILITY C/W (XK1861)

15-Apr-2005 2


QC000000


S.E.I. BAMBI BUCKET TEMPORARILYINSTALLED IAW AWR 1054 DATED 16 APR 04,TO INCLUDE SACKSAFOAM DISPENSINGSYSTEM (XC8756)

15-Apr-2005 1


QC000000


UH-60-05-ASAM-06 ONE TIME INSPECTION OFTROOP SEAT RESTRAINT BUCKLES C/W AT3485 ACFT HRS. (XK1861)

11-Jun-2005 1


QC000000


SOF UH-60-05-02/TB 1-1520-237-20-266ENHANCED SCHEDULED MAINTNENANCE(ESM) PROGRAM IMPLEMENTATION ACFTPLACED ON ESM AT 3549.4 ACFT HRS. PMIDUE AT 3757.0 ACFT HRS. (XK1861)

07-Jul-2005 1


QC000000


UH-60-05-ASAM-09 CRASHWORTHYEXTERNAL FUEL SYSTEM (CEFS)INSTALLATION BOLTS C/W AT 3559.3 ACFTHRS, ACFT NOT MODIFIED FOR CEFS.(XK1861)

02-Aug-2005 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF 3 2 OHARNGAIRWORTHINESS RELEASE (AWR) FORGARMIN GPSMAP 696,496,495,396,296, OR 295ON US AMRY UH/HH-60A/L/M HELICOPTERSAWR 1466 DTD 01 DEC 10 REV 3.

01-Dec-2010 2

COLUMBUS, OH 43217

FD441686

AASF 3 2 OHARNGAIRWORTHINESS RELEASE (AWR) FORGARMIN GPSMAP 696,496,495,396,296, OR 295ON US AMRY UH/HH-60A/L/M HELICOPTERSAWR 1466 DTD 31 AUG 11 REV 4.

31-Aug-2011 1

COLUMBUS, OH 43217

FD441686




8.7.DATE

6.REMARKS

4. 5.



AASF# 2 OHARNGH-60-10-AMAM-05 UNIT LEVEL LOGISTICSSYSTEM-AVIATION (ENHANCED)(ULLS-A(E))INTERGRATED MATERIEL MANAGEMENTCENTER (IMMC) LEGITIMATE CODE FILE (LCF)CHANGE 60B REQUIREMENTS. COMPLIEDWITH 20100118 @4457.3 ACFT HRS.

18-Nov-2009 1


FD441686




8.7.DATE

6.REMARKS

4. 5.



AASF#1H-60-14-AMAM-12 MAIN ROTOR (MR) SPINDLENUT RETIREMENT LIFE EXTENSIONCOMPLIED WITH

25-Apr-2014 1

FTIG

PL544246




8.7.DATE

6.REMARKS

4. 5.



AASF#2H-60-09-ASAM-11 CARGO DOOR WINDOWEMERGENCY JETTISON HANDLE ASSEMBLY.C/W 20090625 @ 4359.9 ACFT HRS.

24-Jun-2009 1

COLUMBUS, OH 43217

FD441686

AASF#2H-60-09-ASAM-11 CORRECTED COPY CARGODOOR WINDOW EMERGENCY JETTISONHANDLE ASSEMBLY. SEE ENTRY 24-JUN-2009

25-Jun-2009 1

COLUMBUS, OH 43217

FD441686




8.7.DATE

6.REMARKS

4. 5.



AASF#2 OHARNGH-60-13-AMAM-06 CRASHWORTHY EXTERNALFUEL SYSTEM COMPLIED WITH 20130213 @5059.0 ACFT HRS.

11-Feb-2013 2

COLUMBUS, OH 43217

CB769770




8.7.DATE

6.REMARKS

4. 5.



AASF#2 OHIOMAINTENANCE ENGINEERING CALL(MEC)MEC #F159460; ACFT HAS TWELVE LOOSEFASTENERS LOCATED AT STATION 327 ANDWL 261 ALONG THE MAIN GEARBOXSUPPORT. REPAIRED

11-Jan-2013 1

COLUMBUS, OH 43217

CB769770

AASF#2 OHIOMAINTENANCE ENGINEERING CALL(MEC)MEC #F159913; AUTHORIZATION TO DEFERREPLACEMENT OF LOOSE FASTENERS (3EA)FOR 100 FLIGHT HOURS NOT TO EXCEED5185.0 OR UNTIL INDUCTION INTO OCM, ATWHICH TIME TRANSMISSION WILL BEREMOVED TO FACILITATE REPLACEMENT OFAFOREMENTIONED FASTENERS.

22-Jan-2013 1

COLUMBUS, OH 43217

CB769770




8.7.DATE

6.REMARKS

4. 5.



AASF#2 WIARNGPMS-2 COMPLETED AT 1966 ACFT HRS. NEXTPMS-2 DUE AT 2466 ACFT. HRS. (RK1861)

25-Mar-1997 1


QC000000

AASF#2 WIARNG(AWR 888) FOR ALL UH-60A HELICOPTERSAUTHORIZING THE INSTALLATION OF THEPHOENIX MODIFIED DRIP PAN & 2408-13-1PERPETUATED VISUAL INSP. WRITE-UP I/A/WAWR DTD 7 APR 00 C/W. (XR4264)

27-Jul-2000 1


QC000000

AASF#2 WIARNGUH-60-04-ASAM-05 RESTRAINT SYSTEMINSPECTION C/W AT 3384 A/C HRS (XC8756)

05-Oct-2004 1

MADISON WI 53704

QC000000

AASF#2 WIARNGH-60-08-ASAM-05 REPLACEMENT OF T/RSPRING CAPSULES INITIAL REQUIREMENTSCOMPLIED WITH (XC8756)

17-Dec-2007 1


QC000000

AASF#2 WIARNGH-60-08-ASAM-04 PILOT'S LOWER SEAT RAILCHAFFING ELECTRICAL HARNESS C/W(XC8756)

21-Dec-2007 1


QC000000

AASF#2 WIARNGINSP A673 48 MONTH FUEL CELL CORROSIONINSPECTION COMPLETED. MINOR AMOUNTSOF MOLD NOTED IN AREAS L306, L408, R110,R209, AND R407. IAW WP 1706 OF TM 1-1520-237-23-12 DTD 17 APR 06, WITH CHG #3:REINSPECT FUEL CELL AREA AT NEXT PMI,SCHEDULED FOR 4460.3 A/C HRS. REMOVEFUEL CELLS AND REPAIR AIRFRAME AT NEXTA673, SCHEDULED FOR 7 FEB 2013

03-Feb-2009 1

Madison, WI 53704-2517

RC728756

AASF#2 WIARNGH-60-09-ASAM-04 C/W. NO HOIST INSTALLED,ASAM IS N/A THIS AIRCRAFT

04-Mar-2009 1


RC728756




8.7.DATE

6.REMARKS

4. 5.



AASF#2 WIARNG / 1-147TH AVIATION

S.E.I BAMBI BUCKET TEMPORARILYINSTALLED IAW AWR 1054 DATED 28 MAR 05,WHICH SUPERCEDES AWR 1054 DATED 16APR 04. EMC CHECK PREVIOSLY COMPLIEDWITH ON A/C 7923269 ON 09 APR 2003.(XC8756)

27-Apr-2005 1


QC000000


COMMUNICATION EAR PLUG (CEP) HAS BEENINCORPORATED INTO MWO 1-8415-216-20--1.AWR DATED 14 JUL 99 IS NO LONGERREQUIRED (XC8756)

01-Jun-2005 1


QC000000


AWR 1227 DATED 21 DEC 05, SUPERCEDESAWR DATED 05 NOV 04. (DAVID CLARK ICS)ONE TIME EMC CHECK P/C/W ON UH-60A8123554 ON 17 NOV 05 (XC8756)

05-Jan-2006 1


QC000000


T/R BIAS SET 07 MAR 06 AT 3643.3 A/C HOURSBIAS READINGS: RED INITIAL=4.767FINAL=5.095 VALUE=.328BLUE INITIAL=4.078FINAL=4.402 VALUE=.324YELLOWINITIAL=4.772 FINAL=5.092 VALUE=.320BLACKINITIAL=4.080 FINAL=4.416 VALUE=.336(XC8756)

07-Mar-2006 1


QC000000


UH-60-06-ASAM-02 INSPECTION OF MAINROTOR PITCH CHANGE LINK HARDWARECOMPLIED WITH. NO DEFECTS FOUND(XC8756)

10-Apr-2006 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF#2 WIARNG / 1-147TH AVN

H-60-08-SOF-01 MAIN ROTOR EXPANDABLEPIN INSPECTION INTERVAL. C/W (JW3316)

02-Feb-2008 2


QC000000

AASF#2 WIARNG / 1-147TH AVN

H-60-08-AMAM-05 INTERNAL RESCUE HOISTCONVERSION C/W (JW3316)

02-Feb-2008 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF#2 WIARNG / 1-147TH AVN BN

H-60-08-AMAM-06 COMMON MISSILEWARNING SYSTEM INSPECTION COMPLIEDWITH (DC8756)

06-Feb-2008 2


QC000000


H-60-08-ASAM-04 COCKPIT DOORJETTISONABLE WINDOW SEAL MODIFICATIONCOMPLIED WITH (XC8756)

06-Feb-2008 1


QC000000


AWR 1054 R7 DATED 06JUN07 SEI BAMBIBUCKET SUPERCEDES AWR 1054 R6 DATED22SEP05 (XL5732)

17-Feb-2008 4


QC000000


AWR 888 R1 DATED 01SEP06 PHOENIXMODIFIED DRIP PAN SUPERCEDES AWR 888DATED 07APR00 (XL5732)

17-Feb-2008 3


QC000000


INSTALLATION OF HELIBASKET WITH ELLIAW AWR 1127 DATED 22SEP06 EMC CHECKPCW ON ACFT UH-60 9526610 21AUG06 AT2152.6 A/C HOURS (XL5732)

17-Feb-2008 2


QC000000


INSTALLATION OF AIRCRAFT WIRELESSINTERCOM SYSTEM IAW AWR 1329 DATED07SEP06 EMC CHECK PCW ON AIRCRAFT UH-60 8123607 ON 17JAN07 AT 4697.6 A/C HOURS(XL5732)

17-Feb-2008 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF#2 WIARNG1/147TH AVIATION

UH-60-02-ASAM-10 INSP AERIAL REFUELINGPROBE, N/A THIS AIRFRAME (XC8756)

02-Jul-2002 1

MADISON WI 53704

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF#2 WIARNG1/147TH AVN BN

UH-60-00-ASAM-07/TB 1-1520-237-20-224INSPECT WIRE HARNESSES CONNECTINGTHE #1 AND #2 JUNCTION BOXES C/W(XC8756)

31-Aug-2000 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF#2 WIARNG/ 1-147TH AVN

UH-60-04-02 DISABLING COCKPIT AIRBAGSYSTEM. CABS NOT INSTALLED THISAIRCRAFT. (XC8756)

11-Jun-2004 1


QC000000

AASF#2 WIARNG/ 1-147TH AVN

A/C DEPLOYED TO CONUS THEATER OFOPERATIONS VIA SEA TRANSPORT AT 3346.8A/C HOURS (XC8756)

12-Jun-2004 1

MADISON WI 53714

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF#2 WIARNG/1-147TH AVN BN

UH-60-06-ASAM-04 CABS ECSU DRAIN PLUGSN/A THIS ACFT CABS NOT INSTALLED(XM0958)

26-Jun-2006 1

MADISON WI

QC000000


H-60-08-ASAM-01 TROOP/GUNNBER SEATUPPER ENERGY ATTENUATING WIRES INSPCOMPLIED WITH AT 4104.2 ACFT HRS ON 19AUG 08 (XO8975)

10-Aug-2008 1


QC000000


H-60-09-SOF-01 HYDRO-MECHANICAL UNIT(HMU) INSPECTION COMPLIED WITH.

21-Oct-2008 1


TW823045




8.7.DATE

6.REMARKS

4. 5.



AASF#2, OHARNGLEFT SIDE BEADED PANEL REPAIRED IAWMEC F112519.

29-Jul-2010 2

COLUMBUS, OH 43217

GG540327

AASF#2, OHARNGAirworthiness Release (AWR) for Use of ForestPenetrator (NSN 4240-00-199-7353, P/N K26-1000-9), Forest Penetrator (NSN 4240-01-500-8115, P/N K26-1000-105), Survivor’s Sling,SKED Rescue Systems, Rescue Net, RescueStrop, and Rescue Seat with UH/HH-60A/L/MHelicopters Equipped with a Rescue Hoist(AWR 980R8 16DEC11)

16-Dec-2011 1

COLUMBUS, OH 43217

GG540327




8.7.DATE

6.REMARKS

4. 5.



AASF#2, WIARNGH-60-08-ASAM-12 INSPECTION OF PARKERAEROSPACE AIR TURBINE STARTERINSTALLATION C/W

21-Oct-2008 2


RC728756




8.7.DATE

6.REMARKS

4. 5.



AASF#2, WIARNG1/147TH AVIATION

UH-60-02-ASAM-09 INSP T/R QUADRANT FORCORRECT HARDWARE C/W (XC8756)

28-Jun-2002 1

MADISON, WI 53704

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF#2,WIARING1/147TH AVIATION

UH-60-02-ASAM-08 INSPECT AN/ARC-220WIRING FOR CHAFING (XC8756)

25-Jun-2002 1

MADISON WI 53704

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF#2/1-147THAVIATION BN, WIARNG

S.E.I. BAMBI BUCKET (AWR DTD 08 SEP 05)NO LONGER USED FOR MISSIONS ORTRAINING DUE TO CLIMACTIC CONDITIONS(XL5732)

08-Dec-2005 1


QC000000

AASF#2/1-147THAVIATION BN, WIARNG

UH-60-06-SOF-02 DISABLING OF COCKPITAIRBAG SYSTEM COMPLIED WITH AT 3707.8AIRCRAFT HOURS (XL5732)

27-Jun-2006 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF#2/1-147TH AVNACFT RETURNED TO HOME STATION AFTERSEA TRANSPORT TO JACKSONVILLE, FL AT3595.1 AIRCRAFT HOURS. (XL5732)

03-Dec-2005 1


QC000000

AASF#2/1-147TH AVNUH-60-05-ASAM-11 WIRE HARNESS CHAFINGINSPECTION COMPLIED WITH AT 3606.5AIRCRAFT HOURS. (XL5732)

20-Dec-2005 1

MADISON, WI

QC000000

AASF#2/1-147TH AVNH-60-08-ASAM-06 MAIN ROTOR PYLONSLIDING FORWARD FAIRING COMPLIED WITH(XL5732)

03-Mar-2008 1


QC000000

AASF#2/1-147TH AVNH-60-08-AMAM-07 AN/ASN-128/D/B DOPPLERGPS NAVIGATION SET INSP COMPLIED WITH(XL5732)

03-Apr-2008 1


QC000000

AASF#2/1-147TH AVNH-60-08-AMAM-08 FLIGHT CONTROL RIGGINGUPDATE C/W (XD2386)

18-Jun-2008 1


QC000000

AASF#2/1-147TH AVNH-60-08-ASAM-12 PARKER AEROSPACE AIRTURBINE INSPECTION COMPLIED WITH

16-Sep-2008 1


DL785732

AASF#2/1-147TH AVNH-60-08-ASAM-12 PARKER AEROSPACE AIRTURBINE INSPECTION COMPLIED WITH

18-Sep-2008 1


DL785732

AASF#2/1-147TH AVNH-60-09-SOF-02 (AN/ALQ-144 IRCMS)COMPLIED WITH

10-Nov-2008 1


DL785732

AASF#2/1-147TH AVNH-60-09-SOF-03 POSSIBLE RETIREMENT LIFEOVER-FLIGHT, COMPLIED WITH

20-Nov-2008 1


MO668975

AASF#2/1-147TH AVNH-60-08-ASAM-10 ELECTRICAL WIRE CHAFFISSUES COMPLIED WITH

02-Jan-2009 1


DL785732

AASF#2/1-147TH AVNH-60-09-ASAM-05 (T/R SPRING CAPSULE LIFELIMITS) COMPLIED WITH

03-Mar-2009 1


DL785732




8.7.DATE

6.REMARKS

4. 5.



AASF#2/1-147TH AVNH-60-08-ASAM-11 FLIGHT CONTROLINSPECTION COMPLIED WITH (XL5732)

11-Sep-2008 1


QC000000

AASF#2/1-147TH AVNALQ-144 WITH FILTER MOD INSTALLED IAWAWR 1159 DATED 06AUG08 (XL5732)

24-Sep-2008 3


QC000000

AASF#2/1-147TH AVNAWR 1372 R1 TFM-138B INSTALLATION DATED25JUN08 SUPERCEDED AWR 913 DATED01AUG03 (XL5732)

24-Sep-2008 2


QC000000

AASF#2/1-147TH AVNAWR 1372 R 1 WIRELESS INTERCOM DATED30JUN08 SUPERCEDES AWR 1379 DATED07SEP06 (XL5732)

24-Sep-2008 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF#2/1-147TH AVN,WIARNG

UH-60-05-ASAM-07 AIR INTRUSION OFHYDRAULIC SYSTEM AND BLEEDING OF SASACTUATORS C/W AT 3485 ACFT HRS.(XK1861)

11-Jun-2005 2


QC000000


UH-60-06-ASAM-01 TAIL LANDING GEARSHOCK STRUT C/W AT 3652.7 AIRCRAFTHOURS (XL5732)

28-Mar-2006 1


QC000000


S.E.I. BAMBI BUCKET TEMPORARILYINSTALLED IAW AWR 1054 DATED 22 SEP 05,EMC PREVIOUSLY COMPLETED WITHAIRCRAFT 7923269 ON 09 APR 2003 (XL5732)

28-Apr-2006 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF-1 FTIGH-60-14-AMAM-19 ULLS-A(E) LEGITIMATECODE CHANGE 66 REQUIREMENTS COMPLIEDWITH

30-Nov-2014 1


AT562754

AASF-1 FTIGH-60-15-ASAM-01 LIGHT EMITTING DIODE(LED) CAUTION ADVISORY PANEL (CAP)COMPLIED WITH.

04-Dec-2014 1


AT562754




8.7.DATE

6.REMARKS

4. 5.



AATDEMC TEST FOR DUST-OFF LANDING SYSTEMCOMPLETED ON THIS DATE IAW AWR DATED10 AUG 2004. (JD9989)

12-Aug-2004 1

FT EUSTIS, VA 23604

QC000000




8.7.DATE

6.REMARKS

4. 5.



BHMODDYNAELECTRON CORP

MOD WI029 UPDATE TO ADD CAPS TO XMSNBARREL NUT HOLES COMPLETED (NO PID)

26-Jul-1983 16

FTCKY

QC000000


MOD WI028 UPDATE TO ADD SECOND DRAINLINE TO NOSE DOOR COMPLETED. (NO PID)

26-Jul-1983 15

FTCKY

QC000000


MOD WI027 UPDATE TO IMPROVE DRAINAGEIN NOSE TUB AREA COMPLETED. (NO PID)

26-Jul-1983 14

FTCKY

QC000000


MOD WI026 UPDATE TO ADD TUBES AT XMSNAREA AROUND T/R CABLES COMPLETED.(NO PID)

26-Jul-1983 13

FTCKY

QC000000


MOD WI025 UPDATE TO DRILL HOLES GLIDESLOPE REAR ATTACHMENT COMPLETED.(NO PID)

26-Jul-1983 12

FTCKY

QC000000


MOD WI024 UPDATE OF 16 HOLES IN LOWERTUB AT CARGO HOOK REAR COMPLETED.(NO PID)

26-Jul-1983 11

FTCKY

QC000000


MOD WI023 UPDATE OF SEAL OVERHEADINSIDE CABIN COMPLETED. (NO PID)

26-Jul-1983 10

FTCKY

QC000000


MOD WI022 UPDATE OF SEAL UPPER DECKMATING SURFACES COMPLETED. (NO PID)

26-Jul-1983 9

FTCKY

QC000000


MOD WI021 UPDATE OF NAS1598D3Y WASHERAT ELECTRICAL WIRES TOP DECKCOMPLETED. (NO PID)

26-Jul-1983 8

FTCKY

QC000000


MOD WI016 UPDATE OF SEAL THICKNESS ONCARGO DOOR LEADING EDGE COMPLETED.(NO PID)

26-Jul-1983 7

FTCKY

QC000000


MOD WI 013 UPDATE OF LEFT AND RIGHTGUNNERS WINDOW FORWQARD AIRF. SEALCOMPLETED. (NO PID)

26-Jul-1983 6

FTCKY

QC000000


MOD WI012 UPDATE OF LEFT AND RIGHTGUNNERS WINDOW SEAL COMPLETED. (NOPID)

26-Jul-1983 5

FTCKY

QC000000


MOD WI009 UPDATE OF SEALANT ON FUELLINE SWIVELS COMPLETD. (NO PID)

26-Jul-1983 4

FTCKY

QC000000


MOD WI007 UPDATE TO REPLACE CHINESEHAT FWD TOP DECK COMPLETED. (NO PID)

26-Jul-1983 3

FTCKY

QC000000


MOD WI002 UPDATE OF NAS1598D3Y SEALWASHER SCREW DOOR WINDOWCOMPLETED. (NO PID)

26-Jul-1983 2

FTCKY

QC000000




8.7.DATE

6.REMARKS

4. 5.




MOD WI001 UPDATE OF SEALANT CREWDOOR WINDOW DOUBLER COMPLETED. (NOPID)

26-Jul-1983 1

FTCKY

QC000000


OCM/ACE PERFORMED AT 0196 A/C HOURSAT FT CAMPBELL, KY BY ACE TEAM MEMBER,TSARCOM OCM SEC ST LOUIS MO. (NO PID)

24-Aug-1983 1

FTCKY

QC000000




8.7.DATE

6.REMARKS

4. 5.



CCADUH-60-94-ASAM-09 TB 1-1520-237-20-155REMOVAL OF CERTAIN PRIMARY SERVOASSEMBLIES C/W (JG0000)

16-Aug-1994 76

CORPC, TX

QC000000

CCADUH-60-94-ASAM-07/08 TB 1-1520-237-20-154CHANGE TO UH-60 OVERHAUL & RETIREMENTLIFE TABLE C/W (JG0000)

16-Aug-1994 75

CORPC, TX

QC000000

CCADUH-60-94-ASAM-06 TB 1-1520-237-20-150COCKPIT STANDARDIZATION OFPILOT/COPILOT RESTRAINT RELEASESYSTEM C/W (JG0000)

16-Aug-1994 74

CORPC, TX

QC000000

CCADUH-60-94-ASAM-05 TB 1-1520-237-20-152 ONETIME REMOVAL OF T/R GEARBOX WITHOUTPUT SHAFT PN:70358-06620-101 C/W(JG0000)

16-Aug-1994 73

CORPC, TX

QC000000

CCADUH-60-94-ASAM-04/TB 1-1520-237-20-153REISSUE OF ONE TIME INSPECTION TOREMOVE SUSPECT T/R PITCH BEAMS C/W(JG0000)

16-Aug-1994 72

CORPC, TX

QC000000

CCADTB 1-1520-237-20-151 UH-60-94-ASAM-03/10ONE TIME OF M/R SPINDLE & REPLACEMENTOF CERTAIN M/R TRUST BEARING C/W(JG0000)

16-Aug-1994 71

CORPC, TX

QC000000

CCADTB 1-1520-237-20-149 UH-60-94-ASAM-02RETURN FOR EXCHANGE CERTAIN (ARN) MFGBUCKLE/CROTCH STRAP ASSY PN:04495-28(JG0000)

16-Aug-1994 70

CORPC, TX

QC000000

CCADTB 1-1520-237-20-139 UH-60-94-ASAM-01REWORK OF NIGHT VISION GOGGLE MASTERWARNING PANEL (JG0000)

16-Aug-1994 69

CORPC, TX

QC000000

CCADTB 1-1520-237-20-146 UH-60-93-ASAM-16 ONETIME INSP OF HYDRAULIC PUMP MODKNURLED BLEED/RELIEF KNOB SECURINGPIN C/W (JG0000)

16-Aug-1994 68

CORPC, TX

QC000000

CCADTB 1-1520-237-20-142 UH-60-93-ASAM-11 INSP& REPL ARA CREW RESTRAINTBUCKLE/CROTCH ASSY C/W (JG0000)

16-Aug-1994 67

CORPC, TX

QC000000

CCADTB 1-2840-248-20-1 UH-60-93-01/02 ONE TIMEINSP-TION OF T700-GE-701C MAIN FUELHOSE, N/A THIS ENGINE (JG0000)

16-Aug-1994 66

CORPC, TX

QC000000

CCADTB 1-1520-237-20-141 UH-60-93-ASAM-10 ONETIME & RECURRING INSP/CLEANING OF ESSSVALVES & PNEUMATIC LINES N/A EQUIPMENTNOT INSTALLED ON ACFT (JG0000)

16-Aug-1994 65

CORPC, TX

QC000000

CCADTB 1-1520-237-20-140 UH-60-93-ASAM-09 ONETIME INSP TO DETERMINE COMPLIANCE WITHSYSTEM MWO'S C/W (JG0000)

16-Aug-1994 64

CORPC, TX

QC000000

CCADTB 1-1520-237-20-138 UH-60-93-ASAM-08USING CORRECT T/R RIGGING PROCEDURESON ALL H-60'S ACFT C/W (JG0000)

16-Aug-1994 63

CORPC, TX

QC000000

CCADTB 1-1520-237-20-136 UH-60-93-ASAM-06 ONETIME INSP TO REMOVE SUSPECT TAIL ROTORPITCH BEAMS C/W (JG0000)

16-Aug-1994 62

CORPC, TX

QC000000




8.7.DATE

6.REMARKS

4. 5.



CCADTB 1-1520-237-20-150 UH-60-93-ASAM-03REVISION TO M/R BLADE EXPANDABLE PINSC/W (JG0000)

16-Aug-1994 61

CORPC, TX

QC000000

CCADTB 1-1520-237-20-135 UH-60-93-ASAM-01 ONETIME OPERATIONAL CHECK OF THETRANSMISSION & GEARBOX CHIP DETECTORSYSTEM C/W (JG0000)

16-Aug-1994 60

CORPC, TX

QC000000

CCADTB 1-1520-237-20-134 UH-60-93-ASAM-04/UH-60-92-ASAM-06 INSPECTION FOR IMPROPERHARDWARE ON THE PEDAL ADJUSTER ASSYP/N 70400-01613 C/W (JG0000)

16-Aug-1994 59

CORPC, TX

QC000000

CCADTB 1-1520-237-20-130 UH-60-92-ASAM-05 INSPOF M/R BLADE EXPANDABLE PIN C/W(JG0000)

16-Aug-1994 58

CORPC, TX

QC000000

CCADTB 1-1520-237-20-128 DISCONNECTION OFTHE PITCH BIAS ACTUATOR C/W (JG0000)

16-Aug-1994 57

CORPC, TX

QC000000

CCADUH-60-92-ASAM-02 TB 1-1520-237-20-132 ONETIME INSP FOR ENGINE OUTPUT SHAFT BOLTTORQUE AND VIBRATION LEVEL C/W(JG0000)

16-Aug-1994 56

CORPC, TX

QC000000

CCADGEN-92-ASAM-07 USE OF DISCREPANT LOTSOF SYN-TECH GREASE PN:3913-G1, NSN:9150-00-505-8497 SUBJECT GREASE NOTINSTALLED (JG0000)

16-Aug-1994 55

CORPC, TX

QC000000

CCADTB 55-1520-237-20-129 UH-60-92-ASAM-01 INSPFOR THREE (3) UNSERVICEABLE SPINDLEASSEMBLIES C/W (JG0000)

16-Aug-1994 54

CORPC, TX

QC000000

CCADTB 55-1520-237-20-127 UH-60-91-ASAM-10 ONETIME INSP & REPLACEMENT OF MAINLANDING GEAR, BRAKE ASSY PISTONINSULATOR C/W (JG0000)

16-Aug-1994 53

CORPC, TX

QC000000

CCADTB 55-1520-237-20-126 UH-60-91-ASAM-09CHANGES TO INSP PROCEDURES FOR M/RELASTOMERIC BEARINGS C/W (JG0000)

16-Aug-1994 52

CORPC, TX

QC000000

CCADTB 55-1520-237-20-119 UH-60-91-ASAM-01ONE TIME REPLACEMENT AND 30 HR INSP OFT/R PITCH BEAM RETAINING WASHER C/W(JG0000)

16-Aug-1994 51

CORPC, TX

QC000000

CCADTB 55-1520-237-20-118 UH-60-90-02 ONE TIME& RECURRING INSP OF T/R PITCH BEAMRETAINING WASHER & PITCH BEAMRETAINING NUT C/W (JG0000)

16-Aug-1994 50

CORPC, TX

QC000000

CCADTB 55-1520-237-20-117 ONE TIME INSP OFMAIN ROTOR PITCH CONTROL HORNS C/W(JG0000)

16-Aug-1994 49

CORPC, TX

QC000000

CCADTB 55-1520-237-20-115 SOF UH-60-90-01 ONETIME & RECURRING INSP OF MAIN ROTORBLADE EXPANDABLE PINS C/W (JG0000)

16-Aug-1994 48

CORPC, TX

QC000000

CCADTB 55-1520-237-20-113 INSP FOR DEFECTIVEROSEMOUNT RATE INDICATORS C/W(JG0000)

16-Aug-1994 47

CORPC, TX

QC000000




8.7.DATE

6.REMARKS

4. 5.



CCADTB 55-1520-237-20-111 ONE TIME INSP OFUPPER PRESSURE PLATE & SPINDLE TO HUBATTACHMENT BOLTS C/W (JG0000)

16-Aug-1994 46

CORPC, TX

QC000000

CCADTB 55-1520-237-20-112 SOF UH-60-89-13RESTRICTIONS AGAINST USING ASSEMBLYPN:70700-20433-045 FOR RAPPELLINGPARACHUTING AND TRANSPORTABILITY TIEDOWN OPERATION C/W (JG0000)

16-Aug-1994 45

CORPC, TX

QC000000

CCADTB 55-1520-237-20-109 SOF UH-60-89-11 ONETIME INSP OF OIL COOLER AXIAL FAN C/W(JG0000)

16-Aug-1994 44

CORPC, TX

QC000000

CCADTB 55-1520-237-20-110 SOF UH-60-89-12 ONETIME INSP OF OIL COOLER AXIAL FAN SHAFTC/W (JG0000)

16-Aug-1994 43

CORPC, TX

QC000000

CCADTB 55-1520-237-20-104 SOF UH-60-89-09CORRECTION OF RETIREMENT LIFESCHEDULE FOR UH-60 RETIREMENT LIFECOMPONENTS C/W (JG0000)

16-Aug-1994 42

CORPC, TX

QC000000

CCADTB 55-1520-237-20-108 SOF UH-60-89-08 ONETIME INSP OF FUEL BOOST PUMP HOSEATTACHMENT C/W (JG0000)

16-Aug-1994 41

CORPC, TX

QC000000

CCADTB 55-1520-237-20-107 SOF UH-60-89-06-07ONE TIME INSP OF RIGHT AND LEFT HANDRELAY PANEL ASSEMBLIES FOR SUSPECTGROUNDING MODULES C/W (JG0000)

16-Aug-1994 40

CORPC, TX

QC000000

CCADTB 55-1520-237-20-106 SOF UH-60-60-89-05ONE TIME INSP OF WIRE STRIKE PROTECTIONSYSTEM, C/W (JG0000)

16-Aug-1994 39

CORPC, TX

QC000000

CCADTB 55-1520-237-20-105 SOF UH-60-89-03/04ONE TIME INSP OF ALL MAIN ROTORSPINDLES, ALL PART NUMBERS C/W (JG0000)

16-Aug-1994 38

CORPC, TX

QC000000

CCADSOF UH-60-89-01 TB 55-2840-50-58 ONE TIMEINSP OF T700-GE-700 ENGINE GASGENERATOR STATOR SHROUDS C/W(JG0000)

16-Aug-1994 37

CORPC, TX

QC000000

CCADSOF GEN-88-03 TB 1-1500-200-20-26 ONE TIMEINSP FOR CORRECT INTERNAL FIREEXTINGUISHER HALON CF3BR NSN:4210-00-555-8837 OR REPLACEMENT BOTTLENSN:4210-00-708-0031 C/W (JG0000)

16-Aug-1994 36

CORPC, TX

QC000000

CCADSOF UH-60A-88-08 REVISION TO OVERHAULLIFE FOR THE XMSN OIL COOLER BLOWERC/W (JG0000)

16-Aug-1994 35

CORPC, TX

QC000000

CCADSOF UH-60A-88-09 TB55-1520-237-20-200 ONETIME INSPECTION OF ARA MANUFACTUREDCREW SEATS FOR LOOSE CLEVIS SCREWSC/W (JG0000)

16-Aug-1994 34

CORPC, TX

QC000000

CCADSOF UH-60A-88-07 REVISIONS TO SOF UH-60-88-05 CONCERNING OPERATING TIME, STARTCALCULATIONS AND FORMS INFORMATIONC/W (JG0000)

16-Aug-1994 33

CORPC, TX

QC000000

CCADSOF UH-60A-88-03 TB 55-1520-237-20-97 LIFEEXTENS OF H60 ACFT MAIN MODUAL SHAFTC/W (JG0000)

16-Aug-1994 31

CORPC, TX

QC000000




8.7.DATE

6.REMARKS

4. 5.



CCADTB 55-1520-237-20-93 ONE TIME ANDRECURRING INSP OF ENGINE COWLINGS C/W(JG0000)

16-Aug-1994 30

CORPC, TX

QC000000

CCADTB 5-1520-237-20-86 REMOVAL OF PITCH BIASACTUATOR C/W (JG0000)

16-Aug-1994 29

CORPC, TX

QC000000

CCADTB 5-1520-237-50-2 (UH-60-87-06) ONE TIME &RECUR INSP OF OIL COOLER SPLINES ANDINSTALLATION OF SPLINE WEAR INDICATORSYSTEM C/W (JG0000)

16-Aug-1994 28

CORPC, TX

QC000000

CCADSOF MSG 112000Z APR 87 (UH-60-87-05)STABILATOR OPERATIONAL PROCEDURESN/A THIS ACFT (JG0000)

16-Aug-1994 27

CORPC, TX

QC000000

CCADSOF MSG 182220Z FEB 87 (UH-60A-87-02) TOCORRECT (TB) NUMBER CITED IN SOF MSGUH-60A-87-01 FROM 50-43 TO 50-44 C/W(JG0000)

16-Aug-1994 26

CORPC, TX

QC000000

CCADTB 55-2840-248-50-44 (SOF UH-60A-87-01) ONETIME TORQUE OF THE T700 ENGINE FUELDIFFERENTIAL PRESS INDICATOR C/W(JG0000)

16-Aug-1994 25

CORPC, TX

QC000000

CCADTB 55-1520-237-20-83 REPETITIVE INSPECTIONOF UH-60A/EH-60A/EH-60-A, EYEBOLTS PN:70209-02136-102. NSN: 5306-01-102-8797 C/W(JG0000)

16-Aug-1994 24

CORPC, TX

QC000000

CCADTB 55-1520-237-20-83 SOF UH-60-86-19REPETITIVE INSP OF UH-60 EYEBOLTSPN:70209-02136-102 NSN:5306-01-102-8797 C/W(JG0000)

16-Aug-1994 23

CORPC, TX

QC000000

CCADSOF UH-60-86-18 IMMEDIATE RESTRICTION OFRAPPELING OPERATIONS C/W (JG0000)

16-Aug-1994 22

CORPC, TX

QC000000

CCADTB55-1520-23-20-82 CONTRACTORINSPECTION OF TRANSMISSION OIL COOLERFAN SPLINES AND TAIL ROTOR DRIVESHAFTC/W (JG0000)

16-Aug-1994 21

CORPC, TX

QC000000

CCADSOF UH-60-86-16 UH-60A BLACKHAWK ACFTLEVER ASSY PN: 70400-02623-041, NSN:1560-01-083-6799 C/W (JG0000)

16-Aug-1994 20

CORPC, TX

QC000000

CCADSOF UH-60-86-15 (REV UH-60-86-13) REVISIONTO REMOVAL OF 310-8 NUTS, NSN:5310-00-167-1289 C/W (JG0000)

16-Aug-1994 19

CORPC, TX

QC000000

CCADSOF UH-60-86-04 (TB55-1520-237-23-1)REVISION TO REPLACEMENT OF TAIL ROTORDRIVESHAFT BEARINGS, PN: SB1138-101 C/W(JG0000)

16-Aug-1994 18

CORPC, TX

QC000000

CCADSOF UH-60-85-21 MAIN ROTOR SPINDLE ANDTIE ROD RETIREMENT LIFE CHANGE (JG0000)

16-Aug-1994 17

CORPC, TX

QC000000

CCADSOF UH-60-85-12 ONE TIME AND REPETITIVEINSP OF THE TURBINE ON THE T700-GE-700ENGINES PCW (JG0000)

16-Aug-1994 16

CORPC, TX

QC000000




8.7.DATE

6.REMARKS

4. 5.



CCADSOF UH-60-84-16 T 700-GE-700 ENGINESREMOVAL AND REPLACEMENT OF GASGENERATOR (GG) ROTOR AT CERTAIN LIFELIMITS C/W (JG0000)

16-Aug-1994 15

CORPC, TX

QC000000

CCADSOF UH-60-84-13 TB 55-1520-237-20-57 ONETIME INSP AND REPLACEMENT OF TAILROTOR CONTROL CABLE BRASS TURNBUCKLES C/W (JG0000)

16-Aug-1994 14

CORPC, TX

QC000000

CCADSOF UH-60-88-13 (TB 55-1520-237-20-102) ONETIME INSP OF THE M/R BLADE EXPANDABLERETENTION PIN PN: 70103-08107-101 FORMISSING SEGMENTS C/W (JG0000)

16-Aug-1994 13

CORPC, TX

QC000000

CCADTB 55-1520-237-50-2 ONE TIME ANDRECURRING INSP OF OIL COOLER SPLINESAND INSTALLATION OF SPLINE WEARINDICATOR SYSTEM C/W (JG0000)

16-Aug-1994 12

CORPC, TX

QC000000

CCADTB 55-1520-237-30-1 ONE TIME INSPECTION OFINLET DUCT ASSY PN: 70303-10100 ANDALIGNMENT PIN BRACKT PN:70209-04301-044/045 C/W (JG0000)

16-Aug-1994 11

CORPC, TX

QC000000

CCADTB 55-1520-237-20-77 (SOF UH-60-86-08)REPLACEMENT OF STABILATOR ACTUATORSPN:70400-06641-110 NSN: 1680-01-115-9530P/C/W (JG0000)

16-Aug-1994 10

CORPC, TX

QC000000

CCADTB 55-1520-237-20-63 INSPECTION OF FLIGHTCONTROLS C/W (JG0000)

16-Aug-1994 9

CORPC, TX

QC000000

CCADTB 55-1520-237-20-60 (SOF UH-60-85-03/04)ONE TIME INSPECTION AND REPLACEMENTOF STAB AMPLIFIER PN: 70902-0200-044/045(JG0000)

16-Aug-1994 8

CORPC, TX

QC000000

CCADTB 55-1520-237-20-39 ONE TIME INSPECTIONOF APU COMPRESSOR BLADES C/W (JG0000)

16-Aug-1994 7

CORPC, TX

QC000000

CCADTB 55-1520-237-20-35 ONE TIME INSPECTIONOF YAW TRIM AND ROLL TRIM SERVOS FORIMPROVED SEAL P/C/W (JG0000)

16-Aug-1994 6

CORPC, TX

QC000000

CCADTB 55-1520-237-20-32 ONE TIME INSPECTIONOF MAIN ROTOR SERVO SCREWS C/W(JG0000)

16-Aug-1994 5

CORPC, TX

QC000000

CCADACFT SIX MONTHS FILE WILL BE RETAINEDAT CCAD, IAW TDS # AGEN-X0363 CH 1 DTD 13JAN 84 (JG0000)

16-Aug-1994 4

CORPC, TX

QC000000

CCADACFT EXTERIOR PAINTED WITH LOWREFLECTIVE POLYURETHANE ACFT GREEN,MIL-C-46168 IAW TM 55-1500-345-23 DTD 12JUN 86 AND ECP #0245 (JG0000)

16-Aug-1994 3

CORPC, TX

QC000000

CCADNEXT PMS II DUE AT 1965.9 ACFT HRS(JG0000)

16-Aug-1994 2

CORPC, TX

QC000000

CCADACFT COMPLETEDREFURBISHMENT/STANDARDIZATIONPROGRAM 16 AUG 93 WHICH INCLUDED MWO1-1520-237-55/7 (JG0000)

16-Aug-1994 1

CORPC, TX

QC000000




8.7.DATE

6.REMARKS

4. 5.



CO D, 1-147TH AVN BN,WIARNG

A/C DEPLOYED TO SOUTHWEST ASIATHEATER OF OPERATIONS VIA SEATRANSPORT AT 3105.9 A/C HRS (XC8756)

10-Apr-2003 1

CAMP UDAIRI KUWAITAPO AE09330

QC000000




8.7.DATE

6.REMARKS

4. 5.



CSC RASM-EOCM/ACE PERFORMED AT 4428 ACFT HRS BYTEAM MEMBERS J&DD AMCOM/AFMA

21-Sep-2009 1

FT CAMPBELL KY

JB709001




8.7.DATE

6.REMARKS

4. 5.



CSC RASM-E, FT.CAMPBELL, KY

OCM/ACE PERFORMED AT 4613.1 ACFT HRSBY TEAM MEMBER UU AND QQ

17-Sep-2010 1

COLUMBUS, OH 43217

HM009565




8.7.DATE

6.REMARKS

4. 5.



D CO 1/147TH AV BNMAIN MOD IMPENDING BYPASS BUTTONPOPPED 3909.2 ACFT HRS REPLACED 1STAND 2ND STAGE FILTERS (CA4792)

23-Feb-2007 1

CAMP BONDSTEELKOSOVO

QC000000




8.7.DATE

6.REMARKS

4. 5.



D CO 1/147TH AVN BNH-60 SERIES AIRCRAFT, ARC-220/KY-100START-UP PROCEDURES, UH-60-07-ASAM-05,COMPLIED WITH (WH1187)

25-Jan-2007 1


QC000000

D CO 1/147TH AVN BNISAQ 110 DTD 06FEB04 OPTION II MAVENHEATER HAS BEEN REVISED TO 30MAR06(R2)(WH1187)

11-Apr-2007 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



D CO 1/147TH AVN BNT/F EAGLE

ALL UH/HH-60A/L/M SERIES AIRCRAFT,COMMON MISSILE WARNING SYSTEM (CMWS)UH-60-07-AMAM-01 C/W 28 MAR 07 AT 3918.6A/C HRS, NOT INSTALLED THIS AIRCRAFT(WH1187)

28-Mar-2007 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



D CO 1/147TH AVN BNTF EAGLE

AIWORTHINESS RELEASE (AWR) FOROPERATION OF UH-60A/L HELICOPTERS WITHTHE M-240H MACHINE GUN INSTALLED (AWR1120) DATED 22 SEP 06 (R3) (WH1187)

26-Apr-2007 1


QC000000


ALL UH-60A/L SERIES AIRCRAFT,INSTALLATION OF STATIC BONDINGJUMPERS, UH-60-07-ASAM-07 COMPLIED WITHTHIS DATE AT 3963.8 ACFT HRS, N/A THISACFT (WH1187)

08-May-2007 1

CAMP BONDSTEEL,KOSOVO

QC000000


AMCOM UH-60-07-ASAM-09, ALL UH/HH60LAIRCRAFT, DEFECTIVE DIGITAL ENGINECONTROL UNITS (DECU) COMPLIED WITH AT4071.7 ACFT HRS. N/A THIS ACFT (WH1187)

24-Jul-2007 1

CAMP BONDSTEEL

QC000000


ISAQ 105 HF RADIO HAS BEENINCORPORTATED INTO TM 1-1520-237-10CHANGE 1 DTD 21MAR07 (WH1187)

12-Aug-2007 3


QC000000


AWR 1189 ELT DATED 14JUN04 HAS BEENREVISED WITH DATE OF 26MAR07 R-3(WH1187)

12-Aug-2007 2


QC000000


AIRWORTHINESS RELEASE (AWR) FOROPERATION OF UH-60A/L HELICOPTERS WITHTHE M-240H MACHINE GUN INSTALLED (AWR1120) DATED 22 SEP 06 (R3), HAS BEENREVISED WITH DATE OF 03AUG07 R-4(WH1187)

12-Aug-2007 1


QC000000


UH-60-07-ASAM-10 ALL H-60 SERIESAIRCRAFT, ONE TIME VISUAL INSPECTIONFOR EVIDENCE OF FUEL MANIFOLD CHAFINGON THE ENGINE DIFFUSER FLANGE ANDINSTALLATION OF FUEL MANIFOLD SUPPLYLINE STANDOFF BRACKET. COMPLIED WITHTHIS DATE AT 4100.3 ACFT HRS. (WH1187)

16-Aug-2007 1


QC000000


M/R RIG COMPL DURING PMIYELLOWINITIAL=4.900 BIAS=5.190 DIFF=.290REDINITIAL=4.835 BIAS=5.115 DIFF=.280BLACKINITIAL=4.220 BIAS=4.510 DIFF=.290BLUEINITIAL=4.190 BIAS=4.470 DIFF=.290T/RTENSION = L/H-143, R/H 141, TEMP 22 DEG C(WH1187)

11-Sep-2007 1


QC000000


T/R BIAS COMPLETED FOR INBOARDRETENTION PLATE RETORQUE. COMPLETEDAT 4109.5 ACFT HRSYELLOW INITIAL=4.752BIAS=5.049 DIFF=.297RED INITIAL=4.744BIAS=5.079 DIFF=.335BLACK INITIAL=4.080BIAS=4.409 DIFF=.329BLUE INITIAL=4.040BIAS=4.369 DIFF=.329 (WH1187)

09-Oct-2007 1


QC000000


H-60-08-ASAM-01, MAIN LANDING GEARSHOCK STRUTS, INSPECTION FOR LEAKSAND PROPER VISUAL SERVICING DIMENSION.2408-18 INSPECTION INITIATED AS A806.COMPLIED WITH THIS DATE AT 4118.3 ACFTHRS (WH1187)

16-Oct-2007 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



D CO 1/147TH AVNTASK FORCE EAGLE

ALL UH-60A/L AIRCRAFT, INTERNAL RESCUEHOIST CABLE (GUARD) DEFLECTOR, UH-60-07-ASAM-06 (WH1187)

07-Feb-2007 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



D CO 1/147TH TASKFORCE EAGLE

ALL H-60 AIRCRAFT, REQUIRED HMU PARTNUMBER AND SERIAL NUMBER CHECK IAWUH-60-07-ASAM-08 COMPLIED WITH AT4065.3ACFT HRS (CA4792)

18-Jul-2007 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



D CO 1-147TH AVN BNE/H/UH-60A/L SERIES AIRCRAFT,AUTOROTATIONAL RPM CHARTS, UH-60-07-ASAM-04, MTF COMPLETED AT 3841.2 ACFTHRS 29DEC06 NO ADJUSTMENT REQUIRED(WH1187)

29-Dec-2006 2


QC000000




8.7.DATE

6.REMARKS

4. 5.



D CO 1-147TH AVN BN,WIARNG

SOF UH-60-04-01 ONE TIME INSPECTION OFFORWARD BELLCRANK SUPPORTINSTALLATION HARDWARE. C/W (XK1861)

03-Oct-2003 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



D CO 326 MED BNSOF UH-60-87-03 INSPECTION OF THE FIRSTTHREE T/R D/S COUPLINGS AND THE AREAUNDER THE SEATS TO BE DONE EVERY 10HRS/14 DAYS C/W R. BANVILLE SGT TI CO D326 MED BN, FT. CAMPBELL, KY (RB0000)

13-Mar-1987 1

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNSOF UH-60-87-04 REVISION TO INSPECTIONOF EYEBOLT PN: 70209-02136-102 C/W. SGT TID/326 MED BN, FT. CAMPBELL, KY (AA1889)

26-Mar-1987 1

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNSOF UH-60-87-06 REVISION OF OIL COOLERINSPECTION C/W IPS READINGS ON OILCOOLER, LONGTITUDINAL .8 AXIS ANDVERTICAL .2 AXIS IPS M. ABAC SSG TI D CO326 MED BN, FT. CAMPBELL, KY (MA0000)

08-May-1987 1

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNSOF UH-60-87-07 ONE TIME AND RECURRINGINSPECTIONS OF TWO LONGITUDINAL LINKASSY AND ONE LATERAL CLEVIS ASSY FORCRACKED INNER RACE, C/W R. BANVILL SGTTI CO D 326 MED BN, FT. CAMPBELL, KY(RB0000)

14-May-1987 1

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNSOF GEN 87-02 ONE TIME RECORDS CHECKFOR LOCALLY PROCURED TIME CHANGECOMPONENTS C/W R. BANVILLE D CO 326MED BN, FT. CAMPBELL, KY (RB0000)

30-Jun-1987 1

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNSOF UH-60-87-08 ONE TIME INSPECTION OFTHE CABIN MID SECTION BELL CRANKS C/WR. BANVILLE, SGT TI D CO 326 MED BN, FT.CAMPBELL, KY (RB0000)

01-Jul-1987 1

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNSOF UH-60-87-09 SDF UH-60-87-05 IS INEFFECT TILL SOF UH-60-87-09 IS C/W C/W R.BANVILLE, SGT TI D CO 326 MED BN, FT.CAMPBELL, KY (MM0000)

18-Aug-1987 1

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNSOF UH-60-87-10 ONE TIME INSPECTION OFTHE INPUT FLANGE ASSY FOR SN WG0001THRU WG0107 C/W R. BANVILLE, SGT. TI D CO326 MED BN FT. CAMPBELL, KY (RB0000)

13-Oct-1987 1

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNSOF UH-60-87-11 ONE TIME INSPECTION OFTROUP CARGO UPPER AND LOWER ROLLERASSEMBLIES FOR CRACKS C/W M.MORRISON, SGT. TI, D CO 326 MED BN FT.CAMPBELL KY (MM0000)

04-Nov-1987 1

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNSOF UH-60-87-12 ONE TIME INSPECTION OFS/W OR THE POWER TURBINE MODULES C/WR. BANVILLE, SGT, TI D CO 326 MED BN FT.CAMPBELL, KY (RB0000)

03-Dec-1987 1

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNOCM/ACE PERFORMED AT 1295 ACFT HRS ATFT. CAMPBELL KY BY ACE TEAM MEMBER "P"AVSCOM OCMSEC, ST. LOUIS MO (AA1889)

09-Dec-1987 1

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNMIM UH-60-87-02 ONE TIME AND RECURRINGINSPECTION OF ENGINE COWLINGS C/WMICHAEL K. LANGSTON, SSG, TI D CO 326MED BN FT. CAMPBELL, KY (ML0000)

09-Feb-1988 1

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNSOF UH-60-88-01 ONE TIME INSPECTION FORCERTAIN SN TAIL ROTOR BLADE ASSY C/WMICHAEL K. LANGSTON, SSG TI D CO 326 MEDBN FT. CAMPBELL, KY (ML0000)

16-Feb-1988 1

FT. CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



D CO 326 MED BNSOF UH-60-88-05 TB 55-1520-237-20-98INITIATION OF APU MAOT OF APU OPERATINGHRS, 1000 AND APU STARTS 3000, C/W C.SWEENEY CW3 MO D CO 326 MED BN FT.CAMPBELL, KY (CS0000)

19-Mar-1988 1

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNSOF UH-60-88-03 TB 55-1520-237-20-97 LIFEEXTENSIO OF THE UH-60 ACFT MAIN MODULESHAFTS C/W M. LANGSTON, SSG, TI D CO 326MED BN FT. CAMPBELL, KY (ML0000)

22-Mar-1988 2

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNSOF UH-60-88-02 TB 55-1520-237-20-96 ONETIME INSP OF TAIL ROTOR GEARBOX OUTPUTSHAFT C/W M. LANGSTON SSG, TI D CO 326MED BN FT. CAMPBELL, KY (ML0000)

22-Mar-1988 1

FT. CAMPBELL, KY

QC000000

D CO 326 MED BNSOF UH-60-88-06 (TB 55-1520-237-20-99)OVERHAUL LIFE FOR XMSN OIL COOLERBLOWER C/W SSG D CO 326 MED BN, FT.RUCKER, AL (AA1889)

13-Jul-1988 1

FT. RUCKER, AL

QC000000




8.7.DATE

6.REMARKS

4. 5.



D CO 326TH MED BNSOF INSPECTION OF WIRE HARNESSROUTING FOR FEEDER HARNESS BETWEEN#1 AND #2 JUNCTION BOXES IAW TB 55-1520-23-20-48 UH-60-84-02 C/W SSG CAUDILL, TI COD 326TH MED BN FT. CAMPBELL, KY (FC0000)

16-Mar-1984 1

FT. CAMPBELL, KY

QC000000

D CO 326TH MED BNSOF ONE TIME INSPECTION TAIL ROTORPYLON COVER HINGE BRACKET P/N: 70201-06157-102 I/A/W TB 55-1520-237-20-49 UH-60-84-03 C/W SSG CAUDILL, TI CO D 326TH MED BNFT. CAMPBELL, KY (FC0000)

04-Apr-1984 1

FT. CAMPBELL, KY

QC000000

D CO 326TH MED BNSOF ONE TIME INSPECTION OF STABILATORAMPLIFIERS PN: 70902-02001-044/045 I/A/W TB55-1520-237-50-2 UH-60-84-04 C/W SSGCAUDILL D CO 326TH MED BN FT. CAMPBELL,KY (FC0000)

13-Apr-1984 1

FT. CAMPBELL, KY

QC000000

D CO 326TH MED BNSOF ONE TIME INSPECTION TAIL ROTORGEARBOX AND INTERMEDIATE GEARBOX OILLEVEL PN: 70358-06600-041/042/043 AND70357-06300-042 I/A/W TB 55-1520-237-20-52 UH-60-84-06 C/W G CAUDILL TI D CO 326 MED BNFT. CAMPBELL, KY (GC0000)

23-Apr-1984 2

FT. CAMPBELL, KY

QC000000

D CO 326TH MED BNSOF INSPECTION OF PITCH CONTROL ROTATTACHING BOLTS FOR SECURITY IAW UH-60-84-05 C/W G CAUDILL TI D CO 326 MED BN FT.CAMPBELL, KY (GC0000)

23-Apr-1984 1

FT. CAMPBELL, KY

QC000000

D CO 326TH MED BNSOF ENGINE OUTPU TSHAFT PN:70361-08004-042, NSN: 2835-01-93-4763 AND PN:70361-08004-043 NSN:2835-01-123-7648 VISUALLYINSPECT COUPLING BOLTS TO ENSURE THEYARE MS-9724-0 INSP 17 MAY 84 MS-9724-08-07BOLTS INSTALLED I/A/W TB 55-1520-23-20-53UH-60-84-07 C/W SGT D WATER TI D CO 326MED BN FT. CAMPBELL, KY (DW0000)

10-May-1984 1

FT. CAMPBELL, KY

QC000000

D CO 326TH MED BNSOF ONE TIME INSP OF AEROQUIP CARGOHOOK PRESSURE CARTRIDGE ASSY PN: 7590-65 I/A/W TB 55-1520-237-20-50 UH-60-84-08 C/WSSG G CAUDILL TI D CO 326 MED BN, FT.CAMPBELL, KY (GC0000)

30-May-1984 1

FT. CAMPBELL, KY

QC000000

D CO 326TH MED BNSOF UH-60-84-11 INSP OF LONGITUDNALLINKS PN: 70400-08110-047/048. CLEVISLATERAL 70400-08151-046. SPERICAL BRNGSSB5078-101 IAW TB 55-1520-237-20-56 C/WSSG DAN PLUMMER TI D CO 326 MED BN, FT.CAMPBELL, KY (DP0000)

09-Jul-1984 1

FT. CAMPBELL, KY

QC000000

D CO 326TH MED BNOCM/ACE PERFORMED AT 0377 ACFT HRS ATFT. CAMPBELL KY BY ACE TEAM MEMBER IAVSCOM OCM SEC ST. LOUIS MO (AT0000)

26-Jul-1984 1

FT. CAMPBELL, KY

QC000000

D CO 326TH MED BNSOF UH-60-84-12 INSP OF MAIN ROTORSPINDLE BOLT SS5110-06-04 IAW TB 55-1520-237-20-55 C/W SSG DAN PLUMMER D CO 326MED BN, FT. CAMPBELL, KY (DP0000)

31-Jul-1984 1

FT. CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



D CO 326TH MED BNHIGH SPEED SHAFT VIBRATION TEST WASCONDUCTED ON 21 AUG 84 WITHDRIVESHAFT SN: FOR #1 A275-00253, #2:A25-00599 VIBREX READING WERE #1 1.3, #2:1.1DOUGLAC C WATSON SGT CO D 326 MED BN,FT. CAMPBELL KY (DW0000)

21-Aug-1984 1

FT. CAMPBELL, KY

QC000000

D CO 326TH MED BNSOF UH-60-8-10 ONE TIME INSP ANDPERMANENT INSP OF TAIL CONE CANTEDHINGE BULKHEAD RADIUS BLOCKS PN:70219-05001-108/109/110/111 C/W SGT DWATSON TI D CO 326 MED BN FT. CAMPBELL,KY (DW0000)

24-Aug-1984 1

FT. CAMPBELL, KY

QC000000

D CO 326TH MED BNSOF ONE TIME INSPECTION TAIL ROTORCONTROL CABLES PN: 70400-00511-044 ANDPN 70400-00511-045 FOR PROPER ROUTINGOF CONTROL CABLES AND CABLE TENSIONIAW TB 55-1520-23-20-58 UH-60A 84-14 C/WSGT L. PETROFF D CO 326 MED BN, FT.CAMPBELL, KY (LP0000)

29-Nov-1984 1

FT. CAMPBELL, KY

QC000000

D CO 326TH MED BNSOF UH-60-84-1 ONE TIME AND RECURRINGINSP OF MAIN GEARBOX DOWEL PINS PN70351-08100-053-060 C/W A GARLAND CO D326 MED BN FT. CAMPBELL, KY (AG0000)

02-Jan-1985 1

FT. CAMPBELL, KY

QC000000

D CO 326TH MED BNSOF UH-60-84-02 MAINT MANDATORY MSSGTO CHANGE THE AUTO ROTATION RPMLIMITS ON THE UH-60A BY REMOVINGTRANSPARENT RED TAPE FROM THE MAINROTOR TACHOMETE INDICATORS C/W SGT LPETROFF D CO 326 MED BN, FT. CAMPBELL,KY (LP0000)

28-Feb-1985 1

FT. CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



D CO 526 MED BNSOF UH-60-85-13 ONE TIME INSP ANDMODIFIED FLYABLE STORAGE PROCEDURESC/W SSG D WATSON, TI D CO 326 MED BN, FT.CAMPBELL, KY (DW0000)

16-Mar-1985 1

FT. CAMPBELL, KY

QC000000

D CO 526 MED BNSOF UH-60-85-10 ONE TIME INSPECTION OFBLACKHAWK HELICOPTERS C/W SGT L.PETROFF TI D CO MED BN FT. CAMPBELL, KY(LP0000)

30-Apr-1985 1

FT. CAMPBELL, KY

QC000000

D CO 526 MED BNSOF UH-60-85-15 ONE TIME RECORDS INSP OFM/R HUB C/W SSG D WATSON, TI D CO 326MED BN, FT. CAMPBELL KY (DW0000)

03-Jun-1985 2

FT. CAMPBELL, KY

QC000000

D CO 526 MED BNSOF UH-60-85-14 ONE TIME RECORDS INSP OFM/R SHAFT C/W SSG D WATSON, TI D CO 326MED BN, FT. CAMPBELL KY (DW0000)

03-Jun-1985 1

FT. CAMPBELL, KY

QC000000

D CO 526 MED BNOCM/ACE PERFORMED AT 0502 ACFT HRS ATFT. CAMPBELL KY BY AE TEAM MEMBER KAVSCOM OCM SEC ST. LOUIS MO (DW0000)

19-Jun-1985 1

FT. CAMPBELL, KY

QC000000

D CO 526 MED BNSOF UH-60-85-23 ONE TIME INSP OF T/R D/SVISCOUS DAMPER BEARINGS C/W AGARLAND TI SSG D CO 326 MED BN, FT.CAMPBELL, KY (AG0000)

25-Jul-1985 1

FT. CAMPBELL, KY

QC000000

D CO 526 MED BNSOF UH-60-85-24 UH-60-85-24 SUPPLEMENTTO INSP OF T/R D/S BEARINGS C/W LPETROFF TI SSG D CO 326 MED BN, FT.CAMPBELL, KY (LP0000)

27-Aug-1985 1

FT. CAMPBELL, KY

QC000000

D CO 526 MED BNSOF UH-60-85-18 BLACKHAWK HELICOPTERREQUIREMENTS FOR UNGROUNDING C/W DWATSON TI SSG D CO 326 MED BN, FT.CAMPBELL, KY (DW0000)

25-Sep-1985 2

FT. CAMPBELL, KY

QC000000

D CO 526 MED BNENG VIB CK COMPLETED I/A/W SOF UH-60-85-17 #1 ENG READING .47 #2 ENG READING .41D WATSON TI SSG D CO 326 MED BN, FT.CAMPBELL, KY (DW0000)

25-Sep-1985 1

FT. CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



D CO, 1-147TH AVN BN,WIARNG

AIRWORTHINESS RELEASE (AWR) FOR UH-60A/L DESERT COMBAT OPERATIONS WITHPILOTS AND COPILOTS DOORS REMOVED(AWR 1111) C/W AT 3233.1 ACFT HRS AND TOREMAIN IN AFFECT WHILE ACFT ISSTATIONED IN S/W ASIA THEATER. (XK1861)

07-Aug-2003 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



D CO, 1-147TH AVN BN,WIARNG,

AIRWORTHINESS RELEASE (AWR 1119)OPERATION DURING DESERT COMBATOPERATIONS FOR UH-60A/L RECEIVED ANDC/W. (XK1861)

21-Jul-2003 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



D. CO. 1-147THAWR 1054 DATED 31 OCT 08, SUPERCEDESAWR DATED 06 JUN 07, ARMY REGULATIONSTO OPERATE WITH BAMBI WATERBUCKETS.

10-Jan-2009 3


RD542386

D. CO. 1-147THAWR DATED 22 SEP 06 HELIBASKET WITH ELLHAS EXPIRED, IS NO LONGER APPLICABLETO ACFT.

10-Jan-2009 1


RD542386




8.7.DATE

6.REMARKS

4. 5.



D.CO. 147TH AVN BNM/R BLADE SUDDEN STOPPAGE INSPECTIONFOR AN/ALQ-144 INPACT COMPLETED THISDATE IN CAMP BONDSTEEL KOSOVO(XM0958)

11-Jan-2007 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



DCO 1/147TH AVN BNMAIN MOD OIL FILTER BYPASS BUTTONEXTENDED AT 3909.2M ACFT HRS.REPLACED 1ST AND 2ND STAGE FILTERS.SEVICEABILITY INSP COMPLETED OK.(CA4792)

24-Feb-2007 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



DCO 1/147TH AVN BN TFEAGLE

AIRCRAFT PREPPED FOR SEA SHIPMENT TOGERMANY TEMP DUTY IN HOHENFELSGERMANY (WH1187)

21-Sep-2006 1

CAMP AUTTERBURY ID

QC000000

DCO 1/147TH AVN BN TFEAGLE

ACFT ARRIVE CAMP BONDSTEEL KOSOVOFOR NATO PEACE KEEPING MISSION(WH1187)

12-Nov-2006 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



DCO 1-147TH AVN BNBLUE FORCE TRACKER HARDWAREVERIFICATION UH-60-06-ASAM-05 COMPLIEDWITH AT 3720.5 ACFT HRS MWO NA (CA4792)

21-Jul-2006 1

FT KNOX, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



DDCT-Y DLAUH-60-95-ASAM-01/TB 1-1520-237-20-157HOISTING AND AERIAL RECOVERY OF UH-60/EH-60 ESSS PROVISIONS HELICOPTERS,N/A THIS ACFT. (DB1111)

18-Oct-1994 1

CORPUS CHRISTI, TX

QC000000

DDCT-Y DLAUH-60-95-ASAM-02/TB 1-1520-237-20-159 ALLH-60 ACFT REQUIREMENT TO OPERATE THEFUEL TANK SUBMERGED BOOST PUMPS ONAT ALL TIMES WITH ALL FUELS DURINGGROUND AND FLIGHT OPERATIONS. (DB1111)

21-Oct-1994 1

CORPUS CHRISTI, TX

QC000000




8.7.DATE

6.REMARKS

4. 5.



DYNCORPPMI 1 COMPLETED AT 4100.3 ACFT HRS, PMI 2WILL BE DUE AT 4460.3 ACFT HRS (GM3275)

28-Sep-2007 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



DYNCORP OLRUH-60-02-ASAM-03/TB 1-1520-237-20-245INSPECTION OF ENGINE CONTROLQUADRANT POWER CONTROL LEVER (PCL)WIRING C/W AT 2969.5 ACFT HRS. (NM8992)

25-Feb-2002 1

KAP KILLEEN, TEXAS76543

QC000000

DYNCORP OLRUH-60-02-ASAM-05/TB 1-1520-237-20-251REMOVAL OF CHICAGO RAWHIDE M/RSPINDLE THRUST BEARINGS WITH S/N'S C325-00001 THRU C325-02407 C/W AT 2969.5 ACFTHRS. (NM8992)

02-Apr-2002 1


QC000000

DYNCORP OLRUH-60-02-ASAM-06/TB 1-1520-237-20-252COLLECTIVE AND YAW BOOST SERVOASSEMBLIES SWAGE PIN COLLARS C/W AT2969.5 ACFT HRS. (NM8992)

18-Apr-2002 1


QC000000

DYNCORP OLRACE/CPCE PERFORMED AT 3400 ACFT. HRS.BY TEAM MEMBER W. AMCOM PROJECT OLRKILLEN, TX. (JP2527)

27-Oct-2004 1

SPRINGFIELD, MO

QC000000




8.7.DATE

6.REMARKS

4. 5.



DYNCORP OLR KAPAIRCRAFT MAIN ROTOR HEAD RIGGED I/A/WTM 1-1520-237-23 PARA 11-4-4. FOWARD PRISERVO SHORTENED 1 1/4 TURN, AFTLENGTHENED 1 1/4 TURN, LATERALSHORTENED 3/4 TURN. (NM8992)

08-Mar-2002 1

KILLEEN AIRPORT TX76543

QC000000




8.7.DATE

6.REMARKS

4. 5.



DYNCORP PROJ OLRSOF UH-60-02-03/TB 1-1520-237-20-241 ONETIME INSPECTION OF FLIGHT CONTROLSYSTEM PITCH TRIM ASSY C/W AT 2969.5ACFT HRS AT THIS STATION. (NM8992)

12-Dec-2001 2


QC000000

DYNCORP PROJ OLRSOF UH-60-02-02/TB 1-1520-237-20-237INSPECTION OF M/R HUBS FOR REWORKPROGRAM C/W AT 2969.5 ACFT HRS AT THISSTATION. (NM8992)

12-Dec-2001 1


QC000000

DYNCORP PROJ OLRSOF UH-60-02-04/TB 1-1520-237-20-242 INSPAPU FUEL LINE GROMMET C/W AT THISSTATION AT 2969.5 A/C HOURS. (NM8992)

25-Jan-2002 1


QC000000

DYNCORP PROJ OLRTAIL ROTOR RIGGING COMPLETED AT 2969.5A/C HOURS. (NM8992)

06-Feb-2002 1


QC000000

DYNCORP PROJ OLRUH-60-02-ASAM-02/TB 1-1520-237-20-246INITIAL AND RECURRING INSPECTION OFCONTROL ROD JAM NUTS C/W AT 2969.5ACFT HRS. (NM8992)

20-Feb-2002 1


QC000000

DYNCORP PROJ OLRPMS II COMPLETED AT 2969.5 A/C HOURS.NEXT PMS II DUE AT 3469.5 A/C HOURS.(NM8992)

21-Feb-2002 1


QC000000

DYNCORP PROJ OLRUH-60-02-ASAM-04/TB 1-1520-237-20-244,RESTRAINT SYSTEM INSPECTION C/W(LM2968)

15-Mar-2002 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



DYNCORP PROJECTOLR

SOF UH-60-02-05/TB 1-1520-237-20-243INSPECTION OF M/R EXPANDABLE PINS FORCORRECT SWAGGINE C/W AT 2669.5 ACFTHRS. (NM8992)

05-Feb-2002 1

KILLEEN, TEXAS 76543

QC000000

DYNCORP PROJECTOLR

SOF UH-60-02-06/TB 1-1520-237-20-250REVISION TO MAIN ROTOR HUB NON-DESTRUCTIVE INSPECTION (NDI)PROCEDURES C/W AT 2969.5 ACFT HRS.(NM8992)

01-Mar-2002 1

KILLEEN AIRPORTTEXAS 76543

QC000000




8.7.DATE

6.REMARKS

4. 5.



L-3ACE COMPLETED AT 5148.1 A/C HRS. BY ACETEAM MEMBERS B/G. AFMA, RASME, AMCOM.

04-Jun-2014 1

GROTON, CT 06340

JG389608

L-3ACE COMPLETED AT 5379.9 A/C HRS. BY ACETEAM MEMBERS B/G. AFMA, RASME, AMCOM.

09-Jun-2015 1

GROTON, CT 06340

JG389608




8.7.DATE

6.REMARKS

4. 5.



L3 RASM-E, FTCAMPBELL, KY 42223

OMC/ACE PERFORMED AT 4836.1 ACFT HRSBY TEAM MEMBER UU/QQ.

12-Oct-2011 1

COLUMBUS, OH 43217

GG540327




8.7.DATE

6.REMARKS

4. 5.



L-3 VORTEXPMI #2 COMPLETED AT 3740.4 ACFT HRS.NEXT PMI #1 DUE AT 4100.4 ACFT HRS ANDPMI #2 DUE AT 4460.5 ACFT HRS.SCHEDULED ON 360 PMI IAW UH-60-MIM-2006-006. (MC9992)

23-Aug-2006 1

FT KNOX, KY

QC000000

L-3 VORTEXT/R BIAS SET 18 SEP 06 AT 3744.6 ACFT HRSBIAS READINGS:RED INITIAL=4.972FINIAL=5.299 VALUE=.327BLUE INITIAL=4.250FINIAL=4.584 VALUE=.334YELLOWINITIAL=4.954 FINIAL=5.289VALUE=.335BLACK INITIAL=4.257FINIAL=4.587 VALUE=.330T/R CABLE TENSION= L/H CABLE 167 R/H CABLE 167 AT 29 DEG C(MC9992)

18-Sep-2006 1

FT KNOX, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



LSI MO-AVCRADUH-60-05-ASAM-01 REVISION TO UH-60-04-03/04 FUEL SYSTEM INTEGRITY CHECK.COMPLIED WITH VACCUM & PRESSURE TEST.AIRCRAFT CLEARED FOR OPERATION WITHBOOST PUMPS OFF. 3407.0 ACFT HRS(SK8291)

05-Jan-2005 1

SPRINGFIELD MO 65803

QC000000

LSI MO-AVCRADMAVEN IMPROVED HEATING SYSTEMINSTALLED IAW ISAQ 110 DATED 06 FEB 2004(SK8291)

07-Feb-2005 3


QC000000

LSI MO-AVCRADTB 1-1520-237-30-1 & TB 1-1500-200-20-31ACFT DESERT OPERATIONS SPECIALINSPECTION AND CLEANING REQUIREMENTS(RESET) COMPLETED AT 3407.0 ACFT HRS.(SK8291)

07-Feb-2005 2


QC000000

LSI MO-AVCRADPMS-2/RESET COMPLETED AT 3407.0 ACFTHOURS. NEXT PMS-2 INSPECTION DUE 3907.0ACFT HRS (SK8291)

07-Feb-2005 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



OLR WESTACE PERFORMED @ 4185 A/C HOURS, @MADISON, WI, BY JJ & E (CA866418) (CA6418)

18-Jul-2008 1

FT. LEWIS, WA 98433

QC000000




8.7.DATE

6.REMARKS

4. 5.



PROJECT OLRACE PERFORMED AT 2322 ACFT. HRS ATMADISON WI. BY DD&P. (DD7078)

17-Jul-1998 1

AASF #2 WIARNGMADISON, WI

QC000000

PROJECT OLRACE PERFORMED AT 2465.0 ACFT. HRS. ATMADISON, WI BY P & V. (KS0820)

16-Apr-1999 1

AASF #2 WIARNGMADISON, WI

QC000000

PROJECT OLRJACE PERFORMED AT 2603 ACFT HRS ATMADISON, WI BY HH&V. (KS0820)

25-Jun-2000 1

FT LEWIS, WA

QC000000

PROJECT OLRACE PERFORMED AT 2958 ACFT HRS ATMADISON, WI BY HH&Q. (GC0981)

11-Sep-2001 1

FT LEWIS, WA

QC000000




8.7.DATE

6.REMARKS

4. 5.



PROJECT OLR FT.LEWIS, WA

ACE PERFORMED AT 3407 A/C HRS ATMADISON, WI BY T & P (DD7078)

29-Jun-2005 1

MADISON, WI

QC000000




8.7.DATE

6.REMARKS

4. 5.



SCIENCE ANDENGINEERINGSERVICES LLC

EFFECTIVE THIS DATE, ACFT TRANFERED TOSES FOR INDUCTION INTO B.E.S.T. PROGRAM

04-Mar-2016 1

HUNTSVILLE

ED046014


H-60-15-ASAM-07 (MAIN ROTOR BLADEDEBONDING AND TIP RIB CRACKING) NOTCOMPLIED WITH

08-Mar-2016 1

HUNTSVILLE

ED046014


H-60-16-AMAM-04 (T-CLIP INSTALLATION) NOTCOMPLIED WITH

09-Mar-2016 2

HUNTSVILLE

ED046014


H-60-16-ASAM-02 (DEFECTIVE FUEL HOSES)NOT COMPLIED WITH

09-Mar-2016 1

HUNTSVILLE

ED046014




8.7.DATE

6.REMARKS

4. 5.



SIKORSKY ACFTAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG 70400-00003REV B. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORDANCE. A) LATERALCONTROL SERVO INPUT ROD P/N 70400-02258-046 HAS BEEN LENGTHENED 1/2 TURN, B)AFT CONTROL SERVO INPUT ROD P/N 70400-02258-045 HAS BEEN SHORTENED 1/6 TURN,C) FORWARD CONTROL SERVO INPUT RODP/N 70400-02258-047 HAS BEEN SHORTENED1/2 TURN. WHEN AIRCRAFT RIGGING ISBIASED, RIGGING PIN HOLES ARETEMPORARILY LOST AT THE ABOVE 3POINTS. (NO PID)

02-Mar-1982 1

STRATFORD, CT

QC000000




8.7.DATE

6.REMARKS

4. 5.



SKIORSKY SUPPORTAIRCRAFT RECEIVED AT SKIORSKY SUPPORTSERVICES, INC, TROY, AL AT TOTALAIRCRAFT HOURS 1437.8 FORINCORPORATION OF MWO 55-1520-237-55-3CRASHWORTHY FLIGHT DATA RECORDERI/A/W CONTRACT NO DAAJ09-85-G-A015 JUDYMORGAN RECORDS CLERK (JM0000)

24-Jun-1988 1

TROY, AL

QC000000




8.7.DATE

6.REMARKS

4. 5.



USARMAVCENTWX 031930Z OCT 85, (SOF GEN 85-01) ONETIME INSP OF MS 25224 SWITCH GUARDS ANDTWO POSITIONS TOGGLE SWITCHES C/W(J.SHEHANE, 5144, INSP) (W.COVINGTON,0759) USARMAVCEN, FT. RUCKER, AL(WC0759)

08-Oct-1985 1

FT. RUCKER, AL

QC000000

USARMAVCENSPC 5197 MOD OF OIL FILLER C/W(W.COVINGTON, 0759) USARMAVCEN, FT.RUCKER, AL (WC0759)

29-Oct-1985 1

FT. RUCKER, AL

QC000000

USARMAVCENECN 02264-10-01, REPL OF M/R ANTI FLAPSTOP ROLL PINS C/W (W.COVINGTON, 0759)USARMAVCEN, FT. RUCKER, AL (WC0759)

30-Oct-1985 2

FT. RUCKER, AL

QC000000

USARMAVCENINSTL OF RUBBER TUBING ON ANTI-COLL LT.SW AND LOW RPM AUDIO SW I/A/W COR LTRDTD 27APR84 C/W (W.COVINGTON, 0579)USARMAVCEN, FT. RUCKER, AL (WC0759)

30-Oct-1985 1

FT. RUCKER, AL

QC000000

USARMAVCENSTABILATOR HINGE BOLTS TORQUE CHECKC/W (W.COVINGTON, 0759) USARMAVCEN, FT.RUCKER, AL (WC0759)

07-Nov-1985 2

FT. RUCKER, AL

QC000000

USARMAVCENINST OF FUEL FLAG C/W (W.COVINGTON,0759)USARMAVCEN FT. RUCKER, AL (WC0759)

07-Nov-1985 1

FT. RUCKER, AL

QC000000

USARMAVCENTB 55-1520-237-20-73, (UH-60A) TORQUESTABILIZATIO OF MAIN ROTOR PITCH HORNATTACHMENT BOLTS C/W (INSPECTOR #117)(W.COVINGTON, 0579) USARMAVCEN, FT.RUCKER, AL (WC0759)

11-Dec-1985 1

FT. RUCKER, AL

QC000000

USARMAVCENTB 55-1520-237-23-1 (UH-60A 86-01) REPL OFT/R D/S BEARINGS C/W (W.HEAD, INSP)(W.COVINGTON,0579) USARMAVCEN, FT.RUCKER, AL (WC0759)

25-Feb-1986 1

FT. RUCKER, AL

QC000000

USARMAVCENTB 55-1520-237-20-74 (UH-60A 86-02 & 86-03)ONE TIME INSP OF T/R D/S NUTS C/W(W.HEAD, INSP) (W. COVINGTON, 0579)USARMAVCEN, FT. RUCKER, AL (WC0759)

26-Feb-1986 1

FT. RUCKER, AL

QC000000

USARMAVCENACFT RESTRICTED FROM FLIGHT UNTILFURTHER NOTICE I/A/W TWX (UH-60A-86-05)01223547 MAR 86 C/W (B.MILLS,6188)(W.COVINGTON,0759) USARMAVCEN, FT.RUCKER, AL (WC0759)

12-Mar-1986 1

FT. RUCKER, AL

QC000000

USARMAVCENTB 55-1520-237-20-75 (UH-60A-86-07)REQUIREMENTS FOR UNGROUNDING (UH-60)TDR 156-86 C/W (B.MILLS 6188, INSP)(.COVINGTON,0759) USARMAVCEN, FT.RUCKER, AL (WC0759)

01-May-1986 1

FT. RUCKER, AL

QC000000

USARMAVCENTB 55-1520-237-20-77 REPL OF UH-60A/EH-60ASTAB ACT 70400-06641-110 L.LUNSFORD 6188INSP USARMAVCEN, FT. RUCKER, AL(LL6188)

07-May-1986 1

FT. RUCKER, AL

QC000000

USARMAVCENTB 55-1520-237-20-75 (UH-60A 86-101) ONETIME STAKING OF BRNGS OIL LEVER ASSYC/W (C. BOX 6400 INSP) W. COVINGTON, 0579USARMAVCEN, FT. RUCKER AL (WC0579)

02-Jul-1986 1

FT. RUCKER, AL

QC000000




8.7.DATE

6.REMARKS

4. 5.



USARMAVCENTB 55-1520-237-20-78 (UH-60-86-12) CHANGEOUT OF CERTAIN YAW AND COLLECTIVEBOOST SERVOS (UH-60)(J.SHEHANE,5144,INSP) W. COVINGTON, 0579USARMAVCEN FT. RUCKER, AL (WC0579)

30-Jul-1986 1

FT. RUCKER, AL

QC000000

USARMAVCENTWX 291415Z JUL 86 (UH-60-86-13) REMOVALOF AN 310-8 NUTS (UH-60) C/W(B.MILLS,6188,INSP) W. COVINGTON, 0579USARMAVCEN, FT. RUCKER, AL (WC0579)

01-Aug-1986 1

FT. RUCKER, AL

QC000000

USARMAVCENINSPECTION OF STABILATOR AMPLIFIERSI/A/W LETTER FROM COR DATED 29 AUG 86C/W (J.SHEHANE,5144, INSP W.COVINGTON,0579, USARMAVCEN, FT. RUCKER, AL(WC0579)

05-Sep-1986 1

FT. RUCKER, AL

QC000000

USARMAVCENTB 55-1520-237-20-84 (UH-60-86-20)INSPECTION OF THE FIRST THREE TAILROTOR DRIVE SHAFT SPLINE COUPLINGSAND REMOVAL OF MATERIAL FROM UNDERCREW SEATS C/W INSP B. MILLS 6188, DSTEVENSON, 011315 USARMAVCEN, FT.RUCKER, AL (DS1315)

10-Nov-1986 1

FT. RUCKER, AL

QC000000

USARMAVCENTDR 271-86 TB 55-1520-238-20-85 (UH-60-86-21) ONE TIME INSPECTION OF CREW SEATSFOR LONGITUDINAL MOVEMENT OF LOCK PINADJUSTMENT C/W D STEVENSON, 011315USARMAVCEN, FT. RUCKER, AL (DS1315)

03-Dec-1986 1

FT. RUCKER, AL

QC000000

USARMAVCENTDR 139-86 TORQUE CHECK OF PRIMARYSERVO MOUNT BOLTS I/A/W LTR. FROM THECOR DTD 17 MAR 86 C/W INSP B. MILLS 6188,D STEVENSON, 011315 USARMAVCEN FT.RUCKER, AL (DS1315)

12-Dec-1986 2

FT. RUCKER, AL

QC000000

USARMAVCENTWX 051900Z AUG 86 (MIM-60-MEM-10)INSPECTION/REPAIR OF DROOP STOP NUT,C/W INSP B. MILLS 6188 D STEVENSON,011315, USARMAVCEN, FT. RUCKER, AL(DS1315)

12-Dec-1986 1

FT. RUCKER, AL

QC000000

USARMAVCENTDR 264-86 INSTALLATION OF COPPERSCREEN OVER ANTI-ICE EXIT TUBE IAW ENGSTD A-25-86 C/W NED STEVENSON, 011315USARMAVCEN, FT. RUCKER, AL (DS1315)

17-Dec-1986 1

FT. RUCKER, AL

QC000000

USARMAVCENPHASE INSP #2 COMPLETED AT 997.7 ACFTHRS PHASE INSP #3 TO BE COMPLETED AT1497.7 ACFT HRS D STEVENSON, 011315USARMAVCEN, FT. RUCKER, AL (DS1315)

05-Jan-1987 1

FT. RUCKER, AL

QC000000

USARMAVCENOCM/ACE PERFORMED AT 1006 ACFT HRS ATFT. RUCKER, AL BY ACE TEAM MEMBER S.PARKER AVSCOM OCMSEC ST. LOUIS, MOO(SP0000)

12-Jan-1987 1

FT. RUCKER, AL

QC000000



DATE AC HRS SHAFT VERTICAL REASON FOR VIB CHECKLONGITUDINALLATERAL

IPS READINGS4.

8023506HELICOPTER, UTILITYUH-60A3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Report Date: 09-Mar-2016 1/4

100 HR REQUIREMENTS21-Mar-2002 #1 ENG OUT 0.39002969.5

100 HR REQUIREMENTS21-Mar-2002 TAIL ROTOR 0.08002969.5

100 HR REQUIREMENTS21-Mar-2002 OIL COOLER 0.250.3202969.5

100 HR REQUIREMENTS21-Mar-2002 #2 ENG OUT 0.19002969.5

100 HR INSP02-Dec-2002 #1 ENG OUT 0.34003069.3

100 HR INSP02-Dec-2002 #2 ENG OUT 0.46003069.3

100 HR INSP02-Dec-2002 TAIL ROTOR 0.12003069.3

100 HR INSP02-Dec-2002 OIL COOLER 0.310.1403069.3

T/R EROSION TAPE15-Feb-2003 TAIL ROTOR 0.09003095.9

UNFOLD FROM SEA DEPLOY10-Apr-2003 TAIL ROTOR 0.13003105.9

ENGINE REPLACEMENT14-May-2003 #1 ENG OUT 0.39003132

100 HR REQUIREMENTS14-Aug-2003 #1 ENG OUT 0.15003270.5

100 HR REQUIREMENTS14-Aug-2003 OIL COOLER 0.280.3103270.5


100 HR REQUIREMENTS14-Sep-2003 TAIL ROTOR 0.11003270.5

100 HR REQUIREMENTS25-Jun-2004 #1 ENG OUT 0.43003359.6

100 HR REQUIREMENTS25-Jun-2004 #2 ENG OUT 0.11003359.6

100 HR REQUIREMENTS25-Jun-2004 AXIAL FAN 0.40.3603359.6

100 HR REQUIREMENTS25-Jun-2004 TAIL ROTOR 0.1003359.6

POST PMS2/100HR04-Feb-2005 #1 ENG OUT 0.38003407

POST PMS2/100HR04-Feb-2005 #2 ENG OUT 0.16003407

POST PMS2/100HR04-Feb-2005 TAIL ROTOR 0.14003407

POST PMS2/100HR04-Feb-2005 OIL COOLER 0.270.0703407

100 HR REQUIREMENTS20-May-2005 #1 ENG OUT 0.3003506.3

100 HR REQUIREMENTS20-May-2005 #2 ENG OUT 0.44003506.3

100 HR REQUIREMENTS20-May-2005 AXIAL FAN 0.190.5303506.3

100 HR REQUIREMENTS20-May-2005 T/R G/B 0.13003506.3

EDITION OF JAN 64 IS OBSOLETE For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

DA FORM 2408-15-2 E, OCT 91 AIRCRAFT VIBRATION RECORD


IPS READINGS4.





120 HR REQUIREMENTS04-Aug-2005 AXIAL FAN 0.210.5503559.3

120 HR REQUIREMENTS04-Aug-2005 T/R G/B OU 0.19003559.3

120 HR REQUIREMENTS24-Apr-2006 #1 ENG OUT 0.48003678.2

120 HR REQUIREMENTS24-Apr-2006 #2 ENG OUT 0.41003678.2

120 HR REQUIREMENTS24-Apr-2006 T/R G/B 0.1003678.2

120 HR REQUIREMENTS24-Apr-2006 AXIAL FAN 0.390.4303678.2

PHOST PHASE14-Sep-2006 #1 ENG OUT 0.07003743.4

PHOST PHASE14-Sep-2006 #2 ENG OUT 0.03003743.4

PHOST PHASE14-Sep-2006 OIL COOLER 00.3203743.4

PHOST PHASE14-Sep-2006 TAIL ROTOR 0.13003743.4

UNFOLDING OF BLADES10-Oct-2006 TAIL ROTOR 0.3003749.5

120 HR REQUIREMENTS10-Jan-2007 #1 ENG OUT 0.37003857.6

120 HR INSP.10-Jan-2007 #2 ENG HSS 0.45003857.6

120 HR REQUIREMENTS10-Jan-2007 TAIL ROTOR 0.3003857.6

120 HR REQUIREMENTS10-Jan-2007 OIL COOLER 00.1903857.6

120 HR INSP19-May-2007 OIL COOLER 00.6903975.9

120 HR INSP19-May-2007 T/R 0.07003975.9

120 HR INSP19-May-2007 #2 ENG OUT 0.45003975.9

120 HR INSP19-May-2007 #1 ENG OUT 0.43003975.9

POST PMI27-Sep-2007 OIL COOLER 00.2504100.3

POST PMI27-Sep-2007 T/R 0.06004100.3

POST PMI27-Sep-2007 #2 ENG OUT 0.15004100.3

POST PMI27-Sep-2007 #1 ENG OUT 0.39004100.3

INBOARD RETENTION RETORQ11-Oct-2007 T/R 0.07004109.5

UNFOLD FROM SEA DEPLOY01-Dec-2007 TAIL ROTOR 0.17004134.8




IPS READINGS4.



TAIL PYLON REPLACED11-Jul-2008 #1 HSS 0.41004185

TAIL PYLON REPLACED16-Jul-2008 OIL COOLER 00.204185

TAIL PYLON REPLACED28-Aug-2008 TAIL ROTOR 0.19004185

TAIL PYLON CHANGE02-Sep-2008 #2 HSS 0.02004185

120 H INSP29-Oct-2008 #1 ENG HSS 0.38004216.3

120 H INSP29-Oct-2008 #2 ENG HSS 0.42004216.3

120 H INSP29-Oct-2008 OIL COOLER 00.0904216.3

120 H INSP29-Oct-2008 TAIL ROTOR 0.18004216.3

POST PMI17-Mar-2010 #1 ENG HSS 0.39004457.3

POST PMI17-Mar-2010 #2 ENG HSS 0.19004457.3

POST PMI17-Mar-2010 TAIL ROTOR 0.01004457.3

POST PMI17-Mar-2010 OIL COOLER 00.2204457.3

120 HOUR INSP18-Aug-2010 #1 ENGINE 0.34004577.5

120 HOUR INSP18-Aug-2010 #2 ENGINE 0.02004577.5

120 HOUR INSP18-Aug-2010 OIL COOLER 00.1504577.5

120 HOUR INSP18-Aug-2010 TAIL ROTOR 0.11004577.5

REPLACED BLADE12-Oct-2010 TAIL ROTOR 0004633.5

ROUTINE 120 INSPECTION14-Dec-2010 #1 ENGINE 0.34004696.7

ROUTINE 120 INSPECTION14-Dec-2010 #2 ENGINE 0.41004696.7

ROUTINE 120 INSPECTION14-Dec-2010 OILCOOLER 00.0504696.7

ROUTINE 120 INSPECTION14-Dec-2010 TAIL ROTOR 0.18004696.7

120/PMI 109-Aug-2011 TAIL 0.01004809.4

120/PMI 109-Aug-2011 #2 ENG 0.44004809.4

120 HOUR INSPECTION30-May-2012 #1 ENG 0.37004929

120 HOUR INSPECTION30-May-2012 #2 ENG 0.47004929

120 HOUR INSPECTION30-May-2012 OIL COOLER 0.13004929

120 HOUR INSPECTION30-May-2012 TAIL 0.03004929




IPS READINGS4.



REINSTALL ENG13-Jun-2012 #2 ENG 0.35004942.3

# 2 ENGINE REMOVED AND REINSTALL13-Jun-2012 # 2 ENG 0.35004942.5

H-60-11-AMAM-1722-Aug-2012 TAIL 0.14004965

120 HR04-Dec-2012 #1 ENG 0.4005047.3

120HR04-Dec-2012 #2 ENG 0.38005047.3

120 HR04-Dec-2012 OIL COOLER 00.4405047.3

120 HR04-Dec-2012 TAIL 0.1005047.3

POST-OCM TAIL BALANCE25-Feb-2014 TAIL 0.051005067.3

POST-OCM SHAFT BALANCE25-Feb-2014 #1ENG 0.12005067.3

POST-OCM SHAFT BALANCE25-Feb-2014 #2 ENG 0.031005067.3

POST-OCM BALANCE25-Feb-2014 OIL COOLER 0.060.1805067.3

INNER RETENTION PLATE RETORQUE06-Mar-2014 TAIL 0.031005082.1

REPLACED RED BOOT12-Jul-2014 TAIL 0.08005180.3

RPL SEC 3, #2 VD BEARING04-Sep-2014 OIL COOLER 0.19005212.6

120 HOUR INSP07-Jan-2015 OIL COOLER 0.040.1705307.3

120 HOURS INSP07-Jan-2015 #1ENG 0.15005307.3

120 HOUR INSP07-Jan-2015 #2 ENG 0.032005307.3

6. Remarks




8023506HELICOPTER, UTILITY UH-60A

7. FREQUENCY 4.

5. ITEMS TO BE INSPECTED

2. MODEL 3. SERIAL NUMBER 1. NOMENCLATURE

8. NEXTNO DUE 6. REFERENCE 9. COMPLETED AT

INSP

A020 5384.510TM 1-1520-237-PMDPERFORM M/R SPINDLE LUGS,M/R CUFF, TIP CAPSINSPECTION

5374.5H

A022 Sep 2 201514TM 1-1520-237-23-914 DAY FLYABLE STORAGEENGINE RUN UP

Aug 19 2015D

A092 Sep 13 201530TM 11-6140-203-23&P30 DAY SLAB BATTERYINSPECTION (D8565/11-1)

Aug 14 2015D

A100 Sep 13 201530DA PAM 738-751#1 ENGINE HISTORY RECORDERREADING DUE

Aug 14 2015D

A101 Sep 13 201530DA PAM 738-751#2 ENGINE HISTORY RECORDERREADING DUE

Aug 14 2015D

A103 Sep 26 201530TM 1-1500-344-23AIRCRAFT WASH DUE Aug 27 2015D

A110 538840TM 1-1520-237-PMSPMS 40 HOUR INSPECTION 5348H

A115 Sep 26 201530TM 1-1520-237-23-12LUBE REQUIRMENTS Aug 27 2015D

A115 5419.940TM 1-1520-237-23-12LUBE REQUIRMENTS 5379.9H

A116 5694.5360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

5334.5H

A116 Feb 24 201612H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

Feb 24 2015M

A117 5694.5360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 5334.5H

A117 Feb 24 201612H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE Feb 24 2015M

A140 5425.8120AWR 1346R16, IVHMSIN ACF

DOWNLOAD AND REVIEW IVHMSDATA

5305.8H

A160 Oct 22 201590TM 1-1520-237-23-1290 DAY CORROSIONINSPECTION

Jul 24 2015D

A177 Nov 26 201590AR 95-190 DAY REVIEW/UPDATE OF 365-4 ENTRIES

Aug 28 2015D

A210 5427.3120TM 1-1520-237-23-12120 HOUR INSPECTIONREQUIREMENTS

5307.3H

A211 5694.5360H-60-10-AMAM-11APU OIL SAMPLE 5334.5H

A211 Feb 24 201612H-60-10-AMAM-11APU OIL SAMPLE Feb 24 2015M

A222 Feb 18 2016360TM 1-1680-377-13&PAMSS SURVIVAL KITINSPECTION

Feb 23 2015D

A230 Oct 15 2015120MWO 1-1520-237-50-77INSPECT BATTERYCOMPARTMENT FORCORROSION (SLAB)

Jun 17 2015D

A295 5427.3360TM 1-1520-237-23-12STABILATOR ACTUATOR ASSYLUBE

5067.3H

A296 5427.3360TM 1-1520-237-23-12STABILATOR INSPECTION 5067.3H

A298 5694.5360TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 5334.5H

For use of this form, see DA PAM 738-751; the proponent agency is DCSLOGDA FORM 2408-18, NOV 91, MAY BE USED

DA FORM 2408-18 E, OCT 97 EQUIPMENT INSPECTION LIST

A = APU OPERATING HOURS P = APU STARTS F = HOT SECTION FACTORSFREQUENCY LEGEND: H = ACFT HRS D = DAYS M = MONTHS Y = YEARS R = ROUNDS C = CYCLES S = ENG1 STARTS Z = ENG2 STARTS



7. FREQUENCY 4.




INSP

A298 Feb 18 201612TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING Feb 18 2015M

A299 5694.5360TM 1-1520-237-23-12SWASHPLATE LUBE 5334.5H

A299 Feb 18 201612TM 1-1520-237-23-12SWASHPLATE LUBE Feb 18 2015M

A400 5427.3720TM 1-1520-237-PMIPMI-1 4707.3H

A401 5787.3720TM 1-1520-237-PMIPMI-2 5067.3H

A408 5787.3720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-2, AREA 5 AND 6)

5067.3H

A410 5427.3720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-1, AREA 1 THRU 4)

4707.3H

A415 6054.5720H-60-10-AMAM-11MAIN GEARBOX OIL SAMPLE-PART # 073, 074, 076

5334.5H

A470 5459.81500TM 1-1520-237-23-12REPLACE NUMBER TWOCROSSFEED VALVE

3959.8H

A471 7227.32160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

5067.3H

A472 7227.32160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

5067.3H

A473 7372.62160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

5212.6H

A476 7969.55000TM 1-1520-237-23-12REPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

2969.5H

A477 10067.35000TM 1-1520-237-23-12REPLACEMENT OF STABILATORACTUATOR BOLTS

5067.3H

A480 9100.35000TM 1-1520-237-23-12REPLACE PIVOT BOLT 70400-08159-101,102,103,104

4100.3H

A485 9100.35000TM 1-1520-237-23-12REPLACE BELLCRANK BOLT70400-08159-105,106,107,108

4100.3H

A496 Jan 20 20166TM 1-1500-204-23-1CF3BR FIRE EXTINGUISHERWEIGHT TEST & INSPECTION

Jul 20 2015M

A501 Mar 1 20166TM 1-1520-237-23-12MAIN ROTOR BLADE PRESSURECHECK

Sep 1 2015M

A530 Feb 20 201612DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

Feb 20 2015M

A532 Oct 8 201512TM 1-1500-204-23-4COMPASS SWING / RMI Oct 8 2014M

A533 Feb 19 201612TM 1-1520-237-23-12PITOT STATIC SYSTEMINSPECTION

Feb 19 2015M

A534 Oct 22 201624TM 1-1500-204-23-1FIRST AID KIT INSPECTION Oct 22 2014M

A538 Feb 19 201612TM 1-1520-237-23-12FAT/OAT GAUGEINSPECTION/TEST

Feb 19 2015M

A541 Feb 20 201612TM 1-1520-237-23, C4REPLACE DIGITAL CLOCKBATTERY

Feb 20 2015M

A550 Feb 20 201612AWR1346R16IVHUMS BATTERYREPLACEMENT

Feb 20 2015M






7. FREQUENCY 4.




INSP

A553 Jul 28 201612AR 95-1AIRCRAFT WEIGHINGINVENTORY (365-1)

Jul 28 2015M

A580 Feb 14 201624TM 11-6140-203-23&PRETURN SLAB TO AVIM FORCAPACITY CHECK (VEREY 24MONTH)

Feb 14 2014M

A621 Feb 13 201624AR 95-1AIRCRAFT WEIGHING CLASS 2 Feb 13 2014M

A625 Feb 14 201960TM 11-6140-203-23&PREPLACEMENT OF SLABBATTERY (SLAB)

Feb 14 2014M

A630 Oct 1 2023114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

Apr 1 2014M

A633 Jan 1 2022114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

Jul 1 2012M

A638 Jan 1 2022114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

Jul 1 2012M

A640 Oct 1 2023114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

Apr 1 2014M

A648 Jan 20 2029180TM 1-1520-237-23REPLACE T/R SPRING CAPSULEASSY

Jan 20 2014M

A660 Jan 1 201672TB 9-1300-385REPLACE THRUSTEREMERGENCY RELEASE CARGOHOOK, MJ20

Jan 1 2010M

A665 Feb 18 201848H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

Feb 18 2014M

A670 Feb 18 201848TM 1-1520-237-23-1CABIN TUB INSPECTION Feb 18 2014M

A673 Feb 18 201848TM 1-1520-237-23-12FUEL CELL CORROSIONINSPECTION

Feb 18 2014M

A675 Feb 18 201848TM 1-1520-237-23-12FLIGHT CONTROL ROD INSP Feb 18 2014M

A755 14067.39000H-60-10-ASAM-11PC LINK TO SWASHPLATEBOLTS REPLACEMENT

5067.3H

E040 Sep 15 201590TM 11-5841-294-12APR-39 RADAR/LASERWARNING OPNL CHECK, 5841-01-236-8951

Jun 17 2015D

E135 Feb 15 20166TM 11-5821-333-12AN/ARC-201(V) SINCGARSRADIO HUB BATT REPL

Aug 15 2015M

E155 Jan 8 2016180TM 11-5810-262-23KY-58 BATTERY REPLACEMENT Jul 12 2015D

E165 Jan 8 2016180TM 11-5810-389-13KIT-1C BATTERY REPLACEMENT Jul 12 2015D

E231 5499.9120AWR 1516 EBC-406HMELT

PERFORM MONTHLY/ 120 HOURELT SELF TEST (EBC-406HM)

5379.9H

E901 Apr 14 20157AWR 1516 R2ELT DAILY INSPECTION DUE Apr 7 2015D




h

CONDITION ITEMS

kjifdcba g.

RMVL HR

RMVL HRSWUC HRS)COMPO/H

NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE

SINCEPREVSER NO.ANDNOMENCLATURE DUE

REPLACE

INST HRSTIMEINST HRSNO.COMPONENTPNCOMP REP.O/H ORNOMEN6.

3. PART NUMBER ORMODEL

2. NSN 4. SERIAL NUMBER 5. WUC1. NOMENCLATURE

Report Date: 1/1110-Mar-2016

80235061520010350266 00HELICOPTER, UTILITY

156001113021502C12D

00UNK350670219-05001-044TAIL CONE FITTING CCCC COND COND

162001231183103A01

3135380BEM248170250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001231183103A01

1465213BEM267270250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001421089003B01

10715067K0020026170250-13101-044SHOCK ABSORBER (TAIL) CCCC COND COND

165001285302405A01Z RED

5035067R1060364070106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z BLUE

5615067R1060419770106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z YELLOW

10605067WG1060019770106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z BLACK

25455067WG1060127270106-08100-046DAMPER ASSY, M/R CCCC COND COND

531501537465205A02H LAG BLUE

04457B9410720070103-08108-041SOLID BLADE PIN CCCC COND COND

531501537465205A02H BLK LAG


531501537465205A02H BLUE LEAD


531501537465205A02H RED LAG


531501537465205A02H YEL LEAD


531501537465205A02H BLK LEAD


531501537465205A02H YEL LAG


531501537465205A02H RED LEAD


161501199764605A03A

35154185A107-0011770104-08000-050SWASHPLATE ASSY CCCC COND COND

161501078571806A11 L/H

3511466A2580215170351-08080-043ACCESSORY MODULE CCCC COND COND

161501383899206A11 NO 2

38974439A258-0063770351-08080-045ACCESSORY MODULE CCCC COND COND

For use of this form, see DA PAM 738-751; the proponet agency is DCSLOGEDITION MAY 67 IS OBSOLETE

DA FORM 2408-16-E, OCT 91 AIRCRAFT COMPONENT HISTORICAL RECORD

h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






161501503311506A

34384185A265-0137970351-08100-076MAIN TRANSMISSIONMODULE

CCCC COND COND

161501230621806E #2

5871466A264-0114570351-08001-046INPUT MODULE CCCC COND COND

161501527817506E

05244A2641042370351-08001-050INPUT MODULE CCCC COND COND

168001074515206F

01466A0050100470357-06300-042INTERMEDIATE GEARBOX CCCC COND COND

161501376508906G01

8565067A0060365770358-06600-046TAIL ROTOR GEARBOXASSY

CCCC COND COND

161501524780506H04 RIGHT

04809C845-0185770361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501524780506H04 1

04457C8450404670361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501081277506H06 SECTION 1

3001466A2710040070361-03001-045SHAFT ASSY, T/R DRV SEC1

CCCC COND COND

161501158951706H08


CCCC COND COND

161501082650006H09 SECTION II #1

01466A2720126670361-05001-045SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501294167406H09 SECTION II #3

20561466A2720311270361-05001-050DRIVESHAFT ASSY SECTIII, IV, V

CCCC COND COND

161501158952206H09 SECTION II #2

24481466A2720103470361-05001-051SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501083295306H11

20803407A273-0032070361-05002-045SHAFT ASSY, T/R DRV SEC6

CCCC COND COND

161501158578806H12 SECTION IV


CCCC COND COND

432001207722807A01 #2

03622252169-CABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01 #1

03570K3767ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01

6954682254542ABR70652-02300-050PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

481001102247307B05A #1

03407125763213850-3-1VALVE, SOLENIOD CCCC COND COND

481001102247307B05A #2

0340787593213850-3-1VALVE, SOLENIOD CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






165001222431607B11

034078581817A3197170-5ACCUMULATOR CCCC COND COND

168001342049608B20 R/H

03407375070450-01043-124PANEL INDICATOR (PDU) CCCC COND COND

168001566036608F01

05067143030279-0302IVHMU (CBM MONITORSYSTEM)

CCCC COND COND

611501114969609A01 #1

034072356E70550-02031-111GENERATOR CCCC COND COND

611501114969609A01 #2

30444439528470550-02031-111GENERATOR CCCC COND COND

168001310225911C21

05380B9950156470400-02300-048MIXER ASSEMBLY CCCC COND COND

156001411515011D17 L/H O/B

05067F338-0335370209-22103-105SERVO BEAM FITTING CCCC COND COND

156001411515011D17 R/H O/B


156001411515011D17 R/H I/B


168001261204411D25 1

1427506739470400-06641-117STABILATOR ACTUATOR CCCC COND COND

168001261204411D25 2

18825067C292-0725770400-06641-117STABILATOR ACTUATOR CCCC COND COND

599601316274311D26

167644571284A70902-02001-048STABILATOR AMPLIFIER CCCC COND COND

599601316274311D26

27464840265970902-02001-048STABILATOR AMPLIFIER CCCC COND COND

299501169529115A04

300146675840148163290-100ENGINE SEQUENCINGUNIT

CCCC COND COND

584101245909219E05C

05067026BSM-C-967226INDICATOR HEIGHT CCCC COND COND

661001490516852A

046562614201825050-1-001AUTOMAT FLT CONTCOMPUTER

CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






SIGNIFICANT HISTORICAL EVENTS7.




kjigfdcbaRMVL HR RMVL HRS

NOMEN HRS)COMPO/HO/HLOCATIONNSNWUC

he (ACFTLIFESINCEPRESER NO.ANDAND

INST HRSP/N DUEREPLACE

INST HRSTIMENO.COMPONENTNOMENCLATURE

NOMEN REP.O/H OCOMP6.

4. SERIAL NUMBER3. PART NUMBER OR MODEL2. NSN 5. WUC1. NOMENCLATUR

Report Date:

TIME CHANGE COMPONENTS5/1110-Mar-2016

00

156001081924402C15J STA 649 - 50620000

UNK3506 0070209-06051-043TAIL PYLON FITTING 0020000

161501481695305A01A8007

M451P0252 500340770070-10046-055HUB, M/R ROTOR ASSY 005100

161501442692605A01I12351

A00105329 716506770102-08200-069MAIN ROTOR SPINDLEASSY

008000

161501442692605A01I12376


008000

161501442692605A01I12267


008000

161501442692605A01I12707

D00100066 360506770102-08200-069MAIN ROTOR SPINDLEASSY

008000

161501074515105A01L13984

C28600298 1482146670351-08186-043MAIN ROTOR SHAFTEXTENDER

0014000

161501127738805A01T13000

A23700224 4567456770107-08400-046BIFILAR, M/R ROTORASSY

0013000

161501113818805B0210751

A00902403 4316506770101-31000-043TAIL ROTOR BLADEASSY

0010000

161501113818805B0212131

A00905813 2936506770101-31000-043TAIL ROTOR BLADEASSY

0010000

161501083681206G01B12606

B25700127 4461506770102-11101-042O/B RETENTION PLATE(T/R)

0012000

156001129125607A24 PITCH17369

C11202043 698506770410-02500-049SAS ACTUATOR 0013000

156001129125607A24 YAW17719

C11206581 348506770410-02500-049SAS ACTUATOR 0013000

156001129125607A24 ROLL17363

C11206799 704506770410-02500-049SAS ACTUATOR 0013000

165001305695411C2511949

B30000463 4118506770410-06520-046SERVO ASSY, TAILROTOR

0011000

165001143122611D01 AFT28415

B30310873 10525067274000-1031MAIN ROTOR PRIMARYSERVO

0024400

165001143122611D01 FWD25176

B30303262 4291506770410-02820-054MAIN ROTOR PRIMARYSERVO

0024400

165001143122611D01 LAT26631

B30303985 2836506770410-02820-054MAIN ROTOR PRIMARYSERVO

0024400

156001158968511D0418380

34502770 0538070400-08102-045AFT BELLCRANK 0013000

For use of this form, see DA PAM 738-751; The proponet agency isDCSLOG

EDITION MAY 67 IS OBSOLETE

AIRCRAFT COMPONENT HISTORICALRECORD

DA FORM 2408-16-E, OCT 91


kjigfdcbaRMVL HR RMVL HRS

NOMEN HRS)COMPO/HO/HLOCATIONNSNWUC

he (ACFTLIFESINCEPRESER NO.ANDAND

INST HRSP/N DUEREPLACE

INST HRSTIMENO.COMPONENTNOMENCLATURE

NOMEN REP.O/H OCOMP6.

4. SERIAL NUMBER3. PART NUMBER OR MODEL2. NSN 5. WUC1. NOMENCLATUR

Report Date:

TIME CHANGE COMPONENTS6/1110-Mar-2016

00

156001164416111D0518054

A39100934 412146670400-08112-045AFT TIE ROD SUPTFITTING

0017000

168001164416011D065843

MM00269 0364370400-08111-042AFT TIE ROD ASSY 002200

156001286887011D075866

D39001110 0146670400-08117-049AFT BELLCRANK SPTASSY

004400

304001189971111D0810517

A38000866 3890340770400-08151-050LATERAL SWASHPLATELINK

0011000

168001221286311D0921184

F33701563 3625480970400-08166-041LATERAL SERVOBELLCRANK

0020000

168001158965311D1111000

346-00069 4567456770400-08104-048AFT WALKING BEAM 0011000

156001289269711D1318185

344-02074 0418570400-08115-046LEFT TIE ROD ASSY 0014000

156001296948611D146470

288-00169 0297070400-08114-051RIGHT TIE ROD ASSY 003500

168001158965211D1516120

J35500403 346146670400-08101-046FORWARD BELLCRANK 0015000

156001221261911D169785

B367-04064 0418570400-08162-042FWD BELLCRANK SPTASSY

005600

SIGNIFICANT HISTORICAL EVENTS7.

For use of this form, see DA PAM 738-751; The proponet agency isDCSLOG

EDITION MAY 67 IS OBSOLETE

AIRCRAFT COMPONENT HISTORICALRECORD

DA FORM 2408-16-E, OCT 91

ji kgfdcbaRMVL HRSRMVL HRSCOMPO/HNOMENWUC

HRS)O/HLOCATIONNSN

AND he SINCELIFE (ACFT

PREVSER NO. OAND

NOMENCLATURE PN TIMEINST HRS DUEREPLACE

INST HRSNO.COMPONENTNOMEN REP.O/H ORCOMP6.

1520010350266HELICOPTER,UTILITY

UH-60A 8023506 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 7 of 11

10-Mar-2016

999999

COND

156001113021502C12D

00TAIL CONE FITTING UNK350670219-05001-044 CCCC

20000 20000

1560010819244 STA 649 - 50602C15J

00TAIL PYLON FITTING UNK350670209-06051-043 00

999999

COND

162001231183103A01

3135380FWD FIXED GEARSHOCK

BEM248170250-12051-045 CCCC

999999

COND

162001231183103A01


BEM267270250-12051-045 CCCC

999999

COND

162001421089003B01

10715067SHOCK ABSORBER(TAIL)

K0020026170250-13101-044 CCCC

5100 8007

161501481695305A01A

5003407HUB, M/R ROTOR ASSY M451P025270070-10046-055 00

8000 12351

161501442692605A01I

7165067MAIN ROTOR SPINDLEASSY

A0010532970102-08200-069 00

8000 12376

161501442692605A01I


A0010810770102-08200-069 00

8000 12267

161501442692605A01I


A0010834370102-08200-069 00

8000 12707

161501442692605A01I


D0010006670102-08200-069 00

14000 13984

161501074515105A01L

14821466MAIN ROTOR SHAFTEXTENDER

C2860029870351-08186-043 00

13000 13000

161501127738805A01T

45674567BIFILAR, M/R ROTORASSY

A2370022470107-08400-046 00

999999

COND

1650012853024 RED05A01Z

5035067DAMPER ASSY, M/R R1060364070106-08100-046 CCCC

999999

COND

1650012853024 BLUE05A01Z

5615067DAMPER ASSY, M/R R1060419770106-08100-046 CCCC

999999

COND

1650012853024 YELLOW05A01Z

10605067DAMPER ASSY, M/R WG1060019770106-08100-046 CCCC

999999

COND

1650012853024 BLACK05A01Z

25455067DAMPER ASSY, M/R WG1060127270106-08100-046 CCCC

999999

COND

5315015374652 LAG BLUE05A02H

04457SOLID BLADE PIN B9410720070103-08108-041 CCCC

999999

COND

5315015374652 BLK LAG05A02H


999999

COND

5315015374652 BLUE LEAD05A02H


999999

COND

5315015374652 RED LAG05A02H


999999

COND

5315015374652 YEL LEAD05A02H


EDITION MAY 67 IS OBSOLETE For use of this form, see DA PAM 738-751; the proponet agency is DCSLOG

AIRCRAFT COMPONENT HISTORICAL RECORDDA FORM 2408-16 E, OCT 91


HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 8 of 11

10-Mar-2016

999999

COND

5315015374652 BLK LEAD05A02H


999999

COND

5315015374652 YEL LAG05A02H


999999

COND

5315015374652 RED LEAD05A02H


999999

COND

161501199764605A03A

35154185SWASHPLATE ASSY A107-0011770104-08000-050 CCCC

10000 10751

161501113818805B02

43165067TAIL ROTOR BLADEASSY

A0090240370101-31000-043 00

10000 12131

161501113818805B02

29365067TAIL ROTOR BLADEASSY

A0090581370101-31000-043 00

999999

COND

1615010785718 L/H06A11

3511466ACCESSORY MODULE A2580215170351-08080-043 CCCC

999999

COND

1615013838992 NO 206A11

38974439ACCESSORY MODULE A258-0063770351-08080-045 CCCC

999999

COND

161501503311506A

34384185MAIN TRANSMISSIONMODULE

A265-0137970351-08100-076 CCCC

999999

COND

1615012306218 #206E

5871466INPUT MODULE A264-0114570351-08001-046 CCCC

999999

COND

161501527817506E

05244INPUT MODULE A2641042370351-08001-050 CCCC

999999

COND

168001074515206F

01466INTERMEDIATEGEARBOX

A0050100470357-06300-042 CCCC

999999

COND

161501376508906G01

8565067TAIL ROTOR GEARBOXASSY

A0060365770358-06600-046 CCCC

12000 12606

161501083681206G01B

44615067O/B RETENTION PLATE(T/R)

B2570012770102-11101-042 00

999999

COND

1615015247805 RIGHT06H04

04809DRIVESHAFT ASSYENGINE

C845-0185770361-08014-041 CCCC

999999

COND

1615015247805 106H04

04457DRIVESHAFT ASSYENGINE

C8450404670361-08014-041 CCCC

999999

COND

1615010812775 SECTION 106H06

3001466SHAFT ASSY, T/R DRVSEC 1

A2710040070361-03001-045 CCCC

999999

COND

161501158951706H08


A2700112770361-03009-047 CCCC

999999

COND

1615010826500 SECTION II #106H09

01466SHAFT ASSY, T/R SEC3,4,5

A2720126670361-05001-045 CCCC

999999

COND

1615012941674 SECTION II #306H09

20561466DRIVESHAFT ASSY SECTIII, IV, V

A2720311270361-05001-050 CCCC

999999

COND

1615011589522 SECTION II #206H09

24481466SHAFT ASSY, T/R SEC3,4,5

A2720103470361-05001-051 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 9 of 11

10-Mar-2016

999999

COND

161501083295306H11


A273-0032070361-05002-045 CCCC

999999

COND

1615011585788 SECTION IV06H12


A2740191770361-06002-047 CCCC

2520 7587

414101329342806H23

25205067FAN AXIAL D5120137070361-03005-107 02

999999

COND

4320012077228 #207A01

03622PUMP MODULE ASSY,HYDRAUL

252169-CABR53023-06 CCCC

999999

COND

4320012077228 #107A01


K3767ABR53023-06 CCCC

999999

COND

432001207722807A01


254542ABR70652-02300-050 CCCC

13000 17369

1560011291256 PITCH07A24

6985067SAS ACTUATOR C1120204370410-02500-049 00

13000 17719

1560011291256 YAW07A24

3485067SAS ACTUATOR C1120658170410-02500-049 00

13000 17363

1560011291256 ROLL07A24

7045067SAS ACTUATOR C1120679970410-02500-049 00

999999

COND

4810011022473 #107B05A

03407VALVE, SOLENIOD 125763213850-3-1 CCCC

999999

COND

4810011022473 #207B05A

03407VALVE, SOLENIOD 87593213850-3-1 CCCC

999999

COND

165001222431607B11

03407ACCUMULATOR 8581817A3197170-5 CCCC

999999

COND

1680013420496 R/H08B20

03407PANEL INDICATOR (PDU) 375070450-01043-124 CCCC

99999 COND

168001566036608F01

05067IVHMU (CBM MONITORSYSTEM)

143030279-0302 CCCC

999999

COND

6115011149696 #109A01

03407GENERATOR 2356E70550-02031-111 CCCC

999999

COND

6115011149696 #209A01

30444439GENERATOR 528470550-02031-111 CCCC

999999

COND

168001310225911C21

05380MIXER ASSEMBLY B9950156470400-02300-048 CCCC

2160 6617

161501141753211C23

9664457TAIL ROTOR PITCHCHANGE SHAFT

2330382870400-06100-042 01

11000 11949

165001305695411C25

41185067SERVO ASSY, TAILROTOR

B3000046370410-06520-046 00

24400 28415

1650011431226 AFT11D01

10525067MAIN ROTOR PRIMARYSERVO

B30310873274000-1031 00

24400 25176

1650011431226 FWD11D01


B3030326270410-02820-054 00




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 10 of 11

10-Mar-2016

24400 26631

1650011431226 LAT11D01


B3030398570410-02820-054 00

13000 18380

156001158968511D04

05380AFT BELLCRANK 3450277070400-08102-045 00

17000 18054

156001164416111D05

4121466AFT TIE ROD SUPTFITTING

A3910093470400-08112-045 00

2200 5843

168001164416011D06

03643AFT TIE ROD ASSY MM0026970400-08111-042 00

4400 5866

156001286887011D07

01466AFT BELLCRANK SPTASSY

D3900111070400-08117-049 00

11000 10517

304001189971111D08

38903407LATERAL SWASHPLATELINK

A3800086670400-08151-050 00

20000 21184

168001221286311D09

36254809LATERAL SERVOBELLCRANK

F3370156370400-08166-041 00

11000 11000

168001158965311D11

45674567AFT WALKING BEAM 346-0006970400-08104-048 00

14000 18185

156001289269711D13

04185LEFT TIE ROD ASSY 344-0207470400-08115-046 00

3500 6470

156001296948611D14

02970RIGHT TIE ROD ASSY 288-0016970400-08114-051 00

15000 16120

168001158965211D15

3461466FORWARD BELLCRANK J3550040370400-08101-046 00

5600 9785

156001221261911D16

04185FWD BELLCRANK SPTASSY

B367-0406470400-08162-042 00

999999

COND

1560014115150 L/H O/B11D17

05067SERVO BEAM FITTING F338-0335370209-22103-105 CCCC

999999

COND

1560014115150 R/H O/B11D17


999999

COND

1560014115150 R/H I/B11D17


999999

COND

1680012612044 111D25

14275067STABILATOR ACTUATOR 39470400-06641-117 CCCC

999999

COND

1680012612044 211D25

18825067STABILATOR ACTUATOR C292-0725770400-06641-117 CCCC

999999

COND

599601316274311D26

16764457STABILATOR AMPLIFIER 1284A70902-02001-048 CCCC

999999

COND

599601316274311D26

27464840STABILATOR AMPLIFIER 265970902-02001-048 CCCC

999999

COND

299501169529115A04

3001466ENGINE SEQUENCINGUNIT

75840148163290-100 CCCC

999999

COND

584101245909219E05C

05067INDICATOR HEIGHT 026BSM-C-967226 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 11 of 11

10-Mar-2016

999999

COND

661001490516852A

04656AUTOMAT FLT CONTCOMPUTER

2614201825050-1-001 CCCC

7. SIGNIFICANT HISTORICAL DATA



09-Mar-2016

T700-GE-700ENGINE ASSY, TURBINE

ALT ETFACT TTV°CTIMENUMBERNG %PRESSFATENGINESERIAL 866 +/- 49. TORQUE10.8.7.6.AIRCRAFT REMARKS11. TGTDATE 12.5.4.

GE-E-307027

3. ENGINE SERIAL NUMBER2. ENGINE MODEL1. NOMENCLATUREReport Date: Page 1 of 1

14-Sep-2006 8023506 (NO REMARKS)2500 106 97 197.7203852 847

14-Sep-2006 8023506 POST PHASE/ENG INST2500 106 97 197.7203852 847

29-Sep-2007 8023506 POST PMI HIRSS INST8800 95 89 199.363029 847

23-Sep-2008 8023506 REINSTALLATION-BAFFLESINSTALLED

4500 99 101 0.9897.2162803 846

23-Mar-2010 8023506 BASELINE FROM PMI6000 110 105 199.9104604 843

09-Feb-2011 8023506 MAX POWER FOR ENGINEREPLACEMENT. PTUMIDOLSKY, AASF 2,OHIO NATIONAL GUARD

6000 107 103 196-134852 820

28-Feb-2014 8023506 TGT LIMITER AND MAXPOWER HAD TO BECONDUCTED SEPARATELYDUE TO NG LIMITING

6000 106 101 198.8-185186 809

For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

T700 SERIES TURBINE ENGINE ANALYSIS CHECK RECORDDA FORM 2408-19-2 E, DEC 91


HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM2481 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-Mar-2016

9000 14067

NSN PENDING03A01A

00PISTON MAIN L/GEARSTR

BEM299170250-12065-102 RCRC


