DA Form 2408-5 - Equipment Modification RecordNSN 1520-01-298-4532) MWO:1-1520-237-50-84 Priority Mnt Level 25-Jan-2007 R D USAACE 80 01-May-2012 MODIFICATION INSTRUCTIONS FOR THE

PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN

8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.

8724673EH-60AHELICOPTER, UTILITY

3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE

Report Date: Page 1 of 404-Aug-2016

DR21-Jun-2004

(NOORGANIZATION/PID)

0MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE AN/APX-118 TRANSPONDER MODE STRANSPONDER (CXP) ON UH-60A/LAIRCRAFT (NSN 1520-01-035-0266)(NSN 1520-01-298-4532)

1-1520-237-50-84MWO:

Mnt LevelPriority

DR25-Jan-2007

USAACE 8001-May-2012

MODIFICATION INSTRUCTIONS FORTHE DUAL INSTALLATION OFATTITUDE HEADING REFERENCEUNITS (AHRU) ON THE UH-60A/L, HH-60A, AND HH-60L HELICOPTER (NSN1520-01-035-0266) (EIC: RSA) (NSN1520-01-298-4532) (EIC: RSM) (NSN1520-01-471-6743) (EIC: NA) (NSN 1520-01-459-9468) (EIC: NA)

1-1520-237-20-94MWO:

Mnt LevelPriority

DN01-Mar-1989

DYNCORP OLRFT. HOOD,TX(H.KNIGHT)

41601-SEP-1993

INCORPORATION OF IMPROVEDTIEDOWN FITTINGS

1-1520-237-50-53MWO:

Mnt LevelPriority

DN01-Aug-1991

SIKORSKY(DANIEL LEE)

402-MAR-1989

STAB GROUNDING STRAP55-1520-237-50-54MWO:Mnt LevelPriority

DR01-Jun-1999

MANTECH(JAMES LYTLE)

1003-MAY-1999

CONVERSION OF EH-60AENVIRONMENTAL CONTROL SYSTEM(ECS) AIR CONDITIONINGREFRIGERANT FROM FREON 500 TOR134A

1-1520-237-50-80MWO:

Mnt LevelPriority

KR13-Apr-2001

USAAVNC(TB1027)

9004-JAN-2004

SEALED LEAD ACID BATTERY (SLAB)SYSTEM AND RELOCATION OFUTILITY LIGHT POWER

1-1520-237-50-77MWO:

Mnt LevelPriority

DN01-May-1994

LSSI/OLR HAAF,GA. 31409(R.LEWIS LSSI 425QC CFT)

9805-MAY-1995

INCORPORATION OF IMPROVED FIREEXTINGUISHER CIRCUIT ANDHELLFIRE CONNECTOR (UH-60 A/LAND EH-60A)

1-1520-237-50-66MWO:

Mnt LevelPriority

DR11-Aug-2000

DYNCORP OLRFT. HOODTX(JL8143)

606-JUL-1999

INSTALLATION OF THEPILOT/COPILOT SEATS MA-16(IMPROVED) INERTIA REEL IN ALL UH-60 HELICOPTERS

1-1520-237-50-79MWO:

Mnt LevelPriority

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

DA FORM 2408-5 E, OCT 91 EQUIPMENT MODIFICATION RECORD

PIDMWODATE HRS






DN24-Aug-1992

CECOM(L.MEDINA)

3207-APR-1994

MODIFICATION OFCOUNTERMEASURE SYSTEMS,SPECIAL PURPOSE AN/ALQ151(V)2

32-5865-012-55-2MWO:

Mnt LevelPriority

DR15-Jul-1985

LSSI/OLR(P/C/WLSSI390 CFT)

1212-OCT-1993

MODIFICATION OF DIRECTIONALCONTROL CABLE SYSTEM (UH-60A &EH-60A HELICOPTERS) NATIONALSTOCK NUMBER (NSN) 1520-01-035-0266 & 1520-01-082-0686

55-1520-237-50-34MWO:

Mnt LevelPriority

DN09-Jun-1988

PCW(UNKNOWN)

013-DEC-1989

INCORPORATION OF STABILATORAMPLIFIER IMPROVEMENTS(INCLUDES MODIFICATION OFSTABILIZATION TEST SET) (UH-60AHELICOPTERS)

55-1520-237-50-42MWO:

Mnt LevelPriority

DN23-Jan-1989

PCW(UNKNOWN)

013-DEC-1989

MODIFICATION OF MAIN ROTOR HEADANTI-FLAP BRACKETS (UH-60A ANDEH-60A HELICOPTERS)

55-1520-237-50-44MWO:

Mnt LevelPriority

DN17-Jan-1989

PCW(UNKNOWN)

013-DEC-1989

MODIFICATION OF BEARINGRETAINER SPRING CLIP, TAIL ROTORSERVO (UH/EH-60A HELICOPTERS)

55-1520-237-50-52MWO:

Mnt LevelPriority

DN15-Jan-1991

DYNCORP (OLR)FT. HOOD, TX(H.KNIGHT)

813-JUL-1993

INCORPORATION OF ENGINE DRIVESHAFT BALANCING PROCEDURE (UH-60A/EH-60A HELICOPTERS)

55-1520-237-50-58MWO:

Mnt LevelPriority

DN01-Feb-1993

DYNCORP OLRFT. HOOD,TX.(H. KIGLER)

41613-JUL-1993

INSTALLATION OF THE AN/ARC-201SINCGARS AND TSEC KY-58ENCODER/DECODER UNITS IN THEEH-60A QUICK FIX HELICOPTER

1-1520-237-50-67MWO:

Mnt LevelPriority

DM22-Feb-1991


83.213-JUL-1993

INCORPORATE ELECTRO-MAGNETICENVIRONMENT (EME) PROTECTIONPROVISIONS ON DELIVERED UH-60A/LAND EH-60A HELICOPTERS

1-1520-237-50-59MWO:

Mnt LevelPriority

DN15-Nov-1990


613-JUL-1993

INSTALLATION OF IMPROVEDTIEDOWN RING EYEBOLT (UH-60A/LAND EH-60A)

1-1520-237-50-61MWO:

Mnt LevelPriority



PIDMWODATE HRS






DM01-Sep-1991

DYNCORP OLRFT. HOOD,TX.(H. KIGLER)

213-JUL-1993

IMPROVED ENGINE COWLINGRELEASE HANDLE ASSEMBLY

1-1520-237-50-64MWO:

Mnt LevelPriority

DN30-Jun-2004

USAACE, FT.RUCKER,AL(AFS431)

1614-AUG-2009

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE DOPPLERGPS NAVIGATION SET (DGNS)

1-1520-237-50-92MWO:

Mnt LevelPriority

DN31-Oct-1996

DYNCORP FHSDFT. HOOD,TX(IMAD)

3517-MAR-1998

INSTALLATION OF REDUCEDDIAMETER BALLISTIC TOLERANTFUEL LINES (UH-60A/L AND EH-60AHELICOPTERS)

1-1520-237-50-74MWO:

Mnt LevelPriority

DN15-Jan-1989

LSMSC(UNKNOWN)

1217-OCT-1989

INCORPORATION OFELECTROMAGENTIC INTERFERENCE(EMI) PROTECTION FOR LEFT ANDRIGHT RELAY PANELS (UH-60A/EH-60A HELICOPTERS)

1-5945-237-50-1MWO:

Mnt LevelPriority

FR02-Nov-2009

USAACE 218-Dec-2013

SINGLE INSTALLATION OF ATTITUDEHEADING REFERENCE UNIO (AHRU)

1-1520-237-20-2MWO:

Mnt LevelPriority

DU31-May-1995

LM2/OLR HAAF,GA. 31409(LMQ080 CFT)

2420-SEP-1995

MODIFICATION OF THE ENGINE TRIMBALANCE HARDWARE (EH/UH-60AAND UH-60L HELICOPTERS)

1-1520-237-50-73MWO:

Mnt LevelPriority

DN30-Apr-1997

DYNCORPKILLEN,TX(LM2968)

5225-SEP-2000

INSTALLATION OF THE AVIATOR'SNIGHT VISION IMAGING SYSTEM(ANVIS) LIGHTING UPDATE EH/UH-60A/L

1-1520-237-50-56MWO:

Mnt LevelPriority

DN01-Oct-1988

TRACORAEROSPACE(JAMES L.HICKORAY)

1026-SEP-1989

EH-60A INSTALLATION OF AFCSINLINE FILDER

55-1520-237-55-6MWO:

Mnt LevelPriority

DR27-Apr-1998

DYNCORPKILLEN,TX(UNKNOWN)

027-APR-2000

MODIFICATION OF THE UH/EH/HH-60HELICOPTER AUXILIARY FUELMANAGEMENT SYSTEM EXTERNALSTORES SUPPORT SYSTEM(INDICATOR KIT NSN 1615-01-451-8200) AND EXTENDED RANGE FUELSYSTEM (PROBE KIT NSN 1615-01-451-8207)

1-1520-237-50-78MWO:

Mnt LevelPriority



PIDMWODATE HRS






DU10-Aug-1987

PCW VERIFIEDDYNCOPR FT.HOOD(J.MORROW)

629-AUG-1994

INCORPORATION OF STABILATORSLEW-UP SWITCH (UH-60AHELICOPTER)

55-1520-237-50-46MWO:

Mnt LevelPriority

DR03-Dec-2005

USAACE, FT.RUCKER, AL(MB1137)

12029-Mar-2010

INSTALLATION OF ELECTRONIC DATAMANAGEMENT (EDM) SYSTEM FORBLUE FORCE TRACKING

1-1520-237-50-EDMMWO:

Mnt LevelPriority

DR05-Jan-2010

CSC, USAACE,FT. RUCKER, AL.(MB1137)

12030-Apr-2010

INSTALLATION OF BLUE FORCETRACKING (BFT) ON EH60HELICOPTERS

EH-60-001MWO:

Mnt LevelPriority

DR01-Jul-2008

CSC, USAACE,FT. RUCKER, AL(LW2720)

3030-Apr-2010

INSTALLATION OF ELECTRONIC DATAMANAGEMENT SYSTEM (EDM) FORBLUE FORCE TRACKING (BFT)

RSN LSF01106MWO:

Mnt LevelPriority



NUMBERLOCATIONPIDENTRYORGANIZATION

8.7.DATE

6.REMARKS

4. 5.

EH-60A 8724673HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL


SIKORSKY AIRCRAFTAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-0003REV. E. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A. AFT CONTROL SERVOINPUT ROD HAS BEEN LENGTHENED1/2 TURN.B. LATERAL CONTROL SERVO INPUT RODHAS BEEN SHORTENED 1/4 TURN. C.FORWARD CONTROL INPUT ROD HAS BEENSHRTENED 1/2 TURN. NOTE: WHEN AIRCRAFTRIGGING IS BIASED, RIGGING PIN HOLES ARETEMPORIARILY LOST AT THE ABOVE 3POINTS. (SMITH)

08-Jul-1988 1

STRATFORD, CT

TL026629

SIKORSKY AIRCRAFTAIRCRAFT GOVNMENT FLIGHT ACCEPTED ONTHIS DATE (BRENDA WALSH)

18-Aug-1988 1

STRATFORD, CT

TL026629

SIKORSKY AIRCRAFTS.O.F. MSG. UH-60A-87-12-ONE TIMEINSPECTION OF DEFECTIVE T700-GE-700/701ENGINE POWER TURBINE MODULESCOMPLIED WITH (SMITH)

22-Aug-1988 1

STRATFORD, CT

TL026629

SIKORSKY AIRCRAFTS.OF. MSG. UH-60A-88-07 REVISIONS TO S.O.F.UH-60A-88-05 CONCERNING OPERATINGTIME/START CALCULATIONS AND FORMSINFORMATION COMPLIED WITH (SMITH)

22-Aug-1988 2

STRATFORD, CT

TL026629

SIKORSKY AIRCRAFTS.O.F. MSG. GEN-88-02-ONE TIME INSPECTIONFOR INSTALLATION OF CORRECT INTERNALPORTABLE FIRE EXTINGUISHER COMPLIEDWITH (BRENDA WALSH)

22-Sep-1988 1

STRATFORD, CT

TL026629

AVCRAD FATSOF MSG#UH-60-88-01 ONE TIME INSP OF TAILROTOR BLADES FOR PROPER SERIALNUMBERS C/W AT 33.2 ACFT HRS (THAOMASCALLL)

16-Nov-1988 1

CA

TL026629

AVCRAD FATSOF MSG#UH60-88-09 ONE TIME INSP OF ARAMANUFACTURED SEATS FOR LOOSE CLEVISSCREWS C.W AT 33.2 ACFT HRS (THOMASCALL)

16-Nov-1988 2

CA

TL026629

AVCRAD FATSOF MSG#UH60-88-13--ONE TIME INSP OFMAIN ROTOR BLADE RETAINING PINS FORBROKEN OR MISSING SEGMENTS C/W AT 33.2ACFT HRS (THOMAS CALL)

14-Dec-1988 1

CA

TL026629

TFSI MOJAVEUH-60-89-01 ONE TIME INSPECTION OF T700-GE-700 ENGINE GAS GENERATOR STATORSHROUDS C/W @ 35.6 HRS EH-60 MAINTSUPERVISOR. (UNKNOWN)

14-Feb-1989 1

MOJAVE AIRPORTMOJAVE

TL026629

TFSICORRECTION TO 89-01--ONE TIME INSP OFT700 ENG GAS GENERATOR STATORSHROUDS C/W 35.6 HRS EH-60 MAINTSUPERVISOR (UNKNOWN)

17-Feb-1989 1

MOJAVE AIRPORT

TL026629

TFSIUH-60-89-03---ONE TIME INSPECTION OF ALLMAIN ROTOR SPINDLES. ALL PART NUMBERSC/W @ 65.8 HRS EH-60 MAINT SUPERVISOR(UNKNOWN)

03-Apr-1989 1

MOJAVE AIRPORT,MOJAVE, CA

TL026629

USAICSSOF UH-60-89-05 ONETIME INSP OF WIRESTRIKE PROTECTION SYSTEM C/W ON19JUN89 AT119.6 ACFT HRS (UNKNOWN/LW2720 R CLERK)

20-Jun-1989 1

FT. HUACHUCA, AZ

TL026629

For use of this form, see DA PAM 738-751; the proponent agency is DCSLOGEDITION OF JAN 64 IS OBSOLETEHISTORICAL RECORD FOR AIRCRAFTDA FORM 2408-15 E, OCT 91


8.7.DATE

6.REMARKS

4. 5.



USAICSSOF MSG UH-60-89-06 ONETIME INSP OF LEFTAND RIGHT HAND RELAY PANELS C/W ON 19JULY 89 AT 121.4 ACFT HRS(UNKNOWN/LW2720 R CLERK)

20-Jul-1989 1

FT. HUACHUCA, AZ

TL026629

USAICSSOF MSG UH-60-89-08 ONETIME INSP OF FUELBOOST PUMP ATTACHMENT C/W ON 16 AUG89 AT 122.1 ACFT HRS (UNKNOWN/LW2720 RCLERK)

20-Aug-1989 1

FT. HUACHUCA

TL026629

USAICSMSG UH-60-89-09 CHANGE 10 TO TB 55-1520-237-20-104 C/W ON 21 AUG 89 AT 122.1 ACFTHRS. (UNKNOWN/LW2720 R/ CLERK)

24-Aug-1989 1

FT. HUACHUCA, AZ

TL026629

USAICSSOF MSG UH-60-89-10 ONETIME INSP OF T700-GE-700 ENGINE RG ROTOR AND STATORSC/W ON 26 SEPT 89 AT 159.3 ACFT HRS(UNKNOWN/LW2720 R CLERK)

04-Oct-1989 1

FT. HUACHUCA, AZ

TL026629

DCO 5TH AVN REGTSOF MSG UH/EH-60A-89-11 AND 89-12ONETIME INSP OF MAIN MODULE OIL COOLERBLOWER COMPLETED (DON GREEN)

28-Nov-1989 1

FT. POLK, LA

TL026629

AVSCOM OCM SECOCM/ACE PERFORMED AT 0198 A/C HRS ATFT. POLK, LA BY ACE TEAM MEMBER P(UNKNOWN/ LW2720 R CLERK)

19-Dec-1989 1

ST. LOUIS, MO

TL026629

LSSIDF ANTENNA HOUSING INSULATORSREPLACED WITH P/N 1951-1-4116-4 TOCOMPLY WITH AWR DTD 21 SEP 89(UNKNOWN/LW2720 R/CLERK)

26-Apr-1990 1

FT. RUCKER, AL

TL026629

LSSITB 55-1520-20-111 ONE TIME INSP OF UPPERPRESSURE PLATE BOLSTS, O/N 76683-8-12AND SPINDLE TO HUG ATTACHMENT BOLTSP/N 76683-8-10 C/W ON AUG 90 AT 214.2 ACFTHRS (LANDFORD)

03-Aug-1990 1

FT. RUCKE,R AL

TL026629

AVSCOMOCM/ACE PERFORMED AT 0255 A.C. HRS. ATFT POLK LA BY ACE TEAM MEMBEREASTMAN AVSCOM OCMSEC (EASTMAN)

30-Oct-1990 1

ST. LOUIS , MO

TL026629

D CO 5TH AVN REGTUH-60-91-ASAM-01 (TB55-1520-237-20-119)ONE TIME REPLACEMENT AND 30 HRSPECIAL INSP OF T/R PITCH BEAM RETAININGWASHER DUE BEFORE 17 MARCH 91COMPLETED 12 MAR 91 (UNKNOWN/LW2720 RCLERK)

18-Dec-1990 1

FT. POLK, LA

TL026629

3/5 AVN REGTUH-60-91-ASAM-06 (TB1-1520-237-20-124) ONETIME INSP OF LARGO HOOK INTERNAL WIREBUNDLE ROATING DOES NTO PERTAIN TOTHIS ACPT LARGO HOOK NOT INSTALLED @(DON GREEN)

18-Mar-1991 1

FT. POLK, LA

TL026629

AVSCOMOCM/ACE PERFORMED AT 329 HRS AT FTPOLK, LA BY ACE TEAM MEMBER PARKERAVSCOM, OCMSEC, ST. LOUIS, MO (PARKER)

16-Oct-1991 1

ST. LOUIS, MO

TL026629

3/5 AVN REGTUPON REVIEW OF THESE RECORDS THEFOLLOWING ASAM MSG'S WERE NOTRECORDED, RECORDED AS OF THIS DATE(PERZ)

15-Jan-1992 1

FT. POLK, LA

TL026629

3/5 AVN REGTUH-60-91-ASAM-02 (TB55-1520-237-20-120) ALLH-60 ACFT INVOLVED IN OPERATION DESERTSHIELD. RECURRING INSP OF M/R BLADE TIPCAPS (PERZ)

15-Jan-1992 2

FT. POLK, LA

TL026629



8.7.DATE

6.REMARKS

4. 5.



3/5 AVN REGTGEN-60-91-ASAM-03 ALL EH-60A/EH-1H/OH-581 AUTHORIZATION FOR INSTALLATION ANDUSING CRYPTOGRAPHIC COMPUTER KIT 1C(PERZ)

15-Jan-1992 3

FT. POLK, LA

TL026629

3/5 AVN REGTUH-60-91-ASAM-04 (TB 1-55-1520-237-23-123)OPERATION IN SWA (DESERT STORM) TOPROVIDE GUIDANCE FOR SITUATIONSREQUIRING EXCEEDING THE RETIREMENT(FINITE LIFE OF CERTAIN COMPONENTS(PERZ)

15-Jan-1992 4

FT. POLK

TL026629

3/5 AVN REGTUH-60-91-ASAM-07 ALL UH-60/EH-60/UH-60LSERIES ACFT ADVANCE NOTIFICATION OFMANUAL CHANGES CONCERNING MAINTRANSMISSION MODULES (PAERZ)

15-Jan-1992 5

FT. POLK, LA

TL026629

3/5 AVN REGTUH-60-91-ASAM-08 (TB1-1520-237-20-125) ALLH-60 SERIES ACFT, ONE TIME INSP OF FIREEXTINGUISHING SYSTEM (PERZ)

15-Jan-1992 6

FT. POLK, LA

TL026629

3/5 AVN REGTUH-60-91-ASAM-03 (TB55-1500-200-30-1)EXTENDED TBO HOURS UNDER DESERTSHIELD OPS FOR H-60 A/L OIL COOLERBLOWER & T/R P/C SHAFT BEARINGS (PERZ)

15-Jan-1992 7

FT. POLK, LA

TL026629

3/5 AVN REGTUH-60-91-ASAM-09 (TB1-1520-237-20-126) ALLH-60 SERIES ACFT CHANGES TO INSPPROCEDURES FOR M/R ELASTOMERICBEARINGS (PERZ)

15-Jan-1992 8

FT. POLK, LA

TL026629

3/5 AVN REGTUH-60-91-ASAM-10 (TB1-1520-237-20-127) ONETIME INSP AND REPLACEMENT OF MAINLANDING GEAR BRAKE ASSY PISTONINSULATOR (PERZ)

15-Jan-1992 9

FT. POLK, LA

TL026629

3/5 AVN REGT FT.UH-60-91-ASAM-11 ALL H-60 SERIES ACFT,REQUIREMENT TO OPERATE WITH BOOSTPUMPS ON WHILE BURINING JP(UNKNOWN/LW2720 R/CLERK)

15-Jan-1992 10

POLK, LA

TL026629

3/5 AVN REGTUH-60-92-ASAM-01 (TB1-1520-237-20-128) ALLH-60 SERIES ACFT INSP FOR THREEUNSERVICEABLE SPINDLE ASSEMBLIES(UH60-92-ASAM-001) (RUBY)

15-Jan-1992 11

POLK, LA

TL026629

AVVM CO 3/5 AVN REGTUH-60-92-ASAM-02 (TB1-1520-237-20-132) ONETIME INSP FOR ENGINE OUTPUT SHAFT BOLTTORQUE AND VIBRATION LEVEL DOES NOTPERTAIN TO THIS ACFT (POWELL)

14-May-1992 1

POLK, LA

TL026629

DCO 5TH AVN REGTUH-60-92-ASAM-03 T700-GE-700 GASGENERATOR ROTOR TURBINE BLADEFAILURES ENGINE CLEANING, ENGINE LIFELIMITED COMPONENTS TRACKING ANDSINGLE ENGINE FLIGHT PLANNINGPROCEDURES RECEIVED ASAM (SMITH)

10-Jun-1992 1

FT. POLK, LA

TL026629

DCO 5TH AVN REGTUH-60-92-ASAM-04 USE OF RECOVERY.RECYCLE EQUIPMENT ON AIR-CONDITIONINGOR REFRIGERANT SYSTEMS THAT USECHLOROFLUOROCERBONS RECEIVED ASAM(SMITH)

19-Jun-1992 1

FT. POLK,LA

TL026629



8.7.DATE

6.REMARKS

4. 5.



AVM 3/5 AVN REGTUH-60-92-ASAM-05 (TB1-1520-237-20-130)INSPECTION AND REPLACEMENT OF MAINROTOR BLADE PINS COMPLETED 21 OCT 1992@ 498 ACFT (POWELL)

09-Sep-1992 1

FT. POLK, LA

TL026629

AVN3/5UH-60-92-ASAM-06 ALL H-60 ARMY ACFT, ONETIME INSP FOR PROPER HARDWARE ON THEPEDAL ADJUSTER ASSY (TB1-1520-237-20-134) ENTERED ON PA FORM 2408-13 25 SEPT1992 (POWELL)

02-Oct-1992 1

FT. POLK,LA

TL026629

AVUM 3/5 AVN REGTUH-60-93-ASAM-01 ONETIME CK OFTRANSMISSION AND GEARBOX CHIPDETECTOR SYSTEM (TB1-1520-237-20-135)ENTERED ON DA FORM 2408-13- 13-OCT-1992(POWELL)

10-Oct-1992 1

FT. POLK, LA

TL026629

AVUM CO 3/5UH-60-93-ASAM-02 INFORMATIONAL ALL H-60A ACFT T700-GE-700 GAS GENERATORROTOR TURBINE BLADE FAILURE ENGINECLEANING AND SINGLE ENGINE FLTPLANNING PROCEDURE (POWELL)

20-Oct-1992 1

FT. POLK, LA

TL026629

AVSCOMOCM/ACE PERFORMED AT 0498 A/C HRS ATFT. POLK, LA BY ACE TEAM MEMBER SONSHIOEDRER AVSCOM OCM SEC. ST. LOUIS,NO (SHROEDER)

09-Nov-1992 1

FT. POLK, LA

TL026629

SCO 3/5 AVN REGTUH-60-93-ASAM-03 REVISION TO UH-60-92-ASAM-05, INSP/ REPLACEMENT M/R BLADEEXPANDABLE PINS (POWELL)

09-Dec-1992 1

FT. POLK, LA

TL026629

D CO3/5 AVN REGTUH-60-93-ASAM-04, REVISION TO UH-60-92-ASAM-06, ONE TIME INSP FOR PROPERHARDWARE PEDAL ADJUSTER (POWELL)

09-Dec-1992 2

FT. POLK, LA

TL026629

B CO 3/502 AVNUH-60-93-ASAM-05, INFORMATIONAL, ONETIME INSP. FOR TAIL DRIVE SHAFT VISCOUSDAMPER BEARINGS (POWELL)

29-Dec-1992 1

FT. POLK, LA

TL026629

B CO 3/502 AVNUH-60-93-ASAM-06, ONE TIME INSPECTION TOREMOVE SUSPECT TAIL ROTOR PITCHBEAMS (POWELL)

29-Dec-1992 2

FT. POLK, LA

TL026629

B CO 3/502 AVNUH-60-93-ASAM-07,INFORMATIONAL,REVISION OF CORROSION LIMITS FOR TAILROTOR GEARBOX SERVO MOUNTING BORE(POWELL)

06-Jan-1993 1

FT. POLK, LA

TL026629

B CO 3/502 AVNPMS-2 COMPLETED 29 JAN 1993 @ 498.2ACFT. HRS (POWELL)

29-Jan-1993 1

FT. POLK, LA

TL026629

B CO 3/502 AVNUH-60-93-ASAM-09-ONE TIME INSP, TODETERMINE COMPLIANCE WITH SYSTEMMWO'S (UNKNOWN/LW2720 R/CLERK)

07-Apr-1993 1

FT. POLK, LA

TL026629

B CO 3/502 AVNUH-60-93-ASAM-10 INE TIME INSP ANDRECURRING INSP/CLEANING OF EXTERNALSTORES SUPPORT SYSTEM (UNKNOWN/LW2720 R/ CLERK)

08-Apr-1993 1

FT. POLK, LA

TL026629

B CO 3/502 AVNUH-60-93-01 SOF, ONE TIME INSP OF T700-GE-701C ENG FUEL HOSE ASSY (UNKNOWN/LW2720 R/ CLERK)

13-Apr-1993 1

FT. POLK, LA

TL026629



8.7.DATE

6.REMARKS

4. 5.



B CO 3/502 AVNUH-60-93-02-SOF ONE TIME INSP OF T700-GE-701C ENG. FUEL HOSE ASSY FORADDITIONAL SERIAL NUMBERS (UNKNOWN/LW2720 R / CLERK)

13-Apr-1993 2

FT. POLK, LA

TL026629

B CO 3/502 AVNUH-60-93-ASAM-11 INSP AND REPLACE ARACREW RESTRAINT, BUCKLE CROTCH ASSYTO UH-60-93-ASAM-12 ABRUPT CHANGE INMAIN ROTOR TRACK/VIBRATIONS (POWELL)

29-Apr-1993 1

FT. POLK, LA

TL026629

B CO 3/502 AVNUH-60-93-ASMA-13 ACFT WITH ESSS/ ERFSKITS (UNKNOWN / LW2720 R/ CLERK)

10-Jun-1993 1

FT. POLK, LA

TL026629

B CO 3/502 AVNUH-60-93-ASAM-08, BIAS TAIL ROTORRIGGING 3 DEGREES, READING SHORT 422/64, LONG 5 2/64 (UNKNOWN/ LW2720R/CLERK)

21-Jun-1993 1

FT. POLK, LA

TL026629

B CO 3/502 AVNUH-60-93-ASAM-14 INSP OF ACFTW/ESSS/ERFS KITS (UNKNOWN/ LW2720R/CLERK)

25-Jun-1993 1

FT. POLK, LA

TL026629

B CO 3/502 AVNUH-60-93-ASAM-15. REVISION TO UH-60-93-ASAM-14 (UNKNOWN / LW2720 R/ CLERK)

25-Jun-1993 2

FT. POLK, LA

TL026629

DYNCORP PROJECTOLR

UH-60-93-ASAM-16 (TB1-1520-237-20-146) ONETIME INSP OF HYD. PUMP MODULE (PN 70652-02300-050) KNURLED BLEED/RELEIF KNOBSECURING C/W 10 AUG 1993 AT 598.9AIRCRAFT HOURS (KNIGHT)

10-Aug-1993 1

FT. HOOD, TX

TL026629

C CO 4502 AVNUH-60-94-ASAM-01 UH/EH/MH-60 SERIES ACFTNVG COMPATIBILITY REWORK OF MASTERWARNING PANEL ASSY (KNIGHT)

08-Dec-1993 1

FT. HOOD TX

TL026629

CCO 2/502 AVNUH-60-94-ASAM-03 ONE TIME RERURBISHMENT OF MAIN ROTOR SPINDLE,AND REPLACEMENT OF CERTAIN MAINROTOR THRUST BEARINGS (UNKNOWN/LW2720 R/ CLERK)

19-Jan-1994 1

FT. HOOD TX

TL026629

C CO 4502 AVNUH-60-94-ASAM-02 RETURN FOR EXCHANGEOF CERTAIN (ARA) PN 04495-28MANUFACUTRED BUCKLEWORK STRAPASSEMBLIES (KNIGHT)

19-Jan-1994 2

FT. HOOD TX

TL026629

CCO 2/502 AVNUH-60-94-ASAM--04 REISS OF ONE TIMEINSPECTION TO REMOVE SUSPECT TAILROTOR PITCH BEAM (UNKNOWN/ LW2720R/CLERK)

07-Feb-1994 1

FT. HOOD TX

TL026629

CCO 2/502 AVNUH-60-94-ASAM-05 ONE TIME REMOVAL OFTAIL ------------ WITH TAIL GEARBOX OUTPUTSHAFT PN 7035006620100 FOR REWORK(BAIN)

09-Feb-1994 1

FT. HOOD TX

TL026629

CCO 2/502 AVNUH-60-94-ASAM-06 COCKPIT STANDARZATIONOF PILOT AND CO-PILOT RESTAINT RELEASESYSTEMS I.D. MIX MATCH RESTRAINTRELEASE SYSTEM (BONNER)

09-Feb-1994 2

FT. HOOD, TX

TL026629

OCM SECTION.OCM/ACE PERFORMED AT 629 AC HRS AT FTHOOD, TX (UNKNOWN/ LW2720 R/ CLERK)

28-Feb-1994 1

ST. LOUIS, MO

TL026629

C CO 2/502 AVNUH-60-94-ASAM-070 OVERHAUL RETIREMENTLIFE TABLE RECORD (UNKNOW LW2720 R/CLERK)

08-Mar-1994 1

FT. HOOD, TX

TL026629



8.7.DATE

6.REMARKS

4. 5.



CCO 2/502 AVNUH-60-94-ASAM-08- REVISION TO UH-60-94-ASAM-07 COMPLIED WITH (BONNER)

09-Mar-1994 1

FT. HOOD, TX

TL026629

CCO 2/502 AVNUH-60-94-ASAM-09 REMOVAL OF CERTAINPRIMARY SERVO ASSEMBLIES (BONNER)

05-Apr-1994 1

FT. HOOD, TX

TL026629

CCO 2/502 AVNUH-60-94-ASAM-10, REVISION TO UH-60-94-ASAM-03 (BONNER)

13-Apr-1994 1

FT. HOOD, TX

TL026629

CCO 2/502 AVNUH-60-94-ASAM-11 INFORMATIONAL M/RBLADE DE-ICE HEATER MAT RESTICTANCEMEASUREMENT TTEST (BONNER)

20-Apr-1994 1

FT. HOOD, TX

TL026629

CCO 2/502 AVNUH-60-94-ASAM-12 AUTHORIZATION FOR UH-60L AIRCRAFT TO BE UTILIZED FOREXTERNAL LOAD OPERATIONS (BONNER)

07-Jul-1994 1

FT. HOOD, TX

TL026629

CCO 2/502 AVNUH-60-95-ASAM-01-USE OF THE FWDTIEDOWN RINGS LOCATED BELOW ESSSUPPER HARD POINTS FOR HOISTING ORAIRIAL RECOVERY ALTER MARKING TOINDICATE TIEDOWN ONLY (BONNER)

19-Oct-1994 1

FT. HOOD, TX

TL026629

CCO 2/502 AVNUH-60-95-ASAM-02 REQUIREMENT TOOPERATE THE FALL TANK SUBMERGEDBOOST PUMPS ON AT ALL TIMES WITH ALLFUELS DURING AND FLT OP (BONNER)

19-Oct-1994 2

FT. HOOD, TX

TL026629

CCO 2/502 AVNUH-60-95-ASAM-03 ALL AIRCRAFT SMALLREQUIRE RESHIMMIN OF TAIL ROTORBEARING REQUIRED PROCEDURES ANDCERTAIN BEAR ASSEMBLY WILL BE INSPECTFOR SPECIFIC SERIAL NUMBERS WHICHCONTAIN CERTAIN SEGMENT DIRECT(BONNER)

28-Oct-1994 1

FT. HOOD, TX

TL026629

CCO 2/502 AVNUH-60-98-ASAM-04 ALL H-6 AIRCRAFTREDUCTION OF TORQUE OP SLIF RETAININGPILOTS BOLTS (BONNER)

10-Nov-1994 1

FT. HOOD, TX

TL026629

CCI 2/502 AVNUH-60-95-ASAM-05 CHANGE IN RETIREMENTLIFE FOR SERVO BEAM PART NUMBER 70209-22103-0501052 (BONNER)

25-Jan-1995 1

FT, HOOD, TX

TL026629

CCO 2/502 AVNUH-60-95-SOF-02 CHANGE T/R RETIREMENTLIFE FOR CERTAIN MAIN ROTOR BLADE CUFF(BONNER)

14-Feb-1995 1

FT. HOOD, TX

TL026629

NO ORGANIZATIONAOM/ACE PERFORMED AT 751 AC HRS AT FT.HOOD, TX (BONNER)

30-Mar-1995 1

ST. LOUIS, MO

TL026629

D CO 2/502D AVN REGTUH-60-95-ASAM-06 ONE TIME RECURRINGINSP (100HR) OF MAIN XMSN SUPPORTBEAMS, UPPER AND REMAING 775.0 ACF HRS(BONNER)

21-Jun-1995 1

FT. HOOD, TX

TL026629

D CO 2/502 AVNUH-60-95-ASAM-07, INSPECT ALL H60 ACFTSEATS FOR PROPER HANGING HDWR(JORDAN)

25-Jul-1995 1

FT. HOOD, TX

TL026629

D CO 2/502 AVNUH-60-16-SOF-01 CHANGE IN RETIREMENTLIFE AND REPLACEMENT OF SPECIFIED S/NFORWARD BELLCRANK SUPPORT ASSY(UNKNOWN/ LW2720 R/CLERK)

07-Nov-1995 1

FT. HOOD, TX

TL026629



8.7.DATE

6.REMARKS

4. 5.



D CO 2/502D AVN REGTSOF UH-60-96-01 CHANGE IN RETIREMENTLIFE AND REPLACEMENT OF SPECIFIC S/NFWD BELLCRANK SUPPT ASSY (SP9579)

07-Nov-1995 2

FT. HOOD, AL

TL026629

D CO 2/502D AVN REGTUH-60-96-ASAM-01 REPLACEMENT OFSPECIFIC P/N FLT CONTROL BOLTS (UH-60L)N/A THIS ACFT (SP9579)

14-Nov-1995 1

FT. HOOD, TX

TL026629

D CO 2/502D AVN REGTUH-60-96-ASAM-01 REPLACMENT OF SPECIFICP/N FLT CONTROL BOLTS (UH-60L) N/A THISACFT (SP9579)

14-Nov-1995 2

FT. HOOD, AL

TL026629

D CO 2/502D AVN REGTSOF UH-60-96-01 CHANGE IN RETIREMENTLIFE AND REPLACEMENT OF SPECIFIC S/NFWD BELLCRANK SUPPT ASSY (SP9579)

17-Nov-1995 1

FT. HOOD, TX

TL026629

S CO 2/502 AVN REGTUH-60-96-ASAM-02 ONE TIME INSP FORSUSPECT MAIN ROTOR SHAFT NUT BOLTS.DUE 910.2 ACFT HRS (UNKNOWN, LW2720/R/CLERK)

21-Nov-1995 1

FT. HOOD, TX

TL026629

S CO 2/502D AVN REGTUH-60-96-ASAM-02 ONE TIME INSP OF M/RNUT BOLTS REQUIRED WITHIN 100 FLT HRS(SP9579)

21-Nov-1995 2

FT. HOOD, TX

TL026629

D CO 2/502D AVN REGTUH-60-96-ASAM-02 ONE TIME INSP OF M/RNUT BOLTS REQUIRED WITHIN 100 FLT HRSDUE AT 910.2 ACFT HRS (SP9579)

21-Nov-1995 3

FT. HOOD, TX

TL026629

D CO 2-502 AVN REGUH-60-SOF-96-02 CHECK FOR SPECIFICSERIAL NUMBER T/R I/B RETENTION PLATESCW @ 810.2 ACFT HRS (UNKNOWN, LW2720R/CLERK)

27-Nov-1995 1

FT. HOOD, TX

TL026629

D CO 2/502D AVNSOF UH-60-96-03 TB 1-1520-237-20 -174CHANGE IN RETIREMENT LIFE OF SUSPECTM/R BLADE CUFFS C/W @ 813.5 ACFT HRS.(UNKNOWN, /LW2720 R/CLERK)

27-Nov-1995 2

FT. HOOD, TX

TL026629

D CO 2./502D AVN REGTSOF FU-60-96-02 ONE TIME INSP FORSUSPECT INBOARD T/R RETENTION PLATES(SP9579)

27-Nov-1995 3

FT. HOOD, TX

TL026629

D CO 2/502D AVN REGTSOF UH-60-96-02 ONE TIME INSP FORSUSPECT INBOARD T/R RETENTION PLATES(SP9579)

27-Nov-1995 4

FT. HOOD, TX

TL026629

D CO 2/502D AVN REGTSOF UH-60-96-03 TB 1-1520-237-20-174CHANGE IN RETIREMENT LIFE OF SUSPECTM/R BLADE CUFFS C/W @ 813.5 ACFT HRS(SP9579)

04-Dec-1995 1

FT. HOOD, TX

TL026629

D CO 2/502D AVN REGTSOF UH-60-96-03 TB 1-1520-237-20-174CHANGE IN RETIREMENT LIFE OF SUSPECTM/R BLADE CUFFS C/W @ 813.5 ACFT HRS(SP9579)

04-Dec-1995 2

FT. HOOD, TX

TL026629

DYNCORP FHSDSOF MSG UH-60-96-04 (TB1-1520-237-20-175)REMOVAL OF SPECIFIC SERIAL NUMBEREDAFT. SUPPORT BELLCRANK SUPPORT ASSYPN 70400-08117-049 (G.F. PONTAIL)

13-Dec-1995 1

FT. HOOD, TX

TL026629

S CO 2/502D AVN REGTSOF UH-60-96-04- TB 1-1520-237-20-175REMOVAL OF SPECIFIC S/N AFT BELLCRANKSUPPORT ASSY P/N 70400-08117-049 (SP9579)

13-Dec-1995 2

FT. HOOD, TX

TL026629



8.7.DATE

6.REMARKS

4. 5.



D CO 2/502D AVN REGTSOF UH-60-96-04 TB 1-1520-237-20-175REMOVAL OF SPECIFIC S/N AFT BELLCRANKSUPPORT ASSY P/N 70400-08117-049 (SP9579)

13-Dec-1995 3

FT. HOOD, TX

TL026629

D CO 2/502D AVN REGTUH-60-96-ASAM-03 REVISION TO UH-60-96-ASAM-02 REQURIED WITHIN 100 FLT HRS(SP9579)

08-Jan-1996 1

FT. HOOD, TX

TL026629

D CO 2/4 AVNUH-60-96-ASAM-03---REVISION TO UH-60-ASAM-02 ONETIME INSP FOR SUSPECT M/RSHAFT NUT BOLTS (MA7092)

08-Jan-1996 2

FT. HOOD, TX

TL026629

D CO 2/502D AVN REGTUH-60-96-ASAM-03 REVISION TO UH-60-96-ASAM-02 REQUIRED WITHIN 100 FLT HRS(SP9579)

08-Jan-1996 3

FT. HOOD, TX

TL026629

D CO 2/502D AVN REGTUH-60-96-ASAM-04 ALL H-60 SERIES ACFTWITH FAST ROPE INSERT/EXTRACT SYSTEMREST BY AWR (N/A THIS ACFT) (SP9579)

26-Jan-1996 1

FT. HOOD, TX

TL026629

D CO 2/4 AVNUH-60-96-ASAM-04---ALL UH-60 ACFT WITHTHE FAST ROPE INSERTION EXTRACTION(FRIES) BAR INST UNDER AWR (NA THISACFT) (MA7092)

26-Jan-1996 2

FT. HOOD, TX

TL026629

DCO 2/4 AVN,UH-60-96-ASAM-04 ALL H-60 SERIES ACFTWITH FAST ROPE INSERT/EXTRACT SYSTEMREST BY AWR (N/A THIS ACFT) (SP9579)

26-Jan-1996 3

FT. HOOD, TX

TL026629

PROJECT OLRACE/AACE PERFORM AT 831 ACFT HRS BYLEWIS (PL5573)

18-Mar-1996 1

FT. HOOD, TX

TL026629

DCO 2/4 AVN REGTACFT INITILAIZED UNDER ULLS-A ON THISDATE @ 831 ACFT HRS. BY S. PONTICELLISSG TI (SP9579)

18-Mar-1996 2

FT. HOOD, TX

TL026629

DCO/ 2/4 AVN REGTUH-60-96-ASAM-05 RETIREMENT LIFE ON FWDBELLCRANK SUPPORT ASSEMBLIES, P/N70400-08116-048, S/N'S 1316HMW1 THR1316HMW560 IS NOW 1800 HOURS (SP9579)

18-Mar-1996 3

FT. HOOD, TX

TL026629

D CO 2/4 AVN REGTUH-60-ASAM-07 ONE TIME RECORDS CK FORSUSPECT TIE ROD ASSY, WITH TIME LIFEREDUCTION O F SUSPECT ASSY. S.PONTICELLI SSG D CO 2/4 AVN REGT FT.HOOD TX, 76544 (SP9579)

20-Aug-1996 1

FT. HOOD, TX

TL026629

D CO 2/4 AVN REGTUH-60-96-ASAM-08 ALL H-60 ACFT INCREASEOF FATIGUE LIFE OF AEREX MFG T/RINBOARD RETENTION PLATES P/N 70358-06612-04 BY SPECIFIC S/N C/W 894.6 ACFTHRS (SP9579)

27-Aug-1996 1

FT. HOOD, TX

TL026629

D CO 2/4 AVN REGTUH-60-96-ASAM-09 (TB1-1520-237-20-179) ONETIME INSP @ A TREATMENT OF STABACTUATOR CLEVIS TO BE COMPLIED WITHN/L/T--------- ACFT HRS. (SP9579)

29-Aug-1996 1

FT. HOOD, TX

TL026629

D CO 2/4 AVN REGTUH-60-96-ASAM-10 ONE TIME INSP/RE-OCURRING REPLACEMENT OF M/R SPINDLEASSY BEARING SLEEVE P/N SB5203-202ENTERED @ --------- ACFT HRS (SP9579)

13-Sep-1996 1

FT. HOOD, TX

TL026629

D CO 2/4 AVN REGTUH-60-96-ASAM-11 (TB 1-1520-237-20-183) ALLH-60 ACFT, INCREASE IN FATIGUE LIFE OFTHE FENN MFG M/R BLADE CUFF P/N 70150-09109-041/043 CW ON 23 SEP 96 BY S.PONTICELLI (SP9579)

23-Sep-1996 1

FT. HOOD, TX

TL026629



8.7.DATE

6.REMARKS

4. 5.



D CO 2/4 AVN REGTUH-60-97-ASAM-01 9TB 1-1520-237-20-181) (TB1-1520-250-20-6) ALL H-60 BLACK HAWKHELICOPTERS INSP OF ALL MAIN ROTOR HUBASSY TO BE COMPLIED WITH N/L/T-------- ACFTHRS OR 06 APR 97 (MA7092)

08-Oct-1996 1

FT. HOOD, TX

TL026629

D CO 2/4 AVNUH-60-97-ASAM-03, REPLACEMENT OFUNDAMPED G.G. ROTORS/STATORASSEMBLY COMPLIED (MA7092)

19-Nov-1996 1

FT. HOOD, TX

TL026629

D CO 2/4 AVNSOF-UH-60-97-01, REMOVAL OF CERTAINREWORKED MAIN ROTOR SWASHPLATEASSEMBLIES, BY SERIAL NUMBER.COMPLETED (MA7092)

08-Dec-1996 1

FT. HOOD, TX

TL026629

D CO 2/4 AVNUH-60-97-ASAM-05, ALL UH/EH-60A/L AMD MH-60K, OMETIME INSPECTION FOR REMOVALAND REWORK OF CERTAIN VISCOUS DAMPERBEARING SUPPORT ASSY (MA7092)

07-Jan-1997 1

FT. HOOD, TX 76544

TL026629

D CO 2/4 AVNUH-60-97-ASAM-04, ALL UH/EH-60A/L AND MH-60K, CHANGE IN RETIREMENT LIFE OF MAINROTOR BLADE CUFF, P/N 70150-09109-041AND P/N 70150-09109-043 MANUFACTURED BYFENN MANUFACURING (M07092)

07-Jan-1997 2

FT. HOOD, TX

TL026629

D CO 2/4 AVNUH-60-97-ASAM-05, ALL UH/EH-60A/L AND MH-60K ONETIME INSPECTION FOR REMOVALAND REWORK OF CERTAIN V ISCOUSDAMPER BEARING ASSY (MA7092)

07-Jan-1997 3

FT. HOOD, TX

TL026629

D CO 2/4 AVNSOF UH-60-97-01, ALL UH/EH-60A/L AND MH-60K, REMOVAL OF CERTAIN REWORKED MAINROTOR SWASHPLATE ASSEMBLIES (MA7092)

07-Jan-1997 4

FT. HOOD, TX 76544

TL026629

D CO 2-4 AVNUH-60-97-ASAM-06: ALL H-60 ACFTW/LATERAL BELLCRANK ASSY P/N 70400-08150-045 MFG BY PURDY MFG W/SUSPECTCAGE CODE (15152) WILL HAVE A REDUCEDRETIREMENT LIFE TO TSN OF 360 HRS(JW4727)

08-Jan-1997 1

FT. HOOD, TX

TL026629

D CO 2-4 AVN REGTUH-60-97-ASAM-07: ONE TIME INSP OF ACFTHISTORICAL RECORDS FOR SUSPECT T/RSERVO CLINDER ASSY CONTAINTINGSUSPECT SEALS BY SPECIFIC S/N DUE N/L/TNEXT PMS-1 (SUSPECT S/N SERVOS FOUNDTO BE REPLACED BY NEXT 30 HR INSP OR 25MAR 97, WHICH EVER CONES FIRST (JW4727)

14-Jan-1997 1

FT. HOOD, TX

TL026629

D CO 2-4 AVN REGTUH-60-97-ASAM-08: ONE TIME INSP OFLONGITUDINAL CONTROL ROD FOR SUSPECTP/N WITH CAGE CODE 15152 DUE PRIOR TONEXT PMS-1 (JW4727)

15-Jan-1997 1

FT. HOOD, TX

TL026629

D CO 2-4 AVN REGTUH-60-97-ASAM-09: VISUAL VERIFICATION OFM/R SHAFT EXTENSION P/N 70351-08186-043FOR CAGE CODE 15152 OR 82001, MFG BYPURDY OR FENN W/CERTAIN S/N'S. SUSPECTCOMPONETNS WILL HAVE TBO TIMESREDUCED FROM 14000 TO 2100 HRS (JW4727)

28-Jan-1997 1

FT. HOOD, TX

TL026629

D CO 2-4 AVN REGTUH-60-97-ASAM-10: REDUCTION INRETIREMENT LIFE OF MAIN SUPPORT BRIDGES/N 01201A1 THRU 01686A1 MFG. BY AIRINDUSTIRES COMPLETED AT 946.5 A/CHOURS. SSG COLEMAN (BC9917)

19-Feb-1997 1

FT. HOOD, TX

TL026629



8.7.DATE

6.REMARKS

4. 5.



D CO 2-4 AVNUH-60-97-ASAM-11 CHANGE IN RETIREMENTLIFE OF M/R BLADE CUFFS P/N 70150-09109-041 TO 500 HRS AND P/N 70150-09109-043 TO2200 HRS (EB7875)

01-Apr-1997 1

FT. HOOD, TX

TL026629

D CO 2-4 AVN REGTUH-60-97-ASAM-12: RESTORATION OFSERVICE LIFE ON T/R INBOARD RETENTIONPLATES P/N 70358-06612-042 SSG J. WILSON 2-4 AVN Q.C. FHTX. (JW4727)

23-Apr-1997 1

FT. HOOD, TX

TL026629

D CO 2-4 AVN REGTIJ-60-97-ASAM-13: ALL H-60 SERIESAIRCRAFT, ONE INSP OF MAIN ROTORSPINDLE SHPERICAL ELASTOMERIC BEARINGOFR EXISTIENCE OF INNER SLEEVE BEARINGP/N SB7001-202, ACFT HRS 966.5 (MA7092)

06-Jun-1997 1

FT. HOOD, TX

TL026629

DYNCORP, OLRJACE COMPLETED AT 970 ACFT HRS AT FTHOOD TX BY JIM HERTER (R. LEWIS)

21-Jul-1997 1

FT. HOOD, TX

TL026629

D CO 2-4 AVNUH-60-97-ASAM-14 VISUAL INSP ONBELLCRANK SUPPORT FOR P/N 70400-08158-101 COMPLETED @ 969.5 ACFT HRS (TP0034)

07-Aug-1997 1

FT. HOOD, TX

TL026629

D CO 2-4 AVNUH-60-97-ASAM-15 ONE TIME INSP OF M/R P/CLOWER ROD END FOR P/N 70101-08202-101CAGE #40137 COMPLETED AT 969.5 ACFT HRS(TP0034)

07-Aug-1997 2

FT. HOOD, TX

TL026629

D CO 2-4 AVNUH-60-97-ASAM-16-ONE TIME INSP OFSWASHPLATE LINKAGE, CLEVIS CONNECTORFOR P/N 70400-08151-050 CAGE # 2A622COMPLETED @969.5 ACFT HRS (TP0034)

07-Aug-1997 3

FT. HOOD, TX

TL026629

D CO 2-4-AVNUH-60-97-ASAM-17 ONE TIME INSP OF ALL UH-60 ACFT WITH INTERNAL RESCUE HOISTBRACKET ASSY P/N 70800-02508-046INSTALLED, NOT APPLICABLE THIS ACFT(TP0034)

15-Aug-1997 1

FT. HOOD, TX

TL026629

D CO 2-4-AVNUH-60-97-ASAM-18: REMOVAL OF CERTAINREWORKED SWASHPLATE ASSY'S N/L/T THENEXT 10HR/14D OR 30 SPET 97. (JW4727)

09-Sep-1997 1

FT. HOOD, TX

TL026629

DYNCORP RHSDUH-60-98-ASAM-02 VISUAL INSP OF RLT.CONTROL RODS FOR SPECIFIC PIN & CALECODE COMPLETED THIS DATE AT 995.2 ACFTHRS (PMS-2 INSP) (DS6135)

08-Oct-1997 1

FT. HOOD, TX

TL026629

DYNCORP RHSDUH-60-95-ASAM-03 RESHIMMING OR T/R PIVOTBEARING ASSY IS C/W THIS DATE AT 995.2ACFT HRS (PMS-2 INSP) (LM2738)

29-Oct-1997 1

FT. HOOD, TX

TL026629

DYNCORP RHSDUH-60-98-ASAM-03 INSP FOR & REMOVAL ORSWASHPLATE LINK PIN 70400-08110-054CAGE CODE 65780 C/W, INSP OK AT 995.2ACFT HRS (PMS-2INSP) (DS6135)

03-Nov-1997 1

FT. HOOD, TX

TL026629

DYNCORP RHSDUH-60-96-ASAM-09 ONE TIME INSP &TREATMENT OF STABIALTOR ACTUATORCLEVIS C/W THIS DATE AT 995.2 ACFT HRS(PMS-2 INSP) (DS6135)

20-Nov-1997 1

FT. HOOD, TX

TL026629

DYNCORP RHSDUH-60-97-ASAM-01 INSP ALL M/R HUB ASSY'SC/W THIS DATE AT 995.2 ACFT HRS (PMS-2INSP) HUB HRS 995.2 HUB S/N: A308-01775(DS6135)

20-Nov-1997 2

FT. HOOD, TX

TL026629



8.7.DATE

6.REMARKS

4. 5.



DYNCORP RHSDUH-60-96-ASAM-10 ONETIME & RECURRINGREPLACE OR M/R SPINDLE ASSY BRNGSLEEVE C/W THIS DATE AT 995.2 ACFT HRS(PMS-2 INSP) (DS6135)

20-Nov-1997 3

FT. HOOD, TX

TL026629

DYNCORPPMS-2 INSP (PE#2) COMPLETED 21 NOV 1997AT 995.2 ACFT HRS NEXT PMS-2 INSP DUE AT1495.2 ACFT HRS. (CS9694)

21-Nov-1997 1

FT. HOOD, TX

TL026629

DYNCORPUH-60-98-ASAM-04 ALL H-60 ACFT LOOSEHUCKBOLTS ON OVERHAULED PRIMARY,T/ROTOR COLI AND YAW BOOST SERVOASSY'S C/W 1001.2 (CS9694)

13-Mar-1998 1

FT. HOOD, TX

TL026629

DYNCORP RHSDUH-60-98-ASAM-05 INSP FOR & REMOVAL ORSWASHPLATE LINK PN70400-08110-054/061(CAGE CODE 65780) C/W INSP OK THIS DATEAT 1001.2 ACFT HRS (DS6135)

05-May-1998 1

FT. HOOD, TX

TL026629

PROJECT OLRJACE/CPCE PERFORMED AT 1004 ACFT HRSAT FT. HOOD TX BY JACE TEAM MEMBER C(JH8309)

23-Jul-1998 1

FT. HOOD, TX

TL026629

DYNCORP FHSDUH-60-98-ASAM-07 C/W AT 1004 2 HRS FORLEFT TIE ROD P/N 70400-08115-046 SN E344-01008 (CS9694)

17-Sep-1998 1

FT. HOOD, TX

TL026629

DYNCORP FHSDUH-60-99-ASAM-01 ALL H-60 ACFT UBSO FASABD RESTORATION OF FULL LIFE FORSWASHPLATE LINK ASSY P/N 70400-08110-054/06 MFG BY TEK CAGE69780 CW 1004.2(CS9694)

03-Nov-1998 1

FT. HOOD, TX

TL026629

DYNCORP FHSD,UH-60-99-ASAM-02 ALL H-60 HELICOPTERSWITH PROVISIONS TO INSTALL EXTERNALHOIST NOT APPLICABLE TO THIS ACFT 1004.2HRS (CS9694)

05-Nov-1998 1

FT. HOOD, TX

TL026629

DYNCORP FHSDUH-60-99-ASAM-03 ALL UH-60A AND EH60AONE TIME INSP OF ALL T700-GE-700 ENGINERECORDS C/W AT 1004.2 HRS #1 ENG GE-E-307541/ #2 ENG GE-E-307789 (CS9694)

06-Nov-1998 1

FT. HOOD, TX

TL026629

DYNCORPUH-60-00-ASAM-02 ONE TIME INSPECTION OFCYCLIC STICK WIRING HARNESS. (WM0743)

27-Dec-1999 1

FT. HOOD, TX.

TL026629

DYNCORPUH-60-00-ASAM-03 ONE TIME INSPECTIONAND REMOVAL OF SUSPECT PRIMARY SERVOASSEMBLIES. (WM0743)

29-Dec-1999 1

FT. HOOD, TX

TL026629

DYNCORP FHSDUH-60-97-ASAM-02 ONE TIME INSPECTION OFTAIL DRIVE FLEXIBLE COUPLINGCONNECTIONS C/W 995.2 ACFT HRS (LATEENTRY0 (WM0743)

07-Jan-2000 1

FT. HOOD, TX

TL026629

SCO 2-4 AVNUH-60-00-ASAM-04- ONE TIME VISUAL INSP OFT/R STRUT FOR CERTAIN P/N DOES NOTCOMPLIED WITH ACFT (MH9672)

09-Mar-2000 1

FT. HOOD, TX

TL026629

DYNCORPACE/CPCE INSP COMP AT 1015 A/C HRS ATFT. HOOD TX BY TEAM MEMBER C (JC9399)

01-May-2000 1

FT. HOOD, TX

TL026629

MANTECHMWO 1-1520-237-50-80 03MAY00 (SIKORSKYDH 3816)

03-May-2000 1

FT. HOOD, TX

TL026629



8.7.DATE

6.REMARKS

4. 5.



D CO 2-4 AVNREGTUH-60-00-ASAM-05 INSPECT THE FIREEXTINGUISHER WIRING IN ORDER TOINDENTIFY ALL INSTANCES OF MISROUTINGAND /OR MISLABELING OF WIRES COMPLIDWITH 31 MAY 00 (AG1835)

31-May-2000 1

FT. HOOD, TX

TL026629

SCO 2-4AVN REGTUH60-00-ASAM-06 REVISION TO UH 6000ASAM 05 COMPLIED WITH NATHIS ACFT1051.4 ACFT HRS 07-JUL-00 AG18356 (AG1835)

07-Jul-2000 1

FT. HOOD, TX

TL026629

D CO 2-4 AVN REGTSOF UH-60-00-01 (TB 1-1520-237-20-221) INSPTHE M/R SPINDLE LUGS AND BLADE PINSFOR CRACKS 1051.4 ACFT HRS (MH9672)

12-Jul-2000 1

FT. HOOD, TX

TL026629

D CO-2-4 AVN REGTSPF UH 60-00-02 (TB1-1520-237-20-222) INSPACFT HISTORICAL RECORDS FOR INPUTMOD. G/B ASSEM POTENTIALLY CRACKEDBEVELS GEARS N/A THIS ACFT 1072.3(MH9672)

02-Aug-2000 1

FT. HOOD, TX

TL026629

FT. HOODUH-60-00-ASAM-07-ONETIME INSP OF NO1AND NO.2 JUNCTION BOXES OF ALL UH-60ASERIES ACFT, TAIL NUMBERS 77-22720THROUGH 82-23746 1079.0 ACFTH HRS(MH9672)

05-Sep-2000 1

FT. HOOD, TX`

TL026629

DCO 2/4SOF UH-60-01-02 INSP MMN LND GEAR DRAGBEAM ASSY IAW UH-60-01-02- PRIOR TO NEXTFLT BUT NLT 20010112 (WK9894)

08-Nov-2000 1

FT. HOOD, TX

TL026629

FT. HOODINSP MAIN LANDING GEAR DRAG BEAM ASSYI/A/W SOF -UH60-01-01 (TB1-1520-237-230-225)PRIOR TO NEXT FLT BUT N/L/T 21 NOV 2000C/W 09 NOV 2000 1084.8 ACFT HRS (PB2097)

09-Nov-2000 1

FT. HOOD, TX

TL026629

D CO FHTX 76544SOF UH-60-01-03 INSP LATERAL SERVOBELLCRANK ASSY IAW UH-60-01-03 PRIOR TONEXT FLT BUT NLT 12 JAN 01 1092.2 ACFTHRS (WK4894)

08-Jan-2001 1

FT. HOOD, TX

TL026629

D CO 2/4 FHTXSOF UH-60-01-04 INSP FOR INSTL OF FLIERMONITORING SYS IAW UH-60-01-04 PRIOR TONEXT FLT BUT NLT 19 JAN 01 (WK4894)

10-Jan-2001 1

FT. HOOD, TX

TL026629

DYNCORPTB1-1520-237-20-167 INSP & REPAIR OF STA635 FRAME ASSY FOR TAIL WHEEL STRUTINSTALLTATION CLEARANCE/PREVIOUSLYC/W (RE1756)

23-Mar-2001 1

FT. HOOD, TX

TL026629

DYNCORPSOF UH-60-01-06-INSP SAS ASSY FORINSTALLATION OF SAFETY CABLECOMPLETED (RE1756)

26-Mar-2001 1

FT. HOOD, TX

TL026629

USAAVNCACFT RECEIVED FROM FT. HOOD, TX I/A/WTWX 171843Z JAN 01. ACFT HRS 1110.5 ATDEPARTURE, 1116.6 AT ARRIVAL A FT.RUCKER. ACCEPTANCE INSP COMPLETED BYUSAAVNC PERSONNEL AT FT. HOOD PRIORTO DELIVERY (LW2720)

02-May-2001 1

FT. RUCKER, AL

TL026629

USAAVNCTB1-1520-237-20-232 (SOF UH-60-01-07), INSPOF MAIN ROTOR FLIGHT CONTROL SELFLOCKING BOLTS C/W AT 1117.1 ACFT HRS.(BA2721 R/CLERK)

12-May-2001 1

FT. RUCKER, AL

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAAVNCTB1-1520-237-20-232 (SOF UH-60-01-08), INSPOF MAIN ROTOR FLIGHT CONTROL SELFLOCKING BOLTS C/W AT 1117.1 ACFT HRS.(BA2721 R/CLERK)

12-May-2001 2

FT. RUCKER, AL

TL026629

USAAVNCONE TIME & RECURRING INSP OF BOOSTSERVO & PILOT ASSIST MODULE MANIFOLDBASE PLATE FOR LOOSE MOUNT BOLTSI/A/W DPC UH60-00-01 C/W AT 1116.6 (LW2720)

15-May-2001 1

FT. RUCKER, AL

TL026629

USAAVNCTHE FOLLOWING LIST OF MODIFICATIONSCOMPLETED AT 1116.6 ACFT HRS. I/A/WLOCAL DOCUMENTS FOR SCHOOL FLEETTRAINING: INSTL OF FUEL FLAG, INSTL OFBUZZ NUMBER, INSTL OF HIGH VISIBILITYPAINT SCHEME (LW2720)

15-May-2001 2

FT. RUCKER, AL

TL026629

USAAVNCACFT. OPERATING UNDER AWORTHINESSRELEASE DTD 21 NOV 00. ACFT WILLOPERATE AS UH60A WHILE ASSIGNED TOUSAAVNC. (LW2720)

15-May-2001 3

FT. RUCKER, AL

TL026629

USAAVNCACFT DECONFIGURED I/A/W CECOM FLIGHTACTIVITY CHECKLIST. EQUIPMENT REMOVEDINCLUDES: AN/ALQ-151 9V)2 MISSIONEQUIPMENT PACKAGE, AN/ASN -132INTEGRATED INERTIAL NAVIGATION SYSTEM(IINS), ACFT SURVUVABILTY EQUIPMENT(ASE), ENVIRONMENTAL CONTROL STYSTEM(ECS), MISSION ANTENNA(S) ANDWAVEGUIDE ASSEMBLIES. SUSBJECTCHECKLIST LOCATED IN THE BACK OF THISHISTORICAL RECORD (LW2720)

18-May-2001 1

FT. RUCKER, AL

TL026629

USAAVNC,AIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-00003REV. E SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A. AFT CONTROL SERVOINPUT ROD HAS BEEN LENGTHENED 1/4 TURNLEFT B. LAATERAL CONTROL SERVO INPUTROD HAS BEEN 1 TURN RIGHT C. FORWARDCONTROL SERVO INPUT ROD HAS BEEN 1/4TURN RIGHT AT 1117.0 ACFT. HRS.. (LW2720)

02-Jul-2001 1

FT. RUCKER, AL

TL026629

USAAVNC,TB1-1520-237-20-232 SOF UH-60-01-08,REVISION TO SOF UH-60-01-07, INSP OF M/RFLT CONTROL SELF LOCKING BOLTS. C/W 12-MAY-01 WITH 1117.1 ACFT HRS. (LW2720)

02-Jul-2001 2

FT. RUCKER, AL

TL026629

USAAVNC,GEN-MIM-01-005, IDENTIFICATION OFRECEIVER TRANSMITTERS (R/T) REQUIRINGECP-II SOFTWARE C/W 12-JUL-2001 ACFT.HRS. 1145.7 (LW2720)

13-Jul-2001 1

FT. RUCKER, AL

TL026629

USAAVNC,OCM/ACE PERFORMED AT 1261 A/C HRS BYTEAM MEMBER J AMCOM/OLR FCTKY (F.SCHROEDER 6922)

12-Oct-2001 1

FT. RUCKER, AL

TL026629

USAAVNC,TB1-1520-237-20-241 (SOF UH-60-02-03), ONETIME INSP OF FLIGHT CONTROL SYSTEM,PITCH TRIM ASSY. (WL 5769 T.I.)

10-Dec-2001 1

FT. RUCKER, AL

TL026629

USAAVNC,TB1-1520-237-20-242 (SOF UH-60-02-04) INSPOF APU FUEL LINES FOR PROPER GROMMETAT APU SHROUD ASSY WITH ACFT HRS.1449.1 (LW2720 R/CLERK)

24-Jan-2002 1

FT. RUCKER, AL

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAAVNCTB1-1520-237-20-246 (UH-60-02-ASAM-02)INITIAL AND RECURRING INSPECTION OF THECONTROL ROD JAMNUT. C/W AT 1470.6 ACFTHRS (LW2720 R/CLERK)

09-Feb-2002 1

FT. RUCKER, AL

TL026629

USAAVNCTB1-1520-237-20-244 (UH-60-2-ASAM-04)RESTRAINT SYSTEM INSPECTION. C/W AT1493.3 ACFT HRS (IP2860, R/CLERK)

21-Mar-2002 1

FT. RUCKER, AL

TL026629

USAAVNCTB1-1520-237-20-245 9UH-60-02-ASAM-03),INSPECTION OF ENGINE CONTROLQUADRANT POWER LEVER (PCL) WIRING C/WAT 1493 ACFT HRS (LW2720 R/SPEC)

09-Apr-2002 1

FT. RUCKER, AL

TL026629

USAAVNCTB1-1520-237-20-252 (UH-60-02-ASAM-06),COLLECTIVE AND YAW BOOST SERVOASSEMBLIES SWAGE COLLARS. C/W AT 1493ACFT HRS (LW2720 R/CLERK)

18-Apr-2002 1

FT. RUCKER, AL

TL026629

USAAVNCTB1-1520-237-20-245 (UH-60-02-ASAM-03),INSPECTION OF ENGINE CONTROLQUADRANT POWER LEVER (PCL) WIRING. C/WAT 1493.3 ACFT HRS (LW2720 R/CLERK)

19-Apr-2002 1

FT. RUCKER, AL

TL026629

DYNCOPROCM/ACE PERFORMED AT 1502 ACFT HRS. BYTEAM MEMBER QQ AMCOM PROJECT OLR FT.CKY (L. SANDERS LS 2032)

04-May-2002 1

FT. CAMPBELL, KY

TL026629

USAAVNC#2 CROSSFEED BREAKAWAY VALVEREPLACE I/A/W TB1-1520-237-20-213 THISDATE@ 1493.3 ACFT HRS. (JB2761 R/CLERK)

07-May-2002 1

FT. RUCKER, AL

TL026629

USAAVNC,ACFT. M/R HEAD RIGGED I/A/W SA DWG.70400-00003 REV.E. SYSTEM CONTROLS HAVEBEEN BIASED IN ACCORD.A;AFTCONTROLSERVO INPUT ROD HAS BEEN (LENGTHENED3/4 TURN) . B. LATERAL CONTROL SERVOINPUT ROD HAS BEEN (SHORTENED 3/4TURN). C. FORWARD CONTROL SERVO INPUTROD HAS BEEN (SHORTENED 3/4 TURN). @1493.3 ACFT HRS. (JB2761 R/CLERK)

15-May-2002 1

FT. RUCKER, AL.

TL026629

USAAVNCPMS-2 INSP (500 HR) # 3 COMPLETED AT1493.3 ACFT HR. NEXT #4 DUE @ 1993.3 ACFTHRS. (JB2761 R/CLERK)

15-May-2002 2

FT.RUCKER, AL

TL026629

USAAVNCTB1-1520-237-20-257 (UH-60-02-SDSM-09), INSPOF T/R QUADRANT INSTALLATIONHARDWARE. C/W AT 1513 ACFT HRS (LW2720R/CLERK)

15-Jun-2002 1

FT. RUCKER, AL

TL026629

USAAVNCTB1-1520-237-20-256 (UH-60-02-ASAM-08) INSPOF AN/ARC-220 WIRING FOR CHAFING. C/WAT 1513.1 ACFT HRS. N/A THIS ACFT. (JH5095R/CLK)

16-Jun-2002 1

FT. RUCKER, AL

TL026629

USAAVNCACFT OPERATING UNDER AWOR REL DTD13MAY02 FOR SPECIFIED EH60 ACFT TOOPERATE WITH ALL MISSION EQUIPMENTREMOVED AND SELECTED EQUIPMENTINSTALLED(SEE AWOR REL). THIS AWOR RELSUPERCEDES AWOR REL'S WITH SAMESUBJECT DTD 15JAN02, 06JUN01 AND 21NOV00. (DK1063)

11-Jul-2002 1

FT. RUCKER, AL.

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAAVNCTB1-1520-237-20-261 (UH-60-02-ASAM-11),INSPECT AN/ARC-220 WIRING FOR CHAFINGC/W AT 1513.1 ACFT HRS (LW2720 R/CLERK)

24-Sep-2002 1

FT. RUCKER, AL

TL026629

USAAVNCPLACED ACFT IN INTERMEDIATE STORAGEON 14-JUN-02. REMOVED ACFT FORMINTERMEDIATE STORAGE ON 25-OCT-02 @1513.1 ACFT HRS (LW2720 R/CLERK)

25-Oct-2002 1

FT. RUCKER, AL

TL026629

USAAVNCYELLOW BLADE HAS EVIDENCE AT BIRDSTRIKE LEADING EDGE M.O. POINT OTBLADE. CHECK BLADE NO DAMAGE FOUND1551.0 ACFT HOURS. (LW2720 R/CLERK)

02-Dec-2002 1

FT. RUCKER, AL

TL026629

USAAVNCUH-60-03-ASAM-01, FWD BELLCRANKSUPPORT RETIREMENT LIFE S/N H287-00587.C/W AT 1577 ACFT HOURS (LW2720 R/CLERK)

09-Dec-2002 1

FT. RUCKER, AL

TL026629

USAAVNCUH-60-03-ASAM-02 TAIL ROTOR SERVO ASSYRETIREMENT LIFE C/W AT 1577.4 ACFT HRS.(TB1027 R/SPEC)

09-Dec-2002 2

FT. RUCKER, AL.

TL026629

USAAVNCGEN-03-ASAM-01 SINGLE CHANNEL GROUNDAND AIRBORNE RADIO (SINCGARS) ARC-201BATTERY BOX. C/W AT 1587 ACFT HRS(LW2720 R/CLERK)

17-Dec-2002 1

FT. RUCKER, AL

TL026629

USAAVNCOCM/ACE PERFORMED AT 1596 A/C HRS BYTEAM MEMBER J AM COM/OLR FTCKY (FS6922)

11-Jun-2003 1

FT. RUCKER, AL

TL026629

USAAVNCACFT OPERATING UNDER AWORTHINESSRELEASE DTD 06JUN03 (EH-60 DE-MOD)WHICH SUPERSEDES AWOR RELEASES DTD11OCT02, 13MAY02, 15JAN02, 06JUN01 AND21NOV00. A COPY OF THE AWOR REL ISLOCATED IN THE BACK OF THIS HISTORICALBOOK. (DD3948)

19-Jun-2003 1

FT. RUCKER, AL.

TL026629

USAAVNCSOF-UH-60-04-01 INSP OF FORWARDBELLCRANK SUPPORT INSTALLATIONHARDWARE COMPLETED AT 1595.0 ACFTHRS. (TB1027 R/SPEC)

03-Oct-2003 1

FT. RUCKER, AL.

TL026629

USAAVNCACFT OPERATING UNDER AWORTHINESSRELEASE #1153 DTD 31 DEC 03 (JP-8+100).(TB1027 R/SPEC)

31-Dec-2003 1

FT. RUCKER, AL.

TL026629

USAAVNCAWOR DTD 13 MAY 02 PROVISION FOR THEINSTALLATION OF THE DOPPLER/GPSAN/ASN-128B COMPLETED AT 1594.6 ACFTHRS. (TB1027 R/SPEC)

04-Jan-2004 1

FT. RUCKER, AL.

TL026629

USAAVNCAWOR REL DTD 13 MAY 02 PROVISION FORTHE INSTALLATION AND OPERATION OF ACARGO HOOK COMPLETED AT 1594.6 ACFTHRS. (TB1027 R/SPEC)

04-Jan-2004 2

FT. RUCKER, AL.

TL026629

USAAVNCAWOR DTD 13 MAY 02 PROVISION FOR THEINSTALLATION OF THE ANVIS/HUD AN/ANVIS-7 COMPLETED AT 1594.6 ACFT HRS (TB1027R/SPEC)

04-Jan-2004 3

FT. RUCKER, AL.

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAAVNCAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-00003REV. E. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD A. FWD CONTROL SERVOINPUT ROD SHORTENED 1/4 TURN. B. AFTCONTROL SERVO INPUT ROD HAS BEENLENGTHENED 1/4 TURN. C LATERALCONTROL SERVO INPUT ROD HAS BEENSHORTENED 1/4 TURN. AT 1660.9 ACFT HRS.(TB1027 R/SPEC)

20-Mar-2004 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-04-ASAM-02 "INSP OF T/R D/SHAFTFLANGE NUT" COMPLETED AT 1694 ACFTHRS. (TB1027 R/SPEC)

01-Apr-2004 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-04-ASAM-01 "GLARE SHIELD LIGHTINGCIRCUIT BREAKER REPLACEMENT"COMPLETED AT 1747 ACFT HRS. (TB1027R/SPEC)

16-Apr-2004 1

FT. RUCKER, AL.

TL026629

USAAVNC05 JUN 04 BAT STRIKE ON R/H GUNNERSWINDOW FRAME ACFT HRS. BIRD STRIKEINSP COMPLETED W/NO DAMAGE FOUND AT1870.7 ACFT HRS. (TB1027 R/SPEC)

05-Jun-2004 1

FT. RUCKER, AL.

TL026629

USAAVNCSOF UH-60-04-02 DISABLING OF COCKPITAIRBAG SYSTEM COMPLETED AT 1888.9 ACFTHRS. (TB1027 R/SPEC)

10-Jun-2004 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-MIM-04-008 INSPECTION OF WIRINGAND REPAIR TO POWER WIRING ANDINSULATION SLEEVING OF AIRCRAFTRETRACTABLE LANDING LIGHT COMPLETEDAT 1894.6 ACFT HRS. (TB1027 R/SPEC)

14-Jun-2004 1

FT. RUCKER, AL.

TL026629

AMCOM/OLR FT.C.KY.OCM/ACE PERFORMED AT 1916 ACFT HRS BYTEAM MEMBER 'J' (TB1027 R/SPEC)

01-Jul-2004 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-04-ASAM-03 FUEL SYSTEM INTEGRITYCHECKS C/W AT 1959.2 ACFT HRS. (TB1027R/SPEC)

13-Aug-2004 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-04-ASAM-04, REVISION TO UH-60-04-ASAM-03, FUEL SYSTEM INTEGRITY CHECKSCOMPLETED AT 1959.2 ACFT HRS. (TB1027R/SPEC)

13-Aug-2004 2

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-04-ASAM-05, RESTRAINT SYSTEMINSPECTION COMPLETED AT 1933.3 ACFTHRS. (TB1027 R/SPEC)

27-Sep-2004 1

FT. RUCKER, AL.

TL026629

USAAVNC.UH-60-04-ASAM-03 FUEL SYSTEM INTEGRITYCHECKS C/W AT 1993.3 ACFT HRS. (TB1027R/SPEC)

03-Oct-2004 1

FT. RUCKER, AL.

TL026629

USAAVNCPMS-2 PHASE #4 COMPLETED AT 1993.3 ACFTHRS. NEXT PMI #5 DUE AT 2693.3 ACFT HRS.(TB1027 R/SPEC)

21-Oct-2004 1

FT. RUCKER,AL.

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAAVNCAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-00003REV. E. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD A. FWD CONTROL SERVOINPUT ROD SHORTENED 3/4 TURN. B. AFTCONTROL SERVO INPUT ROD HAS BEENLENGTHENED 3/4TURN. C LATERAL CONTROLSERVO INPUT ROD HAS BEEN SHORTENED1/3 TURN. AT 1993.3 ACFT HRS. (TB1027R/SPEC)

21-Oct-2004 2

FT. RUCKER, AL.

TL026629

USAAAVNCCHANGED FROM PMS-2 TO PMD ANDINTERVAL INCREASED FROM 500 TO 700 HRSI/A/W AWR 1220 @ 1993.3 ACFT HRS. NEXTPHASE # 5 @ 2693.3 ACFT HRS. (VM4663)

22-Oct-2004 1

FT RUCKER, AL

TL026629

USAANVCAIRWORTHINESS RELEASE (AWR DTD 19 OCT04) TO CONDUCT ENHANCED SCHEDULEDMAINTENANCE (ESM) OPERATIONALEVALUATION AT USAAVNC. (TB1027 R/SPEC)

05-Nov-2004 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-05-ASAM-01 , REVISION OF FUELSYSTEM INTEGRITY CHECKS COMPLETED AT2111 ACFT HRS. (TB1027 R/SPEC)

10-Jan-2005 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-05-ASAM-02 INSPECTION FOR BLUEFORCE TRACKER COMPLETED AT 2240.4ACFT HRS.(BFT) NA TO THIS ACFT (TB1027R/SPEC)

02-Mar-2005 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-05-SOF-01 REACTIVATION OF COCKPITAIRBAG SYSTEM (CABS) COMPLETED AT2257.8 ACFT HRS. (NA TO THIS ACFT) (TB1027R/SPEC)

17-Mar-2005 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-05-SOF-02 ENHANCED SCHEDULEDMAINTENANCE (ESM) PROGRAMIMPLEMENTION COMPLETED AT 2274.4 ACFTHRS. (NA TO THIS ACFT) (TB1027 R/SPEC)

25-Mar-2005 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-05-ASAM-04 INSP OF TAIL LANDINGGEAR YOKE ASSY C/W AT 2303 ACFT HRS.(TB1027 R/SPEC)

09-Apr-2005 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-05-ASAM-03 AIRCREW RESTRAINTSYSTEM COMPATIBILITY COMPLETED AT 2322ACFT HRS. (TB1027 R/SPEC)

19-Apr-2005 1

FT. RUCKER, AL.

TL026629

USAAVNCOCM/ACE PERFORMED AT 2342 ACFT HRS BYTEAM MEMBER "M" (TB1027 R/SPEC)

25-Apr-2005 1

FT. RUCKER, AL.

TL026629

USAAVNCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6. RED:5.031/4.685 YELLOW: 5.122/4.785, BLUE:4.303/4.970, BLACK: 4.370/4.034. (TB1027R/SPEC)

27-Apr-2005 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-05-ASAM-06 TROOP SEAT RESTRAINTBUCKLE COMPLETD AT 2343 ACFT HRS.(TB1027 R/SPEC)

28-Apr-2005 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-05-ASAM-07 AIR INTRUSION OFHYDRAULIC SYSTEM COMPLETD AT 2380ACFT HRS. (TB1027 R/SPEC)

20-May-2005 1

FT. RUCKER, AL.

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAAVNCUH-60-05-ASAM-09 CRASHWORTHYEXTERNAL FUEL SYSTEM (CEFS)INSTALLATION BOLTS C/W AT 2501.9 ACFT.HRS. (TB1027 R/SPEC)

02-Aug-2005 1

FT. RUCKER, AL.

TL026629

USAAVNC#1 ENGINE HAS EVIDENCE OF A BIRD STRIKE.BIRD STRIKE INSPECTION COMPLETED OK AT2577.4 ACFT HRS. (TB1027 R/SPEC)

31-Aug-2005 1

FT. RUCKER, AL.

TL026629

USAAVNCACFT. M/R HEAD RIGGED I/A/W SA DWG.70400-00003 REV.E. SYSTEM CONTROLS HAVEBEEN BIASED IN ACCORD.A;AFTCONTROLSERVO INPUT ROD HAS BEEN ( NO ADJ.MADE) . B. LATERAL CONTROL SERVO INPUTROD HAS BEEN (SHORTENED 1/4 TURN). C.FORWARD CONTROL SERVO INPUT ROD HADNO ADJ). @ 2654.0 ACFT HRS. (MB1137)

07-Oct-2005 1

FT. RUCKER,AL.

TL026629

USAAVNCALCL LTR DTD 12 OCT05 ONE TIMEINSPECTION OF TAIL LANDING GEARDEFLECTOR (WIRE CUTTER) IAW EMAILINSTRUCTIONS FROM ACLC C/W AT 2656.3ACFT. HRS. (TB1027 R/SPEC)

16-Oct-2005 1

FT. RUCKER, AL.

TL026629

USAAVNCAWR 1220 AIRWORTHINESS RELEASE 1220 TOCONDUCT ESM OPERATIONAL EVALUATIONAT THE USAAVNC, FT. RUCKER, AL.COMPLETED AT 2656.3 ACFT. HRS. PMIINTERVAL INCREASED FROM 700 TO 720 HRSI/A/W 1220 NEXT PHASE # 5 DUE AT 2713.3ACFT. HRS. (VM4663)

21-Oct-2005 1

FT RUCKER, AL

TL026629

USAAVNCACFT. OPERATING UNDER AIRWORTHINESSRELEASE DTD 06 OCT 05 TO CONDUCT ESMOPERATIONAL EVALUATION AT THEUSAAVNC, FT. RUCKER, AL. (AWR 1220)(VM4663)

21-Oct-2005 2

FT RUCKER

TL026629

USAAVNCM/R RIG CHECK COMPLETED AT 2658.2 ACFTHRS. WITH NO CHANGE. (TB1027 R/SPEC)

22-Nov-2005 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-06-ASAM-01 TAIL LANDING GEARSTRUT C/W AT 2700.1 ACFT. HRS. (TB1027R/SPEC)

07-Jan-2006 1

FT. RUCKER, AL.

TL026629

USAAVNCACFT CONTINUES TO OPERATE UNDER AWR1153, JP-8+100 FUEL, R2 DTD 30JAN06 (TB1027R/SPEC)

01-Feb-2006 1

FT. RUCKER, AL.

TL026629

USAAVNCGEN-MIM-06-001 INSPECTION OF T700 SERIESENGINE OIL FILLER ASSEMBLY COMPLETEDAT 2708.6 ACFT HRS. (TB1027 R/SPEC)

10-Feb-2006 1

FT RUCKER, AL.

TL026629

USAAWCM/R RIG CHECK COMPLETED WITH NOCHANGES @ 2950.2 ACFT (TB1027 R/SPEC)

14-Feb-2006 1

FT. RUCKER, AL.

TL026629

USAAVNCUH-60-05-ASAM-11 WIRING HARNESSCHAFFING C/W AT 2708.6 ACFT. HRS. (TB1027R/SPEC)

15-Feb-2006 1

FT. RUCKER, AL.

TL026629

USAAWCOCM/ACE PERFORMED AT 2709 ACFT HRS BYTEAM MEMBER 'QQ' AMCOM PROJECT OLR(LS2032)

27-Feb-2006 1

FT. RUCKER, AL.

TL026629

USAAWCM/R RIG CK COMPLETED WITH NO CHANGE.(TB1027 R/SPEC)

13-Mar-2006 1

FT. RUCKER, AL.

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAAWCT/R CABLE TENSION CK COMPLETED AT2708.6 ACFT HRS L/CABLE 108 R/CABLE 140 @25 DEGREES FARENHEIGHT (TB1027 R/SPEC)

14-Mar-2006 1

FT. RUCKER,A L.

TL026629

USAAWCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6. RED:4.608/5.010YELLOW: 4.549/4.897 BLUE:4.140/4.486, BLACK: 4.023/4.375 (TB1027R/SPEC)

15-Mar-2006 1

FT. RUCKER, AL.

TL026629

USAAWCPMI PHASE INSPECTION #5 COMPLETED AT2708.6 ACFT HRS. PMI PHASE # 7 DUE AT3428.6 ACFT HRS. (TB1027 R/SPEC)

17-Mar-2006 1

FT. RUCKER, AL.

TL026629

USAAWCT/R CABLE TENSION CK COMPLETED AT2717.2 ACFT HRS. R/H 150, L/H 151, TEMP 27DEGREES C. (TB1027 R/SPEC)

03-Apr-2006 1

FT. RUCKER, AL.

TL026629

USAAWCT/R CABLE TENSION CHECK COMPLETED AT2727.2 ACFT HRS L/H=122, R/H =122 @ 14DEGREES C, (TB1027 R/SPEC)

07-Apr-2006 1

FT. RUCKER, AL.

TL026629

USAAWCUH-60-06-ASAM-02 MAIN ROTOR (M/R) RIGIDCONNECTING LINK/PITCH CONTROLASSEMBLIES C/W AT 2742.8 ACFT. HRS.(TB1027 R/SPEC)

14-Apr-2006 1

FT.R UCKER, AL.

TL026629

USAAWCONE TIME INSP OF CONSOLE CIRCUIT BREAKPANEL ASSY FOR WATER PENETRATIONCOMPLETED @ 2825.6 ACFT HRS I/A/W ACLCE-MAIL DTD 17 MAR 06. (RJ0827, R/SPEC)

13-May-2006 1

FT. RUCKER, AL

TL026629

USAAWCM/R RIG CK COMPLETED@ 2872.9 ACFTHRS.WITH NO CHANGES (TB1027 R/SPEC)

07-Jun-2006 1

FT. RUCKER, AL.

TL026629

USAAWCT/R CABLE TENSION CK COMPLETED AT2872.9 ACFT HRS. R/H 139 - L/H 139 (TB1027R/SPEC)

07-Jun-2006 2

FT. RUCKER, AL.

TL026629

USAAWCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6. RED:4.822/5.160 YELLOW: 4.822/5.160 BLUE:4.315/4.652, BLACK: 4.315/4.652. (TB1027R/SPEC)

09-Jun-2006 1

FT. RUCKER, AL.

TL026629

USAAWCACFT OPERATING UNDER (AWR)FORINSTALLATION OF EYEBOLTS ON UH-60-A/LHELICOPTER BILFILAR ARMS TO SECURESATETY HARNESSES (AWR 1251) DTD 16 MAR05 (TB1027 R/SPEC)

18-Jun-2006 1

FT. RUCKER, AL.

TL026629

USAAWCUH-60-06-SOF-02 DISABLING OF COCKPITAIRBAG SYSTEM (CABS) C/W AT 2915.5 ACFT.HRS. (TB1027 R/SPEC)

22-Jun-2006 1

FT. RUCKER, AL.

TL026629

USAAWCUH-60-06-ASAM-04 COCKPIT AIRBAG SYSTEM(CABS) ELECTRONIC CRASH SENSOR UNIT(ECSU) DRAIN PLUGS COMPLETED AT2915.5ACFT HRS. (TB1027 R/SPEC)

22-Jun-2006 2

FT. RUCKER, AL.

TL026629

USAAWCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6. RED:5.131/4.794 YELLOW: 5.194/4.765 BLUE:4.523/4.189, BLACK: 4.475/4.135 (TB1027R/SPEC)

20-Jul-2006 1

FT. RUCKER, AL.

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAAWCUH-60-06-ASAM-05 BLUE FORCE TRACKERHARDWARE INSTALLATION COMPLETED AT2948.7 ACFT HRS. N/A TO THIS ACFT. (TB1027R/SPEC)

21-Jul-2006 1

FT. RUCKER, AL.

TL026629

USAAWCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6. RED: 5.04/538YELLOW: 4.94/5.27 BLUE: 4.33/4.68, BLACK:4.35/4.68 (TB1027 R/SPEC)

22-Jul-2006 1

FT. RUCKER, AL.

TL026629


07-Aug-2006 1

FT. RUCKER, AL.

TL026629

USAAWCT/R CABLE TENSION CK COMPLETED AT2952.7 ACFT HRS. R/H 3.470; L/H .030 (TB1027R/SPEC)

07-Aug-2006 2

FT. RUCKER, AL.

TL026629

USAAWCM/R RIG CK COMPLETED AT 2949.2 WITH FWDSHORTEN 1/2 TURN, AFT LENGTHENED 1/2TURN, LAT. NO CHG. (TB1027 R/SPEC)

13-Aug-2006 1

FT. RUCKER, AL.

TL026629

USAAWCT/R CABLE TENSION CK COMPLETED AT2958.1 ACFT HRS. R/H .140; L/H .139 (TB1027R/SPEC)

23-Aug-2006 1

FT. RUCKER, AL.

TL026629

USAAWCT/R CABLE TENSION CK COMPLETED AT2969.2 ACFT HRS. R/H - 145, LH -145 AT 27DEGREES C. (TB1027 R/SPEC)

30-Aug-2006 1

FT. RUCKER, AL.

TL026629

USAAWCT/R CABLE TENSION CK COMPLETED AT2980.7 ACFT HRS. L/H=150, R/H=15 @ 27DEGREES 'C' (TB1027 R/SPEC)

12-Sep-2006 1

FT. RUCKER, AL.

TL026629

USAAWC#2 CROSSFEED BREAKAWAY VALVEREPLACED THIS DATE AT 3030 ACFT HRS.(DK1063)

28-Sep-2006 1

FT. RUCKER, AL.

TL026629

USAAWCBIRD STRIKE INSPECTION COMPLETED. NODAMAGE FOUND AT 3062.4 ACFT HRS.(TB1027 R/SPEC)

11-Oct-2006 1

FT. RUCKER, AL.

TL026629

USAAWCM/R RIG CHECK COMPLETED AT 3063.2 ACFTHRS. LATERAL SERVO CONTROL RODSHORTENED 1 FULL TURN (TB1027 R/SPEC)

01-Dec-2006 1

FT. RUCKER, AL.

TL026629

USAAWCUH-60-07-ASAM-01 REQUIREMENTS OF UH-60-07-ASAM-01, (REROUTING OF WHITEENGINE/AIRFRAME HARNESS ASSEMBLY)COMPLIED WITH @ 3063.2 ACFT HRS. (TB1027R/SPEC)

09-Dec-2006 1

FT. RUCKER, AL.

TL026629


11-Dec-2006 1

FT. RUCKER, AL.

TL026629

USAAWCUH-60-07-ASAM-02 REVISION TO UH-60-07-ASAM-01, REROUTING OF WHITEENGINE/AIRFRAME HARNESS ASSEMBLYCOMPLETED AT 3073.2 ACFT HRS. (TB1027R/SPEC)

21-Dec-2006 1

FT. RUCKER, AL.

TL026629



8.7.DATE

6.REMARKS

4. 5.



UWAAWCUH-60-07-ASAM-04 AUTOROTATIONALCHARTS COMPLETED AT 3073.2 ACFT HRS.(TB1027 R/SPEC)

30-Dec-2006 1

FT. RUCKER, AL.

TL026629

USAAWCUH-60-07-ASAM-03 YAW AND COLLECTIVEBOOST SERVOS ROLL PIN COMPLETED AT3073.2 ACFT HRS. (TB1027 R/SPEC)

04-Jan-2007 1

FT. RUCKER, AL.

TL026629

USAAWCOPERATE ACFT I/A/W AIRWORTHINESSRELEASE (AWR) DTD 19 DEC 06 FOR UH-60-A/L/M/Q, EH60A, AND UH-60-L/M HELICOPTERTO OPERATE WITH J-8+100 FUEL (AWR1153)(R-3) (TB1027 R/SPEC)

22-Jan-2007 1

FT. RUCKER, AL.

TL026629

USAAWCUH-60-07-ASAM-05 ARC-220/KY-100 START-UPPROCEDURES (N/A THIS ACFT., KY-100 NOTINSTALLED) AT 3084.5 ACFT. HRS. (TB1027R/SPEC)

25-Jan-2007 1

FT. RUCKER, AL.

TL026629

USAAWCUH-60-07-ASAM-06 INTERNAL RESCUE HOISTCABLE (GUARD) DEFLECTOR C/W AT 3106.8ACFT. HRS. NA TO THIS ACFT. (MF4187R/SPEC.)

08-Feb-2007 1

FT. RUCKER, AL.

TL026629

USAAWCACFT OPERATING UNDER( ISAQ 123)HELICOPTERS EQUIPPED WITH THEBATTELLE CAUTION ADVISORY PANEL (CAP).(TB1027 R/SPEC)

15-Feb-2007 1

FT. RUCKER, AL.

TL026629

USAAWCUH-60-07-AMAM-01 COMMON MISSILEWARNING SYSTEM (CMWS) N/A THIS ACFT. @3195.9 ACFT. HRS. (TB1027 R/SPEC)

27-Mar-2007 1

FT. RUCKER, AL.

TL026629

USAAWCBIRD STRIKE INSP COMPLETED WITH NODEFECTS AT 3259.3 ACFT HRS. (TB1027R/SPEC)

24-Apr-2007 1

FT. RUCKER, AL.

TL026629

USAAWCUH-60-07-ASAM-07 INSTALLATION OF STATICBONDING JUMPERS, N/A TO THIS ACFT. C/WAT 3311.5 ACFT. (TB1027 R/SPEC)

11-May-2007 1

FT. RUCKER, AL.

TL026629

USAAWCACFT OPERATING UNDER (AWR)FORINSTALLATION OF EYEBOLTS ON UH-60-A/LHELICOPTER BILFILAR ARMS TO SECURESATETY HARNESSES (AWR 1251) DTD 16 MAR07 (TB1027 R/SPEC)

14-May-2007 1

FT. RUCKER, AL.

TL026629

USAAWCREPLACED R/H BEADED PANEL @ 3329.7ACFT HRS. (TB1027 R/SPEC)

01-Jun-2007 1

FT. RUCKER, AL.

TL026629

DYNCORP OLR FT.CAMPBELL, KY

OCM/ACE PERFORMED @ 3376 ACFT HRS BYTEAM MEMBER 'R' AMCOM PROJECT OLR(TB1027 R/SPEC)

12-Jul-2007 1

FT. RUCKER, AL.

TL026629

USAACEI/A/W MEC F64873 REPAIR: REPLACE INSERTSIAW DMWR 1-2835-214 (PAGE 4-205, PARA. 4-42.5 B AND PAGE 4-216, PARA. 4-42.5 I) SMRCODE DESIGNATES THE INSERTS AS DEPOTLEVEL MEC F64873 GRANTED TOR REPAIR ASSTATED.

20-Jul-2007 1

LOWE AHP, FT.RUCKER, AL.

DW0950

USAAWCM/R RIG COMPLETED @ 3376.2 ACFT HRS.LATERAL SERVO CONTROL ROD SHORTENED3/4 TURN. AFT SERVO CONTROL RODLENGTHENED 1/2 TURN. FWD SERVOCONTROL ROD SHORTENED 1/2 TURN.(TB1027 R/SPEC)

31-Jul-2007 1

FT. RUCKER, AL.

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAAWCT/R BIAS MEASUREMENTS COMPLETED @3376.2 ACFT HRS I/A/W TM 1 1520-237-237-23,PARA 11-4-6 RED: 508/475; YELLOW 508/475;BLACK 438/405; BLUE: 442.408, (TB1027R/SPEC)

31-Jul-2007 2

FT. RUCKER, AL.

TL026629

USAAWCACFT OPERATING UNDER AWR (1220) TOCONDUCT A MODIFIED ENHANCEDSCHEDULED (ESM) PROGRAM SCHEDULE(REV -3 )@ 3376.2 ACFT HRS. (TB1027 R/SPEC)

02-Aug-2007 1

FT. RUCKER, AL.

TL026629

USAAWCT/R CABLE TENSION CK COMPLETED @3376.6 ACFT HRS L136/R136 @ 25 DEGREES C.(TB1027 R/SPEC)

02-Aug-2007 2

FT. RUCKER, AL.

TL026629

USAAWCPMI PHASE # 6 COMPLETED @ 3376.2 ACFTHRS NEXT PMI # 7 DUE 2 4096.2 ACFT HRS.(TB1027 R/SPEC)

09-Aug-2007 1

FT. RUCKER, AL.

TL026629

USAAWCT/R BIAS MEASUREMENTS COMPLETED AT3376.2 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 508/475 YELLOW: 508/475 BLUE:442/408/4.520, BLACK: 438/405 (TB1027R/SPEC)

15-Aug-2007 1

FT. RUCKER, AL.

TL026629

USAAWCBIRD STRIKE INSP COMPLETED WITH NODAMAGE NOTED @ 3468 ACFT HRS. (TB1027R/SPEC)

01-Oct-2007 1

FT. RUCKER, AL.

TL026629

USAAWCH-60-08-AMAM-01 MAIN LANDING GEARSHOCK STRUTS C/W AT 3313.7 ACFT. HRS.(TB1027 R/SPEC)

03-Nov-2007 1

FT. RUCKER, AL.

TL026629

USAAWCH-60-08-ASAM-02 POWER AVAILABLECONTROL CABLE C/W AT 3523/4 ACFT. HRS.(TB1027 R/SPEC)

09-Nov-2007 1

FT. RUCKER, AL.

TL026629

USAAWCH-60-08-ASAM-04 PILOT'S LOWER SEAT RAILCHAFING ELECTRICAL HARNESSCOMPLETED @ 3550.3 ACFT HRS. (TB1027R/SPEC)

30-Nov-2007 1

FT. RUCKER, AL.

TL026629

USAAWCH-60-08-ASAM-03 CHANGES TO CURRENTFUEL SYSTEM INTEGRITY CHECKS C/W AT3550.3 ACFT. HRS. (TB1027 R/SPEC)

02-Dec-2007 1

FT. RUCKER, AL.

TL026629

USAAWCH-60-08-AMAM-02 TAIL ROTOR OUTBOARDRETENTION PLATE SHIMS COMPLETED @3550.3 ACFT HRS. NA TO THIS ACFT. (TB1027R/SPEC)

03-Dec-2007 1

FT. RUCKER, AL.

TL026629

USAAWCH-60-08-ASAM-05 TAIL ROTOR QUADRANTSPRING CAPSULE ASSEMBLY C/W AT 3563.3ACFT. HRS. (TB1027 R/SPEC)

15-Dec-2007 1

FT. RUCKER, AL.

TL026629

USAAWCH-60-08-SOF-01, MAIN ROTOR BLADEEXPANDABLE PIN INSPECTION CHANGECOMPLETED @ 3623.8 ACFT HRS. (TB1027R/SPEC)

28-Jan-2008 1

FT. RUCKER, AL.

TL026629

USAAWCACFT NO LONGER OPERATING IAWLIMITATIONS AND RESTRICTIONS SPECIFIEDIN AWR 1153 (JP-8+100 FUEL) DTD 19 DEC 06.(TB1027 R/SPEC)

31-Jan-2008 1

FT. RUCKER, AL.

TL026629

USAAWCH-60-08-AMAM-05 GOODRICH INTERNALRESCUE HOISTS COMPLETED @ 3640.4 ACFTHRS. (TB1027 R/SPEC)

04-Feb-2008 1

FT. RUCKER, AL.

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAAWCH-60-08-AMAM-04 H-60-08-AMAM-04 COCKPITDOOR JETTISONABLE WINDOWS COMPLETED@ 3643.0 ACFT HRS. (TB1027 R/SPEC)

08-Feb-2008 1

FT. RUCKER, AL.

TL026629

USAAWCH-60-08-AMAM-06 COMMON MISSILEWARNING SYSTEM (CMWS) SEQUENCERSCOMPLETED @ 3643.0 ACFT HRS. NA TO THISACFT (TB1027 R/SPEC)

08-Feb-2008 2

FT. RUCKER, AL.

TL026629

USAAWCH-60-08-ASAM-06 M/R PYLON SLIDINGFORWARD FAIRING C/W AT 3702.9 ACFT HRS.(TB1027 R/SPEC)

18-Mar-2008 1

FT. RUCKER, AL.

TL026629

USAAWCH-60-08-AMAM-07 AN/ASN-128B/D DOPPLERGPS NAVIGATION SET (DGNS) COMPLETEDAT 3727.7 ACFT HRS. (MB1137)

29-Mar-2008 1

FT. RUCKER, AL.

TL026629

DYNCORP INTL. RASM-EFT. CAMPELL, KY.

OCM/ACE PERFORMED AT 3734 ACFT HRS BYTEAM MEMBER 'R' (TB1027 R/SPEC)

07-Apr-2008 1

USAAWC FT. RUCKER,AL.

TL026629

USAAWCACFT OPERATING UNDER AWR (1220) TOCONDUCT A MODIFIED ENHANCEDSCHEDULED (ESM) PROGRAM SCHEDULE(REV -3 ) SUPERCEDED BY AWR 1220 R-4 DTD22 MAY 08. (TB1027 R/SPEC)

04-Jun-2008 1

FT. RUCKER, AL.

TL026629

USAAWCACFT OPERATING UNDER AWR (1220 R-4 DTD22 MAY 08) TO CONDUCT A MODIFIEDENHANCED SCHEDULED MAINTENANCE(ESM) PROGRAM AT THE UNITED STATESARMY AVIATION WARFIGHTING CENTER(USAAWC) FORT RUCKER, AL. AT3882.0 AFTHRS. (TB1027 R/SPEC)

04-Jun-2008 2

FT. RUCKER, AL.

TL026629

USAAWCH-60-08-AMAM-08 FLIGHT CONTROL RIGGINGCOMPLETED @ 3893.1 ACFT HRS. (BH0315R/SPEC)

07-Jun-2008 1

FT. RUCKER, AL

TL026629

USAACEPERMISSION GRANTED TO MONITOR THEHIRSS ASSY FOR SECURITY AND CHAFING ATEACH 40 HRS PMS OR NEXT 720 HR INSP,WHICHEVER COMES FIRST AS PER MECNUMBER F79723 AT 4027.0 ACFT HRS (DW0950, R/SPEC)

31-Jul-2008 1

FT. RUCKER,AL

TL026629

USAACEINSTALLED REPAIR PLATE ON FWD END OFL/H CARGO DOOR TRACK I/A/W MEC F79844 @4029.4 ACFT HRS. (TB1027 R/SPEC)

07-Aug-2008 1

FT. RUCKER, AL.

TL026629

USAACEUH-60-08-ASAM-01 TROOP/GUNNER SEATUPPER ENERGY ATTENUATING WIRES N/ATHIS ACFT. AT 4050.9 ACFT. HRS. (M.BELFORD 1137)

19-Aug-2008 1

FT. RUCKER, AL.

TL026629

USAACEH-60-08-ASAM-11 COMPLIED WITHREQUIREMENTS OF H-60-08-ASAM-11 FLIGHTCONTROL INSPECTION AT 4066.7 ACFT HRS.(TB1027 R/SPEC)

22-Aug-2008 1

FT. RUCKER, AL.

TL026629

USSACEOPERATE WITHIN LIMITATION ANDRESTRICTIONS SPECIFIED IN THE ENCLOSEDAWR 1251 (REV -2) DTD 01 SEP 08 @ 4090.6ACFT HRS. SUPERCEDES AWR 1241 REV 1.(TB1027 R/SPEC)

25-Sep-2008 1

FT. RUCKER, AL.

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAACEH-60-08-ASAM-13 H-60-08-ASAM-13 FIREEXTINGUISHING TUBE UNION RINGCOMPLETED AT4090.6 ACFT HRS. (TB1027R/SPEC)

29-Sep-2008 1

FT. RUCKER, AL.

TL026629

USAACEI/A/W MEC F82298 BOTH THE L/H & R/HCARGO DOOR UPPER TRACKS ARE CRACKEDAT THE FORWARD END. THE TRACK MAY BEMANUFACTURED BY EITHER A SINGLE-PIECEEXTRUSION ON LATER AIRCRAFT MODELSOR A TWO PIECE TRACK ASSEMBLY ONEARLIER AIRCRAFT MODELS. THIS REPAIR ISONLY FOR THE HORIZONTAL OUTBOARD LEGPORTION OF THE TRACK NOT FOR THEINBOARD VERTICAL LEG. (LW2720 R/SPEC)

01-Oct-2008 1

FT. RUCKER, AL

TL026629

USAACEH-60-08-ASAM-10 ELECTRICAL WIRE CHAFEISSUES COMPLETED @ 4090.6 ACFT HRS.(TB1027 R/SPEC)

03-Oct-2008 1

FT. RUCKER, AL.

TL026629

USAACEBOTH THE L/H AND R/H CARGO DOOR UPPERTRACKS ARE CRACKED AT THE FORWARDEND REPAIRED IAW MEC F82298: CLEANDAMAGED AREA, BREAKS, TEARS ANDWORN AREAS SHOULD BE TRIMMED ANDCLEANED TO CREATE SMOOTH SURFACESBLENDED INTO TRACK. BRUSH ALODINEREWORKED SURFACES AND EPOXY PRIME (1)COAT MIL-P-23377 (LW2720 R/SPEC)

03-Oct-2008 2

FT. RUCKER, AL

TL026629

USAACEH-60-08-ASAM-12 PARKER AEROSPACE AIRTURBINE STARTER (ATS) [email protected] ACFT HRS. (TB1027 R/SPEC)

11-Oct-2008 1

FT. RUCKER, AL.

TL026629

USSACET/R CABLE TENSION CK COMPLETED @4090.6 ACFT HRS. L/H 141, R/H 141 @ 22DEGREES C (TB1027 R/SPEC)

22-Oct-2008 1

FT. RUCKER, AL.

TL026629

USAACEH-60-09-SOF-01 HYDRO-MECHANICAL UNIT(HMU) H-60-09-SOF-01 COMPLETED AT 4090.6ACFT HRS. (TB1027 R/SPEC)

22-Oct-2008 2

FT. RUCKER, AL.

TL026629

USAACET/R BIAS READING COMPLETED @ 4090.6ACFT HRS. BLUE 4.050/4.383/.333, RED4.622/4.960/.338, BLACK 4.017/4.344/.327,YELLOW 4.656/4.988/.332 (TB1027 R/SPEC)

22-Oct-2008 3

FT. RUCKER, AL.

TL026629

USAACEM/R RIG CHECK COMPLETED @ 4090.6 ACFTHRS WITH NO CHANGES. (TB1027 R/SPEC)

23-Oct-2008 1

FT. RUCKER, AL.

TL026629

USAACEPMI - PHASE #7 COMPLETED @ 4090.6 ACFTHRS. PMI -PHASE #8 DUE @ 4810.6 ACFT HRS.(TB1027 R/SPEC)

24-Oct-2008 1

FT. RUCKER, AL.

TL026629

USAACET/R CABLE TENSION CK COMPLETED @ 4100ACFT HRS. R/H 160 , L/H 160 @ 24 DEGREES'C' (TB1027 R/SPEC)

06-Nov-2008 1

FT. RUCKER, AL.

TL026629

USAACEH-60-09-SOF-02 H-60-09-SOF-02 AN/ALQ-144INFRARED COUNTERMEASURE SYSTEM(IRCMS) COMPLETED @ 4104.3 ACFT HRS. NATO THIS ACFT. (TB1027 R/SPEC)

08-Nov-2008 1

FT. RUCKER, AL.

TL026629

USAACET/R CABLE TENSION CK COMPLETED @4110.1 ACFT HRS. R/H 142, L/H 140 AT 24DEGREES 'C' (TB1027 R/SPEC)

14-Nov-2008 1

FT. RUCKER, AL.

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAACEBIRD STRIKE INSP COMPLETED @ 4117.4ACFT HRS. NO DAMAGE NOTED. (TB1027R/SPEC)

18-Nov-2008 1

FT. RUCKER, AL.

TL026629

USAACEH-60-09-SOF-03 POSSIBLERETIREMENT LIFEOVERFLIGHT COMPLETED AT 4120.0 ACFTHRS. (TB1027 R/SPEC)

18-Nov-2008 2

FT. RUCKER, AL.

TL026629

USAACET/R CABLE TENSION CK COMPLETED @4129.4 ACFT HRS. R/H 165, L/H 164 AT 24DEGREES 'C' (TB1027 R/SPEC)

20-Nov-2008 1

FT. RUCKER, AL.

TL026629

USAACEOPERATE ACFT IAW AWR 1479, IMPROVEDMAIN TRANSMISSION PLANETARY CARRIERASSY @ 4140.2 ACFT HRS. (TB1027 R/SPEC)

25-Nov-2008 1

FT. RUCKER, AL.

TL026629

USAACEBLACK LEADING EDGE DROOP STOPUNSEATED. REPLACED BUSHING IAW MEOT5956A DTD 17 SEPT 2007. AFS528 (RC1002)

18-Feb-2009 1

FT. RUCKER, AL.

TL026629

USAACECOMPLIED WITH REQUIREMENTS OF H-60-09-ASAM-04 AT 4289.9 ACFT HRS. AFS728(RC1002)

28-Feb-2009 1

FT. RUCKER, AL

TL026629

USAACECOMPLIED WITH REQUIREMENTS OF H-60-09-ASAM-05 (UPDATE TO LIFE LIMIT CHANGEFOR TAIL ROTOR (TR) QUARANT SPRINGCAPSULES) AT 4302.1 ACFT HRS. AFS728(RC1002)

05-Mar-2009 1

FT. RUCKER, AL

TL026629

USAACEFORT RUCKER REQUEST GUIDANCE ONAXIAL AND RADIAL PLAY. HIRSS INNER DUCTAXIAL AND RADIAL PLAY IS ACCEPTABLEWITHOUT MONITORING UP TO 0.100INCH(MEASURED FROM 12 O'CLOCKPOSITION WITH DIAL INDICATOR MOUNTEDTO OUTER DUCT). IF PLAY EXCEEDS THE0.100 INCH LIMIT, MONITOR THE HIRSSASSEMBLY (AT EACH 40 HOUR PMS) FORSECURITY OF ALL SIX SUPPORT LINKS ANDRIVETS AND FOR CHAFING AROUND THEOUTER SURFACE OF THE INNER DUCT. ONCEIDENTIFIED, HIRSS ASSEMBLIES WITHEXCESSIVE PLAY SHALL REMAIN IN SERVICEAS LONG AS SUPPORT LINKS AND RIVETSARE SECURE AND NO CRACKS ARE FOUND.MEO NO. A5826 REV B. DATED 14 NOV 2008 INCONJUCTION WITH MEC F79684 DATED 31 JU

26-Mar-2009 1

FT. RUCKER, AL

TL026629

USAACEH-60-09-ASAM-07 H-60-09-ASAM-07, FIREEXTINGUISHER WIRING (BREAKAWAYTHREAD) COMPLETED AT 4376 ACFT HRS.(JB2761)

08-Apr-2009 1

FT. RUCKER, AL.

TL026629

USAACECOMPLIED WITH REQUIREMENTS OF H-60-09-ASAM-09 (FIRE EXTINGUISHER WIRING(BREAKAWAY THREAD)) AT 4445.6 ACFT HRS.AFS761 (RC1002)

08-May-2009 1

FT. RUCKER, AL

TL026629

USAACET/R BIAS READING COMPLETED @ 4448.7ACFT HRS. BLUE 3.704/4.001/.279, RED4.310/4.605/.295, BLACK 3.700/3.990/.290,YELLOW 4.315/4.610/.295. (RC1002)

09-May-2009 1

FT. RUCKER, AL

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAACECOMPLIED WITH REQUIREMENTS OF H-60-09-ASAM-09 (FIRE EXTINGUISHER WIRING(BREAKAWAY THREAD)) AT 4445.6 ACFT HRS.AFS761 (RC1002)

12-May-2009 1

FT. RUCKER, AL

TL026629

USAACE#2 CROSSFEED BREAKAWAY VALVE WASREPLACED @ 4469.0 ACFT HRS. (RC1002)

16-May-2009 1

FT. RUCKER, AL

TL026629

USAACEH-60-09-ASAM-08 ENGINE COWLING WEIGHTRESTRICTION COMPLETED AT 4485.4 ACFTHRS. (TB1027 R/SPEC)

24-May-2009 1

FT. RUCKER, AL.

TL026629

USAACECOMPLIED WITH REQUIREMENTS FOR H-60-09-ASAM-11 (CARGO DOOR WINDOWEMERGENCY JETTISON HANDLE ASSEMBLY)@ 4576.9 ACFT HRS. (JC6208 R/SPEC)

27-Jun-2009 1

FT. RUCKER, AL

TL026629

USAACEAIRCRAFT OPERATING WITHIN LIMITATIONSAND RESTRICTIONS SPECIFIED IN AWR 1514,DATED 31 JUL 08. (RC1002)

03-Aug-2009 1

FT. RUCKER, AL

TL026629

USAACEACFT GROUNDED FOR H-60-09-ASAM-07 ANDH-60-09-ASAM-09 NOT COMPLIED WITH.COMPLETED BY AFS510 AT 4636.8 ACFT HRS.(RC1002)

17-Aug-2009 1

FT. RUCKER, AL

TL026629

USAACECOMPLIED WITH REQUIREMENTS OF GEN-09-AMAM-03 ULLS-A (E) AT 4657.6 ACFT HRS.AFS791 NOT APPLICABLE TO THIS ACFT DUENOT UTILIZING ULLS-A(E) SYSTEM. (RC1002)

26-Aug-2009 1

FT. RUCKER, AL

TL026629

USAACEH-60-09-AMAM-04 H-60-09-AMAM-04 CO-PILOTSEAT INTERFERENCE WITH ARMY AIRBORNCOMMAND CONTROL SYSYEM (A2C2S)COMPLETED AT 4667.7 ACFT HRS. *** N/A(A2C2S) NOT INSTALLED. (AFS651). (JB2761R/SPEC)

27-Aug-2009 1

FT. RUCKER, AL.

TL026629

USAACECOMPLIED WITH REQUIREMENTS OF H-60-09-AMAM-06 AT 4657.6 ACFT HRS. CARGO HOOKCARTRIDGE ACTUATED DEVICE (CAD) LIFEREDUCTION. AFS793 (JB2761 R/SPEC)

28-Aug-2009 1

FT. RUCKER, AL.

TL026629

USAACET/R CABLE TENSION CK COMPLETED @4686.0 ACFT HRS. R/H 168, L/H 166 AT 26DEGREES 'C' (DW0950 R/SPEC)

05-Sep-2009 1

FT RUCKER,AL

TL026629

USAACET/R BIAS READING COMPLETED @ 4686.0ACFT HRS RED4.836/4.503/.333 BLUE4.238/3.905/.333 YELLOW4.947/4.613/.334BLACK 4.320/3.987/.333 (DW0950 R/SPEC)

08-Sep-2009 1

FT RUCKER,AL

TL026629

CSC RASM-E AFMAOCM/ACE PERFORMED AT 4689.9 ACFT HR BYTEAM MEMBER QQ AMCOM RASM-E. (LS2032)

14-Sep-2009 1

FT. CAMPBELL, KY.

TL026629

USAACEH-60-09-AMAM-07 HALON HAND-HELD FIREEXTINGUISHERS (HHFE) C/W AT 4696.3 ACFTHRS. AFS784 BOTH FAILED. (RC1002)

17-Sep-2009 1

FT. RUCKER, AL

TL026629

USAACET/R BIAS READING COMPLETED @ 4696.3ACFT HRS RED4.801/5.135/.334 BLUE4.119/4.454/.335 YELLOW4.723/5.061/.338BLACK 4.139/4.472/.333 (RC1002)

17-Sep-2009 2

FT. RUCKER, AL

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAACET/R BIAS READING COMPLETED @ 4696.3ACFT HRS RED4.777/5.092/.315 BLUE4.120/4.435/.315 YELLOW 4.711/5.024/.313BLACK 4.072/4.385/.313 (RC1002)

20-Sep-2009 1

FT. RUCKER, AL

TL026629

USAACET/R CABLE TENSION CK COMPLETED @4696.3 ACFT HRS. R/H 166, L/H 164 AT 24DEGREES 'C' (RC1002)

20-Sep-2009 2

FT. RUCKER, AL

TL026629

USAACETRANSMISSION OIL FILTER IMPENDINGBYPASS BUTTON POPPED. REPLACE STAGE1 FILTER AND RESET BUTTON - NO METALFOUND. (AFS745) TSN FOR TRANSMISSIONSN: A26501483 = 4024. (AIRCRAFT 8724673 AT4696.3 ACFT HRS.) (RC1002)

22-Sep-2009 1

FT. RUCKER, AL

TL026629

USAACET/R CABLE TENSION CK COMPLETED @4696.3 ACFT HRS.(FAILED, READJUSTED) R/H150, L/H 150 AT 24 DEGREES 'C') (MH1534)

25-Sep-2009 1

FT. RUCKER, AL

TL026629

USAACEBOTH THE L/H AND R/H CARGO DOOR UPPERTRACKS ARE CRACKED AT THE FORWARDEND REPAIRED IAW MEC F82298: CLEANDAMAGED AREA, BREAKS, TEARS ANDWORN AREAS SHOULD BE TRIMMED ANDCLEANED TO CREATE SMOOTH SURFACESBLENDED INTO TRACK. BRUSH ALODINEREWORKED SURFACES AND EPOXY PRIME (1)COAT MIL-P-23377 (LW2720 R/SPEC)

03-Oct-2009 1

FT. RUCKER, AL

TL026629

USAACET/R CABLE TENSION CK COMPLETED @4716.3 ACFT HRS.(FAILED, 1ST READING 24*C150, 150; 2ND 22*C 120, 120; ADJ 22*C 135,135.) (RC1002)

07-Oct-2009 1

FT. RUCKER, AL

TL026629

USAACET/R CABLE TENSION CK COMPLETED @10722.3 ACFT HRS L/H 141, R/H 141@ 22DEGREES 'C'. (9-11 HR CHK NOT REQ - NOADJUSTMENTS MADE DURING RIG) (RC1002)

08-Oct-2009 1

FT. RUCKER, AL

TL026629

USAACEPERMISSION TO DEVIATE FROM MANUAL ANDBE ABLE TO REPLACE HARDWARE ON THETAIL ROTOR SYSTEM OF THE UH-60AASSIGNED TO FT. RUCKER WITH LIKEHARDWARE WITHOUT THE REQUIREMENT OFA TAIL ROTOR BALANCE I/A/W MEC F97372. ACOPY OF THIS MEC 97372 IS LOCATED IN THEHISTORICAL RECORDS. (LW2720 R/SPEC)

21-Oct-2009 1

FT. RUCKER, AL

TL026629

USAACEMANUFACTURE DATE JUNE 1988. (LW2720R/SPEC)

02-Nov-2009 1

FT. RUCKER, AL

TL026629

USAACECOMPOSITE SKIN ON LEFT HAND ENGINECOWLING DOOR HAS A VOID IN HONECOMBAPPROXIMATELY 19 X 7 INCHES. REQUESTTO REPAIR USING PROCEDURES IN WP 037900 TM 1-1520-237-23-6 AND TM 1-1500-204-23-10 GENERAL AIRCRAFT MAINTENACEMANUAL I/A/W MEC F100474. A COPY OF THISMEC F100474 IS LOCATED IN THE HISTORICALRECORDS. (LW2720 R/SPEC)

03-Nov-2009 1

FT. RUCKER, AL

TL026629

USAACEAIRCRAFT OPERATING WITHIN LIMITATIONSAND RESTRICTIONS SPECIFIED IN AWR 1455,DATED 23 OCT 09 REV.1 (CAP) @ 4777.5AIRCRAFT HOURS (LW2720 R/SPEC)

05-Nov-2009 1

FT. RUCKER,A L

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAACEH-60-10-AMAM-04 ASN-128 B/C DOPPLERGLOBAL PISITONING SYSTEM GPSNAVIGATION SET C/W @ 4777.5 AIRCRAFTHOURS (LW2720 R/SPEC)

11-Nov-2009 1

FT. RUCKER, AL

TL026629

USAACEH-60-10-ASAM-03 FIRE BOTTLE DISCHARGELINES AND NOZZLE @ 4777.5 AIRCRAFTHOURS. (LW2720 R/SPEC)

18-Nov-2009 1

FT. RUCKER, AL

TL026629

USAACEM/R RIG CHECK COMPLETED @ 4777.5 ACFTHRS WITH NO CHANGES. (LW2720 R/SPEC)

18-Nov-2009 2

FT. RUCKER, AL

TL026629

USAACET/R BIAS READING COMPLETED @ 4777.5:RED: 4.937-4.612=.325, YELLOW: 4.935 - 4.610 =.325, BLACK: 4.362 - 4.037= .325, BLUE: 4.363 -4.038= .325 (LW2720 R/SPEC)

19-Nov-2009 1

FT. RUCKER, AL

TL026629

USAACEH-60-10-ASAM-04 STABILITY AUGMENTATIONSYSTEM (SAS) LINKS. C/W @ 4777.5 AIRCRAFTHOURS. (LW2720 R/SPEC)

19-Nov-2009 2

FT. RUCKER, AL

TL026629

USAACET/R CABLE TENSION CK COMPLETED @4777.5 ACFT HRS L/H 150 @ 18°, R/H 150 @ 18°.(LW2720 R/SPEC)

19-Nov-2009 3

FT. RUCKER, AL

TL026629

USAACE720 HOUR PMI 8 COMPLETED @ 4777.5 ACFTHRS. NEXT PMI 9 DUE @ 5497.5 ACFT HRS.(LW2720 R/SPEC)

20-Nov-2009 1

FT. RUCKER, AL

TL026629

USAACEAIRCRAFT NO LONGER OPERATING IAW 1479DTD 04 JAN 08 (IMPROVED MAINTRANSMISSION PLANETARY CARRIER ASSY)@ 4827 ACFT HRS. (LW2720 R/SPEC)

04-Jan-2010 1

FT. RUCKER, AL

TL026629

USAACEGEN-10-AMAM-02 DISTRIBUTION OF NEWACFT ELECTRONIC LOGBOOK, N/A THISLOCATION, C/W AT 4846.9 (LW2720 R/SPEC)

26-Jan-2010 1

FT. RUCKER, AL

TL026629

USAACEH-60-10-AMAM-11 OIL SAMPLING CHANGESCOMPLETED AT 4853.6 ACFT. HRS. (LW2720R/SPEC)

01-Feb-2010 1

FT. RUCKER, AL

TL026629

USAACECOMPLIED WITH THE REQUIRMENTS OF TB 1-1520-237-23-9 AND TB 1-1520-237-23-10 NLT 31MARCH 2010. (FUEL CELL CORROSIONINSPECTION) @ 4853.6 ACFT HRS. (LW2720R/SPEC)

02-Feb-2010 1

FT. RUCKER,AL

TL026629

USAACEH-60-10-ASAM-06 (AUTO IGNITION ANDTRANSIENT DROOP IMPROVEMENT TDIMODIFICATION) NLT 16 FEB 10 C/W @ 4881.3ACFT HRS. (LW2720 R/SPEC)

10-Feb-2010 1

FT. RUCKER, AL

TL026629

USAACEH-60-10-AMAM-05 ULLSA IMMC LCF CHANGE60B C/W AT 4777.5 ACFT HOURS. (LW2720R/SPEC)

13-Feb-2010 1

FT. RUCKER, AL

TL026629

USAACEAIRCRAFT NO LONGER OPERATING WITHINLIMITATION AND RESTRICTIONS SPECIFIED INTHE ENCLOSED AWR 1251 (REV -2) DTD 01SEP 08 @ 4921.8 ACFT HRS. SUPERCEDES BYAWR 1251 REV 3 DTD 26 FEB 10. (LW2720R/SPEC)

01-Mar-2010 1

FT. RUCKER, AL

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAACEAIRCRAFT OPERATING WIHTIN LIMITATIONSAND RESTRICTIONS SPECIFIED IN THEENCLOSED AWR 1251, DTD 26 FEB 10 REV.3.(EYEBOLT) @ 4921.8 AIRCRAFT HOURS.(LW2720 R/SPEC)

01-Mar-2010 2

FT. RUCKER, AL

TL026629

USAACEACFT OPERATING WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1639DATED 26 JAN 10(BFT/EDM). COMPLETD AT4997.3 ACFT HRS. (MB1137)

25-Mar-2010 1

FT. RUCKER, AL.

TL026629

CSCOCM/ACE PERFORMED AT 4997 ACFT HRS BYTEAM MEMBER DD AMCOM RASME-E (JB9001)

09-Apr-2010 1

FT. CAMPBELL KY

TL026629

USAACECOMPLIED WITH REQUIREMENTS OF H-60-10-AMAM-12 @ 5052.5 ACFT HRS. (IMPROVEDDRAG BEAM) INSP L/H SIDE FAILED. (SC2006,R/SPEC INSP: AFS 758)

04-May-2010 1

FT. RUCKER, AL

TL026629

USAACEAIRCRAFT NO LONGER OPERATING IAWLIMITATIONS AND RESTRICTIONS SPECIFIEDIN AWR 927 DATED 06 JUN 03 (SLAB). (RC1002(AFS 594))

19-May-2010 1

FT. RUCKER, AL

TL026629

USAACEAIRCRAFT OPERATING IAW AWR 1681, DATED10 MAY 10 (EH-60 DEMOD). (RC1002)

19-May-2010 2

FT. RUCKER, AL

TL026629

USAACEH-60-10-ASAM-07 STABILATOR HINGEFITTINGS C/W AT 5106.1 ACFT HRS (CC0409(AFS758))

20-May-2010 1

FT. RUCKER, AL

TL026629

USAACEM/R RIG CHECK COMPLETED @ 5119.7 ACFTHRS. WITH NO CHANGES. (TB1027 R/SPEC)

26-May-2010 1

FT. RUCKER, AL.

TL026629

USAACEACFT NO LONGER OPERATING UNDER AWR(1220 R-4 DTD 22 MAY 08) TO CONDUCT AMODIFIED ENHANCED SCHEDULEDMAINTENANCE (ESM) PROGRAM AT THEUNITED STATES ARMY AVIATIONWARFIGHTING CENTER (USAAWC) FORTRUCKER, AL. AT 5129.5 ACFT HRS.SUPERCEDED BY AWR 1220 REV. 5 DTD 28MAY 10. (LW2720)

02-Jun-2010 1

FT. RUCKER, AL

TL026629

USAACEACFT OPERATING IAW MAINTAIN AIRCRAFTAS PRESCRIBED IN AIRWORTHINESS 1220DTD 28 MAY 10 REV. 5 (ENCHANCEDSCHEDULED MAINTEANCE) ACFT HOURS @5129.5. (LW2720)

02-Jun-2010 2

FT. RUCKER, AL

TL026629

USAACET/R BIAS COMPLETED @ RED: 4.608 -4.270=.338, YELLOW: 4.590 - 4.253= .337 BLACK:3.992 - 3.660 = .332, BLUE: 3.934 - 3.608 = .326(LW2720)

04-Jun-2010 1

FT. RUCKER, AL

TL026629

USAACEH-60-10-ASAM-08 APU AND APU FIREWALLC/W AT 5136.0 ACFT HOURS. (FAILED)(LW2720 R/SPEC)

08-Jun-2010 1

FT. RUCKER,AL

TL026629

USAACEH-60-10-SOF-02 SPINDLE LUG NDI ANDRETIREMENT LIFE CHANGES C/W AT 5158.6AIRCRAFT HOURS. (LW2720 R/SPEC)

22-Jun-2010 1

FT. RUCKER,AL

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAACEH-60-10-AMAM-16 COMMON MISSILEWARNING SYSTEM GUARDED DISPENSESWITCH C/W AT 5168.0 AIRCRAFT HOURS.(LW2720 R/SPEC)

25-Jun-2010 1

FT. RUCKER,AL

TL026629

USAACEAIRCRAFT TRANSFERRED TO HUNTSVILLE,ALFOR PAINT ON THIS DATE @ ACFT HRS5185.9. (DW 0950, REC/SPEC)

12-Jul-2010 1

FT RUCKER,AL

TL026629

USAACEMEC F104952B, WAIVER FROM REQUIREMENTOF TTS 78148 TO INSPECT SEC IVDRIVESHAFT, EXTENDED FOR 90 DAYS FROM19JUL10. THIS ENTRY SERVES FOR NOTICEOF EXPIRATION ALSO AND WILL NOTREQUIRE A SEPARATE ENTRY FOR SUCH.

19-Jul-2010 1


DK011063

SESIAIRCRAFT PAINTED IAW TM 55-1500-345-23AMD M.E.O. A11160D @ 5191.3 ACFT HRSUSING MIL-P-23377 AND MIL-DT1-64159(DH72376)

26-Jul-2010 1

HUNTSVILLE, AL.

TL026629

USAACEAIRCRAFT RETURNED FROM SESI,HUNTSVILLE,ALABAMA AT 5193.9 ACFT HRS.(DW 0950, REC/SPEC)

28-Jul-2010 1

FT. RUCKER, AL.

TL026629

USAACEMEC F112579 - STRUCTURE (COWLING,DOORS, ETC) - RIGHT HAND APU DOOR HASVOID GREATER THAN 2 INCHES IN DIAMETEREXCEEDING REPAIR LIMIT IN TM 1-1520-237-6.ACCORDING TO MEC F112579, USESTANDARD REPAIR AND HONEYCOMBREPLACEMENT IAW TM 1-1520-237-23-6 WP0387 00 AND 1-1500-204-23 SERIES. COPY OFMEC CAN BE FOUND IN HISTORICALRECORDS. 5193.9 ACFT HRS. (RC1002)

29-Jul-2010 1

FT. RUCKER, AL.

TL026629

USAACEAIRCRAFT NO LONGER OPERATING WITHINLIMITATIONS AND RESTRICTIONS SPECIFIEDIN AWR 1514, DATED 31 JUL 08 @ 5704AIRCRAFT HRS. SUPERCEDED BY AWR 1514DTD O3 AUG 10 REV 1. (LW2720 R/ SPEC)

03-Aug-2010 1

FT. RUCKER, AL.

TL026629

USAACEAIRCRAFT OPERATING WITHIN LIMITATIONSAND RESTRICTIONS SPECIFIED IN AWR 1514REF. 1 DTD 03 AUG 10. (LW2720 R/ SPEC)

03-Aug-2010 2

FT. RUCKER, AL.

TL026629

USAACEH-60-10-ASAM-11 COMMON COMPONENTRETIREMENT CHANGE TIMES UPDATE C/W AT5198 AIRCRAFT HOURS. (LW2720 R/ SPEC)

03-Aug-2010 3

FT. RUCKER, AL.

TL026629

USAACEH-60-10-ASAM-12 T700 SERIES ENGINESCOMMON COMPONENT RETIREMENT CHANGETIMES C/W AT 5213.4 AIRCRAFT HOURS.(LW2720 R/ SPEC)

10-Aug-2010 1

FT. RUCKER, AL.

TL026629

USAACEH-60-10-ASAM-15 IMPROVED EXTERNALSTORES SUPORT SYSTEM (ESSS) FUELSYSTEM VENT BLOW @ 5218.7 AIRCRAFTHOURS (LW2720 R/ SPEC)

12-Aug-2010 1

FT. RUCKER, AL.

TL026629



8.7.DATE

6.REMARKS

4. 5.



USAACERIGHT OIL COOLER ACCESS DOOR HASDEBOND GREATER THAN 2 INCHES INDIAMETER EXCEEDING REPAIR LIMITS IN TM 1-1520-237-23-6 AUTHORIZATION IS GRANTEDTO REPAIR IAW MEC F113315 . A COPY OFTHIS MEC IS LOATED IN THE HISTORICALRECORDS @ 5230.1 ACFT HRS. (DW0950 R/SPEC)

13-Aug-2010 1

FT. RUCKER, AL.

TL026629

USAACEACFT NO LONGER OPERATING WITHINLIMITATIONS AND RESTRICTIONS SPECIFIEDIN AWR 1639 DATED 26 JAN 10(BFT/EDM).COMPLETD AT 5239.1 ACFT HRS.SUPERCEDED BY REV. 2 DTD 28 MAY 10.(LW2720 R/ SPEC)

18-Aug-2010 1

FT. RUCKER, AL.

TL026629

USAACEAIRCRAFT OPERATING WITH LIMITATIONSAND RESTRICTIONS SPECIFIED IN AWR 1639REV. 2 DTD 28 MAY 10 (BFT/EDM) @ 5239.1AIRCRAFT HOURS. (LW2720 R/ SPEC)

18-Aug-2010 2

FT. RUCKER, AL.

TL026629

USAACET/R BIAS COMPLETED @ 5253.2 AIRCRAFTHOURS: RED: 5.02 - 4.69 = .33, BLACK: 4.28 -3.95 = .33, YELLOW: 5.02 - 4.69 = .33, BLUE:4.28 - 3.95 = .33 (LW2720 R/ SPEC)

03-Sep-2010 1

FT. RUCKER, AL.

TL026629

USAACEUH-60-10-ASAM-16 RESCURE HOIST CABLECUT HARNESS CONNECTOR @ 5255.3AIRCRAFT HOURS. (LW2720 R/ SPEC)

09-Sep-2010 1

FT. RUCKER, AL.

TL026629

USAACET/R CABLE TENSION COMPLETED @ 5261.7AIRCRAFT HOURS: L/H: 169, R/H: 170 @ 32°(LW2720 R/ SPEC)

14-Sep-2010 1

FT. RUCKER, AL.

TL026629

USAACET/R CABLE TENSION COMPLETED @ 5271.7AIRCRAFT HOURS: L/H: 150, R/H: 150 @ 25°(LW2720 R/ SPEC)

22-Sep-2010 1

FT. RUCKER, AL.

TL026629

USAACET/R BIAS COMPLETED @ 5286.8 AIRCRAFTHOURS: BLACK: 4.29 -3.95= .34, YELLOW: 5.04- 4.70 = .34, BLUE: 4.33 - 4.00= .33, RED: 5.04 -4.70 = .34 (LW2720 R/ SPEC)

30-Sep-2010 1

FT. RUCKER, AL.

TL026629

USAACE, FT. RUCKER,AL

H-60-11-AMAM-03 , OIL COOLER FAN AXIALBEARING C/W AT 5328.9 AIRCRAFT HRS

27-Oct-2010 1

LOWE AHP

LW012211

USAACE, FT.RUCKER,AL

H-60-11-AMAM-04 (ULLS-A(E) (IMMC) LCFCHANGE 61) C/W AT 5328.9 AIRCRAFT HRS

27-Oct-2010 2

LOWE AHP

LW012720


H-60-11-ASAM-03 HAMILTON STANDARDHYDRO-MECHANICAL UNITS (HMU) @ 5379.4AIRCRAFT HOURS

29-Nov-2010 1

LOWE AHP

LW012720

USAACE,FT.RUCKER,AL

H-60-11-ASAM-04 AN/ARN-153 TCN-500 TACANRECEIVER BEARING ERROR C/W AT 5382.7ACFT HRS

02-Dec-2010 1

LOWE AHP

VM4663

USAACE,FT,RUCKER,ALT/R BIAS COMPLTED AT 5460.5 AIRCRAFTHOURS RED; 5.084/4.745=.541,BLACK;4.326/3.990=.336, YELLOW:5.077/4.723=.354, BLUE ; 4.353/4.011=.342

20-Jan-2011 1

LOWE AHP

LW2720



8.7.DATE

6.REMARKS

4. 5.



USAACE,FT,RUCKER,AL

H-60-AA-AMAM-06, MEDICAL CAROUSELREFURBISHMENT C/W AT 5467.5 ACFT HRS

07-Feb-2011 1

LOWE AHP

TP011634


H-60-11-AMAM-06 MEDICAL CAROUSELREFURBISHMENT C/W AT 5467.5 N/A THISACFT

07-Feb-2011 2

LOWE AHP

VM014663


RIGHT HAND BEADED PANEL HAS 7CRACKED BEADS, IN ADDITION THE RIGHT34.5 CHANNEL IS CRACKED AT AFT 308 TAB.AUTHORIZATION GRANTED TO REPAIR 34.5REFERENCING AJM-BL34-1C TM 1-1520-237-23-6 SNF TM 1-1500-204-23 SERIES I/A/W MECF121818A @ 5467.5 ACFT HRS. COPY OF THISMEC IS LOCATED IN THE HISTORICALRECORDS

25-Feb-2011 1

LOWE AHP

DW0950


LEFT ENGINE COWLING HAS 3 VOIDSGREAER THAN 2 INCH IN DIAMETEREXCEEDING LIMITS IN TM 1-1520-237-23-6.AUTHORIZATION GRANTED TO REPAIR BYCORE REPLACEMENT (IF NECESSARY) ANDSKIN OVERLAY I/A/W MEC F122412 @ 5467.5ACFT HRS. A COPY OF THIS MEC IS LOCATEDIN THE HISTORICAL RECORDS

25-Feb-2011 2

LOWE AHP

DC011002


M/R RIG CHECK COMPLETED @ 5467.5 ACFTHRS. PRIMARY SERVO CONTROL ROD BIAS:FWD IS 1 FLAT IN. AFT IS 1 FLAT OUT LAT IS1/4 FLAT IN. (VM4663)

02-Mar-2011 1

LOWE AHP

DC011002

USAACET/R BIAS IS YELLOW 4.722/ 5.045, .334, RED4.715/5.045, .333, BLUE 3.898/4.238, .340,BLACK 3.962/4.296, .334

02-Mar-2011 2

LOWE AHP

DC011002


H-60-11-ASAM-08 LOS / IFF ANTEENA ANDIVHMS ACCELEROMETER CONNECTORSSAFETY WIRE C/W AT 5468 ACFT HRS.

04-Mar-2011 1

LOWE AHP

DC011002


720 HOUR PMI 9 COMPLETED @ 5497.5 ACFTHRS. NEXT PMI 10 DUE @ 6187.5 ACFT HRS.

05-Mar-2011 1

LOWE AHP

DC011002


T/R CABLE TENSION IS L/H 155 AND R/H 155TEMP 23* C @ 5467.5 ACFT HRS.

05-Mar-2011 2

LOWE AHP

DC011002


T/R CABLE TENSION CHECK IS L/H:136, R/H:137 @ 16 C. @ 5478.8 ACFT HRS

09-Mar-2011 1

LOWE AHP

JK015371


H-60-11-ASAM-09 (INTERNAL AUXILIARY FUELTRANSFER SYSTEM) C/W @ 5517.9 AIRCRAFTHOURS--INTERNAL AUXILARY FUELTRANSFER SYSTEM NOT INSTALLED.(LW2720)

29-Mar-2011 1

LOWE AHP

TL026629

USAACEAIRCRAFT OPERATE WITHIN LIMITATIONSAND RESTRICTION SPECIFIED IN AWR 1505REV 3 DTD 21 OCT 09 (MICRON METAL MESHHYD FILTER) C/W @ 5517.9 AIRCRAFT HOURS.(LW2720 R/SPEC)

29-Mar-2011 2


LW012720



8.7.DATE

6.REMARKS

4. 5.



USAACEDELAYED ENTRY: ACFT INDUCTED INTOULLS-A(E) ON (DATE) AT 5517.9 ACFT HRS.

06-Apr-2011 1


DK011063

USAACEH-60-11-AMAM-11 AWR STATUS UPDATE C/W@ 5583.7 ACFT HRS, N/A TO ACFT BY SERIALNUMBER

21-Apr-2011 1


OW010950

USAACE,H-60-11-AMAM-11 AIRWORTHINESS RELEASESTATUS UPDATE C/W @ 6162.3 AIRCRAFTHOURS. N/A TO AIRCRAFT BY SERIALNUMBER.

22-Apr-2011 1


LW012720

USAACEH-60-11-AMAM-09, 19-3 ENGINE COMPONENTOPERATING HOUR RECORD C/W @ 5660.9AIRCRAFT HOURS.

17-May-2011 1


LW012720

CSCOCM/ACE PERFORMED AT 5679.8 ACFT HRSBY TEAM MEMBER . R. AFMA RASM-E.

26-May-2011 1

FT.CAMPBELL, KY.42223

DK011063

USAACEM/R RIG CHECK COMPLETED @ 5680.3 ACFTHR WITH NO CHANGES.( LW2720 R/SPEC)

02-Jun-2011 1


PH012264

USAACEH-60-11-AMAM-13, EXTERNAL RESUCE HOISTMOUNT FITTING C/W @ 5684.9 AIRCRAFTHOURS. N/A TO AIRCRAFT.

13-Jun-2011 1


LW012720

USAACETAIL PYLON RIGHT STABILATOR FITTINGINBOARD BEARING WAS WORN ANDREMOVED FOR REPLACMENT, AFTERREMOVAL IT WAS FOUND THE LINER HADCORROSION DAMGE. AUTHORIZATIONGRANTED TO BE REPLACE THE LINERS ANDSPHERICAL BEARINGS/BUSHINGS ON THERIGHT STABILATOR FITTING REFERENCEINGDMR 1-1520-237-30 I/AW MEC F128488 @5693.5 AIRCRAFT HOURS. COPY OF THIS MECIS LOCATED IN THE HISTORICAL REOCRDS.(LW2720 R/SPEC)

17-Jun-2011 1


LW012720

USAACEINSTRUCTION FOR WORK PERFORMED ONTAIL PYLON RIGHT STABILATOR FITTING,MEC# F128488 SPECIFICALLY REQUESTAUTHORAZATION FOR L/H STABILATORFITTNG REFERENCING DMWR 1-1520-237-3TASK 0349 PARA 2A STEP 1 THRU 19SIKORSKY DRAWING 700700-20588 AND FAN-718. PARA 2B IS INSTRUCTION FOR R/HSTABILATOR FITTING (ACTION TAKEN: MECMODIFIED. MEC F128488 (A) CORRECT ANDAPPLIES TO REPAIR C/W @ 5693.5 AIRCRAFTHOURS. (LW2720 R/SPEC)

23-Jun-2011 1


LW012720

USAACEH-60-11-ASAM-11, ANTI-ICE/START BLEEDVALVE ACUTATOR SHAFTS @ C/W 5703.5AIRCRAFT HOURS. (LW2720 R/SPEC)

30-Jun-2011 1


LW012720

USAACEAIRCRAFT OPERATE WITHIN LIMTATIONSAND RESTRICTIONS SPECIFIED IN AWR 1639R3 DTD 1 JUNE 11 C/W @ 5703.5 AIRCRAFTHOURS. (LW2720 R/SPEC)

01-Jul-2011 1


LW012720



8.7.DATE

6.REMARKS

4. 5.



USAACEAIRCRAFT NO LONGER OPERATING WITHLIMITATIONS AND RESTRICTIONS SPECIFIEDIN AWR 1639 REV. 2 DTD 28 MAY 10 (BFT/EDM)@ 5703.5 AIRCRAFT HOURS. SUPERCEDED BY1639 REV 3 DTD 01 JUNE 11 (LW2720 R/ SPEC)

01-Jul-2011 2


LW012720

USAACEH-60-11-ASAM-13, ENGINE AIR INLET ANTI-ICING VALVE C/W @ 5706.1 AIRCRAFT HOURS(LW2720 R/SPEC)

05-Jul-2011 1


LW012720

USAACEH-60-11-SOF-01, DISCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS C/W @ 5716.9AIRCRAFT HOURS (LW2720 R/SPEC)

08-Jul-2011 1


LW012720

USAACEH-60-11-AMAM-15, IVHMS ACCELEROMETERSC/W @ 5731.9 AIRCRAFT HOURS (LW2720R/SPEC)

19-Jul-2011 1


LW012720

USAACEH-60-11-ASAM-14, ENGINE COWLING REPAIRRESTRICTIONS C/W 5750.5 AIRCRAFT HOURS(LW2720 R/SPEC)

21-Jul-2011 1


LW012720

USAACEDELAYED ENTRY: HUD TGT AMPLIFIERDISCONNECTS PER MEO A6206 REV. A UNITC/W @ 5550.9 GRANTED I/A/W MEC 125063DTD 12 APR 11. COPY OF THIS MEC ISLOCATED IN THE HISTORICAL RECORDS.(LW2720)

10-Aug-2011 1


LW012720

USAACEDELAYED ENTRY: FAN AXIAL SN:9L9700054SB REFERENCING MEC 79159 DTD17 JUL 08. NO LONGER ON AIRCRAFT(LW2720)

10-Aug-2011 2


LW012720

USAACEDELAYED ENTRY: L/H UPPER CARGO DOORTRACK IS CRACKED AT THE FWD END.CURRENTLY THERE IS A LONG LEAD TIMEFOR NEW TRACKS. ONLY ONE REPAIRALLOWED FOR EVERY 24" OF TRACK.AUTHORIZATION GRANTED TOR REPAIR I/A/WMEC F79844 DTD 04 AUG 08. LH UPPER DOORTRACK PART NUMBER 70217-02702-049. ACOYP OF THIS MEC LOCATED IN THEHISTORICAL RECORDS. (LW2720)

10-Aug-2011 3


LW012720

USAACEDELAYED ENTRY: MAIN TRANSMISSION SN:A265-01483 REFERENCING MEC F792554 DTD18 MAY 09. NO LONGER ON AIRCRAFT.(LW2720 R/SPEC)

10-Aug-2011 4


LW012720

USAACEDELAYED ENTRY: INSERTS (ITEM 52, FIGURE13, TM 55-2835-208-23P) ARE STRIPPED OUTON THE APU . AUTHORIZATION GRANTEDI/A/W MEC F64873 DTD 20 JUL 07 REPAIRREPLACE INSERTS IAW DMWR 1-2835-214.(LW2720)

10-Aug-2011 5


LW012720

USAACEDELAYED ENTRY: TAIL ROTOR BLADE SN:A009-04165 REFERENCING MEC F82988 DTD15 OCT 08 NO LONGER ON AIRCRAFT(LW2720)

10-Aug-2011 6


LW012720



8.7.DATE

6.REMARKS

4. 5.



USAACETAIL ROTOR RIG CHECK C/W @ 5824.7AIRCRAFT HOURS: BLUE: 4.105 - 4.437 = 0.332,YELLOW: 4.749 -5.077 = 0.328, BLACK: 4.031 -4.365 = 0.334, RED: 4.761 - 5.093 = 0.332(LW2720 R/SPEC)

04-Sep-2011 1


LW012720

USAACEH-60-11-AMAM-20, AN/ASN-128D DOPPLERAND AMPS SOFTWARE @ 5859.4 AIRCRAFTHOURS. (LW2720 R/SPEC)

22-Sep-2011 1


LW012720

USAACECOMPLIED WITH H-60-12-SOF-01 @ 5891.3ACFT HRS.

08-Oct-2011 1


VM014663

USAACEH-60-12-SOF-02 (TAIL ROTOR INTERMEDIATEGEARBOX) C/W AT 5891.3 ACFT HRS.

11-Oct-2011 1


DC011002

USAACEH-60-12-SOF-03 (TAIL ROTOR INTERMEDIATEGEARBOX) C/W AT 5901.0 ACFT HRS. (AFS494).

14-Oct-2011 1


BH020315

USAACETRANSMISSION FILTER IMPENDING BYPASSINDICATOR BUTTON POPPED FOUND ONPREFLIGHT (ACTION TAKEN: REMOVED,INSPECTED AND REPLACED 1ST AND 2NDSTAGE M/MOD FITLERS IAW WP # 0657) MAINMODULE TSN: 3943 MAIN MODULE HOURS ON(8724673 @ 5901 AIRCRAFT HOURS. (LW2720R/SPEC)

14-Oct-2011 2


LW012720

USAACEH-60-11-AMAM-19 (IMMC LCF CHG 62REQUIREMENTS )C/W @ 5926.3 ACFT HRS

22-Oct-2011 1


JB012761

USAACEAIRCRAFT NO LONGER OPERATE WITHLIMITATION AND RESTRICTION SPECIFIED INAWR 1505 REV 30 DTD 21 OCT 09 (MOCRONMETAL MESH HYD) C/W @ 5926.3 AIRCRAFTHOURS. SUPERCEDED BY AWR 1505 REV. 4DTD 21 OCT 11 (LW2720 R/SPEC)

22-Oct-2011 2


LW012720

USAACEAIRCRAFT OPERATING WITHIN LIMTATIONAND RESTRICTIONS SPECIFIED IN AWR 1505REV. 4 DTD 21 OCT 11 @ 5926.3 AIRCRAFTHOURS. (LW2720 R/SPEC)

22-Oct-2011 3


LW012720

USAACEH-60-12-AMAM-03, TRANSPONDER ANDCOMMON MISSILE WARNING SYSTEM C/W @5942.5 AIRCRAFT HOURS. (CMWO NOTINSTALLED)

31-Oct-2011 1


LW012720

USAACEAIRCRAFT NO LONGER OPERATE WITHINLIMITATIONS AND RESTRICTIONS SPECIFIEDIN AWR 1455 DTD 23 OCT 09 REV 1 (CAP) C/W@ 5947.5 AIRCRAFT HOURS. . SUPERCEDEDBY AWR 1455 DTD 31 OCT 11 REV 2

01-Nov-2011 1


LW012720

USAACEAIRCRAFT OPERATE WITHIN LIMITATIONSAND RESTRICITONS SPECIFIED IN AWR 1455REV 20 DTD 31 OCT 11 @ 5947.5 AIRCRAFTHOURS.

01-Nov-2011 2


LW012720



8.7.DATE

6.REMARKS

4. 5.



USAACETAIL ROTOR SN: A009-07223, DURINGINSPECTION DISCORVERED TAIL ROTOR DE-ICE CONNECTOR MOUNTING FLANGECRACKED AUTHORIZATION GRANTED IAWMEC 136148 REPAIR IAW SIKORSKYINSTRUCTIONS SE 0621T025 @ 5953.1AIRCRAFT HOURS.

08-Nov-2011 1


LW012720

USAACEAIRCRAFT NO LONGER OPERATE WITHINLIMITATIONS AND RESTRICTIONS SPECIFIEDIN AWR 1455 REV. 2 DTD 31 OCT 11 C/W 5972.8AIRCRAFT HOURS. SUPERCEDED BY AWR1455 REV. 3 DTD 10 NOV 11.

22-Nov-2011 1


LW012720

USAACEAIRCRAFT OPERATE WITHIN LIMITATIONSAND RESTRICTIONS SPECIFIED IN AWR 1455REV. 3 DTD 10 NOV 11 @ 5972.8 AIRCRAFTHOURS.

22-Nov-2011 2


LW012720

USAACEAIRCRAFT OPERATE WITHIN LIMITATIONSAND RESTRICTIONS SPECIFIED IN AWR 1153REV 6 DTD 18 NOV 11 @ 5973 AIRCRAFTHOURS. (LW2720 R/SPEC)

06-Dec-2011 1


LW012720

USAACEH-60-12-ASAM-02, DRAG BEAMREPLACEMENT C/W @ 5972.8 AIRCRAFTHOURS.

08-Dec-2011 1


LW012720

USAACEMAIN ROTOR COMPLETED RIG C/W @ 5972.8AIRCRAFT HOURS: FWD-LENGTHEN 1.5 FLTS,AFT-SHORTEN 1.5 FLTS, LAT-SHORTEN 1.5FLATS.

10-Dec-2011 1


LW012720

USAACET/R BIAS C/W @ 5972.8 AIRCRAFT HOURS:YELLOW: 5.241 - 4.912=.329, BLACK: 4.540 -4.208= .332, RED: 5.227- 4.894= .343,BLUE:4.623 - 4.289=.334 (LW2720 R/SPEC)

11-Dec-2011 1


LW012720

USAACET/R CABLE TENSION COMPLETED AT 5981.9ACFT HRS, TURNBUCKLES NOT THREADEDEVENLY . L/H 115, R/H 115 TEMP 14.9

10-Jan-2012 1


TP011634

USAACEDELAYED ENTRY: ACFT OPERATING UNDERAWR 1738 DTD 01FEB11, AN/APX-118 CXP.AWR DOES **NOT** REQUIRE ANY 2408-13-1ENTRIES. THIS AWR SUPERSEDES ISAQ 116.

19-Jan-2012 1


DK011063

USAACEH-60-12-SOF-04 COMPLIED WITH: EQUIPMENTNO INSTALLED ON THIS AIRCRAFT. @ 6069.1ACFT HRS. (AFS 60)

18-Feb-2012 1


DM026217

USAACEH-60-11-ASAM-13 (INLET ANTI-ICE VALVE) C/W@ 6069.1 ACFT HRS.

18-Feb-2012 2


DM026217

USAACET/R BIAS READINGS C/W @ 6069.1 ACFT HRS:RED: 4.834-5.147=.313, YELLOW: 4.800-5.134=.334, BLACK: 4.090-4.428=.338, BLUE4.214-4.553=.339 (DM026217 R/SPEC)

19-Feb-2012 1


DM026217

USAACEACFT OPERATING UNDER AWR 1251, R4 DTD22FEB12, EYEBOLTS ON BIFILAR ARMS,SUPERSEDING 1251 R3.

27-Feb-2012 1


DK011063



8.7.DATE

6.REMARKS

4. 5.



USAACEACFT OPERATING UNDER AWR 1648, R1 DTD26MAY10, MAGNUS LAPTOP.

28-Feb-2012 2


DK011063

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-06 (UPPER BULKHEARD FULE SYSTEMBREAKAWAY VALVE AND FIREEXTINGUISHING SYSTEM DIRECTIONALVALVE) @ 6078.9 ACFT HRS.

01-Mar-2012 1


DM026217

USAACEACE/JACE INSPECTION COMPLETED AT 6161ACFT HRS. (PID RL026538)

12-Mar-2012 1


TB011027

USAACEACFT OPERATING IAW AWR 1648, R2 DTD09MAR12, MAGNUS LAPTOPS, SUPERSEDINGR1.

20-Mar-2012 1


DK011063

USAACEMEO A6055 REV C: AIRCRAFT OPERATINGIAW MEO A6055 DUE TO YELLOW AND REDLEAD M/R DROOPSTOP BUSHINGS DE-BONDED. REPLACEMENT OF BUSHINGSREQUIRED AT THE NEXT PMI INSP. (ACFTHRS: 6160.6)

21-Mar-2012 1


DC011002

USAACEAWR 1750: ACFT OPERATING IAW AWR 1750,R1 DTD 27MAR12, AN/AVS-6 SERIES NVG.

03-Apr-2012 1


DK011063

USAACEH-60-12-SOF-05 (CHG TO DEPOT REPAIREDLEGACY M/R BLADES COMPLIANCE) C/W @6182.8 ACFT HRS.

14-Apr-2012 1


MH021534

USAACEMEC F144810, AUTHORIZATION GRANTED TOUSE LOCALLY FABRICATED TOOLS TOREPLACE BEARING IN THE UPPERSTABILATOR ACTUATOR AIRFRAME FITTING.

23-Apr-2012 1


DK011063

USAACEH-60-12-ASAM-02, DRAG BEAMREPLACEMENT C/W @ 6184.3 AIRCRAFTHOURS. REPLACED WITH P/N: 70250-22010-043.

24-Apr-2012 1


JK015371

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-01 TAIL ROTOR OUPTUT BEVEL BEARNON-DESTRUCTIVE INSPECTION @ 6182.8HOURS.

24-Apr-2012 3


VM014663

USAACECOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-17 (T/R INBOARD/OUTBOARDRETENTION PLATE SHIMS) @ 6184.3 ACFTHRS.

27-Apr-2012 1


RS014443

USAACEAWR 1681: ACFT OPERATING IAW AWR 1681,R2 DTD 14FEB12, EH60 DE-MOD,SUPERSEDING ALL PREVIOUS REVISIONS OF1681.

03-May-2012 1


DK011063

USAACEAWR 1681: ACFT OPERATING IAW AWR 1681,R3 DTD 04MAY12, EH60 DE-MOD,SUPERSEDING REV 2.

08-May-2012 1


DK011063

USAACEINSPECTION A675- FLIGHT CONTROL RODSCOMPLETED @ 6184.3 ACFT HRS. (48 MONTHINSP)

09-May-2012 1


RS014443



8.7.DATE

6.REMARKS

4. 5.



USAACEACFT NO LONGER OPERATING IAW MEOA6055 (YELLOW & RED LEAD M/RDROOPSTOP BUSHINGS DEBONDED)REPLACED DURING PHASE @ 6184.3 ACFTHRS.

09-May-2012 2


RS014443

USAACETAIL ROTOR BLADE BIAS CHECKCOMPLETED @ 6184.3 ACFT HRS: BLUE 4.479-4.145=.334 YELLOW 4.788-5.121=.333 BLACK4.426-4.093=.333 RED 5.158-4.826=.332 DIALCALIPER MR#104675.

14-May-2012 1


RS014443

USAACETAIL ROTOR CABLE TENSION CHECKCOMPLETED @ 6184.3 ACFT HRS: L/H:178 LBSR/H:178 LBS @ 29.4 DEGREES C TENTIOMITERMR#110883.

14-May-2012 2


RS014443

USAACEMAIN ROTOR RIG COMPLETE. FWD:BIAS,AFT:BIAS, LAT:3 FLATS POS. COMPLETED AT6184.8 ACFT HRS.

15-May-2012 1


JK015371

USAACET/R BIAS READINGS: BLUE: 4.188+312=4.500,BLACK: 4.184+312=4.496, YELLOW:4.813+312=5.125, RED: 4.806+312=5.118.COMPLETED AT 6184.3 ACFT HRS.

17-May-2012 1


JK015371

USAACEMCDS SCRUB IS COMPLETE IN CONJUNTIONWITH 720 HR PHASE. COMPLETED AT 6187.0ACFT HRS.

23-May-2012 1


JK015371

USAACECOMPLY WITH REQUIREMENTS OF H-60-12-AMAM-09 (HYDRAULIC LINE CHAFE)COMPLETED AT 6187.0 ACFT HRS.

24-May-2012 1


JK015371

USAACE720 HR PMI #10 COMPLETED AT 6184.3 ACFTHRS. PMI #11 DUE 6904.3 ACFT HRS.

24-May-2012 2


JK015371

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-12-AMAM-09 HYDRAULIC LINE CHAFE @ 6187

24-May-2012 3


VM014663

USAACEAWR 1220: ACFT OPERATING IAW AWR 1220,R6 DTD 25MAY12, ENHANCED SCHEDULEDMAINTENANCE. SUPERSEDING REV 5.

25-May-2012 1


DK011063

USAACEMEC F136148, T/R BLD A009-07223 WASREMOVED FROM THIS ACFT 19FEB12 ANDTURNED-IN TO CCAD, MEC IS NO LONGERAPPLICABLE.

31-May-2012 1


DK011063

L-3 RASM-EOCM/ACE PERFORMED AT 6193.6 AIRCRAFTHOURS BY TEAM MEMBERS QQ AND P

01-Jun-2012 1


JW807912

USAACET/R CABLE TENSION CK COMPLETED @6193.6 ACFT HRS: L/H: 145, R/H: 145 LBS @23.3 DEG C. TENSIONMETER MR#87703,THERMOMETER MR# 107157

01-Jun-2012 2


MH021534

USAACET/R RIG CK COMP @ 6193.6 ACFT HRS.BLACK: 4.115/4.453 = .338, YELLOW:4.845/5.200 = .355, BLUE: 4.189/4.525 = .336,RED: 4.934/5.275 = .341 MR# 098646

01-Jun-2012 3


MH021534



8.7.DATE

6.REMARKS

4. 5.



USAACET/R CABLE TENSION CK COMPLETED AT6204.1 ACFT HRS. L/H=150 LBS, R/H=150LBS, TEMP @ 27.5 'C'

07-Jun-2012 1


TB011027

USAACET/R BIAS CK COMPLETED AT 6204.1 ACFT HRSBLACK 4.04/4.38/.34, YELLOW 4.77/5.10/.33,BLUE 4.10/4.43/.33, RED 4.79/5.12/.33

07-Jun-2012 2


TB011027

USAACEH-60-12-AMAM-12, RESCINDED COMMONCOMPONENT REMOVAL DATE, COMPLETED @6296.7 ACFT HRS.

11-Jul-2012 1


JK015371

USAACEAWR 1841: ACFT OPERATING IAW AWR 1841,22MAY12, HONEYWELL ATS TESTING.STARTER SN 02 INSTALLED IN THE #2POSITION THIS DATE AT 6307.5 ACFT HRS.

12-Jul-2012 1


DK011063

USAACEMEC F149486, AUTHORIZATION GRANTED TOUSE HYSOL 9309.3NA IN LIEU OF PR-1826PROSEAL TO BOND THE WASHER TO THETAIL WHEEL YOKE. 6307.5 ACFT HRS.

13-Jul-2012 1


DK011063

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-08 @ 6325.1 ACFT HRS.

19-Jul-2012 1


JK015371

USAACEAWR 1841: ACFT OPERATING IAW AWR 1841,R1 DTD 23JUL12, HONEYWELL ATS 3505300-10ATS, SUPERSEDING THE ORIGINAL ISSUE OFTHIS AWR.

24-Jul-2012 1


DK011063

USAACEMAIN ROTOR COMPLETE RIG READINGS:FWD: 0, AFT: 0, LAT: 0

24-Jul-2012 2


JK015371

USAACETAIL ROTOR CABLE TENSION READINGS: L/H:167, R/H: 167 @ 28.9°C. @ 6330.0 ACFT HRS.

24-Jul-2012 3


JK015371

USAACET/R BIAS READINGS: BLACK: 4.541/4.217=.334,RED: 5.242/4.908=.334, BLUE: 4.543/4.204=.339,YELLOW: 5.231/4.900=.331. COMPLETED AT6330.0 ACFT HRS.

25-Jul-2012 1


JK015371

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-07 (ELECTRICAL WIRING CHAFE)COMPLETED AT 6330.0 ACFT HRS.

26-Jul-2012 1


JK015371

USAACEAWR 1303: ACFT OPERATING IAW AWR 1303,R4 DTD 05JUL12, DAVID CLARK VIP ICS.EQUIPMENT MAY BE INSTALLED/REMOVEDPER MISSION REQUIREMENTS.

30-Jul-2012 1


DK011063

USAACEAWR 1514: ACFT OPERATING IAW AWR 1514,R2 DTD 27JUL12, DGNS-P3I AN/ASN-128D AAND B KIT, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.

01-Aug-2012 1


DK011063

USAACEAWR 1220: ACFT OPERATING IAW AWR 1220,R7 DTD 31JUL12, ESM, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

01-Aug-2012 2


DK011063



8.7.DATE

6.REMARKS

4. 5.



USAACEAWR 1800: ACFT OPERATING IAW AWR 1800,R1 DTD 20JUL12, EDM AND/OR BFT,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

02-Aug-2012 1


DK011063

USAACEAWR 1153: ACFT OPERATING IAW AWR 1153R6 DATED 18 NOV 11. (JP-8 +100)SUPERCEDING ALL OTHER AWR 1153

18-Aug-2012 1


JK015371

USAACECOMLIED WITH REQUIREMENTS FOR H-60-12-ASAM-09 (BREEZE EASTERN EXTERNALRESCUE HOIST CARTRIDGE ACTUATEDDEVICE) NA THIS ACFT. COMPLETED AT6399.2 ACFT HRS.

23-Aug-2012 1


JK015371

USAACEAWR 1153: ACFT OPERATING IAW AWR 1153,R7 DTD 24AUG12, JP-8+100, SUPERSEDINGALL PRIOR REVISIONS OF THIS AWR.

29-Aug-2012 1


DK011063

USAACEACFT OPERATING IAW MEO A6577, DATED 26JUL 12. TAIL WHEEL YOKE ASSEMBLY,BONDING OF TEFLON COATED WASHERS,CHANGING FROM PROSEAL SEALANT MIL-S-8802 A-2 TO HYSOL EA 9309.3NA ADHESIVE.AT 6415.0 ACFT HRS.

30-Aug-2012 1


JK015371

USAACEAWR 1251: ACFT OPERATING IAW AWR 1251,R5 DTD 31AUG12, EYEBOLTS, SUPERSEDINGANY PRIOR REVISIONS OF THIS AWR.

31-Aug-2012 1


DK011063

USAACEACFT NO LONGER OPERATING UNDER MEOA6577, DATED 26 JUL 12. TAIL WHEEL YOKEASSEMBLY, BONDING OF TEFLON COATEDWASHERS, CHANGING FROM PROSEALSEALANT MIL-S-8802 A-2 TO HYSOL EA9309.3NA ADHESIVE. COMPLETED AT 6427.2ACFT HRS.

07-Sep-2012 3


JK015371

USAACECOMPLY WITH REQUIREMENTS OF H-60-12-AMAM-15 (TRIM ACTUATORS) COMPLETED AT6457.2 ACFT HRS.

18-Sep-2012 1


JK015371

USAACEDELAYED ENTRY: ACFT NO LONGEROPERATING UNDER MEO A5826 REV B, MECF79723. GUIDANCE FOR EVALUATING AXIALAND RADIAL PLAY IN HIRSS INNER DUCTASSEMBLY TO INCLUDE PREMATUREREMOVAL AND MAINTENANCE. . ACFT HRS6284.4 ACFT HRS.

21-Sep-2012 1


JK015371

USAACEAWR 1455: ACFT OPERATING IAW AWR 1455,R4 DTD 18SEP12, BATTELLE CAP,SUPERSEDING ANY PRIOR REVISIONS OFTHIS AWR. THIS AWR ALSO REPLACES ISAQ123 (2MAR06).

21-Sep-2012 2


DK011063

USAACEMEC F154149, AUTHORIZATION GRANTEDFOR A DEVIATION OF THE PEDAL ADJUSTACCESS COVER INSTALLATION PN 70209-01013-101/102. BOLT PN AN3-3A MAY BE USEDIN LIEU OF SCREW MS27039-1-07.

15-Oct-2012 1


DK011063



8.7.DATE

6.REMARKS

4. 5.



USAACEMEC F154440, Aircraft flew 2.0 hours with theleft tailstrut access panel loose. AviationEngineering Directorate has reviewed requestand has the following disposition. Visuallyinspect the immediate area inside and out forany signs of damage or cracks. Re-inspect atthe next 40 hr. If any damage is found contactthis office for further disposition. Annotateaircraft's historical record. 6513.0 ACFT HRS.

23-Oct-2012 1


DK011063

USAACEAWR 1220: ACFT OPERATING IAW AWR 1220,R8 DTD 01NOV12, ENHANCED SCHEDULEDMAINTENANCE, SUPERSEDING ANY PRIORREVISIONS OF THIS AWR.

01-Nov-2012 1


DK011063

USAACECOMPLY WITH REQUIREMENTS OF H-60-13-AMAM-02 (AHRS) COMPLETED AT 6536.5 ACFTHRS.

13-Nov-2012 1


JK015371

USAACEDELAYED ENTRY, AWR 1529: ACFTOPERATING IAW AWR 1529, R2 DTD 07OCT11,AHRS/AHRU.

19-Nov-2012 1


DK011063

USAACETAIL ROTOR BIAS RECORD; RED: 4.833 IN -5.154 IN = 0.321 IN @ 3°. BLACK: 4.048 IN -4.372 IN = 0.324 IN @ 3°. YELLOW: 4.850 IN -5.152 IN = 0.302 IN @ 3°. BLUE: 4.119 IN - 4.448IN = 0.329 IN @ 3°. MR# 114688. @ 6540.9 ACFTHRS.

28-Nov-2012 1


DM026217

USAACECOMPLY WITH REQUIREMENTS OF H-60-13-AMAM-03 (DECU/EDECU TGT BIAS) NLT 04DEC 2012

30-Nov-2012 1


JK015371

USAACECOMPLY WITH REQUIREMENTS OF H-60-13-ASAM-01 (ANTI-COLLISION LIGHTS POWERSUPPLY) COMPLETED AT 6540.9 ACFT HRS.

30-Nov-2012 2


JK015371

USAACECOMPLY WITH REQUIREMENTS OF H-60-13-AMAM-04 COMPLETED AT 6593.6 ACFT HRS.

08-Jan-2013 1


JK015371

USAACEH-60-13-AMAM-05 (MLG BRAKES) COMPLETEDAT 6623.1 A/C HOURS. BOTH PASS. AFS 594.

23-Jan-2013 1


JS026222

USAACEACFT OPERATING UNDER MEO A6055 REV CFOR RED DROOP STOP BUSHING DISBONDED@ 6637.0 ACFT HRS.

26-Jan-2013 1


BK026292

USAACEAWR 1738: ACFT OPERATING IAW AWR 1738,R1 DTD 01FEB13, AN/APX-118 COMMONTRANSPONDER, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR AND ISAQ 116 WITHALL REVISIONS.

04-Feb-2013 1


DK011063

USAACECOMPLY WITH REQUIREMENTS OF H-60-13-AMAM-06 ( CEFS ) @ 6657.9 A/C HOURS. ( NOTAPPLICABLE TO THIS A/C ).

11-Feb-2013 1


JS026222

USAACEAWR 1251: ACFT OPERATING IAW AWR 1251,R6 DTD 28FEB13, EYEBOLTS ON BIFILARARMS, SUPERSEDING ALL PRIOR VERSIONSOF THIS AWR.

01-Mar-2013 1


DK011063



8.7.DATE

6.REMARKS

4. 5.



USAACECOMPLY WITH REQUIREMENTS OF H-60-13-ASAM-04 (PLASTIC MEDIS BLAST AND OXIDEFLAKE RESIDUE) COMPLETED AT 6733.4 ACFTHRS. ALL PASSED.

27-Mar-2013 1


JK015371

USAACECOMPLY WITH REQUIREMENTS OF H-60-13-AMAM-07 (LOAD DEMAND SPINDLE CABLECLEARANCE) COMPLETED AT 6733.4 ACFTHRS. PASSED.

27-Mar-2013 2


JK015371

USAACEAWR 1750: ACFT OPERATING IAW AWR 1750,R2 DTD 29MAR13, AN/AVS-6 NVG,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND THE AMSRD-AMR-AE-T AWR FOROPERATION OF THE ANVIS AN/AVS-6 SERIESNVG IN ARMY AIRCRAFT DTD 26JUN06.

29-Mar-2013 1


DK011063

USAACECOMPLY WITH REQUIREMENTS OF H-60-13-ASAM-05 (ELECTRIC RESCUE HOIST) PRIORTO THE NEXT LIVE EXTERNAL HOISTOPERATIONS. COMPLETED AT 6768.4 ACFTHRS.

09-Apr-2013 1


JK015371

USAACEAWR 1800: ACFT OPERATING IAW AWR 1800,R2 DTD 22MAR13, EDM AND/OR BFT,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND AWR'S 1284, 1347, 1414 AND 1639.

11-Apr-2013 1


DK011063

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-13-ASAM-06 (PMI CHECKLIST CHANGES) AT6818.1 ACFT HRS

10-May-2013 1


TP011634

USAACEH-60-13-SOF-01 ATTITUDE HEADINGREFERENCE SET (AHRS) COMPLETED AT6833.3 ACFT HRS, (DUAL AHRS INSTALLED)

31-May-2013 1


OW010950

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-13-AMAM-11 (MAIN TRANSMISSION FILTERBOWL) AT 6877.8 ACFT HRS

03-Jul-2013 1


TP011634

USAACEGEN-13-AMAM-04 AN/APN-209 RADARALTIMETER SET COMPONENT TRACKINGCOMPLETED AT 6885 ACFT HRS

17-Jul-2013 1


TP011634

USAACECOMPLETED INSPECTION FOR THE 34.5 BEAMAT 308 BEAM BEADED PANEL REPAIR AT6901.0 ACFT HRS

02-Aug-2013 1


TP011634

DCR RASM-COCM/ACE PERFORMED AT 6904.0 AIRCRAFTHOURS BY TEAM MEMBER QQ

22-Aug-2013 1


JW807912

USAACECOMPLY WITH REQUIREMENTS OF H-60-13-ASAM-10 (WOODWARD HMU P3 TUBE)COMPLETED AT 6904.0 ACFT HRS.

22-Aug-2013 2


JK015371

USAACEAWR 1251: ACFT OPERATING IAW AWR 1251,R7 DTD 28AUG13, EYEBOLTS, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR.

29-Aug-2013 1


DK011063

USAACECOMPLY WITH REQUIREMENTS OF H-60-13-AMAM-10 (CHANGE 64) COMPLETED AT 6904.0ACFT HRS.

13-Sep-2013 1


JK015371



8.7.DATE

6.REMARKS

4. 5.



USAACECOMPLY WITH REQUIREMENTS OF H-60-13-AMAM-15. (CEFS). CEFS NOT INSTALLED.PASSED @ 6904.0 ACFT HRS

26-Sep-2013 1


JK015371

USAACEDAGR SERIAL NUMBER VERIFIED AS: 218870,AT 6904.0 ACFT HRS.

16-Oct-2013 1


CN014192

USAACEAWR 1505: ACFT OPERATING IAW AWR 1505,R5 DTD 18OCT13, 5-M HYD FILTER,SUPERSEDING ANY PRIOR VERSION OF THISAWR.

22-Oct-2013 1


DK011063

USAACEMEC F174326, AUTHORIZATION GRANTED TOREPAIR AN APPROX 0.187" CRACK IN UPPERFWD CORNER OF LH TS ACCESS OPENING.

25-Oct-2013 1


DK011063

USAACEAWR 1529: ACFT OPERATING IAW AWR 1529,R3 DTD 30OCT13, DUAL AHRS, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR.

31-Oct-2013 1


DK011063

USAACEMEC F174628, AUTHORIZATION GRANTED TOREPAIR 2 VOIDS IN LH ESSS PLATFORMPANEL. 6904.O ACFT HRS.

01-Nov-2013 1


DK011063

USAACEMEC F174627, AUTHORIZATION GRANTED TOREPAIR 2 VOIDS IN RH ENG COWLING. 6904.0ACFT HRS.

01-Nov-2013 2


DK011063

USAACEH-60-14-SOF-01 ,INSPECTION FOR BREEZEEASTERN EXTERNAL RESCUE HOISTINSTALLATION, COMPLETED AT 6904.0 ACFTHRS. NOT INSTALLED ON THIS AIRFRAME ATTHIS TIME.

03-Nov-2013 1


CN014192

USAACEDAGR SERIAL NUMBER VERIFIED AS SN:218870, AT 6904.0 ACFT HRS.

04-Nov-2013 1


CN014192

USAACETAIL ROTOR BIAS RECORDS: RED DIM A-4.839, DIM B5.154, DIFF .315; YELLOW DIM A4.841, DIM B 5.154 DIFF .313; BLACK DIM A-4.059; DIM B 4.369; DIFF .310; BLUE ROTORBIAS DIM A-4.138; DIMB 4.448, [email protected] ACFT HRS.

08-Nov-2013 1


FT020709

USAACETAIL ROTOR CABLE TENSION CHECK CHECKCOMPLETED AT 6904.5 ACFT HRS. L/H: 133,R/H: 134, AT 21.0 DEG C.

08-Nov-2013 2


CN014192

USAACEMAIN ROTOR RIGGING CHECK COMPLETEDAT 6904.5 ACFT HRS. FWD: NO ADJUSTMENT,AFT :NO ADJUSTMENT, LAT: NOADJUSTMENT.

08-Nov-2013 3


CN014192

USAACE720 HOUR PHASE # 11, COMPLETED AT 6904.0ACFT HRS. THE NEXT 720 HOUR PHASE (#12)IS DUE AT 7624.0 ACFT HRS.

12-Nov-2013 1


CN014192

USAACEH-60-AMAM-01, FLIGHT CONTROL RIGGINGPROCEDURES, C/W AT 6904.0 ACFT HRS.

12-Nov-2013 2


CN014192



8.7.DATE

6.REMARKS

4. 5.



USAACEDATE OF MANUFACTURE TAKEN FROM THESERIAL NUMBER CHECK - JUN 88

12-Nov-2013 3


OW010950

USAACEAWR 1251: ACFT OPERATING IAW AWR 1251,R8 DTD 26NOV13, EYEBOLTS ON BIFILARARMS, SUPERSEDING ALL PRIOR VERSIONSOF THIS AWR.

25-Nov-2013 1


DK011063

USAACECOMPLY WITH THE REQUIREMENTS OF H-60-14-ASAM-02 BY DEC 8, 2013 (HUMS) (DOESNOT APPLY TO THIS ACFT) @ ACFT HRS7590.1

26-Nov-2013 1


FT020709

USAACEINSTALLATION OF 12 POINTS BOLT MAINTRANSMISSION OIL FILTER ATTACHMENTHARDWARE REQUIRED PER H-60-13-AMAM-11BY 31 JAN. 2014, WITH ACFT HRS 6923.8

10-Dec-2013 1


FT020709

USAACEAWR 1529: ACFT IS NO LONGER OPERATINGIAW AWR 1529, ALL REVISIONS. ACFTRECONFIGURED FROM DUAL AHRS TOSINGLE AHRS. SEE AWR 1444.

18-Dec-2013 1


DK011063

USAACEAWR 1444: ACFT OPERATING IAW AWR 1444,R6 DTD 11JUL13, SINGLE AHRS.

18-Dec-2013 2


DK011063

USAACECOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-03 (DISCREPANT CONNECTING LINKS)@ ACFT HRS 6953.3 INSPECTION COMP, N/AIAW PAR 7.1 (AFS 19)

03-Jan-2014 1


FT020709

USAACECOMPLIED WITH H-60-14-ASAM-03 (ENGINEINLET BARRIER FILTER BRKT REMOVAL) AT6974.1 ACFT HRS.

14-Jan-2014 1


MW020956

USAACECOMPLIED WITH H-60-14-AMAM-08(COMMUNICATION CONSOLE CIRCUITBREAKER PROTECTION) AT 7012.9 ACFT HRS.

06-Mar-2014 1


MW020956

USAACEAWR 1648: ACFT OPERATING IAW AWR 1648,R3 DTD 28MAR14, MAGNUS LAPTOP,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

27-Mar-2014 1


DK011063

USAACEH-60-14-AMAM-05 LEGITIMATE CODE FILECHANGE 65 REQUIREMENTS COMPLETED AT7070.0 ACFT HRS.

05-Apr-2014 1


JB012761

USAACET/R BIAS MEASUREMENTS COMPLETED IAWTM1-1520-237-23 PARA 11-4-6. RED= DIM A:4.795, DIM B: 5.129, DIFF: 0.334, BLACK= DIMA: 4.059, DIM B: 4.383, DIFF: 0.324, YELLOW:DIM A: 4.81, DIM B: 5.132, DIFF: 0.322, BLUE=DIM A: 4.106, DIM B: 4.428, DIFF: 0.322.COMPLETED AT 7077.5 ACFT HRS.

11-Apr-2014 1


MW020956

USAACET/R CABLE TENSION CK COMPLETED @7077.5 ACFT HRS. L/H: 155, R/H: 155 @ 25.7'C.

11-Apr-2014 2


MW020956



8.7.DATE

6.REMARKS

4. 5.



USAACEAWR 1444: ACFT OPERATING IAW AWR 1444,R7 DTD 14APR14, SINGLE AHRS,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

16-Apr-2014 1


DK011063

USAACEH-60-14-AMAM-10 HONTEK COATED M/RBLADE REMOVAL COMPLETED AT 7077.5ACFT HRS.

16-Apr-2014 2


MW020956

USAACET/R BIAS MEASUREMENTS COMPLETED IAWTM 1-1520-237-23 PARA 11-4-6. RED= 2.84 DEG,BLACK= 3.01 DEG, YELLOW= 2.91 DEG, BLUE=2.82 DEG

22-Apr-2014 1


MW020956

USAACEH-60-14- ASAM-06 (FLIGHT CONTROL MIXERASSY) C/W AT 7090.8 ACFT HRS.

24-Apr-2014 1


MW020956

USAACEH-60-14-ASAM-06 CW @ 7090.8 HRS 29-Apr-2014 1


MT021154

USAACEH-60-14-AMAM-12 MAIN ROTOR SPINDLE NUTRETIREMENT LIFE COMPLIED WITH

29-Apr-2014 2


MT021154

USAACEACFT OPERATING IAW AWR 1681, R4 DTD30APR14, EH DE-MOD, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND AWR'S927 AND 890.

06-May-2014 1


DK011063

DCR RASM-COCM/ACE PERFORMED AT 7108.6 ACFT. HRS.BY TEAM MEMBER UU AND R AMCOM RASM-C.

19-May-2014 1

FT. CAMPBELL KY42223

BD011103

USSACECOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-14 (IVHMS CABLING) @ 7108.6 MWONOT APPLIED INSPECTION COMPLETE

29-May-2014 1


CB020588

USAACEACFT OPERATING IAW AWR 1505, R6 DTD03JUN14, 5M HYD FILTER, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

04-Jun-2014 1


DK011063

USAACEACFT OPERATING IAW AWR 1251, R9 DTD06JUN14, EYEBOLTS, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

06-Jun-2014 1


DK011063

USAACECOMPLIED WITH H-60-14-SOF-03(DISCREPANTHEXAGON NUTS) @ 7108.6 ACFT HRSPASSED

23-Jun-2014 1


OW010950

USAACEMAIN ROTOR RIGGING CHECK COMPLETEDAT 7108.6 ACFT HRS. FWD: NOADJUSTMENTS. AFT NO ADJUSTMENTS, LAT1/2 TURN

03-Jul-2014 1


CB020588

USAACEACFT OPERATING IAW AWR 1800, R3 DTD16JUL14, EDM AND/OR BFT, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR ANDAWR'S 1284, 1347, 1414, 1639.

25-Jul-2014 1


DK011063



8.7.DATE

6.REMARKS

4. 5.



USAACEACFT OPERATING IAW AWR 1841, R3 DTD16JUL14, HONEYWELL STARTER PN 3505300-10, SUPERSEDING ALL PRIOR VERSIONS OFTHIS AWR.

25-Jul-2014 2


DK011063

USAACERECEIVED TAIL ROTOR BIAS WORKSHEETWITH ONLY THE BLADE SET (DEG) ON IT.THEY WERE AS FOLLOWED: RED-3.1; BLACK-3.1; YELLOW-2.9; BLUE- 2.9.

25-Jul-2014 3


CB020588

USAACEACFT OPERATING IAW AWR 1514, R3 DTD31JUL14, DGNS, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.

31-Jul-2014 1


DK011063

USAACECOMPLIED WITH H-60-14-ASAM-09 (ENGINEOUTPUT SHAFT) @ 7128.3 ACFT HRSCOMPLETED

31-Jul-2014 2


CB020588


15-Aug-2014 1


CB020588

USAACEMEC F188676, Authorization is granted forCCAD Depot Field Team to replace left handbeadedpanel with new beaded panel kit, P/N70070-20470-013. Replace the beaded panel perthe mod 50-5 kit in DMWR 1-1520-237 WP 0333,Left Hand side only. The following kits shall beinstalled: 1.a.)Plating kit, NSN 1680-01-513-69901.b.)Stringer Kit, NSN 1680-01-551-79831.c.)Window kit, NSN 1680-01-551-0092 1.d.) BL34.5 Modification Kit(50-7), NSN 1680-01-551-8405. 7140.0 ACFT HRS.

27-Aug-2014 1


DK011063

USSACET/R CABLE TENSION CK COMPLETED @7167.6 ACFT HRS. L/H: 170, R/H: 170 @ 30'C.

28-Aug-2014 1


CB020588

USAACECOMPILED WITH REQUIREMENTS OF H-60-14-SOF-04 (OPERATORS AND CREWMEMBERSCHECKLIST) @ 7167.6 ACFT HRS COMPLETE

29-Aug-2014 1


CB020588

USAACECOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-10 (MAIN TRANSMISSION PLANATORYCARRIER ASSEMBLY) @ 7168.0 ACFT HRS

09-Sep-2014 1


CB020588


11-Sep-2014 1


CB020588

USAACET/R CABLE TENSION CK COMPLETED @7196.1 ACFT HRS. L/H 150, R/H 150 @ 24.2'C

19-Sep-2014 1


CB020588

USAACET/R CABLE TENSION CK COMPLETED @7205.2 ACFT HRS R/H 165 L/H 165 @ 29.1 'C

23-Sep-2014 1


CB020588

USAACEACFT OPERATING IAW AWR 1153, R8 DTD10OCT14, JP-8+100 FUEL, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

27-Oct-2014 1


DK011063



8.7.DATE

6.REMARKS

4. 5.



USAACEDELAYED ENTRY: MEC F189394, YOKE SN STI-1898 REPAIRED UNDER THIS MEC INSTALLEDTHIS ACFT AT UNKNOWN ACFT HRS. THISYOKE MUST BE REMOVED PRIOR TO ACFTTRANSFER. THIS ENTRY IS ONLY VALIDWHILE THIS SERIALIZED YOKE IS INSTALLED.THIS MEC IS NO LONGER APPLICABLE TOTHIS ACFT WHEN THIS SERIALIZED YOKE ISREMOVED.

27-Oct-2014 2


DK011063

USAACEH-60-15-SOF-01, OIL COOLER FAN AXIALBEARING, COMPLETED AT 7268.2 ACFT HRS.

29-Oct-2014 1


MB011137

USAACETAIL ROTOR BIAS COMPLETED AT 7268.2ACFT HRS. RED 4.836/5.156=.032, 1ST DEG 2.6,2ND DEG 3.0, FINAL DEG 3.0. BLACK4.075/4.413=0.338, 1ST DEG 2.7, 2ND DEG 3.0,FINAL DEG 3.0. YELLOW 4.832/5.173=0.341,1ST DEG 2.5, 2ND DEG 3.0, FINAL DEG 3.0.BLUE 4.149/4.455=0.306, 1ST DEG 2.5, 2ND 3.0,FINAL DEG 3.0.

30-Oct-2014 1


MB011137

USAACEACFT OPERATING IAW AWR 1220, R9 DTD31OCT14, ESM, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.

03-Nov-2014 1


DK011063

USAACEACFT OPERATING IAW AWR 1455, R5 DTD28OCT14, BATTELLE CAP, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

03-Nov-2014 2


DK011063

USAACEMEC F191848, AUTHORIZATION GRANTEDFOR CCAD DFT TO REPLACE SERVO BEAMRAIL (70209-22103-065) IAW DMWR 1-1520-237-1 DTD 09SEP13 WP 0133. 7268.2 ACFT HRS.

06-Nov-2014 1


DK011063

USAACEACFT OPERATING IAW AWR 1153, R9 DTD05NOV14, JP-8+100 OR F-24+100 FUEL,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

07-Nov-2014 1


DK011063

USAACECOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-19 (ULLS-A(E) LCF CHANGE 66) ON 08NOV 14 AT 7268.2 ACFT. HRS.

08-Nov-2014 1


MB011137

USAACEH-60-15-ASAM-01, MAINT. MANDATORY LIGHTEMITTING DIODE(LED) CAUTION ADVISORYPANEL(CAP). COMPLETED AT 7268.2 ACFTHRS.

18-Nov-2014 1


MB011137

USAACEACFT OPERATING IAW AWR 1251, R10 DTD26NOV14, EYEBOLTS, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

25-Nov-2014 1


MB011137

USAACEACFT OPERATING IAW AWR 1251, R10 DTD26NOV14, EYEBOLTS, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

25-Nov-2014 2


AS011060

USAACEMEC F188676A, Authorization granted toperform dye penetrant inspect the hole(s) andeddy current inspect around the sureface.

11-Dec-2014 1


DK011063



8.7.DATE

6.REMARKS

4. 5.



USAACEMEC F193510, XMSN MOUNT PAD WORN ONSTA 360.115 FITTING. AUTHORIZATIONGRANTED FOR CCAD DFT TO REPLACE THEAFT XMSN BEAM. 7268.2 ACFT HRS.

12-Dec-2014 1


DK011063

USAACEMEC F193511, RIGHT 34.5 CHANNEL ISSPLICED AND HAS WORKING RIVETS AT THE308 TAB. AUTHORIZATION GRANTED FORCCAD DFT TO REPLACE RH 34.5 CHANNELIAW DMWR 1-1520-237. 7268.2 ACFT HRS.

12-Dec-2014 2


DK011063

USAACECOMPLIED WITH H-60-15-AMAM-05, AHRSEMERGENCY PROCEDURES ON 12 DEC 14 AT7268.2 ACFT. HRS.

12-Dec-2014 3


MB011137

USAACEMEC F193595, MOUNT LOOSE IN OBSERVERSEAT LEFT RAIL GUIDE. AUTHORIZATIONGRANTED TO INSTALL/SECURE THEFORWARD ISOLATION MOUNT WITH HYSOLEA9309.3NA. 7268.2 ACFT HRS.

23-Dec-2014 1


DK011063

USAACEMEC F194547, AUTHORIZATION GRANTED TOREPAIR 2 HOLES IN THE 308 BEAM RH TAB.

14-Jan-2015 1


DK011063

USAACEMEC F194547A, STA 308 RH FWD TAB, FWDHOLE IS .350" DIAMETER WITH EDGEDISTANCE OF .450". STA 308 RH AFT TAB, AFTHOLE IS .439" AND HAS EDGE DISTANCES OF.410" INBOARD AND .498" AFT. BOTH HOLESHAVE BEEN NDI INSPECTED AND NO CRACKSPRESENT. AUTHORIZATION GRANTED TOFABRICATE AND INSTALL FREEZE PLUG(S).

15-Jan-2015 1


DK011063

USAACEMEC F194547B, AUTHORIZATION GRANTEDTO OMIT STEP 1 IN THE DISPOSITION OFADDENDUM A. NDI WAS PREVIOUSLYPERFORMED AND NO CRACKS ARE PRESENT.

16-Jan-2015 1


DK011063

USAACEDELAYED ENTRY @ 7268.2 ACFT HRS:AIRCRAFT OPERATING UNDER MEO #A6116INSTALLATION OF FUEL FLAG FOR E/UH-60FLEET AT FT. RUCKER.

26-Jan-2015 1


MB011137

USAACEMEC F193511A, DURING THE ABOVE REPAIR,STA 308 RH AFT INBOARD TAB HOLES WEREOVERSIZED AND REQUIRED FREEZE PLUGS(VIA MEC F194547B). AUTHORIZATIONGRANTED TO OMIT COLD WORKING ONTHESE TWO (QTY:2) FREEZEPLUGGED HOLESAND TO INSTALL A 0.125" 7075-T6 'L' SHAPEDDOUBLER ON THE UNDERSIDE OF THE RHAFT STA 308 BEAM TAB. 7268.2 ACFT HRS.

30-Jan-2015 1


DK011063

USAACEACFT OPERATING IAW AWR 1738, R2 DTD23JAN15, AN/APX-118 CXP, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR ANDISAQ 116.

04-Feb-2015 1


DK011063

USAACEACFT OPERATING IAW AWR 1220, R10 DTD26JAN15, ESM, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.

11-Feb-2015 1


DK011063



8.7.DATE

6.REMARKS

4. 5.



USAACECOMPLY WITH REQUIREMENTS OF H-60-15-AMAM-06 (IDENTIFICATION OF AVIATIONSERVIVABILITY EQUIPMENT) COMPLETEDAT7268.2 ACFT HRS. NA

13-Feb-2015 1


MB011137

USAACEACFT IS NO LONGER OPERATING IAW AWR1514, ALL VERSIONS. ACFT IS OPERATINGIAW AWR 1753, R5 DTD 30JAN15, DGNSAN/ASN-128B/D, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR AND AWR'S 1467,1292 AND 1514.

19-Feb-2015 1


DK011063

USAACEACFT OPERATING IAW AWR 1965, R0 DTD08OCT14, APPLE IPAD DEVICES.

04-Mar-2015 1


DK011063

USAACEACFT NO LONGER OPERATING IAW AWR1841, ALL VERSIONS. TEST STARTER SN 02REMOVED THIS DATE AT 7268 ACFT HRSWITH 961 TTSN.

18-Mar-2015 1


DK011063

DCR RASM-COCM/ACE PERFORMED AT 7268.2 AIRCRAFTHOURS BY TEAM MEMBERS P AND UU

19-Mar-2015 1


JW807912

USAACEACFT OPERATING IAW AWR 1750, R3 DTD31MAR15, AN/AVS-6 NVG, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND THEAMSRD-AMR-AE-T AWR DTD 26JUN06.

09-Apr-2015 1


DK011063

USAACEH-60-15-ASAM-03 (TROOP/GUNNER SEATUSAACE ENERGY ATTENUATORS) C/W THISDATE AT 7268.2 ACFT HRS. N/A THISACFT(AFS 765)

14-Apr-2015 1


MB011137

USAACEMEC F198691, AUTHORIZATION GRANTED TOREMOVE/REPLACE TRANSMISSION MOUNTBEAM BUSHINGS USINGSTANDARDMAINTENANCE PRACTICES AND IAW DMWR 1-1520-237-1 (WP 0036 00).

17-Apr-2015 1


DK011063

USAACEMEC F198687A, AUTHORIZATION GRANTEDTO SPOTFACE THE SURFACE OF THE UPPERDECK UP TO A MAXIMUM OF 1.00" X 0.005"DEEP AT FS307.450/RBL13.705 ANDFS307.250/RBL11.080 ON AIRCRAFT S/N 87-24673 TO INSTALL THE 70652-02150 FLIGHTCONTROL MANIFOLD IAW EM0013 WP 0774 00.7268.2 ACFT HRS.

23-Apr-2015 1


DK011063

USAACEENTRY #1 DTD 23APR15 FOR MEC F198687ASHOULD HAVE BEEN DTD 17APR15.

23-Apr-2015 2


DK011063

USAACEH-60-15-AMAM-10, AV-DEC GASKETINSPECTION COMPLETED AT 7268.2 ACFTHRS.

07-May-2015 1


MB011137

USAACEACFT OPERATING IAW AWR 1505, R7 DTD13MAY15, 5M HYD FILTERS, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR.

13-May-2015 1


DK011063

USAACEH-60-15-AMAM-11 (MODE-S TRANSPONDERADDRESS REVIEW) COMPLETED AT 7268.2ACFT HRS. NA

27-May-2015 1


MB011137



8.7.DATE

6.REMARKS

4. 5.



USAACEACFT OPERATING IAW AWR 1251, R11 DTD27MAY15, EYEBOLTS ON BIFILAR,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

28-May-2015 1


DK011063

USAACEMEC F198687B, 7268.2 ACFT HRS, (ADDENDUMA: SPOT FACING OF THE UPPDER DECKSURFACES AS DESCRIBED ABOVE IS TO BEACCOMPLISHED BY QUALIFIED AMSSMACHINIST ONLY.) AFTER MACHINING,LOCATION 9 IS REQUIRING A 0.001" SHIM.ENSURE THAT THE MACHINED STRAP THATWAS MACHINED HAS BEEN PRIMED/PAINTEDIAW EM 0013. AUTHORIZATION GRANTED TOINSTALL MANIFOLD WITH NO SHIM ATLOCATION 9. ENSURE THAT ALL OTHERLOCATIONS ARE SHIMMED TO MATCH THEHEIGHT OF LOCATION 9 TO MAKE SURE THEMANIFOLD IS ON THE SAME PLANE. ONCEINSTALLED AND LEAK CHECKS AREPERFORMED, MAKE SURE NO LEAKS AREPRESENT AT LOCATION 9. IF LEAKS AREPRESENT, CONTACT THE UNDER SIGNED FORFURTHER DISPOSTION.

29-May-2015 1


DK011063

USAACEGEN-12-AMAM-07, INSTALLATION OFGENERAL PURPOSE FIRST AID KITS.COMPLETED AT 7268.2 ACFT HRS.

04-Jun-2015 1


MB011137

USAACEACFT OPERATING IAW AWR 1681, R5 DTD22JUN15, EH DE-MOD, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR ANDAWR'S927 AND 890.

24-Jun-2015 1


DK011063

USAACEMAIN ROTOR RIG CHECK COMPLETED AT7868.2. FWD=N/A, AFT=N/A, LAT=N/A. (LOWCOLL ANGLE) LOW COLL NEUTRAL CYCLICNEUTRAL YAW- 90* R=8.6, 180* FWD= -2.7, 270*LEFT= -10.8, 0* AFT= 0, TOTAL*= -4.9, AVG*= -1.225, TOLERANCE= -1.3* TO 0.0* (BLADES ON)+ 1.0* TO 0.0* (BLADE OFF).(HIGH COLLANGLE) HIGH COLL NEUTRAL YAW - 90*RIGHT=20, 180* FWD= 10.5, 270* LEFT= 10.4, 0*AFT= 19.7, TOTAL= 60.6, TOLERANCE= 15.5MINIMUM RANGE, COLLECTIVE RANGE=16.375. (FWD CYCLIC ANGLE) HIGH COLLNEUTRAL LAT FWD CYCLIC NEUTRAL YAW-90* RIGHT= -2.4, 270* LEFT= 31.2, TOTAL*=33.6, TOLERANCE= DIFFERENCE BETWEEN270* & 90* POSITIONS +33.0 MIN. (AFT CYCLEANGLE) HIGH COLL NEUTRAL LAT AFTCYCLEIC NEUTRAL YAW= 90* RIGHT= 26.1,270* LEFT= 3.6, TOTAL= 22.5, TOLERANCE=DIFFERENCE BETWEEN 90* & 270* POSITIONSNOT LESS THAN +19*. (LEFT CYCLE ANGLE)LOW COLL NEUTRAL LONG LEFT CYCLICNEUTRAL YAW= 180* FWD= -9, 0* AFT= 6.8,TOTAL= 15.8, TOLERANCE= SUM OF 180* & 0*POSITION TO BE 15* TO 17*. (RIGHT CYCLICANGLE) LOW COLL NEUTRAL LONG RIGHTCYCLIC NEUTRAL YAW= 180* FWD=7.3, 0*AFT= -8.2, TOTAL= 15.5, TOLERANCE= SUM OF180* & 0* POSITION TO BE 14* TO 16*.

09-Jul-2015 1


MB011137



8.7.DATE

6.REMARKS

4. 5.



USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-15-AMAM-14 ( ULLS-A (E) CHANGE 67 AT7268.2 ACFT HRS.

25-Jul-2015 1


MJ026211

USAACETAIL ROTOR CABLE TENSION CHECKCOMPLETED AT 7268.2 ACFT HRS. R/H=186,L/H=186, @ 32.6 DEGREES CEL.

26-Jul-2015 1


MB011137

USAACETAIL ROTOR BIAS COMPLETED AT 7268.2ACFT HRS. RED- DIM=4.77", DIMB=5.093",DIFF=0.323", BLADE SET= 0.1 DEG. FINAL= 3.0DEG. YELLOW- DIM A= 4.73", DIM B= 5.102",DIFF= 0.372", FINAL= 3.0 DEG. BLACK- DIMA=4.026", DIM B= 4.339", DIFF= 0.313", BLADESET= 0.3 DEG. FINAL= 3.0 DEG. BLUE- DIMA=4.045", DIM B= 4.406" DIFF= 0.361, BLADESET= 0.3 DEG. FINAL= 3.0 DEG.

26-Jul-2015 2


MB011137

USAACEACFT OPERATING IAW AWR 1738, R3 DTD17JUL15, AN/APX-118 CXP, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

28-Jul-2015 1


DK011063

USAACECABLE TENSION CHECK COMPLETED AT7289.5 ACFT HOURS. R/H= 165, L/H 167 @ 29.6DEGREES CEL.

14-Sep-2015 1


CP027629

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-15-SOF-02 (FRIES RELEASE CABLE) @ 7324.1ACFT HOURS. N/A, RELEASE CABLE NOTINSTALLED.

24-Sep-2015 1


CP027629

USAACEMAIN MOD CHIP LIGHT AT 7324.1 ACFTHOURS DURING RUN UP. INSPECTED MAINMOD CHIP DETECTOR AND FOUND SMALLHAIRLIKE SLIVER. SERVICEABLE AS IS IAWEM 0013 WP 0627

29-Sep-2015 1


CP027629

FORT RUCKER, ALACFT OPERATING IAW AWR 1965, R1 DTD 16SEP 15, APPLE IPAD DEVICES, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR.

14-Oct-2015 1


USAACE

USAACEH-60-15-AMAM-18 MEDICAL EVACUATION(MEDEVAC) CAROUSEL C/W @ 7354.4 ACFTHRS. (NOT INSTALLED ON THIS ACFT).

15-Oct-2015 1


MH021534

USAACEMAIN MOD CHIP CAUTION APPEARED AT 7360ACFT HOURS. INSPECTED CHIP DETECTORIAW EM0284 WP 0656, DURING INSPECTIONFOUND MINIMUM AMOUNTS OF FUZZ SEETEST PILOT MOC

16-Oct-2015 1


CP027629

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-16-AMAM-01 (EIBF FRAMES) AT 7377.3 ACFTHOURS. NOT INSTALLED ON THIS AIRCRAFT.

27-Oct-2015 1


CP027629

USAACEA670 48-MONTH INSPECTION (CABIN TUBINSPECTION) COMPLETED AT 7,391.5 ACFTHOURS.

08-Nov-2015 1


CP027629

USAACECOMPLIED WITH THE REQUIREMENTS OFASAM-H-60-16-ASAM-01 (INBOARDRETENTION PLATE TORQUE CHECK) AT7391.5 ACFT HOURS.

10-Nov-2015 1


CP027629



8.7.DATE

6.REMARKS

4. 5.



USAACEACFT OPERATING IAW AWR 1251, R12 DTD30NOV15, EYEBOLTS ON BIFILAR,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

01-Dec-2015 1


DK011063

USAACEACFT NO LONGER OPERATING IAW AWR 1648R3 (MAGNUS LAPTOP)

23-Dec-2015 1


CP027629

USAACEACFT OPERATING IAW AWR 1913 R1 DATED06NOV15 (ACN ELECTRONIC LOGBOOK)

23-Dec-2015 2


CP027629

USAACEACFT OPERATING IAW AWR 1738, R4 DATED28DEC15 (AN/APX-118 CXP). SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR ANDISAQ 116.

05-Jan-2016 1


CP027629

USAACEACFT OPERATING IAW AWR 1800, R4 DTD05JAN16, SINGLE EDM AND/OR BFT,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND AWR'S 1284, 1347, 1414 AND 1639.

08-Jan-2016 1


DK011063

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-16-ASAM-02, DEFECTIVE FUEL HOSES AT7442 ACFT HOURS, BOTH PASS.

08-Jan-2016 2


CP027629

USAACEACFT NO LONGER OPERATING UNDER AWR1251, ALL VERSIONS. AWR WAS ALLOWED TOTERMINATE ON 31JAN16 AND EYEBOLTS AREBEING REMOVED.

02-Feb-2016 1


DK011063

USAACE#2 CROSSFEED BREAKAWAY VALVEREPLACED IAW TB1-1520-237-20-213 AT 7472.2ACFT HOURS.

04-Feb-2016 1


CP027629

USAACEACFT OPERATING IAW AWR 1913, R2 DTD12FEB16, ACN LOGBOOK, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

17-Feb-2016 1


DK011063

USAACEACFT OPERATING IAW AWR 1681, R6 DTD13APR16, EH60A DEMOD, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND AWR'S927 AND 890.

13-Apr-2016 1


DK011063

USAACEH-60-16-AMAM-06, T-CLIP INSTALLATION C/WAT 7580.8 ACFT. HRS.

26-Apr-2016 1


LS027644

USAACEH-60-16-AMAM-06, T-CLIP INSTALLATION C/WAT 7580.8 ACFT HRS.

26-Apr-2016 2


LS027644

USAACEACFT OPERATING IAW AWR 1800 R5 DTD27APR16, FOR THE SINGLE ELECTRONICDATA MANAGER(EDM) AND /OR BLUE FORCETRACKING SYSTEM(BFT). THIS AWRSUPERSEDES AWR'S 1284,1347,1414, AND1639

13-May-2016 1


LS027644

USAACEH-60-16-ASAM-05, MAIN ROTOR BLADEDEBONDING, COMPLIED WITH AT 7598.2 ACFTHRS.

20-May-2016 1


LS027644



8.7.DATE

6.REMARKS

4. 5.



USAACECORRECTIVE ENTRY; ENTRY #1 20MAY2016INTER IN ERROR H-60-16-ASAM-05, MAINROTOR BLADE DEBONDING. ENTERCORRECTLY ON 2408-5-1 AS REQUIRED.

20-May-2016 2


LS027644

USAACEACFT OPERATING IAW AWR 1444, R8 DTD25MAY16, SINGLE AHRS, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

01-Jun-2016 1


DK011063

USAACEACFT NO LONGER OPERATING IAW AWR1505, ALL VERSIONS. SAMPLING VALVE NOTINSTALLED AND 5M FILTERS PN 7596335-101,NSN 4330-01-601-1254 ARE NOW STANDARDH60 IETM EQUIPMENT.

02-Jun-2016 1


DK011063

USAACEGEN-16-AMAM-04, TRANSPONDER BATTERYREPLACEMENT C/W @ ACFT HRS 7616.1(JF014874)

06-Jun-2016 1


LS027644

USAACEDELAYED ENTRY DTD 7 NOV 95 ENTRY #1 SOFENTERED IN ERROR

21-Jun-2016 1


LS027644

USAACEH-60-16-AMAM-09- ULLS-S (E) COMPONENTDUPLICATION, COMPLETED AT 7619.8 ACFTHRS. THIS ACFT IS NOT AFFECTED.

21-Jun-2016 2


CN014192

USAACEH-60-16-SOF-01- UPPER CABIN FRAMECRACKING INSPECTION, COMPLETED AT7619.8 ACFT HRS. NO CRACKS NOTED.

22-Jun-2016 1


CN014192

LOCKHEED MARTINRASM-C

OCM/ACE PERFORMED AT 7619.8 AIRCRAFTHOURS BY TEAM MEMBERS P AND F

22-Jun-2016 2


JW807912

USAACEMEC F313967, 7619.8 ACFT HRS,AUTHORIZATION GRANTED TO REPAIR PICYCLIC STICK YOKE HOUSING IAW DMWR 1-1680-323 DTD 30DEC11 PG 3-13, PARA 3-12.REMOVING MINIMAL MATERIAL NOT TOEXCEED DEPTH. MEC NUMBER WILL BESTENCILED ON HOUSING. (ACTUAL DATE22JUN16)

23-Jun-2016 1


DK011063

USAACEMEC F313969, 7619.8 ACFT HRS,AUTHORIZATION GRANTED TO REPAIR CPCYCLIC STICK YOKE HOUSING IAW DMWR 1-1680-323 DTD 30DEC11 PG 3-13, PARA 3-12.REMOVING MINIMAL MATERIAL NOT TOEXCEED DEPTH. MEC NUMBER WILL BESTENCILED ON HOUSING. (ACTUAL DATE22JUN16)

23-Jun-2016 2


DK011063

USAACEMEC F314232 IS CANCELLED WITHOUTDISPOSITION.

07-Jul-2016 1


DK011063

USAACEMEC F314480 IS CANCELLED WITHOUTDISPOSITION.

08-Jul-2016 1


DK011063



8.7.DATE

6.REMARKS

4. 5.



USAACEAIRCRAFT TRANSFERRED FROM FTRUCKER,AL TO SCIENCE AND ENGINEERINGSERVICES (SES) , HUNTSVILLE,AL - BESTPROGRAM, UTILITY HELICOPTERS PROJECTOFFICE ON THID DATE WITH 7619.8 ACFT HRS.

27-Jul-2016 1


OW010950

SCIENCE ANDENGINEERINGSERVICES LLC

H-60-16-AMAM-10 NOT COMPLIED WITH. 04-Aug-2016 1

HUNTSVILLE

JH902419

SCIENCE ANDENGINEERINGSERVICES LLC

H-60-16-ASAM-07 NOT COMPLIED WITH. 04-Aug-2016 2

HUNTSVILLE

JH902419


UNCLASSIFIED For Official use Only (FOUO)

MWO NO. /RELATED

PUBLICATION

1. NOMENCLATURE 2. COMPONENT SERIAL NUMBER 3. AIRCRAFT SERIAL NUMBER

MWO TITLE MANHOURSDATE

APPLIED

PIDORGANIZATION

APPLYING MWO

SERVO, PRIMARY MAIN ROTOR B30307943 70410-02820-054

DMWR 1-1650-381 RECAPPED W0MUAA OA0161 13-May-2013 25

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

DA FORM 2408-5-1, OCT 91 EQUIPMENT MODIFICATION RECORD (COMPONENT)

70410-02820-054 B30307943


DATE AC HRS SHAFT VERTICAL REASON FOR VIB CHECKLONGITUDINALLATERAL

IPS READINGS4.

8724673HELICOPTER, UTILITYEH-60A3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Report Date: 03-Aug-2016 1/9

MWO 1-1520-237-50-73 APPLIED CLOCK ANGLE18-Dec-1995 A275-03436 00.160817.1

A1001-1520-237-50-73 APPLIED CLOCK ANGLE18-Dec-1995 A275-03437 00.4070817.1

100 HR INSP30-Jul-1996 A275-03436 00.4880895.5

100 HR INSP30-Jul-1996 A275-03437 00.1150895.5

100 HR INSP30-Jul-1996 OIL COOLER 0.09200895.5

PMS-2 COMPLETION19-Dec-1997 #1EN.DRSH 00.080999.2

PMS-2 COMPLETION19-Dec-1997 #2EN.DRSHA 00.320999.2

PMS-2 COMPLETION19-Dec-1997 OIL COOLER 00.1930.08999.2

PMS-2 COMPLETION19-Dec-1997 T/R ASSY 00.090999.2

REM & REINSTL & VIB CHECK TQ=3722-Jun-2001 #1EN.DRSH 00.3201117.1

REM & REINSTL & VIB CHECK TQ=3722-Jun-2001 #2EN.DRSHA 00.4201117.1

REM & REINSTL22-Jun-2001 OIL COOLER 0.0630.1501117.1

VIBRATION LEVEL CHECK DUE11-Sep-2001 L/H ENG OS 00.301198.6

VIBRATION LEVEL CHECK DUE11-Sep-2001 OIL COOLER 0.090.0201198.6

VIBRATION LEVEL CHECK11-Sep-2001 R/H ENG OS 00.2601198.6

CHECK TQ=3620-Oct-2001 L/H ENG OS 00.2501301.4

VIBRATION LEVEL CHECK20-Oct-2001 OIL COOLER 0.230.2101301.4

CHECK TQ=3520-Oct-2001 R/H ENG OS 00.1701301.4

CHECK TQ=3703-Dec-2001 L/H ENG OS 00.301403.9

VIBRATION CHECK03-Dec-2001 OIL COOLER 0.60.0901403.9

CHECK TQ=3803-Dec-2001 R/H ENG OS 00.3301403.9

500 HR. INSP. VIB CK TQ=3622-May-2002 L/H ENG 0.14001493.3

500 HR INSP VIB CK.22-May-2002 OIL COOLER 0.060.1701493.3

500 HR INSP VIB CK TQ=3522-May-2002 R/H ENG 0.35001493.3

100 HR INSP TQ=3723-Jan-2004 L/H ENG 0.14001594.6

100 HR INSP23-Jan-2004 OIL COOLER 0.160.3201594.6

100 HR INSP TQ=3723-Jan-2004 R/H ENG 0.04001594.6

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.



100 HR INSP TQ=3631-Mar-2004 L/H ENG 0.31001694

100 HR INSP31-Mar-2004 OIL COOLER 0.320.1401694

100 HR INSP TQ=3831-Mar-2004 R/H ENG 0.3001694

100 HR INSP TQ=3630-Apr-2004 L/H ENG 0.34001795.8

100 HR INSP30-Apr-2004 OIL COOLER 0.110.0301795.8

100 HR INSP TQ=3730-Apr-2004 R/H ENG 0.36001795.8

100 HR INSP TQ=3516-Jun-2004 L/H ENG 0.27001894.6

100 HR INSP16-Jun-2004 OIL COOLER 0.130.3401894.6

100 HR INSP TQ=3616-Jun-2004 R/H ENG 0.32001894.6

VIBE CK TQ=3429-Oct-2004 L/H ENG 0.06001933.3

VIBE CK29-Oct-2004 OIL COOLER 0.020.1801933.3

VIBE CK TQ=3629-Oct-2004 R/H ENG 0.19001933.3

120 HR INSP12-Nov-2004 OIL COOLER 0.020.1102018.1

120 HR INSP TQ=3812-Nov-2004 L/H ENG 0.11002018.1

120 HR INSP TQ=3812-Nov-2004 R/H ENG 0.11002018.1

BALANCE CK FOR REM/REINSTALLATION OF ENG20-Nov-2004 L/H ENG 0.35002034.8

120 HR INSP TQ=3727-Jan-2005 L/H ENG 0.34002137.3

120 HR INSP27-Jan-2005 OIL COOLER 0.050.1202137.3

120 HR INSP TQ=3727-Jan-2005 R/H ENG 0.37002137.3

120 HR INSP TQ=.3412-Mar-2005 L/H ENG 0.3002254.6

120 HR INSP12-Mar-2005 OIL COOLER 0.030.2102254.6

120 HR INSP TQ=3512-Mar-2005 R/H ENG 0.12002254.6

REINSTALLATION OF D/SHAFT24-Apr-2005 OIL COOLER 0.110.2702343.4

REPLACED O-RING29-Apr-2005 OIL COOLER 0.140.1102343

REPL ENG TQ=3714-May-2005 #2 ENG 0.24002360.5

120 HR INSP TQ=3621-May-2005 #1 ENG 0.18002379.5

120 HR INSP TQ=3421-May-2005 #2 ENG 0.32002379.5




IPS READINGS4.



120 HR INSP21-May-2005 OIL COOLER 0.090.1402379.5

120 HR INSP TQ=.3827-Jul-2005 #1 ENG 0.21002496.9

120 HR INSP TQ=.3327-Jul-2005 #2 ENG 0.33002496.9

120 HR INSP27-Jul-2005 OIL COOLER 0.140.1902496.9

120 HR INSP TQ=3421-Sep-2005 #1 ENG 0.15002616.8

120 HR INSP TQ=3521-Sep-2005 #2 ENG 0.26002616.8

120 HR INSP21-Sep-2005 OIL COOLER 0.120.202616.8

120 HR INSP(PHASE #5) TQ=3720-Mar-2006 #1 ENG 0.28002708.6

120 HR INSP (PHASE #5) TQ=3820-Mar-2006 #2 ENG 0.41002708.6

120 HR INS (PHASE #5)20-Mar-2006 OIL COOLER 0.110.102708.6

120 HR INSP TQ=3617-May-2006 #1 ENG 0.35002832.6

120 HR INSP TQ=3617-May-2006 #2 ENG 0.43002832.6

120 HR INSP17-May-2006 OIL COOLER 0.160.1602832.6

120 HR INSP TQ=3520-Jul-2006 #1 ENG 0.34002948.7

120 HR INSP TQ=3520-Jul-2006 #2 ENG 0.42002948.7

120 HR INSP20-Jul-2006 OIL COOLER 0.160.1202948.7

RESHIMMED BEARING-NO LONG PROVIDED28-Nov-2006 OIL COOLER 0.25003062.4

120 HR INSP - NO TQ PROVIDED27-Dec-2006 #1 ENG 0.11003073.2

120 HR INSP - NO TQ PROVIDED27-Dec-2006 #2 ENG 0.17003073.2

120 HR INSP - NO VERT PROVIDED27-Dec-2006 OIL COOLER 00.0603073.2

120 HR INSP - NO TQ PROVIDED27-Mar-2007 #1 ENG 0.41003192.9

120 HR INSP - NO TQ PROVIDED27-Mar-2007 #2 ENG 0.09003192.9

120 HR INSP - NO VERT PROVIDED27-Mar-2007 OIL COOLER 00.103192.9

120 HR INSP - NO TQ PROVIDED14-May-2007 #1 ENG 0.41003311.5

120 HR INSP - NO TQ PROVIDED14-May-2007 #2 ENG 0.09003311.5

120 HR INSP - NO VERT PROVIDED14-May-2007 OIL COOLER 00.0203311.5

ENG REM/INST - NO TQ PROVIDED06-Jun-2007 #2 ENG 0.11003329.7




IPS READINGS4.



120 HR INSP/PHASE #6 - NO TQ PROVIDED10-Aug-2007 #1 ENG 0.09003376.2

120 HR INSP/PHASE #6 - NO TQ PROVIDED10-Aug-2007 #2 ENG 0.15003376.2

120 HR INSP/PHASE #6 - NO VERT PROVIDED10-Aug-2007 OIL COOLER 00.1103376.2

120 HR INSP - NO TQ PROVIDED15-Oct-2007 #1 ENG 0.19003497.1

120 HR INSP - NO TQ PROVIDED15-Oct-2007 #2 ENG 0.2003497.1

120 HR INSP - NO VERT PROVIDED15-Oct-2007 OIL COOLER 00.3403497.1

120 HR INSP26-Jan-2008 #1 ENG 0.36003621.1

120 HR INSP26-Jan-2008 #2 ENG 0.18003621.1

120 HR INSP26-Jan-2008 OIL COOLER 00.2603621.1

120 HR INSP12-Apr-2008 #1ENG 0.21003735.5

120 HR INSP12-Apr-2008 #2 ENG 0.31003735.5

120 HR INSP12-Apr-2008 OIL COOLER 00.2403735.5

120 HR INSP25-May-2008 #1 ENG 0.08003858.7

120 HR INSP25-May-2008 #2 ENG 0.49003858.7

120 HR INSP25-May-2008 OIL COOLER 00.3103858.7

D/SHAFT INSTALLATION30-Jun-2008 #1 ENG 0.22003947.4

120 HR INSP12-Jul-2008 #1 ENG 0.39003978

120 HR INSP12-Jul-2008 #2 ENG 0.4003978

120 HR INSP12-Jul-2008 OIL COOLER 00.103978

120 HR INSP24-Oct-2008 #1 ENG 0.25004096.6

120 HR INSP24-Oct-2008 #2 ENG 0.06004096.6

120 HR INSP24-Oct-2008 OIL COOLER 00.3404096.6

120 HR INSP18-Jan-2009 #1 ENG 0.33004213.2

120 HR INSP18-Jan-2009 #2 ENG 0.29004213.2

120 HR INSP18-Jan-2009 OIL COOLER 00.1104213.2

120 HR INSP. NO TQ PROVIDED20-Mar-2009 #1 ENG 0.41004333.7

120 HR INSP. NO TQ PROVIDED20-Mar-2009 #2 ENG 0.13004333.7




IPS READINGS4.



120 HR INSP. NO TQ PROVIDED20-Mar-2009 OIL COOLER 00.304333.7

120 HR INSP. NO TQ PROVIDED20-Mar-2009 TAIL ROTOR 0.16004333.7

120 HR INSP. NO TQ PROVIDED10-May-2009 #1 ENG 0.45004448.7

120 HR INSP. NO TQ PROVIDED10-May-2009 #2 ENG 0.15004448.7

120 HR INSP. NO TQ PROVIDED10-May-2009 OIL COOLER 00.1204448.7

120 HR MTP MOC DUE. TQ: 35%28-Jun-2009 #1 ENGINE 0.37004574.9

120 HR MTP MOC DUE- TQ: 33%28-Jun-2009 #2 ENGINE 0.15004574.9

120 HR MTP MOC DUE- NO TQ PROVIDED28-Jun-2009 OIL COOLER 00.1504574.9

120 HR MTP MOC DUE - NO TQ PROVIDED21-Sep-2009 #1 ENGINE 0.43004696.3

120 HR MTP MOC DUE - NO TQ PROVIDED21-Sep-2009 #2 ENGINE 0.13004696.3

120 HR MTP MOC DUE - NO TQ PROVIDED21-Sep-2009 OIL COOLER 00.0204696.3

REMD/REINST OIL COOLER - NO TQ PROVIDED01-Oct-2009 OIL COOLER 00.1504710.5

REPL #1 DRIVESHAFT - NO Q PROVIDED.02-Oct-2009 OIL COOLER 00.1804711

720 HOUR PMI # 8 = NO TQ PROVIDED.21-Nov-2009 #1 ENG 0.33004777.5

720 HOUR PMI #8 = NO TQ PROVIDED.21-Nov-2009 #2 ENG 0.35004777.5

720 HOUR PMI #8 = NO TQ PROVIDED.21-Nov-2009 OIL COOLER 00.3904777.5

TQ 37% 120 MTP MOC24-Apr-2010 # 2 ENG 0.08005020.9

TQ 36 % 120 HR MTP MOC24-Apr-2010 #1 ENG 0.31005020.9

120 MTP MOC24-Apr-2010 OIL COOLER 00.5605020.9

120 HOUR MTP MOC. NO TQ PROVIDED.06-Jun-2010 #1 ENG 0.25005135.5

120 HOUR MTP MOC. NO TQ PROVIDED.06-Jun-2010 #2 ENG 0.15005135.5

120 HOUR MTP MOC. NO TQ PROVIDED.06-Jun-2010 OIL COOLER 00.5705135.5

120 HOUR INSP; NO TQ PROVIDED30-Aug-2010 #1 ENG 0.26005253.2

120 HOUR INSP; NO TQ PROVIDED30-Aug-2010 #2 ENG 0.21005253.2

120 HOUR INSP; NO TQ PROVIDED30-Aug-2010 OIL COOLER 00.605253.2

120 HR NO TQ PROVIDED20-Nov-2010 #1 ENG 0.29005397.4

120 HR NO TQ PROVIDED20-Nov-2010 #2 ENG 0.19005397.4




IPS READINGS4.



120 HR INSP; NO TQ PROVIDED20-Nov-2010 OIL COOLER 00.5105397.4

120 MTP MOC FOR PHASE NO TQ04-Mar-2011 #1 ENG 0.19005467.5

120 MTP MOC FOR PHASE NO TQ04-Mar-2011 #2 ENG 0.21005467.5

120 MTP MOC FOR PHASE04-Mar-2011 OIL COOLER 00.2705467.5

120 HOUR INSP. NO TORQUE PROVIDED26-Apr-2011 #1 ENG 0.21005592.6

120 HOUR INSP. NO TORQUE PROVIDED26-Apr-2011 #2 ENG 0.23005592.6

120 HOUR INSP; NO TORQUE PROVIDED26-Apr-2011 OIL COOLER 00.2305592.6

VIBE CHECK; NO TQ PROVIDED06-Jun-2011 OIL COOLER 00.205678.8

AVA CHECK; NO TQ PROVIDED06-Jun-2011 #1 ENG 0.2005678.8

AVA CHECK; NO TQ PROVIDED06-Jun-2011 #2 ENG 0.18005679.8

120 HOUR INSP; TQ-3507-Jul-2011 #1 ENG 0.12005709.5

120 HOUR INSP; TQ-3507-Jul-2011 #2 ENG 0.47005709.5

120 HOUR INSP; NO TQ PROVIDED07-Jul-2011 OIL COOLER 00.1605709.5

120 HOUR INSP; NO TQ PROVIDED07-Jul-2011 T/R 00.1505709.5

360 HOUR INSP; NO TQ PROVIDED06-Sep-2011 #1 ENG 0.23005824.7

360 HOUR INSP; NO TQ PROVIDED06-Sep-2011 #2 ENG 0.37005824.7

360 HOUR INSP; NO TQ PROVIDED06-Sep-2011 OIL COOLER 00.1905824.7

360 HOUR INSP; NO TQ PROVIDED06-Sep-2011 TAIL ROTOR 00.0705824.7

120 HOUR INSP; NO TORQUE PROVIDED04-Nov-2011 #1 ENG 0.1005947.5

120 HOUR INSP; NO TORQUE PROVIDIED04-Nov-2011 # 2 ENG 0.29005947.5

120 HOUR INSP; NO TORQUE PROVIDED04-Nov-2011 OIL COOLER 00.1205947.5

120 HOUR INSP; NO TORQUE PROVIDED04-Nov-2011 TAIL ROTOR 00.105947.5

VIBRATION CHECK DUE FOR REPAIR T/R10-Nov-2011 TAIL ROTOR 00.1505953.1

120 HR MOC22-Feb-2012 #1 ENG 0.29006069.1

120 HR MOC22-Feb-2012 #2 ENG 0.3006069.1

120 HR MOC22-Feb-2012 OIL COOLER 00.2406069.1

120 HR MOC22-Feb-2012 T/R 00.1706069.1




IPS READINGS4.



REPLACED #1 ENGINE24-Mar-2012 #1 ENG 0.24006164.1

BALANCE 720HR PMI16-May-2012 T/R 00.0406184.3

720HR PMI BALANCE CK16-May-2012 OIL COOLER 00.2106148.3

TRQ @ 30 IN LB 1/4 IN 720PMI16-May-2012 #2 ENG 0.07006184.3

720HR PMI16-May-2012 #1 ENG 0.22006184.3

MTP TEST FLIGHT21-May-2012 T/R 0.01006184.3

REM/INST ENG01-Jun-2012 #1 0.033006204.1

T/R BLADE REM/REINSTALLED04-Jun-2012 TAIL ROTOR 00.0706193.6

REMOVAL/REINST OF #1 ENGINE04-Jun-2012 #1 ENGINE 0.33006193.6

REM/INST PC LINK08-Jun-2012 TAIL ROTOR 00.0606204.1

REPLACEMENT OF SEC 2 DRIVE SHAFT21-Jun-2012 OIL COOLER 00.0706249.9

M/R RIG27-Jul-2012 TAIL ROTOR 00.0506330

ENG CHANGE TBO11-Aug-2012 #1 ENG 0.37006363.2

FOR T/R ABRASION STRIP AFTER CURE TIME.22-Aug-2012 T/R 00.0206391.2

120 HR08-Sep-2012 OIL COOLER 00.0606427.2

120 HR08-Sep-2012 #1 ENG 0.39006427.2

120 HR08-Sep-2012 #2 ENG 0.04006427.2

120 HR08-Sep-2012 T/R D/S 00.0306427.2

REPLACEMENT OF #2 ENG08-Nov-2012 #2 ENG 0.24006536

HSS BALANCE CHK30-Nov-2012 #1 ENG 0.45006540.9

HSS BALANCE CHK30-Nov-2012 #2 ENG 0.17006540.9

TAIL ROTOR RIG CHECK30-Nov-2012 T/R D/S 00.0506540.9

120 HR14-Feb-2013 #1 ENG 0.58006657.9

120 HR14-Feb-2013 #2 ENG 0.31006657.9

120 HR14-Feb-2013 OIL COOLER 00.0706657.9

120 HR14-Feb-2013 T/R 01.1706657.9

120 HR14-Feb-2013 #1 ENG 0.11006657.9




IPS READINGS4.



120 HR14-Feb-2013 T/R 00.0306657.9

120 HR13-Apr-2013 TAIL ROTOR 00.1406785

120 HR13-Apr-2013 OIL COOLER 00.0906785

120 HR13-Apr-2013 #1 ENG 0.12006785

120 HR13-Apr-2013 #2 ENG 0.23006785

120 HOUR14-Nov-2013 #1 ENG 0.3006904

120 HOUR14-Nov-2013 #2 ENG 0.3006904

120 HOUR14-Nov-2013 OIL COOLER 00.1406904

120 HOUR14-Nov-2013 TAIL ROTOR 00.1506904

POST PHASE18-Nov-2013 #1 ENG 0.3006905.1

POST PHASE18-Nov-2013 #2 ENG 0.31006905.1

POST PHASE18-Nov-2013 OIL COOLER 0.14006905.1

POST PHASE18-Nov-2013 T/R D/S 00.1506905.1

120 HR VIBE CHK17-Mar-2014 #2 ENG 0.16007025.4

120 HR VIB CHK17-Mar-2014 OIL COOLER 00.1607025.4

120 HR VIB CHK17-Mar-2014 T/R D/S 00.0307025.4

MAIN MOD CHANGE10-Jul-2014 #1 ENG 0.39007108.6

MAIN MOD CHANGE10-Jul-2014 #2 ENG 0.2007108.6

MAIN MOD CHANGE10-Jul-2014 OIL COOLER 00.1207108.6

120 HOUR VIB CHECK15-Aug-2014 #1 ENG 0.32007147.8

120 HOUR VIBE CHECK15-Aug-2014 #2 ENG 0.04007147.8

120 HOUR VIBE CHECK15-Aug-2014 OIL COOLER 00.1407147.8

120 HOUR VIBE CHECK15-Aug-2014 T/R D/S 00.0307147.8

120 HOUR VIBE CHECK16-Aug-2015 T/R 00.0507268.2



120 HOUR VIBE CHECK16-Aug-2015 OIL COOLER 00.0507268.2




IPS READINGS4.



120 HR09-Nov-2015 #1 ENG 0.25007391.5

120 HR09-Nov-2015 #2 ENG 0.32007391.5

120 HR09-Nov-2015 OIL COOLER 00.0907391.5

120 HR09-Nov-2015 T/R 00.1507391.5

120 HR19-Mar-2016 #1 ENG 0.27007506.8

120 HR19-Mar-2016 #2 ENG 0.39007506.8

120 HR19-Mar-2016 OIL COOLER 00.1507506.8

120 HR19-Mar-2016 T/R 00.0907506.8

6. Remarks



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: 1/1210-Aug-2016

87246731520010820686 00HELICOPTER, UTILITY

156001095713502C12D

00B497-0032070219-05001-042TAIL CONE FITTING CCCC COND COND

162001231183103A01

06184BEM048970250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001231183103A01

737620BEM176570250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001421089003B01

4537268BMC76770250-13101-044TAIL SHOCK STRUT ASSY CCCC COND COND

165001285302405A01Z

11677268A106-0666670106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z

03491A106-1140570106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z

6926696R106-0030470106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z

07025WG30058-00114

70106-08100-046DAMPER ASSY, M/R CCCC COND COND

531501537465205A02H

8697392B9412197470103-08108-041SOLID BLADE PIN CCCC COND COND

531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


161501199764605A03A

00A107-0138270104-08000-050SWASHPLATE ASSY CCCC COND COND

161501078571806A11

00A258-0316670351-08080-043ACCESSORY MODULE CCCC COND COND

161501383899206A11

38467109A258-0715370351-08080-045ACCESSORY 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

42737109A2650006770351-08100-076MAIN TRANSMISSIONMODULE

CCCC COND COND

161501241611006E

42667109A2640056270351-08001-047INPUT MODULE CCCC COND COND

161501527817506E

8537109A2640939470351-08001-050INPUT MODULE CCCC COND COND

168001074515206F

00A005-0165370357-06300-042INTERMEDIATE GEARBOX CCCC COND COND

161501376508906G01

4197128A006-0322370358-06600-046TAIL ROTOR GEARBOXASSY

CCCC COND COND

161501524780506H04

07268C8450860170361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501524780506H04

07268C8450882970361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501081277506H06

04711WG300220010770361-03001-045SHAFT ASSY, T/R DRV SEC1

CCCC COND COND

161501158951706H08

20827620C2700036570361-03009-047SHAFT ASSY, T/R DRV SEC2

CCCC COND COND

161501158952206H09

00A272-0412770361-05001-051SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501158952206H09


CCCC COND COND

161501158952206H09


CCCC COND COND

161501083295306H11

17901595A273-0119970361-05002-045SHAFT ASSY, T/R DRV SEC6

CCCC COND COND

161501158578806H12

00A2740136970361-06002-047SHAFT ASSY, T/R DRV SEC7

CCCC COND COND

432001207722807A01

13076579K4025ABR53023-06PUMP MODULE,HYDRAULIC

CCCC COND COND

432001207722807A01

12677455416741ABR70652-02300-050PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01

21547268K2603ABR70652-02300-050PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

481001102247307B05A

05680186593213850-3-1VALVE, SOLENIOD CCCC COND COND

481001102247307B05A

06184204483213850-3-1VALVE, SOLENIOD CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






165001222431607B11

53342149663454A3197170-5ACCUMULATOR CCCC COND COND

168001342049608B20

526576201068100-601561-000PANEL INDICATOR (PDU) CCCC COND COND

168001342049608B20

40297620130670450-01043-124PANEL INDICATOR (PDU) CCCC COND COND

611501114969609A01

1564649283A105328B302-8-DMGENERATOR CCCC COND COND

611501114969609A01

15377109WOMUAA1228B302-8-DMGENERATOR CCCC COND COND

161501260074911C21

07087TMD0464374304

70400-02300-046MIXER ASSEMBLY CCCC COND COND

168001261204411D25

113153281467DL2155M20STABILATOR ACTUATOR CCCC COND COND

168001261204411D25

146761841998DL2155M20STABILATOR ACTUATOR CCCC COND COND

599601316274311D26

21704922176A70902-02001-048STABILATOR AMPLIFIER CCCC COND COND

599601316274311D26

79775248248670902-02001-048STABILATOR AMPLIFIER CCCC COND COND

299501496368615A04

357585723664504587ENGINE SEQUENCINGUNIT

CCCC COND COND

NSN PENDING19E04B

132673442835P320A002-03SDC - DOPPLERNAVIGATION

CCCC COND COND

589501245909019E05A

0726828DDSM-C-967292RECEIVER-TRANSMITTERRADAR

CCCC COND COND

584101245909319E05C

070721319FFA3060591INDICATOR HEIGHT CCCC COND COND

660501503528419E06A

0726811132765100-20ATTITUDE HEADINGREFERENCE UNIT

CCCC COND COND

661001490516852A

071163569691825050-1-001AUTOMAT 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 COMPONENTS5/1210-Aug-2016

00

156001081924402C15J14853

D496-00100 7140199370209-06051-043TAIL PYLON FITTING RCRC20000

161501450483405A01A10252

15152-00833 821597370103-08112-047HUB, M/R ROTOR ASSY RCRC5100

161501442692605A01I10491

A001-07947 3529762070102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501442692605A01I10491


RCRC6400

161501442692605A01I12373


RCRC6400

161501442692605A01I14020

D00112117 0762070102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501074515105A01L14000

C286-00681 0070351-08186-043MAIN ROTOR SHAFTEXTENDER

RCRC14000

161501127738805A01T13000

A327-00626 5191519170107-08400-046BIFILAR, M/R ROTORASSY

RCRC13000

161501106190305A0210407

A007-04553 6813762070150-09100-043MAIN ROTOR BLADEASSY

RCRC9600

161501106190305A0213783

A007-07618 3437762070150-09100-043MAIN ROTOR BLADEASSY

RCRC9600

161501106190305A0212073

A00700388 5147762070150-09100-043MAIN ROTOR BLADEASSY

RCRC9600

161501106190305A0211294

A00705484 5926762070150-09100-043MAIN ROTOR BLADEASSY

RCRC9600

161501113818805B0213620

A009-04890 4000762070101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501113818805B0213297

A00901721 4323762070101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501083681206G01B13040

A25700322 4785582570102-11101-042O/B RETENTION PLATE(T/R)

RCRC12000

414101329342806H238388

3900346SB 4577762070361-03005-107FAN AXIAL 175232520

156001129125607A2419247C112-06787 891713870410-02500-049SAS ACTUATOR RCRC

13000

156001129125607A2417088C11204053 1380546870410-02500-049SAS ACTUATOR RCRC

13000

156001129125607A2419101C11251843 1068716970410-02500-049SAS ACTUATOR RCRC

13000

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









Report Date:


00

161501141753211C238344

A233-00362 2287618470400-06100-042TAIL ROTOR PITCHCHANGE SHAFT

022160

165001305695411C2515295C300-05094 3325762070410-06520-046SERVO ASSY, TAIL

ROTORRCRC

11000

165001143122611D0129290B30310388 27307620274000-1031MAIN ROTOR PRIMARY

SERVORCRC

24400

165001143122611D0125834B303-00838 6186762070410-02820-054MAIN ROTOR PRIMARY

SERVORCRC

24400

165001143122611D0125831B303-07943 3489762070410-02820-054MAIN ROTOR PRIMARY

SERVORCRC

24400

156001158968511D041868034501050 1429710970400-08102-045AFT BELLCRANK RCRC

13000

156001164416111D0524268

E39102599 0726870400-08112-045AFT TIE ROD SUPTFITTING

RCRC17000

168001164416011D069468

M39210674 0726870400-08111-042AFT TIE ROD ASSY RCRC2200

156001286887011D0710730

390-02786 0633070400-08117-049AFT BELLCRANK SPTASSY

RCRC4400

304001287243811D0816792A380-04113 1317710970400-08151-061LATERAL SWASHPLATE

LINKRCRC

11000

168001221286311D0915231F337-02869 2878710970400-08166-041LATERAL SERVO

BELLCRANKRCRC

11000

168001158965311D111534465 2560690470400-08104-048AFT WALKING BEAM RCRC

11000

156001289269711D1310068

344-01778 0546870400-08115-046LEFT TIE ROD ASSY RCRC4600

156001296948611D1410474

28801015 0697470400-08114-051RIGHT TIE ROD ASSY RCRC3500

168001158965211D1518263803 3846710970400-08101-046FORWARD BELLCRANK RCRC

15000

156001221261911D168863B367-04518 3846710970400-08162-042FWD BELLCRANK SPT

ASSYRCRC

5600













Report Date:


00

SIGNIFICANT HISTORICAL EVENTS7.





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.

1520010820686HELICOPTER,UTILITY

EH-60A 8724673 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 8 of 12

10-Aug-2016

COND COND

156001095713502C12D

00TAIL CONE FITTING B497-0032070219-05001-042 CCCC

20000 14853

156001081924402C15J

71401993TAIL PYLON FITTING D496-0010070209-06051-043 RCRC

COND COND

162001231183103A01

06184FWD FIXED GEARSHOCK

BEM048970250-12051-045 CCCC

COND COND

162001231183103A01


BEM176570250-12051-045 CCCC

COND COND

162001421089003B01

4537268TAIL SHOCK STRUTASSY

BMC76770250-13101-044 CCCC

5100 10252

161501450483405A01A

8215973HUB, M/R ROTOR ASSY 15152-0083370103-08112-047 RCRC

6400 10491

161501442692605A01I

35297620MAIN ROTOR SPINDLEASSY

A001-0794770102-08200-069 RCRC

6400 10491

161501442692605A01I


A001-0812170102-08200-069 RCRC

6400 12373

161501442692605A01I


A001-1059770102-08200-069 RCRC

6400 14020

161501442692605A01I


D0011211770102-08200-069 RCRC

14000 14000

161501074515105A01L

00MAIN ROTOR SHAFTEXTENDER

C286-0068170351-08186-043 RCRC

13000 13000

161501127738805A01T

51915191BIFILAR, M/R ROTORASSY

A327-0062670107-08400-046 RCRC

COND COND

165001285302405A01Z

11677268DAMPER ASSY, M/R A106-0666670106-08100-046 CCCC

COND COND

165001285302405A01Z

03491DAMPER ASSY, M/R A106-1140570106-08100-046 CCCC

COND COND

165001285302405A01Z

6926696DAMPER ASSY, M/R R106-0030470106-08100-046 CCCC

COND COND

165001285302405A01Z

07025DAMPER ASSY, M/R WG30058-0011470106-08100-046 CCCC

9600 10407

161501106190305A02

68137620MAIN ROTOR BLADEASSY

A007-0455370150-09100-043 RCRC

9600 13783

161501106190305A02


A007-0761870150-09100-043 RCRC

9600 12073

161501106190305A02


A0070038870150-09100-043 RCRC

9600 11294

161501106190305A02


A0070548470150-09100-043 RCRC

COND COND

531501537465205A02H

8697392SOLID BLADE PIN B9412197470103-08108-041 CCCC

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 9 of 12

10-Aug-2016

COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

161501199764605A03A

00SWASHPLATE ASSY A107-0138270104-08000-050 CCCC

10000 13620

161501113818805B02

40007620TAIL ROTOR BLADEASSY

A009-0489070101-31000-043 RCRC

10000 13297

161501113818805B02

43237620TAIL ROTOR BLADEASSY

A0090172170101-31000-043 RCRC

COND COND

161501078571806A11

00ACCESSORY MODULE A258-0316670351-08080-043 CCCC

COND COND

161501383899206A11

38467109ACCESSORY MODULE A258-0715370351-08080-045 CCCC

COND COND

161501503311506A

42737109MAIN TRANSMISSIONMODULE

A2650006770351-08100-076 CCCC

COND COND

161501241611006E

42667109INPUT MODULE A2640056270351-08001-047 CCCC

COND COND

161501527817506E

8537109INPUT MODULE A2640939470351-08001-050 CCCC

COND COND

168001074515206F

00INTERMEDIATEGEARBOX

A005-0165370357-06300-042 CCCC

COND COND

161501376508906G01

4197128TAIL ROTOR GEARBOXASSY

A006-0322370358-06600-046 CCCC

12000 13040

161501083681206G01B

47855825O/B RETENTION PLATE(T/R)

A2570032270102-11101-042 RCRC

COND COND

161501524780506H04

07268DRIVESHAFT ASSYENGINE

C8450860170361-08014-041 CCCC

COND COND

161501524780506H04

07268DRIVESHAFT ASSYENGINE

C8450882970361-08014-041 CCCC

COND COND

161501081277506H06

04711SHAFT ASSY, T/R DRVSEC 1

WG300220010770361-03001-045 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 10 of 12

10-Aug-2016

COND COND

161501158951706H08


C2700036570361-03009-047 CCCC

COND COND

161501158952206H09

00SHAFT ASSY, T/R SEC3,4,5

A272-0412770361-05001-051 CCCC

COND COND

161501158952206H09


A272-0413870361-05001-051 CCCC

COND COND

161501158952206H09


A272-0413970361-05001-051 CCCC

COND COND

161501083295306H11


A273-0119970361-05002-045 CCCC

COND COND

161501158578806H12


A2740136970361-06002-047 CCCC

2520 8388

414101329342806H23

45777620FAN AXIAL 3900346SB70361-03005-107 17523

COND COND

432001207722807A01

13076579PUMP MODULE,HYDRAULIC

K4025ABR53023-06 CCCC

COND COND

432001207722807A01

12677455PUMP MODULE ASSY,HYDRAUL

416741ABR70652-02300-050 CCCC

COND COND

432001207722807A01

21547268PUMP MODULE ASSY,HYDRAUL

K2603ABR70652-02300-050 CCCC

13000 19247156001129125607A24

8917138SAS ACTUATOR C112-0678770410-02500-049 RCRC

13000 17088156001129125607A24

13805468SAS ACTUATOR C1120405370410-02500-049 RCRC

13000 19101156001129125607A24

10687169SAS ACTUATOR C1125184370410-02500-049 RCRC

COND COND

481001102247307B05A

05680VALVE, SOLENIOD 186593213850-3-1 CCCC

COND COND

481001102247307B05A

06184VALVE, SOLENIOD 204483213850-3-1 CCCC

COND COND

165001222431607B11

5334214ACCUMULATOR 9663454A3197170-5 CCCC

COND COND

168001342049608B20

52657620PANEL INDICATOR (PDU) 1068100-601561-000 CCCC

COND COND

168001342049608B20

40297620PANEL INDICATOR (PDU) 130670450-01043-124 CCCC

COND COND

611501114969609A01

15646492GENERATOR 83A105328B302-8-DM CCCC

COND COND

611501114969609A01

15377109GENERATOR WOMUAA1228B302-8-DM CCCC

COND COND

161501260074911C21

07087MIXER ASSEMBLY TMD046437430470400-02300-046 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 11 of 12

10-Aug-2016

2160 8344

161501141753211C23

22876184TAIL ROTOR PITCHCHANGE SHAFT

A233-0036270400-06100-042 02

11000 15295165001305695411C25

33257620SERVO ASSY, TAILROTOR

C300-0509470410-06520-046 RCRC

24400 29290165001143122611D01

27307620MAIN ROTOR PRIMARYSERVO

B30310388274000-1031 RCRC

24400 25834165001143122611D01


B303-0083870410-02820-054 RCRC

24400 28531165001143122611D01


B303-0794370410-02820-054 RCRC

13000 18680156001158968511D04

14297109AFT BELLCRANK 3450105070400-08102-045 RCRC

17000 24268

156001164416111D05

07268AFT TIE ROD SUPTFITTING

E3910259970400-08112-045 RCRC

2200 9468

168001164416011D06

07268AFT TIE ROD ASSY M3921067470400-08111-042 RCRC

4400 10730

156001286887011D07

06330AFT BELLCRANK SPTASSY

390-0278670400-08117-049 RCRC

11000 16792304001287243811D08

13177109LATERAL SWASHPLATELINK

A380-0411370400-08151-061 RCRC

11000 15231168001221286311D09

28787109LATERAL SERVOBELLCRANK

F337-0286970400-08166-041 RCRC

11000 15344168001158965311D11

25606904AFT WALKING BEAM 6570400-08104-048 RCRC

4600 10068

156001289269711D13

05468LEFT TIE ROD ASSY 344-0177870400-08115-046 RCRC

3500 10474

156001296948611D14

06974RIGHT TIE ROD ASSY 2880101570400-08114-051 RCRC

15000 18263168001158965211D15

38467109FORWARD BELLCRANK 80370400-08101-046 RCRC

5600 8863156001221261911D16

38467109FWD BELLCRANK SPTASSY

B367-0451870400-08162-042 RCRC

COND COND

168001261204411D25

11315328STABILATOR ACTUATOR 1467DL2155M20 CCCC

COND COND

168001261204411D25

14676184STABILATOR ACTUATOR 1998DL2155M20 CCCC

COND COND

599601316274311D26

21704922STABILATOR AMPLIFIER 176A70902-02001-048 CCCC

COND COND

599601316274311D26

79775248STABILATOR AMPLIFIER 248670902-02001-048 CCCC

COND COND

299501496368615A04

3575857ENGINE SEQUENCINGUNIT

23664504587 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 12 of 12

10-Aug-2016

COND COND

NSN PENDING19E04B

13267344SDC - DOPPLERNAVIGATION

2835P320A002-03 CCCC

COND COND

589501245909019E05A

07268RECEIVER-TRANSMITTER RADAR

28DDSM-C-967292 CCCC

COND COND

584101245909319E05C

07072INDICATOR HEIGHT 1319FFA3060591 CCCC

COND COND

660501503528419E06A

07268ATTITUDE HEADINGREFERENCE UNIT

11132765100-20 CCCC

COND COND

661001490516852A

07116AUTOMAT FLT CONTCOMPUTER

3569691825050-1-001 CCCC

7. SIGNIFICANT HISTORICAL DATA




HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM0489 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-Aug-2016

9000 15184

165001125090703A01A

00PISTON, MAIN L/GEARSTR

BEM251270250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

10-Aug-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

10-Aug-2016

9000 16547

165001125090703A01A

00PISTON, MAIN L/GEARSTR

BEM176570250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

10-Aug-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615014426926MAIN ROTORSPINDLE ASSY

70102-08200-069 A001-07947 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-Aug-2016

COND COND

311001158960705A01I02C

23522410THRUST BEARING B32528800SB7002-048 CCCC

COND COND

161501161437305A01I02

02813ELASTOMERIC BEARING LK8033SB7001-048 CCCC

13000 17091

531001126944405A01I04

00M/R SPINDLE NUT C479-1517570102-08105-102 RCRC

6400 10491

530601460602005A01I06

00TIE ROD (M/R SPINDLE) C504-0596238023-10372-101 RCRC

10000 14091

161501214914005A01I07

00CONTROL HORN ASSY A241-1902870102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

10-Aug-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

10-Aug-2016

COND COND

311001158960705A01I02C

2592382THRUST BEARING B325-34787SB7002-048 CCCC

COND COND

161501161437305A01I02


13000 17091

531001126944405A01I04

00M/R SPINDLE NUT C479-1541670102-08105-102 RCRC

6400 10491

530601460602005A01I06


10000 14091

161501214914005A01I07

00CONTROL HORN ASSY A241-1911270102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

10-Aug-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

10-Aug-2016

COND COND

311001158960705A01I02C

470470THRUST BEARING B325-35424SB7002-048 CCCC

COND COND

161501161437305A01I02

470470ELASTOMERIC BEARING B32424266SB7001-048 CCCC

13000 18973

531001126944405A01I04

00M/R SPINDLE NUT F479-0590970102-08105-102 RCRC

6400 12373

530601460602005A01I06


10000 15973

161501214914005A01I07

00CONTROL HORN ASSY H241-0072770102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

10-Aug-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 D00112117 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-Aug-2016

COND COND

311001158960705A01I02C

42930THRUST BEARING B32534002SB7002-048 CCCC

COND COND

161501161437305A01I02


13000 20620

531001126944405A01I04

00M/R SPINDLE NUT F4790496070102-08105-102 RCRC

6400 14020

530601460602005A01I06

00TIE ROD (M/R SPINDLE) C5041140238023-10372-101 RCRC

10000 17620

161501214914005A01I07

00CONTROL HORN ASSY G2410172470102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 D00112117 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

10-Aug-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70150-09100-043 A007-04553 05A024. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-Aug-2016

COND COND

156001447977405A02E

12365606M/R BLADE TIP CAP A849-1207070150-09207-041 CCCC

5000 11413

161501099234105A02I

05606CUFF ASSY E237-0022770150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

10-Aug-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

10-Aug-2016

COND COND

156001447977405A02E

31902832M/R BLADE TIP CAP A849-0228670150-09207-041 CCCC

5000 10574

161501099234105A02I

14412832CUFF ASSY E237-0060870150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

10-Aug-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70150-09100-043 A00700388 05A024. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-Aug-2016

COND COND

156001447977405A02E

8914470M/R BLADE TIP CAP A8491119870150-09207-041 CCCC

5000 8677

161501099234105A02I

32664470CUFF ASSY A2370597370150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

10-Aug-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

10-Aug-2016

COND COND

156001447977405A02E

20925207M/R BLADE TIP CAP A8490071670150-09207-041 CCCC

5000 9957

161501099234105A02I

19445207CUFF ASSY A2371419870150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

10-Aug-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615011997646SWASHPLATE ASSY 70104-08000-050 A107-01382 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-Aug-2016

COND COND

161501087160205A03A01

55715571STATIONARYSWASHPLATE

A222-0313070104-08010-044 CCCC

11000 11000

1615013575089 09905A03A02

00ROTATINGSWASHPLATE

A326-0115270104-08001-045 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615011997646SWASHPLATE ASSY 70104-08000-050 A107-01382 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

10-Aug-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

10-Aug-2016

17000 24109

161501078571106A08

04273SWASHPLATE GUIDE AER0204870351-08227-041 RCRC

3000 9037

161501110149106A13

10724273HOUSING ASSY MGB SKY009270351-08110-045 RCRC

7600 14088

304001415838806A18

6214273MAIN ROTOR SHAFT E2530372470351-08131-048 RCRC

12000 19109

161501497725706A19

04273PLANETARY CARRIERASSY

F2401004970351-08175-046 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

10-Aug-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615013765089TAIL ROTORGEARBOX ASSY

70358-06600-046 A006-03223 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-Aug-2016

12000 19075

161501074515306G01C

53419I/B RETENTION PLATET/R

FM341270358-06612-042 RCRC

5000 12128

304001292161706G01D

0419GEARSHAFT, BEVEL G3200142770358-06620-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615013765089TAIL ROTORGEARBOX ASSY

70358-06600-046 A006-03223 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

10-Aug-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



4141013293428FAN AXIAL 70361-03005-107 3900346SB 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-Aug-2016

2520 8388

311001127300506H23A

02825BALL BRNG ANN (OILCOOLER FWD)

4807210SFFC3 RCRC

2520 8388

311001127300506H23A

02825BALL BRNG ANN (OILCOOLER FWD)

4828210SFFC3 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



4141013293428FAN AXIAL 70361-03005-107 3900346SB 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

10-Aug-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70400-06100-042 A233-00362 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-Aug-2016

2160 8344

311001113828811C23A

02287BRNG T/R PITCH CHGSHAFT

C84010190SB1162-102 RCRC

COND COND

534001094578911C23C

22872287CLEVIS, ROD END A2330036220072010

70400-06702-041 CCCC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70400-06100-042 A233-00362 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

10-Aug-2016





MWO NO. /RELATED

PUBLICATION



APPLIED

PIDORGANIZATION

APPLYING MWO

MAIN ROTOR BLADE ASSY A00705484 70150-09100-043

H-60-10-SOF-01 DEPOT REPAIRED LEGACY

MAIN ROTOR BLADES

AASF #1 ST. PAUL

MN.

CH7883 29-Apr-2010 2

14-Apr-2010 M O

D.M.W.R. 1-1615-281 C1

15- SEP-2005

RECAP REQUIREMENTS FOR

THE UH-60 M/R BLADE P/N:

70150-09100-043, N/S/N:

1615-01-106-1903

CCAD/W0MUAA RS1005 01-Oct-2013 130

H-60-12-SOF-05 CHANGE TO DEPOT

REPAIRED LEGACY MAIN

ROTOR BLADES

COMPLIANCE DATE


9-Apr-2012



70150-09100-043 A00705484



MWO NO. /RELATED

PUBLICATION



APPLIED

PIDORGANIZATION

APPLYING MWO


D.M.W.R. 1-1615-281 C1

15- SEP-2005



70150-09100-043, N/S/N:

1615-01-106-1903




ROTOR BLADES

COMPLIANCE DATE


9-Apr-2012



70150-09100-043 A00707618



MWO NO. /RELATED

PUBLICATION



APPLIED

PIDORGANIZATION

APPLYING MWO

TAIL ROTOR BLADE ASSY A00901721 70101-31000-043

DMWR 1-1615-287 C1

15-SEP-05 R D

RECAPPED CCAD / W0MUAA AJ3147 16-Feb-2010 151

UH-60-02-ASAM-01

TB 1-1520-237-20-239

INITIAL AND RECURRING

INSPECTION OF THE TAIL

ROTOR FAIRING ASSEMBLY

CCAD / W0MUAA AJ3147 16-Feb-2010 1

14-Nov-2001 M O

DMWR 1-1615-287 C1

15 SEP 05 RD


THE UH-60 TAIL ROTOR

BLADE

P/N:70101-31000-043

NSN:1615-01-113-8188

CCAD/W0MUAA MF2034 24-May-2012 151

UH-60-02-ASAM-01

TB 1-1520-237-20-239





14-Nov-2001 M O



70101-31000-043 A00901721



MWO NO. /RELATED

PUBLICATION



APPLIED

PIDORGANIZATION

APPLYING MWO

TAIL ROTOR BLADE ASSY A00904890 70101-31000-043

RECAP REQUIREMENTS

FOR THE UH-60 TAIL

ROTOR BLADE

P/N:70101-31000-043

NSN:1615-01-113-8188

DMWR 1-1615-287 C1

15 SEP 05 RD


UH-60-02-ASAM-01

TB 1-1520-237-20-239





14-Nov-2001 M O

DMWR 1-1615-287

17-JUNE-13


THE UH-60 TAIL ROTOR

BLADE P/N:70101-31000-043

NSN: 1615-01-113-8188

CCAD/W0MUAA RC1982 17-Feb-2016 151

UH-60-02-ASAM-01

TB 1-1520-237-20-239




CCAD/W0MUAA RC1982 17-Feb-2016 1

14-Nov-2001 M O



70101-31000-043 A00904890



MWO NO. /RELATED

PUBLICATION



APPLIED

PIDORGANIZATION

APPLYING MWO


REPLACED NICKEL EROSION

STRIP IAW SRA AX 185409R4.

HEATER MAT RESISTANCE

CHECK COMPLETED, FOUND

WITHIN LIMITS. SPAR

PRESSURE SERVICED TO

10.50 PSI @ 73 DEG. F. 4 EC.

UPPER AND LOWER CUFF

BUSHINGS REPLACED.

STATIC WEIGHT AND

BALANCE COMPLETED W/

AVION BALANCER.

1109TH AVCRAD SB2729 01-Apr-2010 33.0

DMWR 1-1615-281 C1

15-SEP-2005



70150-09100-043, N/S/N:

1615-01-106-1903

CCAD/WOMMUA JB6971 23-Aug-2012 130

H-60-10-SOF-01 DEPOT REPAIRED LEGACY

MAIN ROTOR BLADES

CCA/WOMMUA JB6971 23-Aug-2012 3

14-Apr-2010 M O



ROTOR BLADES

COMPLIANCE DATE

CCAD/WOMMUA JB6971 23-Aug-2012 1

9-Apr-2012



70150-09100-043 A00704553



MWO NO. /RELATED

PUBLICATION



APPLIED

PIDORGANIZATION

APPLYING MWO

T700-GE-700 ENGINE ASSY GEE207533 6035T00G01

MWO 55-2840-248-50-29 INSTALLATION OF PTO

DRIVE ASSEMBLY (P/N

5044T27G02 FOR T701 AND

T700 ENGINES); REMOVE

AND REPLACE

W0MUAA MT5543 01-Oct-2010 1.5

MWO 55-2840-248-50-28 INSTALLATION OF

SELF-SEALING ADAPTER

ASSY. P/N 416-1255

(T700-GE-700 & 701

ENGINES); REMOVE AND

REPLACE

W0MUAA MT5543 01-Oct-2010 1.5

MWO 55-2840-248-50-32 MODIFICATION OF GAS

GENERATOR ROTOR

ASSEMBLY T700-T701;

REWORK & REPLACE

W0MUAA MT5543 01-Oct-2010 33

MWO 1-2840-248-20-2 ONE TIME INSPECTION &

CONVERSION OF FORMS

W0MUAA MT5543 01-Oct-2010 1

UH-60-99-ASAM-03

TB 1-2840-248-20-22

ONE TIME INSPECTION OF

ALL T700-GE-700 ENGINE

RECORDS

W0MUAA MT5543 01-Oct-2010 1

5-Nov-1998 M

AH-64-08-ASAM-05 INSPECTION FOR SUSPECT

ENGINE HARNESSES

W0MUAA MT5543 01-Oct-2010 1

22-Sep-2008 R O

UH-60-08-ASAM-14 INSPECTION FOR SUSPECT

ENGINE HARNESSES

W0MUAA MT5543 01-Oct-2010 1

22-Sep-2008 R O



6035T00G01 GEE207533



8724673HELICOPTER, UTILITY EH-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

A092 12 Jun 201630TM 11-6140-203-23&P30 DAY SLAB BATTERYINSPECTION (D8565/11-1)

13 May 2016D

A110 7630.440TM 1-1520-237-PMSPMS 40 HOUR INSPECTION (ESMONLY)

7590.4H

A115 01 Jul 201630TM 1-1520-237-23-1LUBE REQUIRMENTS (ESMONLY)

01 Jun 2016D

A115 7640.740TM 1-1520-237-23-1LUBE REQUIRMENTS (ESMONLY)

7600.7H

A116 7624360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE (ESM ONLY)

7264H

A116 16 Aug 201612H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE (ESM ONLY)

16 Aug 2015M

A117 7624360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE(ESM ONLY)

7264H

A117 16 Aug 201612H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE(ESM ONLY)

16 Aug 2015M

A160 02 Aug 201690TM 1-1520-237-23-1ESM 90 DAY CORROSIONINSPECTION

04 May 2016D

A210 7624120TM 1-1520-237-23-1120 HOUR INSPECTIONREQUIREMENTS (ESM ONLY)

7504H

A211 7624360H-60-10-AMAM-11APU OIL SAMPLE (ESM ONLY) 7264H

A211 16 Aug 201612H-60-10-AMAM-11APU OIL SAMPLE (ESM ONLY) 16 Aug 2015M

A213 7739.8120TB 1-1520-237-20-266ENGINE COMPRESSORCLEANING (ESM ONLY)

7619.8H

A295 7624360TM 1-1520-237-PMISTABILATOR ACTUATOR ASSYLUBE (ESM ONLY)

7264H

A298 7624360TM 1-1520-237-23-1LUBE TAIL WHEEL BEARING(ESM ONLY)

7264H

A298 20 May 201612TM 1-1520-237-23-1LUBE TAIL WHEEL BEARING(ESM ONLY)

20 May 2015M

A299 7624360TM 1-1520-237-23-1SWASHPLATE LUBE (ESM ONLY) 7264H

A299 24 Dec 201612TM 1-1520-237-23-1SWASHPLATE LUBE (ESM ONLY) 24 Dec 2015M

A440 7624720TM 1-1520-237-23-1CLEAN TAIL WHEEL LOCKPIN 6904H

A470 8972.21500UH60 IETMREPLACE NUMBER TWOCROSSFEED VALVE

7472.2H

A471 8409.92160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

6249.9H

A472 8409.92160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

6249.9H

A473 8409.92160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

6249.9H

A476 9997.35000TM 1-1520-237-23-1REPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

4997.3H

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

A477 9997.35000TM 1-1520-237-23-1REPLACEMENT OF STABILATORACTUATOR BOLTS

4997.3H

A480 9997.35000TM 1-1520-237-23, C4REPLACE PIVOT BOLT 70400-08159-101,102,103,104

4997.3H

A485 9997.35000TM 1-1520-237-23, C4REPLACE BELLCRANK BOLT70400-08159-105,106,107,108

4997.3H

A496 28 Sep 2016180TM 1-1500-204-23-1CF3BR FIRE EXTINGUISHERWEIGHT TEST & INSPECTION

01 Apr 2016D

A501 07 Aug 2016180TM 1-1520-237-23-1MAIN ROTOR BLADE PRESSURECHECK

09 Feb 2016D

A502 31 Oct 2016180TM 1-1520-237-23INSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

04 May 2016D

A530 11 May 201712DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

11 May 2016M

A532 27 Aug 201612TM 1-1500-204-23-4COMPASS SWING / RMI SWING 27 Aug 2015M

A533 31 Jul 201612TM 1-1520-237-23-1PITOT STATIC SYSTEMINSPECTION

31 Jul 2015M

A534 30 Jun 201612TM 1-1500-204-23-1FIRST AID KIT INSPECTION 30 Jun 2015M

A538 10 May 201612TM 1-1520-237-23-1FAT/OAT GAUGEINSPECTION/TEST

10 May 2015M

A553 07 Aug 201612AR 95-1ANNUAL WEIGHT AND BALANCEINVENTORY (365-1)

07 Aug 2015M

A580 09 Apr 201724TM 11-6140-203-23&PRETURN SLAB TO AVIM FORCAPACITY CHECK (EVERY 24MONTH)

09 Apr 2015M

A621 13 Feb 201824AR 95-1AIRCRAFT WEIGHING CLASS 1 13 Feb 2016M

A625 09 Apr 201760TM 11-6140-203-23&PREPLACEMENT OF SLABBATTERY (SLAB)

09 Apr 2012M

A630 01 Nov 2022114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 May 2013M

A633 01 Nov 2022114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE DODIC MH92

01 May 2013M

A638 01 Nov 2022114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #2,CARTRIDGE DODIC MH92

01 May 2013M

A640 01 Nov 2022114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE CARTRIDGE,31512AS105, 30903824-1

01 May 2013M

A642 01 Sep 202172TB 9-1300-385CARGO HOOK CARTRIDGEREPLACEMENT, MJ21

01 Sep 2015M

A648 20 Oct 2023180TM 1-1520-237-23REPLACE T/R SPRING CAPSULEASSY

20 Oct 2008M

A660 01 Nov 202172TB 9-1300-385,REPLACE THRUSTEREMERGENCY RELEASE CARGOHOOK, MJ20

01 Nov 2015M






7. FREQUENCY 4.




INSP

A665 09 Aug 201948H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

09 Aug 2015M

A670 08 Nov 201948TM 1-1520-237-23-12CABIN TUB INSPECTION 08 Nov 2015M

A675 09 May 201648TM 1-1520-237-23-12FLIGHT CONTROL ROD INSP 09 May 2012M

A695 7624720H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

6904H

A695 19 Apr 201848H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

19 Apr 2014M

A755 90009000H-60-10-ASAM-11PC LINK TO SWASHPLATEBOLTS REPLACEMENT

0H




05-Aug-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-207533

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

10-Oct-2012 8524475 REPLACED ENG6000 101 97 197.4122204 848

08-Nov-2012 8724673 ENG CHANGE6000 103 100 198.473763 849

18-Nov-2013 8724673 POST PHASE3000 108 104 198.2194124 845

18-Nov-2013 8724673 POST PHASE3000 107 104 198.1194124 847

28-Aug-2015 8724673 ENGINE REINSTALLED.5000 103 98 198.6184471 847


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

05-Aug-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-207370

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

11-Aug-2012 8724673 ENG CHG FOR TBO4000 107 100 198.8204806 847

18-Nov-2013 8724673 POST PHASE3000 107 104 198.1195373 847

13-Sep-2014 8724673 RE-ESTABLISH BASELINE4000 105 98 198.5235664 848

28-Aug-2015 8724673 ENGINE REINSTALLED.5000 103 98 198.2185746 847


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

T/T I HIST RCDR SNSERIAL NO. OP HRSLCF-2LCF-1POSHOURSAIRCRAFT AIRCRAFT ENGINE SERIAL NO. 13.12.11. 14.10.9.8.7.6.

(256)123-3456HUNTSVILLEK08DD23. UIC 5. TELEPHONE NUMBER4. LOCATION

16228 SESI

2. Organization

CSGLD-1052

REQUIREMENT CONTROL SYMBOL(Julian)1. PERIOD ENDING DATE


1GE-E-307057 CAO0054150081410730539577187978624568

2GE-E-307026 ECDH06219258753525464396287978624568

1GE-E-207370 CAO004694186200368597218476208724673

2GE-E-207533 ECDH0817328389667540164776208724673

1GEE207783 ECDH0338456914716375777055468123582

2GEE306017 CAO0120853389042352771755468123582


ENGINE COMPONENT OPERATING HOURS RECORDDA FORM 2408-19-3 E, DEC 1991

PIDMWODATE HRS



ACCESSORY MODULE 8724673A258-031661. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 FM

JK01537127-Mar-2013

3USAACE, FT.RUCKER, AL

COMPLY WITH THE REQUIREMENTSOF H-60-13-ASAM-04(PMB) PLASTICMEDIA BLAST AND OXIDE FLAKERESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level


EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1-E, OCT 91

PIDMWODATE HRS



ACCESSORY MODULE 8724673A258-071531. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 OM

BK02629227-Mar-2013

5USAACEPLASTIC MEDIA BLAST (PMB) ANDOXIDE FLAKE RESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



ANTI-ICE VALVE 8724673B61661. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


22-Jun-2011 OM

DM02621706-Oct-2012

0.3USAACEANTI-ICE / START BLEED VALVEACTUATOR SHAFTS

H-60-11-ASAM-11MWO:

Priority Mnt Level



PIDMWODATE HRS



ANTI-ICE VALVE 8724673COMH20301. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 OM

JK01537107-Sep-2012


ENGINE ANTI-ICE/START BLEEDVALVE (AISBV)

H-60-12-ASAM-10MWO:

Priority Mnt Level




8724673116305-302AUXILIARY POWER UNITSPE041069

224

1117

1167

6726

1152

1152

1

1

5=

TOTAL COMPONENT COUNTS

COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-

READING AT INSTALLATION OF

MODULE/RECORDER3

READING AT REMOVAL OF

7. HISTORY RECORDER S/N

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE

OPERATING HOURSTEMP/TEMP INDEXLCF - 2LCF - 1

HISTORICAL COUNTS ON COMPONENT/MODULE

7. HISTORY RECORDER S/N6.

5. NHA - Serial Number4. P/N3. NOMENCLATURE2. Serial Number1. MODEL

**Note - APU Information LCF1 = NUMBER OF OVERHAULS LCF2 = STARTS SINCEOVERHAUL TTI = STARTS SINCE NEW OPH = ONLY FOR APU's WITH HOUR METERINSTALLED - ENTER TIME ON METER

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

HISTORY RECORDER, COMPONENT, MODULE RECORDDA FORM 2408-16-1-E, OCT91

OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-

12.HISTORY COUNTS AT LAST DEPOTREPL

11.

O/H OR

10.

SERIAL NUMBER9.PART NUMBERNOMENCLATURE

8.

ReportDate:

Major Nomenclature Major Part NumberMajor Wuc Major Serial Number

03-Aug-2016 2/2

15B 116305-302 AUXILIARY POWER UNIT SPE041069

893557401

0000SIF47494502902WHEEL,COMPRESSOR

6015

6000

893557401

0000S2634503991WHEEL, TURBINE

6015

6000


10/13/200912:00:00 AM

1 13OCT09:RECEIVED APU FOR RESET INSPECTION. REPLACED ALLFILTERS, CLEANED/INSPECTED TURBINE AND HOT SECTION. MOCCOMPLETED. METER REPLACEED WITH NEW AT STS 2424, HRS 396 . TBOTIME FOR THIS APU IS 3576 METER EVENTS AT 6000 TOTAL APU STARTS.ENTERED BY KF7892 ESRA, FTCKY. DSN 635-6201 4036 THIS DATE,RECEIVED APU S/N: SP-E041069 FOR AN OVERHAUL. READINGS ATRECEIPT: METER HOUR: 0497; START METER: 3150; TSN: 0893 ; SSN: 5574.INITIATED NEW FORM. 4226 THIS DATE, APU S/N: SP-E041069 WASOVERHAULED AND PROCESSED IN ACCORDANCE WITH DMWR 1-2835-209AS SUPPLEMENTED BY NAVAIRDEPOT MCAS CHPT LES CP23-0-LL-173,REV C AND IS SERVICEABLE FOR INSTALLATION AND CONTINUEDSERVICE. WORK PERFORMED IS AS FOLLOWS:INSTALLED: NEW C/W; NEWT/W; FUEL CONTROL S/N: 07-04-104. NEW METER INSTALLED AT TSN: 0893SSN: 5574. METER READINGS AT INSTALL: HOURS: 0000; STARTS:0015.READINGS AT COMPLETION: METER HOURS: 0001; METER STARTS:0024;TSN: 0894; SSN: 5583.

AG3612 FRC EAST CHERRY POINT NC

9/23/201412:00:00 AM

1 INSTALLED APU SN: SPE041069, ON ACFT 8724674, AT 7785 ACFT HRS,WITH TTSN: 894, TSSN: 5583, 1 PRIOR O/H, AND TSSO: 9. METER READINGS:STARTS: 24, HOURS: 1.

CN014192 USAACE FT RUCKER,AL.

7/13/201612:00:00 AM

1 INSTALLED UNSERVICEABLE (LEAKING) APU SN: SPE41069, ON ACFT8724673 (SCHEDULED FOR TURN-IN), AT 7620 ACFT HRS, WITH TTSN: 1117,TSSN: 6726, TSSO: 1152, AND 1 PRIOR O/H. METER READINGS:STARTS/EVENTS: 1167, HRS: 224.

CN014192 USAACE FT. RUCKER,AL.

REVERSE OF DA FORM 2408-16-1 E, OCT 91

0

360

7787

8724673 1152 0

e. ACFT HRS INSTALLEDc. TIME SINCE NEW OR OVERHAULc. SERIAL NUMBER

EH-60A SPE041069 Days

b. MAKE OR TYPE d. ACFT HRS LAST OIL CHANGEb. SERIAL NUMBER

HELICOPTER, UTILITY AUXILIARY POWER UNIT Hrs

a. NOMENCLATURE AND TYPEa. NOMENCLATUREFREQUENCY

COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b

SAMPLE DATE PIDSAMPLELAST OILEND ITEM

RESULTSDATE RESULTS RECEIVED7. 8.6. REASON FORHOURS5.4.

COMPONENTCHANGE

VM01466330-Oct-2014ABNORMALBASELINE0.0894778529-Oct-2014

VM01466305-Nov-2014ABNORMALLAB REQUES1.0894778631-Oct-2014

VM01466307-Nov-2014NORMALLAB REQUES2.0894778705-Nov-2014

KG01419110-Aug-2015NORMALROUTINE359.112558145.607-Aug-2015

31OCT14 - LAB REQUEST CODE C BASELINE- ROUTINE, POST PHASE

9. REMARKS:

For use of this form, see DA PAMs 738-751; the proponent agency is DCSLOGDA FORM 2408-20, DEC 91, MAY BE USED

OIL ANALYSIS LOGDA FORM 2408-20, OCT 1997

REMARKS

UNSERVICABLE APU, LEAKING. FAILURE CODE IS 381. ULLS WILL NOT ALLOW EDITING OF FAIL CODE UPON INSTALLATION.

APD LF v1.00DA FORM 2410, JAN 97, IS OBSOLETEDA FORM 2410, MCDS

COMPONENT REMOVAL / REPAIR / INSTALL / GAIN / LOSS RECORD

For use of this form, see DA PAM 738-751; the proponent agency is DCS, G-4

SECTION I - MAINTENANCE ACTION

SECTION II - IDENTIFICATION

INSTALL REMOVE REPAIR GAIN/LOSS

5. MII 6. CAGE CODE 7. LANDINGS 8. NO. OF PREV

O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE

4. SERIAL NUMBER3. PART NUMBER2. NSN1. NOMENCLATURE

21. VERSION

d. OP HOURSc. TTIb. LCF 2a. LCF 1

17. COMPONENT CUMULATIVE COUNT / HOURS16. CONFIG CODE13. METER HRS

18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H

SECTION III - NEXT HIGHER ASSEMBLY (NHA) INSTALL / REMOVE INFORMATION

24. NHA PART NUMBER23. NHA NSN22. NHA NOMENCLATURE

25. NHA SERIAL NUMBER 26. NHA HOURS 27. START METER 28. METER HRS

31. WHEN DISCOVERED30. MALFUNCTION CODE29. HISTORY RECORDER SN

32. HISTORY RECORDER READING 33. NHA CUMULATIVE COUNT / HOURS

SECTION IV - GAIN / LOSS / REPAIR / ADMIN INFORMATION

d. OP HRSc. TTIb. LCF 2a. LCF 1d. OP HRSc. TTIb. LCF 2a. LCF 1

44. DATE

47. LOST / SHIPPED TO 48. LOCATION

45. PID AND TELEPHONE NUMBER 46. AKO USER NAME

43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL

38. ACTUAL FAILURE CODE 39. MAINTENANCE LEVEL

MWO

RECAP

40. MANHOURS 41. SRA 42. UIC

37. NEW NSN36. NEW PART NUMBER35. GAIN OR

LOSS CODE

34. INSPECTION ACTION CODES

X

15-Jul-2016 CN0141 334-503-3807

1 W0U91TF

0 0 0 0 0 0 0 7620

7620 1117 224

HELICOPTER, UTILITY 1520010820686 EH-60A

8724673

0 0 0 1152 6726

15B 0 0

55820 1 0 1117 224 381

SPE041069116305-3022835013692818AUXILIARY POWER UNIT

1117



RDMR-AEU

DEPARTMENT OF THE ARMY US ARMY RESEARCH, DEVELOPMENT AND ENGINEERING COMMAND

AVIATION AND MISSILE RESEARCH, DEVELOPMENT, AND ENGINEERING CENTER 5400 FOWLER ROAD

REDSTONE ARSENAL, ALABAMA 35898-5000

MEMORANDUM FOR

Utility Helicopters Project Office, (SFAE-AV-UH/Wally Newcomb), Building 5308, Redstone Arsenal, AL 35898-5000

US Army Aviation Center of Excellence (USAACE), Fort Rucker, AL 36362-5000

SUBJECT: Airworthiness Release (A WR) to Conduct a Modified Enhanced Scheduled Maintenance (ESM) Program Schedule (AWR 1220)

26 Jan 15 I RIO 19 Oct 04

1. Scope: This memorandum constitutes an A WR in accordance with (IA W) Army Regulation (AR) 70-62 for all UH-60A/L, EH-60A, and UH-60M helicopters assigned to, and in support of, the USAACE, to include those assigned to the US Army Aeromedical Research Laboratory (USAARL), Fort Rucker, AL, to conduct revised maintenance inspection procedures cited within the referenced documents.

2. ·validity: This AWR is terminated 1Nov16, upon transfer of the helicopter, or upon issuance of a later A WR, whichever occurs first.

3. List of Appendices: This memorandum and Appendix A will be carried in the logbook, and a complete A WR copy with all appendices shall be kept in the aircraft historical record file.

Appendix A. Restrictions and Operating Information Appendix B. Configuration and Installation Detail Appendix C. Inspections, Maintenance, and Logbook Instructions Appendix D. References

4. The point of contact for this Airworthiness Release is Mr. Mark Coble, DSN 897-3117, commercial (256) 313-3104, or e-mail: [email protected]. An alternate point of contact is Scott Oberman (Contractor, IronMountain Solutions, Inc.) commercial (256) 313-3142, DSN 897-3142, or email: [email protected] or ae-u-tts amrdec.arm .mil.

Director Aviation Engineering

Printed on • Recycled Paper

RDMR-AEU 26 Jan 15 I RIO 19 Oct 04

SUBJECT: Airworthiness Release (A WR) to Conduct a Modified Enhanced Scheduled Maintenance (ESM) Program Schedule (A WR 1220)

Appendix A. Restrictions and Operating Information:

Operate the UH-60A/L and EH-60A IAW the aircraft Operators Manual (reference 5), except as modified by this AWR. Operate the UH-60M IAW the aircraft Operators Manual (reference 13) and AWRl 726 (reference 14), except as modified by this AWR.

Appendix B. Configuration and Installation Detail:

The basic UH-60A/L helicopter is defined in reference 5, with exceptions as noted within this Airworthiness Release. The basic UH-60M helicopter is defined in references 13 and 14, with exceptions as noted within this Airworthiness Release.

NOTE

Any deviation from the instructions as stated herein is not authorized. Deviation from instructions shall void this A WR.

Per TM 1-1500-328-23 (reference 9), recurring special inspections may be accomplished within a window of plus or minus 10% of the inspection interval, not to exceed 5 flight hours or 30 calendar days, unless otherwise stipulated.

2

RDMR-AEU 26 Jan 15 I RlO 19 Oct 04


Appendix C. Inspections, Maintenance, and Logbook Instructions:

1. A comprehensive Phase inspection cycle for all H-60A/L/M series aircraft assigned to, and in support of, USAA CE, to include those assigned to USAARL will be performed at 720 hours, IA W reference 4 or 17. A 360-hour Special Inspection cycle, unless otherwise directed within this A WR, will be implemented for the following items:

a. Perform a torque check on tail rotor inboard retention plate attaching bolts per reference 1 or 15, Tail Gear Box Inboard Retention Plate Torque Check - 9 to 11 Hours.

b. Inspect tail rotor blade spar for wear or damage, comer to fairing clearance, and delamination and splinters on spar in areas of fairing inner lip, per reference 1or15, Tail Rotor Blade Inspections.

c. Replace non-ducted oil cooler housing aft bearing in accordance with procedures of reference 1 or 15, Aircraft General Life Limited Components and Drive System Oil Cooler. Replacement interval for the UH-60 oil cooler exit bearing equipped with slotted duct, PIN 70361-03011-105, will be IAW reference 4 or 17.

d. Perform Stabilator inspection requirements IA W reference 1 or 15, Aircraft General Every 360 Hours.

e. Deleted

f. Lubricate swashplate per reference 1 or 15, Aircraft General Lubricate Swashplate.

g. For main rotor blades equipped with Aluminum Tip Caps only, remove and inspect tip cap interior, blade tip rib for cracks, and tip block for corrosion and condition per reference 1, Rotor System Main Rotor Blade Inspections.

UH-60M only:

h. (PMI item) 3.8: Check transition section to tailcone bolts for proper torque.

i. 6.7: Inspect Aft bellcrank for bearing play, looseness, and the exposed portions of lug areas for damage and corrosion. Do not disconnect hardware to inspect lugs:

j. 6.38/6.44: Inspect engine aft mounts. Support engine to relieve pressure on mount struts. Visually inspect engine struts and mount bearings for security, condition and evidence of wear. If bearing damage or excessive wear is evident, refer to inspection of aft engine mounts IA W applicable maintenance manual for corrective action.

3

26 Jan 15 I RIO RDMR-AEU 19 Oct 04 SUBJECT: Airworthiness Release (A WR) to Conduct a Modified Enhanced Scheduled Maintenance (ESM) Program Schedule (A WR 1220)

k. 6.53: Inspect IRCM transmitter, shock mounts, mounting support, and shroud for security, racks, and damage.

2. through 4. Deleted

5. Lubrication requirements will be IAW reference 1 or 15, and scheduled at 720 hours in conjunction with the reference 4 or 17, 720 hour PMI Inspection:

a. Mixer Bellcranks, Aircraft General Lubricate Mixer Bellcranks b. Engine Rotary Inputs, Aircraft General Lubricate Rotary Inputs c. Windshield Wiper Converter, Aircraft General Lubricate Windshield Wiper Converter d. Tail Wheel Locking Pin, Aircraft General Lubricate Tail Wheel Lockpin e. Door Locks, Aircraft General Lubricate Door Locks f. BRU-22A/A Ejector Rack, Aircraft General Lubricate BRU-22A/A Ejector Rack

6. The following lubrication requirements will be recorded on DA Form 2408-18, and performed · during the reference 3 or 18, 40 hour PMS inspection or 30 days, whichever interval occurs first:

a. Lubricate Bifilar, Aircraft General Lubricate Bifilar. b. Lubricate Landing Gear Struts, Aircraft General Lubricate Landing Gear Shock Struts. c. Lubricate Stabilator Actuator, Aircraft General Lubricate Stabilator Actuator Assembly. d. Lubricate Windshield Wiper Studs, Aircraft General Lubricate Windshield Wiper Pivot

Studs. e. Lubricate Windshield Wiper Converter Splines, Aircraft General Lubricate Windshield

Wiper Converter.

7. Engine inspections will be IAW references 2, 3, 4 and 7, or 16, 17, 18 and 7.

8. Abbreviated (above fuel cell) Fuel Feed System Integrity Test requirements ofreference 1 or 15, Fuel System Fuel Feed System, will be accomplished at the 720 hour PMI Inspection or 24 calendar month intervals, which ever interval occurs first. A Complete System Integrity Test is required every 48 months following fuel cello-ring replacement IA W reference 1 or 15, Aircraft General Retirement Schedule.

9. Deleted

10. Engine compressor cleaning requirements, as outlined in reference 7, will be performed at a 120 hour interval, or earlier, at the discretion of the Contracting Officer or his/her designated representative.

4



11. Army Oil Analysis Program (AOAP) scheduling requirements of reference 10 will apply at 360-hour intervals. Main transmissions equipped with 3 micron filtration are exempt from routine oil analysis requirements, however, sampling for oil physical properties is required during 720 hour phase inspection.

12. Main Rotor Expandable Blade Pin Inspection will be managed as a 10 hour Special Inspection on aircraft DA Form 2408-18. Inspection requirements will be IAW reference 12, and conducted IAW reference 1 or 15, Aircraft General Ten Hour Inspection.

13. Replacement interval for the main rotor spindle elastomeric sleeve bearing will be IA W the reference 4 or 1 7 document.

14. Operational checks will be IAW reference 4 or 17.

NOTE

Any anomalies or deviations to current requirements, except as outlined in this A WR, shall be reported to the point of contact for this A WR.

15. Logbook Entries:

a. In accordance with Department of the Army (DA) Pamphlet 738-751, the following entry shall be made on the DA Form 2408-13-1/2408-13-1-E and shall be perpetuated on each form during the period of installation or until superseded by another Airworthiness Release:

Place a circled "X" in the Status block IA W DA Pamphlet 738-751. In the Faults/Remarks block, make the following entry: "Maintain aircraft as prescribed in A WR1220, dated 26 Jan 15."

b. The remaining blocks in the Fault Information block will be completed per DA Pamphlet 738-751.

c. Unit Level Logistics System-Aviation (ULLS-A) users shall use the equivalent electronic form.

5

26 Jan 15 I RIO RDMR-AEU 19 Oct 04 SUBJECT: Airworthiness Release (A WR) to Conduct a Modified Enhanced Scheduled Maintenance (ESM) Program Schedule (AWR 1220)

Appendix D. Referen~es:

1. EM 0013, TM 1-1520-237-23&P, Aviation Unit and Intermediate Maintenance for Army Models UH-60A, UH-60L, EH-60A, HH-60A, and HH-60L Helicopter, 30 May 14.

2. Technical Manual 1-1520-237-PMD, Preventive Maintenance Services Daily Inspection Checklist for UH-60A, UH-60L, EH-60A, UH-60Q and HH-60L Helicopters, 25 Sep 09, with all changes.

3. Technical Manual 1-1520-237-PMS, Preventive Maintenance Services 40-Hour Checklist for UH-60A, UH-60L, EH-60A, HH-60A and HH-60L Helicopters, 25 Sep 09, with all changes.

4. Technical Manual 1-1520-237-PMI, Phased Maintenance Inspection Checklist for Helicopters, Utility Tactical Transport UH-60A, UH-60L, EH-60A, HH-60A and HH-60L Helicopters, 25 Sep 09, with all changes.

5. Technical Manual 1-1520-237-10, Operator's Manual for UH-60A, UH-60L and EH-60A Helicopters, 25 Sep 09, with all changes.

6. Deleted

7. Interactive Electronic Technical Manual (EM) 0271, Technical Manual 1-2840-248-23&P, Aviation Unit and Intermediate Maintenance Manual, Including Repair Parts and Special Tools List for Engine, Aircraft Turboshaft, T700-GE-700/701/701C and 701D, 31Aug10.

8. Deleted

9. Technical Manual 1-1500-328-23, Aeronautical Equipment Maintenance Management Policies and Procedures, 30 Jul 99, with all changes.

10. Technical Bulletin 43-0211, Army Oil Analysis Program (AOAP), 30 Apr 10.

11. Sikorsky Technical Report TRS-DO 0038, Analysis of Government Proposed Inspection Changes, Contract DAAH23-00-01-148/0038, 23 Sep 03.

12. Safety of Flight Message UH-60-08-SOF-01, All H-60 Series Aircraft, Main Rotor Blade Expandable Pin Inspection Change, 28 Jan 08.

13. Technical Manual, TM 1-1520-280-10, Operator's Manual for Army Models UH-60M and HH-60M Helicopter, 14 Aug 09, with all changes.

14. Memorandum, Aviation Engineering Directorate, RDMR-AEU, 22 Mar 11, with latest revision, subject: Airworthiness Release (A WR) for US Army UH/HH-60M Helicopters (A WR 1726).

6


SUBJECT: Airworthiness Release (A WR) to Conduct a Modified Enhanced Scheduled Maintenance (ESM) Program Schedule (A WR 1220)

15. EM 0284 TM 1-1520-280-23&P, Aviation Unit and Intermediate Maintenance for Army Models UH-60M and HH-60M Helicopter, 30 Apr 13.

16. Technical Manual 1-1520-280-PMD, Preventative Maintenance Services, Preventative Maintenance Daily for Helicopters, Utility Tactical Transport, UH-60M, HH-60M, 14 Aug 09, with all changes.,

17. Technical Manual 1-1520-280-PMI, Phased Maintenance Inspection Checklist for Helicopters, Utility Tactical Transport, UH-60M, HH-60M, 14 Aug 09, with all changes.

18. 280-PMS, Preventive Maintenance (PM) Services Inspection Checklist for Helicopters, Utility Tactical Transport, UH-60M, HH-60M, 14 Aug 09, with all changes.

7

PIDMWODATE HRS



CONTROL HORN ASSY 8724673A241-190281. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


10-Dec-1998 OM

MB01113703-Oct-2008

0.5USAACE FT.RUCKER, AL(TB1027)

ALL H-60 SERIES AIRCRAFT,INSPECTION AND REVISEDRETIREMENT LIFE OF MAIN ROTORPITCH HORNS, P/N 70102-08111-047

UH-60-99-ASAM-06MWO:

Priority Mnt Level



PIDMWODATE HRS



CONTROL HORN ASSY 8724673A241-191121. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


10-Dec-1998 OM

MB01113703-Oct-2008

0.5USAACE FT.RUCKER, AL(TB1027)

ALL H-60 SERIES AIRCRAFT,INSPECTION AND REVISEDRETIREMENT LIFE OF MAIN ROTORPITCH HORNS, P/N 70102-08111-047


Priority Mnt Level



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

08-Aug-2012 JB6971 (361)961-6345 john.bonawitz

32 W0MUAAD

0 0 0 0 0 0 0 5606

5606 0 0

MAIN ROTOR BLADE ASSY 1615011061903 70150-09100-043

A00704553

0 0 0 0 0

05A02I 0 0

78286 0 0 0 0 0 799

E2370022770150-09109-0411615010992341M/R BLADE CUFF

0



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

19-Sep-2013 RS1005 3619616474 ruby.a.sanchez

32 W0MUAAD

0 0 0 0 0 0 0 5207

5207 0 0


A00705484

0 0 0 0 0

05A02I 0 0

78286 0 0 0 1944 0 799

A2371419870150-09109-0411615010992341M/R BLADE CUFF

1944



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

03-Oct-2013 RS1005 3619616474 ruby.a.sanchez

32 W0MUAAD

0 0 0 0 0 0 0 2832

2832 0 0


A00707618

0 0 0 0 0

05A02I 0 0

78286 0 0 0 1441 0 799

E2370060870150-09109-0411615010992341M/R BLADE CUFF

1441



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

18-Apr-2012 AF0603 961-6215 albert.flores

3 W0MUAAD

0 0 0 0 0 0 0 4470

4470 0 0


A00700388

0 0 0 0 0

05A02I 0 0

78286 0 0 0 3266 0 799

A2370597370150-09109-0411615010992341M/R BLADE CUFF

3266




CAO00469

87246736035T00G01ENGINE ASSY, TURBINEGE-E-207370

4185

6113

20036

23694

8595

18169

2182

4392

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE





T700-GE-700




OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 2/13

04A 6035T00G01 ENGINE ASSY, TURBINE GE-E-207370

480423301167853952

398936075115942906GE-C-0077386035T02G01COLD SECTIONMODULE

COND

COND

4804000

3260000GGMBC2346039T58G02COMBUSTION LINER

COND

COND

480423301167853952

24522003456921543MRSG07036055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

4804000

4535000AMDA02625043T24G14STAGE 1 NOZZLEASSY

COND

COND

480423301167853952

2473762965202556GE-L-0069836064T98G01POWER TURBINEMODULE

COND

COND

4804000

2771000GED0373176035T01G01ACCESSORY MODULE

COND

COND

4804000

4464000SUS015506034T62P13PARTICLESEPARATOR BLOWER

COND

COND

5370000

2289000J83695074T79G07FUEL CONTROL

COND

COND

4804000

1878000APM778RR4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

4806000

3224000ECD004974046T29G13ELECTRICALCONTROL UNIT

COND

COND

480423301167853952

28711964372021740CAO004694046T26G03HISTORY RECORDER

COND

COND


11/14/201312:00:00 AM

OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 3/13


4804000

0000UDDK29024046T25G06COOLER, OIL

COND

COND

4804000

1661000COMH20304046T28G14ANTI-ICE VALVE

COND

COND


4/23/201012:00:00 AM

1 ENGINE REPAIRED 21APR10 IAW DMWR 1-2840-248 & CHANGES ANDRECAPPED DTD 03DEC01. /S/M. BENAVIDES, AIRCRAFT DATATECHNICIAN

CCAD NOT GIVEN

8/1/201212:00:00 AM

1 ECU ECD00497 INSTALLED ON UNINSTALLED ENGINE WITH TTSN 3224.ENGINE CUM CTS= LCF1 3954 LCF2 16790 TTI 23384 OP HR 4806. H/R S/NCAO00469 READINGS= LCF1 1742 LCF2 7207 TTI 19726 OP HRS 2873 (OWILLIAMS 0950)

OW010950 USAAVNC FT RUCKER, AL

8/1/201212:00:00 AM

2 FUEL CONTROL S/N J8045 INSTALLED ON UNINSTALLED ENGINE WITHTTSN 4531. ENGINE CUM CTS= LCF1 3954 LCF2 16790 TTI 23384 OP HR 4806.H/R S/N CAO00469 READINGS= LCF1 1742 LCF2 7207 TTI 19726 OP HRS 2873(O WILLIAMS 0950)

OW010950 USAAVNC FT RUCKER, AL

8/11/201212:00:00 AM

1 INSTALLED ENGINE (GE-E-207370) WITH CTS: 3954/16790/23384/4806 ONACFT 8724673 @ 6363.2 ACFT HRS. HIS REC (CAO00469) READINGS:1742/7207/19726/2873.

BK026292 USAACE FT RUCKER, AL

10/18/201212:00:00 AM

1 REMOVED FUEL CONTROL S/N: J8045 W/TSN: 4685 FROM ENGINE S/N:GE-E-207370 (ACFT 8724673 @ 6513.0 ACFT HRS). IAW 12-ASAM-11. ENGINECUMM CNTS: 4008, 16955, 23467, 4960. ENGINE H/R (S/N: CAO00469)READINGS: 1796, 7372, 19809, 3027.

JK015371 USAACE FT. RUCKER, AL

10/18/201212:00:00 AM

2 INSTALLED FUEL CONTROL S/N: UDAJ6042 W/TSN: 4982, TTSO: 0 ONENGINE S/N:GE-E-207370 (ACFT 8724673 @ 6513.0 ACFT HRS). IAW 12-ASAM-11. ENGINE CUMM CNTS: 4008, 16955, 23467, 4960. ENGINE H/R (S/N:CAO00469) READINGS: 1796, 7372, 19809, 3027.

JK015371 USAACE FT. RUCKER, AL

1 REMOVED FUEL CONTROL SN: UDAJ6042, WITH TSN: 5392, FROM ENG SN:GE-E-207370, AT ENG CUMMULATIVE COUNTS: LCF1: 4124, LCF2: 17394,TTI: 23584, OP HRS: 5370. H.R. READINGS: LCF1: 1912, LCF2: 7811, TTI: 19926,OP HRS: 3437. REMOVED FOR INTERNAL FAILURE. (ACFT 8724673 AT 6904ACFT HRS).


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 4/13


11/14/201312:00:00 AM

REMOVED FUEL CONTROL SN: UDAJ6042, WITH TSN: 5392, FROM ENG SN:GE-E-207370, AT ENG CUMMULATIVE COUNTS: LCF1: 4124, LCF2: 17394,TTI: 23584, OP HRS: 5370. H.R. READINGS: LCF1: 1912, LCF2: 7811, TTI: 19926,OP HRS: 3437. REMOVED FOR INTERNAL FAILURE. (ACFT 8724673 AT 6904ACFT HRS).


11/14/201312:00:00 AM

2 INSTALLED FUEL CONTROL SN: J8369, WITH TSN: 2289, ON ENG SN: GE-E-207370, AT ENG CUMMULATIVE COUNTS: LCF1: 4124, LCF2: 17394, TTI:23584, OP HRS: 5370. H.R. READINGS: LCF1: 1912, LCF2: 7811, TTI: 19926, OPHRS: 3437. ( ACFT 8724673 AT 6904 ACFT HRS).


5/13/201512:00:00 AM

1 Engine s/n: 207370 removed from acft 8724673 at 7268.2 acft hrs with ttsn: 5746, dueto lubrication(over or under) or absent. cum counts: lcf1=4262, lcf2=17805, tti=23668,hours=5746. h/r s/n: CAO00469 readings: lcf1=2050, lcf2=8222, tti=20010,hours=3813.

MB011137 USAACE FT. RUCKER, AL.

5/28/201512:00:00 AM

1 ENGINE PLACED IN LONG TERM STORAGE 27 MAY 2015. ENGINE RUN FORSERVICEABILITY REQUIRED BEFORE USE. HISTORY RECORDER ( S/N:CAO00469) READINGS- LCF1: 02052, LCF2: 08231, INDEX: 20010, HRS: 3818.COMP CUM COUNTS -LCF1: 4262, LCF2: 17805, TTI: 23668, OP HRS: 5746.TTSN: 5746, WORK ORDER NO: 502643.

CM011247 USAACE (AMSS) FT. RUCKER, AL.

6/3/201512:00:00 AM

1 INSTALLED ENG. SN: (GE-E-207370) ON AIRCRAFT SN: (8724673) WITH7268.2 AIRCRAFT HOURS. HISTORY RECORDER SN: (CAO00469) WITHREADINGS OF LCF-1=2052, LCF-2=8231, TTI=20010, HOURS=3818. ENGINECUMULATIVE COUNTS ARE LCF-1=4262, LCF-2=17805, TTI=23668,HOURS=5746.

TM027105 USAACE FT. RUCKER, AL.

7/7/201612:00:00 AM

1 REMOVED ENGINE S/N GE-E-207370 FROM POSITION 1 FORPRESERVATION. HISTORY RECORDER READINGS: LCF1: 2184, LCF2: 8597,TTI: 20036 & OP HRS 4186. ENGINE CUMULATIVE COUNTS: LCF1: 4394,LCF2: 18171, TTI: 23694 & OP HRS 6114. FROM ACFT 8724673

TM014571 USAACE FT RUCKER, AL

7/12/201612:00:00 AM

1 INSTALLED ENGINE S/N GE-E-207370 W/ TSN 6113 HRS. HISTORYRECORDER (S/N CAO00469) READINGS AS FOLLOWS: LCF1: 2182, LCF2:8595, TTI: 20036, OP HRS: 4185. ENGINE CUMMULATIVE COUNTS: LCF1:4392, LCF2: 18169, TTI: 23694, OP HRS 6113. ON ACFT 8724673 @ 7320 ACFTHRS




CAO00469

GE-E-2073706035T02G01COLD SECTION MODULEGE-C-007738

2871

3989

19643

36075

7202

11594

1740

2906

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 6/13

04A01 6035T02G01 COLD SECTION MODULE GE-C-007738

398936075115942906

312611415101091844SAP277185056T66G02POWER TAKEOFFDRIVE

COND

COND

398936075115942906

398936075115942906GLB004836035T77G10COMPRESSORROTOR ASSEMBLY

COND

COND

398936075115942906

51201133795002401GAT021896035T88P03GAS GENERATORTURBINE SHAFT

8751

11000

398936075115942906

0000WESN53825036T95P01INNER BALANCEPISTON SE

COND

COND

398936075115942906

0000BIW039V56035T79P04COMPRESSORDISCHARGE SEAL

COND

COND

398936075115942906

0000FIAAPW276035T83P01COMPRESSOR REARSHAFT

7871

5000

398936075115942906

0000VAEBU0605044T07P01NO 3 LABYRINTHSEAL

COND

COND

398936075115942906

23181243651181271BIWCC3535035T57P02VORTEX SPOILER

COND

COND

398936075115942906

31561906141681754GATRB1205043T04P02TIE ROD,COMPRESSOR

9715

10000

398936075115942906

34501809082022135GATN08414045T08P01RING, SPACERCOMPRESSOR

9421

10000

398936075115942906

0000GLHTKFT26055T59P01COMPRESSORIMPELLER

7871

5000


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 7/13


398936075115942906

53562479998072211GGAM28086039T56G04OUTPUT SHAFT ASSY

COND

COND

398936075115942906

0000GLHTH8D16032T26G09STAGE 1 BLISK

7871

5000

398936075115942906

0000GLHTM64K6032T27P08STAGE 2 BLISK

9871

7000

398936075115942906

0000GLHTM5F96038T08P04STAGE 3 & 4 BLISK

9871

7000

398936075115942906

0000GLHTM26E6038T09P04STAGE 5 BLISK

9871

7000

398936075115942906

765154824530264FCAK94636064T35P02NO 3 BALL BEARING

COND

COND

398936075115942906

5661633502210FCAG34116064T15P03NO 4 ROLLERBEARING

COND

COND


4/23/201012:00:00 AM

1 C/S MOD REPAIRED 21APR10 IAW DMWR 1-2840-248 & CHANGES ANDRECAPPED DTD 03DEC01. FUEL INJECTORS CLEANED AND FLOWED PERDMWR AT C/S TSN 3989 ON 21APR10 /S/M. BENAVIDES, AIRCRAFT DATATECHNICIAN

CCAD NOT GIVEN



CAO00469

GE-C-0077386039T56G04OUTPUT SHAFT ASSYGGAM2808

2871

5356

19643

24799

7202

9807

1740

2211

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 9/13

04A01G 6039T56G04 OUTPUT SHAFT ASSY GGAM2808

53562479998072211

5507551251330FCAG52276064T34P02NO 1 BALL BEARING

COND

COND

53562479998072211

0000TMKAFG9N5035T69P01NO 2 ROLLERBEARING

COND

COND


4/23/201012:00:00 AM

1 OUTPUT SHAFT INSTALLED ON 21APR10, SERVICEABLE. /S/M.BENAVIDES, AURCRAFT DATA TECHNICIAN

CCAD NOT GIVEN



CAO00469

GE-E-2073706055T20G05MTCHD ROTOR/STATORASSY

MRSG0703

2871

2452

19643

20034

7202

5692

1740

1543

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 11/13

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRSG0703

24522003456921543

2910696733121145GAT4995P6064T85P01STAGE 1 TURBINEDISK

4961

5000

24522003456921543

24522003456921543GGAAM0536039T57G24G/G STATOR ASSY

COND

COND

24522003456921543

457958272259GATHG79P6064T86P01STAGE 2 TURBINEDISK

7414

5000

24522003456921543

197234983835927PAMR67696064T81P01STAGE 1 FWDCOOLING PLATE

5899

5000

24522003456921543

77635242190558GFF59NW46064T82P01STAGE 1 REARCOOLING PLATE

7095

5000

24522003456921543

1415588431561174BIWCL8216039T52P03STAGE 2 FWDCOOLING PLATE

5456

4000

24522003456921543

281265497180GFF5CE4K6064T84P02STAGE 2 REARCOOLING PLATE

7590

5000

24522003456921543

24522003456921543GGAG07036039T54G13G/G ROTORASSEMBLY

COND

COND


4/23/201012:00:00 AM

1 MATCHED GG ROTOR/STATOR REPAIRED 21APR10 IAW DMWR 1-2840-248AND CHANGES AND RECAPPED DTD 03DEC01 /S/M. BENAVIDES,AIRCRAFT DATA TECHNICIAN.

CCAD NONE GIVEN



CAO00469

GE-E-2073706064T98G01POWER TURBINE MODULEGE-L-006983

2871

2473

19643

7629

7202

6520

1740

2556

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 13/13

04A03 6064T98G01 POWER TURBINE MODULE GE-L-006983

2473762965202556

2473762965202556GGA091495043T75G07POWER TURBINEROTOR

COND

COND

2473762965202556

161952033469731GAT6991K6038T32P01STAGE 3 TURBINEDISK

6252

5000

2473762965202556

17691565928961306GAT8685P6038T34P05STAGE 4 TURBINEDISK

6102

5000

2473762965202556

32019012858579GATHJFJ65125T92G01POWER TURBINESHAFT

7551

5000

2473762965202556

1885125584236989MAB3A4265034T27P01NO 5 ROLLERBEARING

COND

COND

2473762965202556

15841422529101259MAB1V3566064T36P01NO 6 BALL BEARING

COND

COND


4/23/201012:00:00 AM

1 POWER TURBINE REPAIRED 21APR10 IAW DMWR 1-2840-248 & CHANGESAND RECAPPED DTD 03DEC01 /S/M. BENAVIDES

CCAD NOT GIVEN



ECDH0817

87246736035T00G01ENGINE ASSY, TURBINEGE-E-207533

3282

4818

8966

52078

7537

8172

1646

1844

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE





T700-GE-700




OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 2/12


37625185649761335

567223817149493159GE-C-0377086035T02G01COLD SECTIONMODULE

COND

COND

3736000

283000GGM9A2406064T55G01COMBUSTION LINER

COND

COND

37365171149331318

23631745985951783MRSG44836055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

3736000

2557000AMDA14995043T24G14STAGE 1 NOZZLEASSY

COND

COND

37365171149331318

364922862123442868GE-L-0068896064T98G01POWER TURBINEMODULE

COND

COND

3739000

5009000GE-D-0062876035T01G01ACCESSORY MODULE

COND

COND

3736000

3628000SUSJ30076034T62P16PARTICLESEPARATOR BLOWER

COND

COND

45955171149331318

3679000WYG544314046T52G39FUEL CONTROL

COND

COND

3739000

2739000APM045RS4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

3740000

6217000ECD007684046T29G13ELECTRICALCONTROL UNIT

COND

COND

37365171149331318

2200859942981120ECDH08174046T26G03HISTORY RECORDER

COND

COND


10/25/201212:00:00 AM

2 - C/S Mod Assy S/N: GE-C-037708 with component cumulative counts of LCF1-3159;LCF2-14949; TTI-23817;OP HR-5672 Installed on engine GEE207533 with enginecumulative counts of LCF1-1325; LCF2-4976; TTI-51856; OP HR-3762> HistoryRecorder (ECDH0817) with readings of LCF1-1137; LCF2-4341; TTI-8744; OP HR-2226. JB012761 Records Specialist, Lowe Field, Ft. Rucker, Al.

OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 3/12


3739000

2021000UDC107994046T25G06COOLER, OIL

COND

COND

3736000

549000B61665066T38G08ANTI-ICE VALVE

COND

COND


10/6/201212:00:00 AM

1 25OCT10 CCAD ENGINE REPAIRED 22OCT10 IAW DMWR 1-2840-248 &CHANGES AND RECAPPED DTD 03DEC01. /S/ M.THORN, AIRCRAFT DATATECHNICIAN.


10/6/201212:00:00 AM

2 20 SEP 12 - FUEL CONTROL S/N 13691078 INSTALLED ON ENGINE WITHTTSN 1040. H/R S/N ECDH0817 CTS = LCF1 1127 LCF2 4313 TTI 8736 OP HRS2204.. ENG CUM CTS = LCF1 1325 LCF2 4948 TTI 51848 OP HRS 3740, D.WILLIAMS 0950 USAACE FT RUCKER,AL


10/6/201212:00:00 AM

3 20 SEP 12 - ECU S/N ECD00768 INSTALLED ON ENGINE WITH TTSN 6217.H/R S/N ECDH0817 CTS = LCF1 1127 LCF2 4313 TTI 8736 OP HRS 2204.. ENGCUM CTS = LCF1 1325 LCF2 4948 TTI 51848 OP HRS 3740, D. WILLIAMS 0950USAACE FT RUCKER,AL


10/6/201212:00:00 AM

4 INSTALLED ENG GE-E-207533 WITH CTS: 1325/4948/51848/3740 ON ACFT8524475 @ 6929.7 ACFT HRS. HIS REC ECDH0817 READINGS:1127/4313/8736/2204


10/20/201212:00:00 AM

1 REMOVED ENG (GE-E-207533) WITH CTS: 1335 - 4976 - 51856 - 3762 FROMACFT 8524475 @ 6951.2 ACFT HRS FOR LEAKING FROM COMPRESSORLEAKAGE TUBE. HIS REC (ECDH0817) 1137 - 4341 - 8744 - 2226.


10/25/201212:00:00 AM

1 C/S Mod Assy S/N: GE-C-007533 removed for "oil Leaking" w/cumulative counts ofLCF1-1335; LCF2-4976; TTI-51856; Op Hr--3762 from UNINSTALLED engineGEE207533 with engine cumulative counts of LCF1-1325; LCF2-4976; TTI-51856;OP HR-3762> History Recorder (ECDH0817) with readings of LCF1-1137; LCF2-4341; TTI-8744; OP HR-2226. JB012761 Records Specialist, Lowe Field, Ft. Rucker,Al.

JB012761 USAACE FT. RUCKER, AL.


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 4/12


10/25/201212:00:00 AM



11/7/201212:00:00 AM

1 ENGINE ASSY INSTALLED ON ACFT 8724673 AT 6536 ACFT HRS WITHENGINE CUMULATIVE COUNTS = LCF1-1335; LCF2-4976; TTI-51856; OP HR-3762. H.R. (ECDH0817) READINGS OF LCF1-1137; LCF2-4341; TTI-8744; OP HR-2226


11/14/201312:00:00 AM

1 REMOVED FUEL CONTROL SN: 13691078, WITH TSN: 1421, FROM ENG SN:GE-E-207533, AT ENG CUMMULATIVE COUNTS: LCF1: 1499, LCF2: 5989, TTI:52005, OP HRS: 4122. H.R. READINGS: LCF1: 1301, LCF2: 5354, TTI: 8893, OPHRS: 2586. REMOVED FOR INTERNAL FAILURE. (ACFT 8724673 AT 6904ACFT HRS)

CN014192 USAACE FT RUCKER, AL

11/14/201312:00:00 AM

2 INSTALLED FUEL CONTROL SN: UDAJ5283, WITH TSN: 4079, ON ENG SN:GE-E-207533, AT ENG CUMMULATIVE COUNTS: LCF1: 1499, LCF2: 5989, TTI:52005, OP HRS: 4122. H.R. READINGS: LCF1: 1301, LCF2: 5354, TTI: 8893, OPHRS: 2586. (ACFT 8724673 AT 6904 ACFT HRS)


5/13/201512:00:00 AM

1 Engine s/n: GE-E-207533 removed from acft 8724673 at 7268.2 acft hrs with ttsn:4471. removed due to lubrication(over or under) or absent. cum counts: kcf1=1673,lcf2=6919, tti=52055, hours=4471. H/R s/n ecdh0817 readings: lcf1=1475, lcf2=6284,tti=8943, hours= 2935.

MB011137 USAACE FT. RUCKER, AL.

5/29/201512:00:00 AM

1 PLACED ENGINE INTO LONG TERM STORAGE 29 MAY 2015. RUN/TESTREQUIRED PRIOR TO USE. HISTORY RECORDER (S/N: ECDH0817) LCF1:01477, LCF2: 06295, INDEX: 08943, HOURS: 2941. COMP. CUM. HRS.- LCF1:1673, LCF2: 6919, TTI: 52055, OP HRS: 4471. TTSN: 4471. WORK ORDER NO:502644.

CM011247 USAACE (AMSS) FT. RUCKER, AL.

6/3/201512:00:00 AM

1 INSTALLED SN: GE-E-207533 ON AIRCRAFT SN: 8724673 AT 7268.2AIRCRAFT HOURS. ENGINE CUMULATIVE COUNTS ARE LCF-1=1673, LCF-2=6919, TTI=52055, HOURS=4471. HISTORY RECORDER SN: (ECDH0817)READINGS OF LCF-1=1477, LCF-2=6295, TTI=8943, HOURS=2941.

TM027105 USAACE FT. RUCKER, AL.

11/28/201512:00:00 AM

1 REMOVED FUEL CONTROL SN UDAJ5283 FROM AIRCRAFT 8724673 AT 7392ACFT HOURS DUE TO INTERNAL FAILURE. TSN: 4558. ENGINECUMULATIVE COUNTS: 1742/7360/52076/4595. HISTORY RECORDER SNECDH0817 READINGS 1546/6736/8964/3065.


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 5/12


REMOVED FUEL CONTROL SN UDAJ5283 FROM AIRCRAFT 8724673 AT 7392ACFT HOURS DUE TO INTERNAL FAILURE. TSN: 4558. ENGINECUMULATIVE COUNTS: 1742/7360/52076/4595. HISTORY RECORDER SNECDH0817 READINGS 1546/6736/8964/3065.

CP027629 USAACE FORT RUCKER, AL

11/28/201512:00:00 AM

2 INSTALLED FUEL CONTROL SN WYG54431 WITH TSN OF 3679 ONAIRCRAFT 8724673 AT 7392 AIRCRAFT HOURS. ENGINE CUMULATIVECOUNTS 1742/7360/52076/4595. HISTORY RECORDER SN ECDH0817READINGS 1546/6736/8964/3065.

CP027629 USAACE FORT RUCKER, AL

7/7/201612:00:00 AM

1 REMOVED ENGINE S/N GE-E-207533 FROM ACFT 8724673, POSITION 2 FORBROKEN STUD ON EXHAUST CONE MOUNT. HISTORY RECORDERREADINGS: LCF1: 1647, LCF2: 7540, TTI: 8966, OP HRS: 3283; ENGINECUMULATIVE COUNTS: LCF1: 1845, CLF2: 8175, TTI: 52078, OP HRS: 4819.


7/12/201612:00:00 AM

1 INSTALLED ENGINE S/N GE-E-207533 W/TSN 4818 (UNSERVICABLE DUE TOAIRCRAFT SCHEDULED TO BE TURNED IN). HISTORY RECORDER S/NECDH0817 WITH H.R. READINGS: LCF1: 1646, LCF2: 7537, TTI: 8966 & OP HRS3282. CUMMULATIVE COUNTS: LCF1: 1844, LCF2: 8172, TTI: 52078 & OP HRS4818.




ECDH0817

GE-E-2075336035T02G01COLD SECTION MODULEGE-C-037708

2226

5672

8744

23817

4341

14949

1137

3159

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 7/12


567221756149413157

523514577113093083SAP086345044T27G02POWER TAKEOFFDRIVE

COND

COND

567221756149413157

567221756149413157GLH231056035T77G19COMPRESSORROTOR ASSEMBLY

COND

COND

567221756149413157

98937972813873NCE598CP6035T88P07GAS GENERATORTURBINE SHAFT

12237

11000

567221756149413157

98937972813873GATHJ98L5036T95P01INNER BALANCEPISTON SE

COND

COND

567221756149413157

98937972813873MMTF80886035T79P04COMPRESSORDISCHARGE SEAL

COND

COND

567221756149413157

0000FIAAW67J6035T83P01COMPRESSOR REARSHAFT

7226

5000

567221756149413157

98937972813873VAEAC4375044T07P01NO 3 LABYRINTHSEAL

COND

COND

567221756149413157

391312348108182927GLHH32915035T57P02VORTEX SPOILER

COND

COND

567221756149413157

43362681194922433GATRB1565043T04P02TIE ROD,COMPRESSOR

7890

10000

567221756149413157

3853824763362213GATR67734045T08P01RING, SPACERCOMPRESSOR

8373

10000

567221756149413157

0000GLHTMN6P6055T59P01COMPRESSORIMPELLER

7226

5000


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 8/12


567221756149413157

624828329217894529GGA122466039T56G04OUTPUT SHAFT ASSY

COND

COND

567221756149413157

0000GLHTPFEH6032T26G09STAGE 1 BLISK

7226

5000

567221756149413157

0000GLHTPFR26032T27P08STAGE 2 BLISK

9226

7000

567221756149413157

0000GLHTPH6T6038T08P04STAGE 3 & 4 BLISK

9226

7000

567221756149413157

0000GLHTPFKG6038T09P04STAGE 5 BLISK

9226

7000

567221756149413157

0000FCAAM7936064T35P02NO 3 BALL BEARING

COND

COND

567221756149413157

1355878437231045FCAH24836064T15P03NO 4 ROLLERBEARING

COND

COND


8/30/201212:00:00 AM

1 COLD SECTION GEC037708, T700-700 WAS RECAPPED IAW DMWR 1-2840-248-1/2 CHANGE 12. COLD SECTION MODULE TIMES: LCF1-3157; LCF2-14941; TTI-21756; EOH-5672. OUTPUT SHAFT TIMES: LXCF1-4529; LCF2-21789; TTI-28329; EOH-6248. RECORDS ARE ON FILE AT THIS FACILITYUNDER WORK ORDER 412951. SHERYL HARPER, T700 ENGINE ANALYSTGEES/STROTHER.

GEES/STROTHER KANSAS

10/25/201212:00:00 AM





ECDH0817

GE-E-2075336055T20G05MTCHD ROTOR/STATORASSY

MRSG4483

2200

2363

8599

17459

4298

8595

1120

1783

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 10/12

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRSG4483

23631745985951783

1314603335551387GATADA566064T85P01STAGE 1 TURBINEDISK

5886

5000

23631745985951783

23631745985951783GGAC34806039T57G24G/G STATOR ASSY

COND

COND

23631745985951783

28591376050511202GATACP546064T86P01STAGE 2 TURBINEDISK

4341

5000

23631745985951783

1182647642941240GFFR89986064T81P01STAGE 1 FWDCOOLING PLATE

6018

5000

23631745985951783

2358426438291224GATM73116039T50P04STAGE 1 REARCOOLING PLATE

3842

4000

23631745985951783

1497718140401291GFFR855W6064T83P01STG 2 FWD COOLINGPLATE

5703

5000

23631745985951783

13450413238GFF5CR0J6064T84P02STAGE 2 REARCOOLING PLATE

7066

5000

23631745985951783

23631745985951783GGAG44836039T54G13G/G ROTORASSEMBLY

COND

COND


10/6/201212:00:00 AM

1 25OCT10 CCAD MATCHED GG ROTOR/STATOR REPAIRED 22OCT10 IAWDMWR 1-2840-248 & CHANGES AND RECAPPED DTD 03DEC01. /S/M.THORN, AIRCRAFT DATA TECHNICIAN.




ECDH0817

GE-E-2075336064T98G01POWER TURBINE MODULEGE-L-006889

2200

3649

8599

22862

4298

12344

1120

2868

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


03-Aug-2016 12/12

04A03 6064T98G01 POWER TURBINE MODULE GE-L-006889

364922862123442868

364922862123442868GGA095095043T75G07POWER TURBINEROTOR

COND

COND

364922862123442868

40223401859333GATHCNTK6038T32P01STAGE 3 TURBINEDISK

6798

5000

364922862123442868

40223401859333GATHE98A6038T34P05STAGE 4 TURBINEDISK

6798

5000

364922862123442868

3370705942721860GATHY4155125T92G01REPOWER TURBINESHAFT

3830

5000

364922862123442868

21071739258931580TMKAAWSV5034T27P01NO 5 ROLLERBEARING

COND

COND

364922862123442868

137659744039969TMKABJ976064T36P01NO 6 BALL BEARING

COND

COND


10/6/201212:00:00 AM

1 25OCT10 CCAD POWER TURBINE MODULE REPAIRED 22OCT10 IAW DMWR1-2840-248 & CHANGES AND RECAPPED DTD 03DEC01. /S/ M. THORN,AIRCRAFT DATA TECHNICIAN.

BK026292 USAACE` FT RUCKER, AL


PIDMWODATE HRS



ENGINE ASSY, TURBINE 8724673GE-E-2073701. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


31-Dec-1986 DM

MB254121-Apr-2010

1W0MUAAMOD OF PTO BEVEL GEAR SHAFTMWO 1-2840-248-50-27MWO:

Priority Mnt Level

19-Jan-1988 DM

MB254121-Apr-2010

1W0MUAASELF-SEAL ADAPTER ASSYMWO 1-2840-248-50-28MWO:

Priority Mnt Level

13-Jul-1989 DM

MB254121-Apr-2010

1W0MUAAMODIFICATION OF GAS GENERATORROTOR ASEMB. T700-700/701REWORK & REPLACE 33.0MANHOURS

MWO 55-2840-248-50-32MWO:

Priority Mnt Level

01-Jul-1992 DM

MB254121-Apr-2010

1W0MUAAINSTALLATION OF PTO DRIVE ASSYMWO 55-2840-248-50-29MWO:

Priority Mnt Level

30-Jun-1994 OR

MB254121-Apr-2010

1W0MUAAONE TIME INSPECTION ANDCONVERSION OF FORMS ANDRECORDS FOR T700-GE-700, -701AND -701C SERIES GAS TURBINEENGINES

1-2840-248-20-2MWO:

Priority Mnt Level

05-Nov-1999 OR

MB254121-Apr-2010

1W0MUAANEW LIFE LIMITS ON GG ROTORSAND COMPONENTS

TB 1-2840-248-20-22 / UH-MWO:

Priority Mnt Level

22-Sep-2008 OM

MB254121-Apr-2010

1W0MUAAALL H-60 AND H-64 SERIESAIRCRAFT, SUSPECT ENGINEHARNESSES

H-64-08-ASAM-05MWO:

Priority Mnt Level

22-Sep-2008 OM

MB254121-Apr-2010

1W0MUAAALL H-60 SERIES AIRCRAFT,SUSPECT ENGINE ELECTRICALHARNESSES.


Priority Mnt Level

30-Jul-2014 FM

CB02058831-Jul-2014

1USAACEHYDRO-MECHANICAL UNIT (HMU)QUICK DISCONNECT PINS

H-60-14-ASAM-08MWO:

Priority Mnt Level



DM026217

PIDMWODATE HRS





31-Jul-1989 OM

MT554301-Oct-2010

33W0MUAAMODIFICATION OF GG ROTORASSEMBLY T700/701 REWORK T700ENGINES

55-2840-248-50-32MWO:

Priority Mnt Level

30-Mar-1990 OM

MT554301-Oct-2010

1.5W0MUAAINSTALLATION OF POWER TAKEOFF ASSEMBLY

55-2840-248-50-29MWO:

Priority Mnt Level

15-Aug-1990 OM

MT554301-Oct-2010

1.5W0MUAAINSTALLATION OF SELF SEALADAPTER ASSEMBLY

55-2840-248-50-28MWO:

Priority Mnt Level

30-Jun-1994 OR

MT554301-Oct-2010

1W0MUAAONE TIME INSPECTION ANDCONVERSION OF FORMS ANDRECORDS FOR T700-GE-700, -701AND -701C SERIES GAS TURBINEENGINES

1-2840-248-20-2MWO:

Priority Mnt Level

15-Dec-1998 OU

MT554301-Oct-2010

1W0MUAAALL UH-60A & EH-60A SERIESHELICOPTERS, ONE TIMEINSPECTION OF ALL T700-GE-700ENGINE RECORDS

1-2840-248-20-22MWO:

Priority Mnt Level

16-Aug-1999 OM

DM02621706-Oct-2012

0.5USAACEALL UH-60A, EH-60A AND UH-60QAIRCRAFT, SUBJECT: INSPECTIONINTERVAL CHANGE FOR HAMILTONSTANDARD HYDRO MECHANICALUNITS (HMU) P/NS 4046T52G01,4046T52G04, 4046T52G06,4046T52G09 AND 4046T52G11 USEDON THE T700-GE-700 ENGINE


Priority Mnt Level

16-Jul-2007 OM

DM02621706-Oct-2012

0.3USAACEALL H-60 SERIES AIRCRAFT,HAMILTON-SUNDSTRAND HYDRO-MECHANICAL UNITS PN 4046T52G01AND 4046T52G04 REMOVE FROMSERVICE


Priority Mnt Level

13-Aug-2007 OM

DM02621706-Oct-2012

0.5USAACEALL H-60 SERIES AIRCRAFT, MAINFUEL MANIFOLD CHAFING


Priority Mnt Level

20-Dec-2007 OM

DM02621706-Oct-2012

0.5USAACEINSPECTION TO DETERMINE IFENGINE HAS BEEN SERVICED WITHMIL-PRF-23699 HTS OIL

UH-60-08-AMAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS





22-Sep-2008 OM

DM02621706-Oct-2012

0.4USAACEALL H-60 AND H-64 SERIESAIRCRAFT, SUSPECT ENGINEHARNESSES.

H-60-08-ASAM-14MWO:

Priority Mnt Level

22-Sep-2008 OM

MT554301-Oct-2010

1W0MUAAALL H-60 AND H-64 SERIESAIRCRAFT, SUSPECT ENGINEHARNESSES

H-64-08-ASAM-05MWO:

Priority Mnt Level

22-Sep-2008 OM

MT554301-Oct-2010

1W0MUAAALL H-60 SERIES AIRCRAFT,SUSPECT ENGINE ELECTRICALHARNESSES.


Priority Mnt Level

12-Jan-2009 FM

DM02621706-Oct-2012

0.5USAACEALL H-60A/K/L AND AH-64 SERIESAIRCRAFT, T701C GAS GENERATORROTOR ASSEMBLIES, FOR SN'SINSTALLED.


Priority Mnt Level

01-Oct-2009 OM

DM02621706-Oct-2012

0.3USAACEALL H-60A SERIES AIRCRAFT,HAMILTON-SUNDSTRAND HYDRO-MECHANICAL UNITS.

H-60-10-ASAM-01MWO:

Priority Mnt Level

30-Jul-2014 FM

CB02058831-Jul-2014

1USAACEHYDRO-MECHANICAL UNIT (HMU)QUICK DISCONNECT PINS

H-60-14-ASAM-08MWO:

Priority Mnt Level



REMARKS

PART UNSERVICABLE. AIRCRAFT DUE TO BE TURNED IN. ULLS UNABLE TO INSTALL UNSERVICABLE PARTS. FAILURE CODE OF 070, BROKEN STUD

ON EXHAUST CONE MOUNT.








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H








44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

12-Jul-2016 TM0145 334-598-0670

1 W0U91TF

1646 7537 8966 3282 0 0 0 7620

7620 0


8724673

ECDH0817

52078 8172 1844 0 00

04A 0 0

99207 0 0 4818 0 070

GEE2075336035T00G012840010701003T700-GE-700 ENGINE ASSY

4818



PIDMWODATE HRS



FAN AXIAL 87246733900346SB1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


01-Jan-2009 DR

FR462619-Feb-2009

22CCAD/W0MUAARECAPPEDDMWR 1-4140-228MWO:

Priority Mnt Level



PIDMWODATE HRS



FUEL CONTROL 8724673J83691. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


19-Aug-2013 FM

TB01102714-Nov-2013

0.5USAACE FT.RUCKER, AL.

WOODWARD HYDRO-MECHANICALUNIT (HMU) P3 TUBE.

H-60-13-ASAM-10MWO:

Priority Mnt Level



REMARKS

UNSERVICEABLE COMPONENT. FAILURE CODE 381. AIRCRAFT SCHEULED TO BE TURNED IN. SES HUNTSVILLE, AL.








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

08-Aug-2016 MS5116 910-729-0711 mike.schutz

1 K08DD2F

0 0 0 0 0 0 0 7620

7620 0 0


8724673

0 0 0 0 0

03A01 0 0

29560 0 0 0 73 0 674

BEM176570250-12051-0451620012311831FWD FIXED GEAR SHOCK

73



0

360

7268.2

8724673 7619.8 0


EH-60A A005-01653 Days


HELICOPTER, UTILITY INTERMEDIATE GEARBOX Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

SC200608-Mar-2011NORMALSPECIAL3223.05468546804-Mar-2011

LW272007-Sep-2011NORMALROUTINE3580.05825582506-Sep-2011

VM01466322-May-2012NORMALROUTINE0.061856184.821-May-2012

JK01537105-Dec-2012NORMALROUTINE363.06548654804-Dec-2012

FT02070918-Nov-2013NOT_TESTEDROUTINE0.06904690414-Nov-2013

FT02070921-Nov-2013NORMALBASELINE2.06906690618-Nov-2013

FT02070925-Nov-2013NORMALROUTINE9.06913691322-Nov-2013

TM02710519-Aug-2015ABNORMALROUTINE355.27268.27268.216-Aug-2015

CP02762925-Aug-2015NORMALLAB REQUES0.57268.77268.722-Aug-2015

19AUG15 - OIL SAMPLE IS ABNORMAL DUE TO "WATER". CODE J. DRAIN & FLUSH SYSTEM. SUBMIT RESAMPLE AFTER 1ST FLIGHT CYCLE. USAACE, FT.RUCKER, AL. TM02710518NOV13- INADEQUATE AMOUNT OF SAMPLES SUBMITTED. NOT ENOUGH SAMPLE TO ANALYSIS OIL LAB REQUESTED SUBMISSION OF RESAMPLE ASOUTLINED IN TB43-0211

9. REMARKS:



PIDMWODATE HRS



INPUT MODULE 8724673A264093941. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 OM

BK02629227-Mar-2013

5USAACEPLASTIC MEDIA BLAST (PMB) ANDOXIDE FLAKE RESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



INTERMEDIATE GEARBOX 8724673A005-016531. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 OM

JK01537127-Mar-2013


PLASTIC MEDIA BLAST (PMB) ANDOXIDE FLAKE RESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



LATERAL SERVO BELLCRANK 8724673F337-028691. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


07-Jan-1997 OM

MB01113712-Feb-2008

1.3UDAAWC, FT.RUCKER, AL(RC1002)

ALL H-60 AIRCRAFT WITH THELATERAL BELLCRANK ASSEMBLY,P/N 70400-08150-045,MANUFACTURED BY PURDYMACHINE COMPANY (CAGE CODE15152)


Priority Mnt Level

05-Jan-2001 OT

MB01113712-Feb-2008

3USAAWC, FT.RUCKER, AL(RC1002)

H-60 SERIES AIRCRAFT, REMOVALOF LATERAL SERVO BELLCRANKASSEMBLY MANUFACTURED BY THEPURDY MACHINE COMPANY, CAGECODE 15152

UH-60-01-03MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR BLADE ASSY 8724673A007-045531. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


DR

JB697123-Jun-2012

130CCAD/W0MMUAMAIN ROTOR BLADE ASSEMBLY P/N:70150-09100-041 (NSN 1615-01-074-5150) AND P/N 70150-09100-043 (NSN1615-01-106-1903)

1-1615-281 C1MWO:

Priority Mnt Level

30-Oct-2001 ON

SB272901-Apr-2010

331109TH AVCRADREPLACEMENT OF NICKELABRASION STRIP

1615-314-030MWO:

Priority Mnt Level

08-Sep-2002 OT

RJ02082711-Oct-2012

2USAACEONE TIME INSP OF ALL M/R BLADECUFF ASSY.

SOF UH-60-02-11MWO:

Priority Mnt Level

01-Jul-2003 DU

RJ02082711-Oct-2012

2USAACEONE TIME INSPECTION OF M/RBLADE CUFF ASSY.

SOF UH-60-02-12MWO:

Priority Mnt Level

15-Apr-2010 OT

JB697123-Aug-2012

3CAD/W0MUAAALL H-60A/K/L SERIES AIRCRAFT,DEPOT REPAIRED LEGACY MAINROTOR BLADES

H-60-10-SOF-01MWO:

Priority Mnt Level

09-Apr-2012 OT

JB697123-Aug-2012

1CCAD/W0MUAACHANGE TO DEPOT REPAIREDLEGACY MAIN ROTOR BLADECOMPLIANCE DATE

H-60-12-SOF-05MWO:

Priority Mnt Level

04-May-2015 FM

MH0215309-May-2015

1.5USAACE, FTRUCKER, AL

MAIN ROTOR BLADE DEBONDINGH-60-15-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR BLADE ASSY 8724673A007-076181. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


DT

RS100519-Oct-2013

130CCAD/W0MUAARECAPDMWR 1-1615-281MWO:

Priority Mnt Level

09-Apr-2012 OT

RS100519-Oct-2013


H-60-12-SOF-05MWO:

Priority Mnt Level

04-May-2015 FM

JC01123205-May-2015

1USAACE,FT.RUCKER,AL.


Priority Mnt Level

11-Aug-2015 FM

CN01419214-Apr-2016

1USAACE, FT.RUCKER, AL.

MAIN ROTOR BLADE DEBONDINGAND TIP RIB CRACKING.

H-60-15-ASAM-07MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR BLADE ASSY 8724673A007003881. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


DR

AF060320-Apr-2012

150CCAD/W0MUAAMAIN ROTOR BLADE ASSEMBLY P/N:70150-09100-041 (NSN 1615-01-074-5150) AND P/N 70150-09100-043 (NSN1615-01-106-1903)

1-1615-281 C1MWO:

Priority Mnt Level

OM

AF060320-Apr-2012

1CCAD/W0MUAAINCREASE IN FATIGUE LIFE FORTHE M/R BLADE CUFFS P/N 70150-09109-041 & P/N 70150-09109-043

TB 1520-250-2016MWO:

Priority Mnt Level

12-Aug-2002 OT

AF060320-Apr-2012

1CCAD/W0MUAAALL H-60 SERIES AIRCRAFT,REVISION TO UH-60-02-11, ONE-TIMEINSPECTION OF MAIN ROTORBLADE CUFF ASSEMBLY

UH-60-02-12MWO:

Priority Mnt Level

08-Sep-2002 OT

DM02621704-May-2012

2USAACEONE TIME INSP OF ALL M/R BLADECUFF ASSY.

SOF UH-60-02-11MWO:

Priority Mnt Level

07-Jan-2003 DU

AF060320-Apr-2012

1CCAD/W0MUAAONE TIME INSPECTION OF M/RBLADE CUFF ASSY

SOF UH-60-03--2MWO:

Priority Mnt Level

15-Apr-2010 OT

AF060320-Apr-2012

3CCAD/W0MUAAALL H-60A/K/L SERIES AIRCRAFT,DEPOT REPAIRED LEGACY MAINROTOR BLADES

H-60-10-SOF-01MWO:

Priority Mnt Level

09-Apr-2012 OT

AF060320-Apr-2012


H-60-12-SOF-05MWO:

Priority Mnt Level

04-May-2015 FM

MB01113709-Jun-2015

1.5USAACE, FT.RUCKER,AL


Priority Mnt Level

11-Aug-2015 FM

CN01419214-Apr-2016

1USAACE, FT.RUCKER, AL.

MAIN ROTOR BLADE DEBONDINGAND TIP RIB CRACKING.

H-60-15-ASAM-07MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR BLADE ASSY 8724673A007054841. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


04-May-2015 FM

JC01123207-May-2015

1USAACE,FT.RUCKER,AL.


Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR PRIMARY SERVO 8724673B303-008381. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


10-Mar-1998 OM

TL02662927-Apr-2006

1USAAWC, FT.RUCKER, AL.(MF4187)

ALL H-60 AIRCRAFT, LOOSE HUCKBOLTS ON OVERHAULED PRIMARYSERVOS, YAW BOOST SERVOS,COLLECTIVE BOOST SERVOS ANDTAIL ROTOR SERVOS


Priority Mnt Level

29-Dec-1999 OM

TL02662927-Apr-2006

1USAAWC, FT.RUCKER, AL.(MF4187)

ALL H-60 AIRCRAFT, INSPECTIONAND REMOVAL OF SUSPECTPRIMARY SERVO ASSEMBLIES


Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR PRIMARY SERVO 8724673B303-079431. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


18-Feb-2006 DM

OA016113-May-2013

25W0MUAARETORQUEING OF PRIMARY SERVOINPUT LINKAGE ASSYEMBLE NUTI/A/W DMWR 1-1650-281

DMWR 1-1650-381MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR PRIMARY SERVO 8724673B303103881. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Dec-2003 DM

AE01079411-Apr-2009

25CCAD/WOUMUAA CORPUSCHRISTI, TX

ROTARY WING HEAD SERVOASSEMBLY (P/N: 274000-1027, NSN1650-01-114-9538), (P/N 274000-1031,NSN: 1650-01-143-1226)

1-1650-381MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SHAFT EXTENDER 8724673C286-006811. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


22-Jan-1997 OM

MB01113725-May-2001

2USAAVNC FT.RUCKER, AL(TB1027)

ALL H-60 AIRCRAFT WITH THE MAINROTOR SHAFT EXTENSIONASSEMBLY, P/N 70351-08186-043,MANUFACTURED BY FENNMANUFACTURING COMPANY (CAGECODE 82001) OR THE PURDYCORPORATION (CAGE CODE 15152)


Priority Mnt Level

01-Oct-1997 OM

MB01113725-May-2001

0.5USAAVNC FT.RUCKER, AL(TB1027)

ALL H-60 AIRCRAFT, MAIN ROTORSHAFT EXTENSION ASSEMBLY, P/N70351-08186-043 MANUFACTUREDBY FENN MANUFACTURINGCOMPANY (CAGE CODE 82001) ORTHE PURDY CORPORATION (CAGECODE 15152)


Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 8724673A001-105971. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 FM

JK01537122-Sep-2012


ALL H-60 SERIES AIRCRAFT, MAINROTOR SPINDLE SUB-COMPONENTTRACKING REQUIREMENTS

H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 OM

JK01537127-Feb-2013


MAIN ROTOR SPINDLE ANTI-FLAPASSEMBLIES

H-60-13-ASAM-03MWO:

Priority Mnt Level

19-May-2016 FM

DK01131523-Jun-2016

1USAACE (AMSS),FT. RUCKER, AL.

AUTHORIZATION TO USE LOCALLYFABRICATED TOOLS. (TOOLNUMBERS 28-1-8 AND 28-1-13).

F305943 AMWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN TRANSMISSION MODULE 8724673A265000671. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


26-Mar-2014 FM

08-Jul-20141USAACE, FT

RUCKER, ALMAIN TRANSMISSION FILTER BOWLAND CHIP DETECTOR ATTACHMENTHARDWARE

H-60-14-AMAM-09MWO:

Priority Mnt Level



0

720

7268.7

8724673 4783.8 7109


EH-60A A26500067 Days


HELICOPTER, UTILITY MAIN TRANSMISSION MODULE Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

FG02096710-Jul-2014NORMALBASELINE0.04273710909-Jul-2014


CP02762925-Aug-2015ABNORMALLAB REQUES0.54432.77268.722-Aug-2015


25 AUG 2015- OIL SAMPLE IS ABNORMAL DUE TO WATER. CODE J. DRAIN & FLISH SYSTEM. SUBMIT RESAMPLE AFTER 1ST FLIGHT CYCLE. USAACE, FTRUCKER, AL. CP02762919 AUG 2015 - OIL SAMPLE IS ABNORMAL DUE TO "WATER". CODE C (AERONAUTICAL ONLY). DO NOT CHANGE OIL! SUBMIT RESAMPLE TO LAB AFTERNEXT FLIGHT CYCLE. USAACE, FT. RUCKER, AL. TM027105.

9. REMARKS:



REMARKS

FAILURE CODE 190. GROUNG SHIPPED TO BEST PROGRAM HUNTSVILLE, AL








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H








44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

25-Jul-2016 BD0111 334-598-0670

1 W0U91TF

0 0 0 0 0 0 0 7620

7620 0


8724673

0 0 0 0 0

05A02 0 0

78286 0 0 6813 0 190

A0070455370150-09100-0431615011061903MAIN ROTOR BLADE ASSY

6813



REMARKS

UNSERVICABLE PART WITH A FAILURE CODE OF 804 PART BEING TRUCKED TO THE BEST PROGRAM.








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H








44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

27-Jul-2016 JC0112 334-598-0670

1 W0U91TF

0 0 0 0 0 0 0 7620

7620 0


8724673

0 0 0 0 0

05A02 0 0

78286 0 0 5926 0 804


5926



REMARKS

FAILURE CODE 190. ACFT LEAVING








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H








44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

27-Jul-2016 TP0116 334-598-0670

1 W0U91TF

0 0 0 0 0 0 0 7620

7620 0


8724673

0 0 0 0 0

05A02 0 0

78286 0 0 3437 0 190


3437



PIDMWODATE HRS



CUFF ASSY 8724673A237059731. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


07-Mar-1997 OU

DM02621708-May-2012

0.2USAACEINCREASE IN FATIGUE LIFE FORTHE MAIN ROTOR BLADE CUFFS,P/N 70150-09109-041 AND 70150-09109-043 ALL EH-60A /L, UH-60A/L,MH-60L AND MH-60K AIRCRAFT

1-1520-237-20-192MWO:

Priority Mnt Level

01-Jul-2003 OM

DM02621708-May-2012

6USAACEINSPECTION OF MAIN ROTORBLADE CUFF ASSY

SOF UH-60-03-02MWO:

Priority Mnt Level



PIDMWODATE HRS



CUFF ASSY 8724673E237-002271. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


07-Mar-1997 OU

RJ02082711-Oct-2012

0.2USAACE, FT.RUCKER, AL

INCREASE IN FATIGUE LIFE FORTHE MAIN ROTOR BLADE CUFFS,P/N 70150-09109-041 AND 70150-09109-043 ALL EH-60A /L, UH-60A/L,MH-60L AND MH-60K AIRCRAFT

1-1520-237-20-192MWO:

Priority Mnt Level

01-Jul-2003 OM

RJ02082711-Oct-2012


INSPECTION OF MAIN ROTORBLADE CUFF ASSY

SOF UH-60-03-02MWO:

Priority Mnt Level



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X1615011061903

08-May-2006 ET0732 788-8960 ed.thompson

1 W0H9AAD

M 70150-09100-043

0 0 0 0 0 0 0

0 0

0 0 0 0 0

05A02 0 0

78286 0 0 0 2985 0 801


2985



PIDMWODATE HRS



HUB, M/R ROTOR ASSY 872467315152-008331. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


30-Dec-2013 OM

FT02070904-Jan-2014

0.3USAACEALL H-60 SERIES AIRCRAFT, MAINROTOR (MR) HUB ASSEMBLY

H-60-14-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS





05-Sep-2012 FM

JK01537122-Sep-2012



H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 OM

JK01537127-Feb-2013



H-60-13-ASAM-03MWO:

Priority Mnt Level

22-Jan-2016 FM

DK01106323-Jun-2016

1USAACE. FT.RUCKER, AL.

AUTHORIZATION TO USE MACHINESHOP DESIGNED PULLER.

F305943MWO:

Priority Mnt Level



PIDMWODATE HRS





05-Sep-2012 FM

JK01537122-Sep-2012



H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 OM

JK01537127-Feb-2013



H-60-13-ASAM-03MWO:

Priority Mnt Level

19-May-2016 FM

DK01131523-Jun-2016

1USAACE, (AMSS)FT. RUCKER, AL.

AUTHORIZATION TO USE LOCALLYFABRICATED TOOLS. (TOOLNUMBERS 28-1-8 AND 28-1-13).

F305943 AMWO:

Priority Mnt Level



PIDMWODATE HRS



MTCHD ROTOR/STATOR ASSY 8724673MRSG07031. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


31-Jul-1989 OM

MB254121-Apr-2010

33W0MUAAMODIFICATION OF GG ROTORASSEMBLY T700/701 REWORK T700ENGINES

55-2840-248-50-32MWO:

Priority Mnt Level

30-Jun-1994 OM

MB254121-Apr-2010

1W0MUAAONE TIME INSPEC/CONVERSION OFFORMS & RECORDS FORQ700/T701/T701C ENGINES

1-2840-20-2MWO:

Priority Mnt Level

05-Nov-1998 DM

MB254121-Apr-2010

1W0MUAANEW LIFE LIMITS ON GG ROTORSAND COMPONENTS

TB 1-2840-248-20-22/UH-6MWO:

Priority Mnt Level



PIDMWODATE HRS



MTCHD ROTOR/STATOR ASSY 8724673MRSG44831. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


30-Oct-1996 OU

DM02621706-Oct-2012

0.5USAACEREPLACEMENT OF UNDAMPED GASGENERATOR ROTOR/STATORASSEMBLIES FOR ALL UH-60A ANDEH-60A AIRCRAFT WITH T700-GE-700ENGINES

1-2840-248-20-19MWO:

Priority Mnt Level



REMARKS

INSTALLED BASED ON NHA SHIPPING RECORDS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

22-Sep-2010 AB2462 256-842-7910 alex.brock

SPRRA109D0014

0 W0H9AAD

0 0 0 0 0 0 0 0

0 0 0

FWD FIXED GEAR SHOCK 1620012311831 70250-12051-045

BEM1765

0 0 0 0 0

03A01A 0

29560 0 0 0 0 0 799

BEM176570250-12067-1021650011250907PISTON, MAIN L/GEAR STR

0



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H








44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

19-Jul-2016 KG0141 334-598-0670

2 W0U91TF

0 0 0 0 0 0 0 7620

7620 0


8724673

0 0 0 0 0

11D01 0 0

78286 0 0 3489 0 381

B3030794370410-02820-0541650011431226SERVO, PRIMARY MAIN ROTOR

3489



REMARKS

UNSERVICEABLE COMPONENT. FAILURE CODE 381. ULLS WILL NOT ALLOW EDITING OF FAILCODE UPON INSTALL.








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

09-Jul-2016 CN0141 334-503-3807

1 W0U91TF

0 0 0 0 0 0 0 7620

7620 0


8724673

0 0 0 0 0

11D01 0 0

82106 0 0 2730 0 381

B30310388274000-10311650011431226SERVO, PRIMARY MAIN ROTOR

2730



REMARKS

PART UNSERVICEABLE BUT ULLS DOES NOT ALLOW THE FAIL CODE TO BE CHANGED. AIRCRAFT SCHEDULED TO BE TURNED IN. FAIL CODE 381.








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H








44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

12-Jul-2016 TM0145 334-598-0670

1 W0U91TF

0 0 0 0 0 0 0 7620

7620 0


8724673

0 0 0 0 0

11D01 0 0

78286 0 0 6186 0 381

B3030083870410-02820-0541650011431226SERVO, PRIMARY MAIN ROTOR

6186



PIDMWODATE HRS



PUMP MODULE, HYDRAULIC 8724673K4025ABR1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


29-Jul-2005 DM

SS090704-Oct-2012

54CCADRECAPPED1-4320-271MWO:

Priority Mnt Level



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

08-Aug-2014 CB0588 3345033850

6 W0U92AF

0 0 0 0 0 0 0 7138

7138 0


8724673

0 0 0 0 0

07A24 0 0

4SQG0 0 0 891 0 799

C1120678770410-02500-0491560011291256SAS ACTUATOR

891



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

09-Sep-2014 CB0588 3345980670

8 W0U92AF

0 0 0 0 0 0 0 7169

7169 0


8724673

0 0 0 0 0

07A24 0 0

78286 0 0 1068 0 799

C1125184370410-02500-0491560011291256SAS ACTUATOR

1068



PIDMWODATE HRS



SAS ACTUATOR 8724673C112040531. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


04-Apr-2001 FU

MB01113724-Apr-2008

1USAAWC, FT.RUCKER, AL(MB1137)

ALL H-60 AIRCRAFT, INSPECTION OFALL SAS ACTUATORS

1-1520-237-20-231MWO:

Priority Mnt Level



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

24-Feb-2011 BK6292 3345033753 brandi.n.jochen

0 W0U92AO

0 0 0 0 0 0 0 5468

5468 0 0


8724673

0 0 0 0 0

07A24 0 0

78286 0 0 0 1380 0 799

C1120405370410-02500-0491560011291256SAS ACTUATOR

1380



SECTION I COCKPITEH-60A_BASELINE

4. EQUIPMENT CHECKLIST

8724673 EH-60A

3. AREA NAME 2. MODEL 1. SERIAL NUMBER


1RECEIVER RADIO -R-1496A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER

QTY REQ:NOMENCLATURITEM NO

2DISPLACEMENT GYRO - CN-1314/A (9000C)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GYRO, DIRECTIONAL - CN-998/ASN-43

Unt

UUUUUUnt

Unt

Un

Unt

Un0

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SIGNAL DATA CONVERTER - CV-3338A/ASN-128B

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U

Unt

UUUUUUnt

Unt

Un

Unt

Un1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER - R-2139/ARN-123(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING - MT-4834/ARN-123(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMMAND INSTR SYS PROCESSOR - 70600-01038-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING RACK - 70600-01038-102

Unt

UUUUUUnt

Unt

Un

Unt

Un1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SAS AMPLIFIER - 70901-02908-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY - 70600-01047-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO - TRU-2A/A

Unt

UUUUUUnt

Unt

Un

Unt

Un1

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3MOUNT FOR TSEC/KY58 - S1660-60036-001

Unt

UUUUUUnt

Unt

Un

Unt

Un3

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3BATTERY FOR KY 58 - BA-1372/U

Unt

UUUUUUnt

Unt

Un

Unt

Un0

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3INTERFACE ADAPTER (KY-58) - Z-AHQ/TSEC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

AIRCRAFT INVENTORY RECORDDA FORM 2408-17 E, NOV 91



8724673 EH-60A



3REMOTE CONTROL UNIT (KY-58) - Z-AHP/YSEC

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UUUUUUnt

Unt

Un

Unt

Un0

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1AMPLIFIER IMPEDANCE - AM-4859A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM ANTENNA COUPLER - 70600-01010-104

Unt

UUUUUUnt

Unt

Un

Unt

Un0

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1VHF/AM ANTENNA FILTER - 70600-01012-102

Unt

UUUUUUnt

Unt

Un

Unt

Un0

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2VHF/FM ANTENNA FILTER - 70600-01011-103

Unt

UUUUUUnt

Unt

Un

Unt

Un2

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2ANTENNA - AS-3831/APN-209(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un2

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GLIDE SLOPE ANTENNA - 70600-01043-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM, VHF-AM SENSE ANTENNA - 70600-01019-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2FIRST AID KIT - 6545-00-919-6650

Unt

UUUUUUnt

Unt

Un

Unt

Un0

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRE EXTINGUISHER - FR23-4-11848

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UUUUUUnt

Unt

Un

Unt

Un0

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BAROMETERIC ALTIMETER - AAU-32/A

Unt

UUUUUUnt

Unt

Un

Unt

Un2

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CREW SEAT - D3801-2

Unt

UUUUUUnt

Unt

Un

Unt

Un3

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2AIRCRAFT CLOCK - ABU-11A

Unt

UUUUUUnt

Unt

Un

Unt

Un2

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER - RT-1477/ARC-201

Unt

UUUUUUnt

Unt

Un

Unt

Un0

29

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2INTERPHONE CONTROL - C6533/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un2

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8724673 EH-60A



1RECEIVER/TRANSMITTER - RT-1115D/APN-209

Unt

UUUUUUnt

Unt

Un

Unt

Un1

31

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1INDICATOR ALTIMETER - ID-1917C/APN-209

Unt

UUUUUUnt

Unt

Un

Unt

Un1

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL RADIO SET - C-7392/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

33

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL - C-10604(V)6/ARN-184

Unt

UUUUUUnt

Unt

Un

Unt

Un1

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL - C-11466A/ARC-201

Unt

UUUUUUnt

Unt

Un

Unt

Un0

35

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPARATOR SIGNAL DATA - CM482/ARC186(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

36

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3MOUNT - MT-6051/ARC-186

Unt

UUUUUUnt

Unt

Un

Unt

Un3

37

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER - RT-1296A/APX-100

Unt

UUUUUUnt

Unt

Un

Unt

Un1

38

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CIVIL NAVIGATION CONTROL - C-10048/ARN-123(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

39

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS SET CONTROLLER - C-8021E/ASN-75

Unt

UUUUUUnt

Unt

Un

Unt

Un1

40

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADIO RETRANSMISSION PANEL -70550-01008-042

Unt

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Unt

Un

Unt

Un1

41

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MAGNETIC COMPASS - MS17983-4

Unt

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Unt

Un

Unt

Un1

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2OUTSIDE AIR TEMP INDICATOR - MS28028-1

Unt

UUUUUUnt

Unt

Un

Unt

Un2

43

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOR WING PANEL - 70500-01152-093

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Unt

Un

Unt

Un0

44

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOR WING PANEL - 70500-01152-094

Unt

UUUUUUnt

Unt

Un

Unt

Un0

45

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8724673 EH-60A



1STABILATOR/FLT CONT PNL - 70902-01070-048

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UUUUUUnt

Unt

Un

Unt

Un1

46

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL-INDICATOR ASN-132 C-11097/ASN-132

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Unt

Un

Unt

Un0

47

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SIGNAL DATA CONVERTER ASN-132CV-3739/ASN-132

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UUUUUUnt

Unt

Un

Unt

Un0

48

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT FOR ASN-132 MT-4915/A

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Unt

Un

Unt

Un0

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1DATA PROCESS SET AN/UYK-64(V)2

Unt

UUUUUUnt

Unt

Un

Unt

Un0

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TACAN RECEIVER/TRANSMITTER RT-1159/A

Unt

UUUUUUnt

Unt

Un

Unt

Un0

51

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ELECTRONIC SEQUENCE UNIT, 163290-100-E

Unt

UUUUUUnt

Unt

Un

Unt

Un1

52

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADAR DETECTION SET SIGNAL AN/APR39

Unt

UUUUUUnt

Unt

Un

Unt

Un0

53

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IR JAMMER COUNTERMEASURES SET AN/ALQ-144(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

54

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1DISPENSER GENERAL PURPOSE AIRCRAFT M130

Unt

UUUUUUnt

Unt

Un

Unt

Un0

55

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3SECURE SPEECH UNIT TSEC/KY-58

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UUUUUUnt

Unt

Un

Unt

Un0

56

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3CONTROL INDICATOR (KY-58) C-8157/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

57

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1KY-100 AIRTERM 0N616736-1

Unt

UUUUUUnt

Unt

Un

Unt

Un0

58

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL DISPLAY UNIT C-12346/URC

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Unt

Un

Unt

Un0

59

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER




5/7Report Date: 09-Aug-2016AREA NAMEMODELSERIAL NUMBER

SECTION I COCKPITEH-60A_BASELIN8724673 EH-60A

NAME OR PIDNUMBER DATE

db c

DATE NUMBER RANKRANK NAME OR PID

CHECK CHECK

ba ad

5. VERIFICATION

c

JH9024191 CIV 09-Aug-2016

b. LOCATION/REMARKSCHECK NO.

6. LOCATION OR REMARKS

a. ITEM NUMBER

Nomenclature

DISPLACEMENT GYRO - CN-1314/A (9000C)

1 CURRENT ACFT CONFIGURATION.2

GYRO, DIRECTIONAL - CN-998/ASN-43


BATTERY FOR KY 58 - BA-1372/U


INTERFACE ADAPTER (KY-58)- Z-AHQ/TSEC


REMOTE CONTROL UNIT (KY-58) - Z-AHP/YSEC


#2 VHF-FM ANTENNACOUPLER - 70600-01010-104


VHF/AM ANTENNA FILTER -70600-01012-102


FIRST AID KIT - 6545-00-919-6650


FIRE EXTINGUISHER - FR23-4-11848


BAROMETERIC ALTIMETER -AAU-32/A


REVERSE OF DA FORM 2408-17 E, NOV 91

RADAR DETECTION SETSIGNAL AN/APR39





db c


CHECK CHECK

ba ad

5. VERIFICATION

c

JH9024191 CIV 09-Aug-2016

CREW SEAT - D3801-21 CURRENT ACFT CONFIGURATION.27

RECEIVER/TRANSMITTER - RT-1477/ARC-201


CONTROL - C-11466A/ARC-2011 CURRENT ACFT CONFIGURATION.35

ARMOR WING PANEL - 70500-01152-093


ARMOR WING PANEL - 70500-01152-094


CONTROL-INDICATOR ASN-132 C-11097/ASN-132


SIGNAL DATA CONVERTERASN-132CV-3739/ASN-132


MOUNT FOR ASN-132 MT-4915/A


DATA PROCESS SET AN/UYK-64(V)2


TACANRECEIVER/TRANSMITTER RT-1159/A






db c


CHECK CHECK

ba ad

5. VERIFICATION

c

JH9024191 CIV 09-Aug-2016

RADAR DETECTION SETSIGNAL AN/APR39


IR JAMMERCOUNTERMEASURES SETAN/ALQ-144(V)


DISPENSER GENERALPURPOSE AIRCRAFT M130


SECURE SPEECH UNITTSEC/KY-58


CONTROL INDICATOR (KY-58)C-8157/ARC


KY-100 AIRTERM 0N616736-11 CURRENT ACFT CONFIGURATION.58

CONTROL DISPLAY UNIT C-12346/URC



SECTION II CABINEH-60A_BASELINE


8724673 EH-60A



1INERTIAL NAVIGATION SET - AN/ASN-141

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Unt

Un

Unt

Un0

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BEARING, DISTANCE, HEADING INDICATOR - ID2301/U

Unt

UUUUUUnt

Unt

Un

Unt

Un0

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MARKER BEACON ANTENNA - 70600-02011-103

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-105

Unt

UUUUUUnt

Unt

Un

Unt

Un1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRST AID KIT - 6545-00919-6650

Unt

UUUUUUnt

Unt

Un

Unt

Un0

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRE EXTINGUISHER - FR23-4-11848

Unt

UUUUUUnt

Unt

Un

Unt

Un0

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRASH AXE - 56D6221

Unt

UUUUUUnt

Unt

Un

Unt

Un1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HAND SET - H-250/U

Unt

UUUUUUnt

Unt

Un

Unt

Un1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SLAB BATTERY - D8565/11-1

Unt

UUUUUUnt

Unt

Un

Unt

Un1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3INTERPHONE CONTROL - C6533/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un3

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ADAPTER FUEL DRAIN - 70307-03018-102

Unt

UUUUUUnt

Unt

Un

Unt

Un0

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4LOCK ASSY BLADE TIEDOWN - 70700-20369-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2PLUG ASSY INTAKE - HIRSS SUPP - 70700-20515-041/042

Unt

UUUUUUnt

Unt

Un

Unt

Un0

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2PLUG ASSY EXHAUST - HIRSS - 70700-20515-043

Unt

UUUUUUnt

Unt

Un

Unt

Un0

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8724673 EH-60A



1PLUG ASSY APU EXHAUST - 70700-20509-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER ASSY OIL COOLER - 70700-20511-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BLADE FOLD SET - 70700-20412-011

Unt

UUUUUUnt

Unt

Un

Unt

Un0

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER PITOT TUBE - 70700-20460-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


7TROOP SEATS - 70500-02151-045

Unt

UUUUUUnt

Unt

Un

Unt

Un0

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER ENGINE INLET - 83DSCC-D006

Unt

UUUUUUnt

Unt

Un

Unt

Un0

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PINTLE MOUNT ASSY - L/H - 70751-02023-043

Unt

UUUUUUnt

Unt

Un

Unt

Un0

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PINTLE MOUNT ASSY - R/H - 70751-02023-044

Unt

UUUUUUnt

Unt

Un

Unt

Un0

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ICS WALK-AROUND CORD - 70602-02016-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PORTABLE INSP. FLOOD LIGHT - 15-0366-1

Unt

UUUUUUnt

Unt

Un

Unt

Un0

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HYD. PUMP HANDLE - 15400-50126

Unt

UUUUUUnt

Unt

Un

Unt

Un1

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2EQUIPMENT LOGBOOK - MIL-D-43064

Unt

UUUUUUnt

Unt

Un

Unt

Un2

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPUTER LOGBOOK

Unt

UUUUUUnt

Unt

Un

Unt

Un0

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1WEIGHT AND BALANCE HANDBOOK - TM 55-1500-342-23

Unt

UUUUUUnt

Unt

Un

Unt

Un1

29

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4TIEDOWN ASSEMBLY, TOW - 70700-20433-045

Unt

UUUUUUnt

Unt

Un

Unt

Un0

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8724673 EH-60A



1ELECTRONIC SEQUENCE UNIT, 163290-100-E

Unt

UUUUUUnt

Unt

Un

Unt

Un1

52

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION II CABINEH-60A_BASELIN8724673 EH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

JH9024191 CIV 09-Aug-2016



a. ITEM NUMBER

Nomenclature

INERTIAL NAVIGATION SET -AN/ASN-141


BEARING, DISTANCE,HEADING INDICATOR -ID2301/U


FIRST AID KIT - 6545-00919-6650


FIRE EXTINGUISHER - FR23-4-11848


ADAPTER FUEL DRAIN - 70307-03018-102


LOCK ASSY BLADE TIEDOWN- 70700-20369-041


PLUG ASSY INTAKE - HIRSSSUPP - 70700-20515-041/042


PLUG ASSY EXHAUST - HIRSS- 70700-20515-043


PLUG ASSY APU EXHAUST -70700-20509-041


COVER ASSY OIL COOLER -70700-20511-041




SECTION II CABINEH-60A_BASELIN8724673 EH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

JH9024191 CIV 09-Aug-2016

BLADE FOLD SET - 70700-20412-011


COVER PITOT TUBE - 70700-20460-041


TROOP SEATS - 70500-02151-045


COVER ENGINE INLET -83DSCC-D006


PINTLE MOUNT ASSY - L/H -70751-02023-043


PINTLE MOUNT ASSY - R/H -70751-02023-044


ICS WALK-AROUND CORD -70602-02016-041


PORTABLE INSP. FLOODLIGHT - 15-0366-1


COMPUTER LOGBOOK1 CURRENT ACFT CONFIGURATION.28

TIEDOWN ASSEMBLY, TOW -70700-20433-045



SECTION III TRANSITION SECTIONEH-60A_BASELINE


8724673 EH-60A



1ANTENNA, LOOP - AS-2108A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2IFF ANTENNA - 70600-02010-103

Unt

UUUUUUnt

Unt

Un

Unt

Un2

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF/AM ANTENNA 70600-03002-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PUMP FUEL SAMPLER - 82829/4P156-3

Unt

UUUUUUnt

Unt

Un

Unt

Un0

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPENSATOR MAGNETIC FLUX - CN-405/ASN

Unt

UUUUUUnt

Unt

Un

Unt

Un1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS TRANSMITTER - T-611/ASN-43

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS ANTENNA 22433-40

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF AMPLIFIER AM-7531/URC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER RT-1749/URC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IR JAMMER COUNTERMEASURES SET AN/ALQ-144(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

54

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION III TRANSITION SECTIONEH-60A_BASELIN8724673 EH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

JH9024191 CIV 09-Aug-2016



a. ITEM NUMBER

Nomenclature

PUMP FUEL SAMPLER -82829/4P156-3


HF AMPLIFIER AM-7531/URC1 CURRENT ACFT CONFIGURATION.8

RECEIVER/TRANSMITTER RT-1749/URC


IR JAMMERCOUNTERMEASURES SETAN/ALQ-144(V)



SECTION IV TAIL CONEEH-60A_BASELINE


8724673 EH-60A



2VOR/LOC ANTENNA - 70600-05002-101

Unt

UUUUUUnt

Unt

Un

Unt

Un2

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF ANTENNA 4700516-30

Unt

UUUUUUnt

Unt

Un

Unt

Un0

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1DISPENSER GENERAL PURPOSE AIRCRAFT M130

Unt

UUUUUUnt

Unt

Un

Unt

Un0

55

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION IV TAIL CONEEH-60A_BASELIN8724673 EH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

JH9024191 CIV 09-Aug-2016



a. ITEM NUMBER

Nomenclature

HF ANTENNA 4700516-301 CURRENT ACFT CONFIGURATION.2

DISPENSER GENERALPURPOSE AIRCRAFT M130



SECTION V TAIL ROTOR PYLONEH-60A_BASELINE


8724673 EH-60A

3. AREA NAME2. MODEL1. SERIAL NUMBER


1TROOP COMMANDER ANTENNA - 70600-06001-104

Unt

UUUUUUnt

Unt

Unt

Un

n1

1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#1 VHF-FM ANTENNA - 70600-06002-105

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION V TAIL ROTOR PYLONEH-60A_BASELIN8724673 EH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

JH9024191 CIV 09-Aug-2016



a. ITEM NUMBER

Nomenclature


PIDMWODATE HRS



SERVO ASSY, TAIL ROTOR 8724673C300-050941. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


16-May-2016 FM

TM01457108-Jun-2016

0.5USAACE FTRUCKER, AL

TAIL ROTOR SAFETY CABLE.H-60-16-AMAM-07MWO:

Priority Mnt Level



REMARKS

UNSERVICEABLE COMPONENT. FAILURE CODE 381. ULLS WILL NOT ALLOW EDITING OF FAILCODE UPON INSTALL.








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H








44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

09-Jul-2016 CN0141 334-503-3807

1 W0U91TF

0 0 0 0 0 0 0 7620

7620 0


8724673

0 0 0 0 0

11D01 0 0

82106 0 0 2730 0 381

B30310388274000-10311650011431226SERVO, PRIMARY MAIN ROTOR

2730



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

20-Nov-2015 SH0276 334-598-0670

2 W0U91TF

0 0 0 0 0 0 0 7392

7392 0


8724673

0 0 0 0 0

05A02H 0 0

78286 0 0 869 0 799

B9412197470103-08108-0415315015374652BLADE PIN, SOLID

869



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

25-Jul-2012 JK5371 334-503-3753

3 W0U92AO

0 0 0 0 0 0 0 6330

6330 0


8724673

0 0 0 0 0

05A02H 0 0

78286 0 0 0 0 799

B9413223270103-08108-0415315015374652BLADE PIN, SOLID

0



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

25-Jul-2012 JK5371 334-503-3753

3 W0U92AO

0 0 0 0 0 0 0 6330

6330 0


8724673

0 0 0 0 0

05A02H 0 0

78286 0 0 0 0 799

B9413240370103-08108-0415315015374652BLADE PIN, SOLID

0



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

25-Jul-2012 JK5371 334-503-3753

3 W0U92AO

0 0 0 0 0 0 0 6330

6330 0


8724673

0 0 0 0 0

05A02H 0 0

78286 0 0 0 0 799

B9413241670103-08108-0415315015374652BLADE PIN, SOLID

0



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

20-Nov-2015 SH0276 334-598-0670

2 W0U91TF

0 0 0 0 0 0 0 7392

7392 0


8724673

0 0 0 0 0

05A02H 0 0

78286 0 0 1024 0 799

B9413253170103-08108-0415315015374652BLADE PIN, SOLID

1024



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

25-Jul-2012 JK5371 334-503-3753

3 W0U92AO

0 0 0 0 0 0 0 6330

6330 0


8724673

0 0 0 0 0

05A02H 0 0

78286 0 0 0 0 799

B9413811970103-08108-0415315015374652BLADE PIN, SOLID

0



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

25-Jul-2012 JK5371 334-503-3753

3 W0U92AO

0 0 0 0 0 0 0 6330

6330 0


8724673

0 0 0 0 0

05A02H 0 0

78286 0 0 0 0 799

B9413812170103-08108-0415315015374652BLADE PIN, SOLID

0



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

25-Jul-2012 JK5371 334-503-3753

3 W0U92AO

0 0 0 0 0 0 0 6330

6330 0


8724673

0 0 0 0 0

05A02H 0 0

78286 0 0 0 0 799

B9413903370103-08108-0415315015374652BLADE PIN, SOLID

0



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

30-Apr-2012 JK5371 334-503-3403

1 W0U92AO

0 0 0 0 0 0 0 6184

6184 0


8724673

0 0 0 0 0

07B05A 0 0

59364 0 0 0 0 799

204483213850-3-14810011022473VALVE, SOLENIOD

0



REMARKS

CONTROL # 1090753








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

07-Jun-2011 LW2720 3345980670

2 W0U92AO

0 0 0 0 0 0 0 5680

5680 0


8724673

0 0 0 0 0

07B05A 0 0

59364 0 0 0 0 799

186593213850-3-14810011022473VALVE, SOLENIOD

0



PIDMWODATE HRS



SWASHPLATE ASSY 8724673A107-013821. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


02-Dec-1996 OT

MB01113709-Sep-1997

0.5D CO 2-4 AVN,FT. HOOD, TX.(JW4727)

REMOVAL OF CERTAIN REWORKEDMAIN ROTOR SWASHPLATEASSEMBLIES, ALL UH-60A, UH-60L,EM-60A, AND MH-60K HELICOPTERS

UH-60-97-01MWO:

Priority Mnt Level

08-Sep-1997 OM

MB01113709-Sep-1997

0.5D CO 2-4 AVN,FT. HOOD, TX.(JW4727)

ALL UH-60A, UH-60L, EH-60A,REMOVAL OF SPECIFIC SUSPECTREWORKED MAIN ROTORSWASHPLATE ASSEMBLIES


Priority Mnt Level

30-Apr-1998 OM

MB01113705-May-1998

0.5DYNCORP,FHSD FT. HOOD,TX. (DS6135)

ALL H-60 AIRCRAFT WITH THESWASHPLATE LINK ASSEMBLY, P/N70400-08110-054/-061,MANUFACTURED BY TEK (CAGECODE 65780)


Priority Mnt Level

20-Dec-2005 OT

MB01113712-Jun-2006

2USAAWC, FT.RUCKER, AL.(TB1027)

ALL H-60 SERIES AIRCRAFT, MAINROTOR (M/R) HUB ASSEMBLY

UH-60-06-SOF-01MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR BLADE ASSY 8724673A009-048901. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


29-Nov-2001 OM

MF203417-May-2012

1CCAD/W0MUAAINSP FAIRING ASSY PN 70104-11104-044

UH-60-02-ASAM-01/TB1-15MWO:

Priority Mnt Level

15-Sep-2005 DR

MF203417-May-2012

151CCAD/W0MUAAALL UH-60 AIRCRAFT SHALLREQUIRE RE-SHIMMING OF TAILROTOR PIVOT BEARINGS PERREVISED PROCEDURES ANDCERTAIN BLADE ASSEMBLIES WILLBE INSPECTED FOR SPECIFIEDSERIAL NUMBERS WHICH CONTAINCOMPOSITE PIVOT BEARINGRETAINERS.

1-1615-281 C1MWO:

Priority Mnt Level

15-Sep-2005 DR

QC17-Feb-2016

151CCAD\W0MUAARECAPPED1-1615-287 C1MWO:

Priority Mnt Level

23-Apr-2008 DN

QC00000017-Feb-2016

1CCAD\W0MUAARECURRING INSPECTION OF TAILROTOR FAIRING ASSY

ASAM UH-60-02-01MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR PITCH CHANGE SHAFT 8724673A233-003621. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


24-Jan-2014 OM

MW02095627-Jan-2014

2.1USAACETAIL ROTOR PITCH CHANGE SHAFTASSEMBLY

H-60-14-SOF-02MWO:

Priority Mnt Level



0

360

7268.2

8724673 910.8 7128


EH-60A A006-03223 Days


HELICOPTER, UTILITY TAIL ROTOR GEARBOX ASSY Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

BD01110306-Aug-2014NORMALBASELINE1.0420712905-Aug-2014



19 AUG 2015 - OIL SAMPLE IS ABNORMAL DUE TO "WATER". CODE J. DRAIN & FLUSH SYSTEM. SUBMIT RESAMPLE AFTER 1ST FLIGHT CYCLE. USAACE,FT. RUCKER, AL. TM027105.

9. REMARKS:



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

23-Aug-2012 JB6971 (361)961-6345 john.bonawitz

3 W0MUAAD

0 0 0 0 0 0 0 5606

5606 0 0


A00704553

0 0 0 0 0

05A02E 0 0

78286 0 0 0 1236 0 799

A8491207070150-09207-0411560014479774M/R BLADE TIP CAP

1236



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

30-Sep-2013 RS1005 3619616474 ruby.a.sanchez

3 W0MUAAD

0 0 0 0 0 0 0 5207

5207 0 0


A00705484

0 0 0 0 0

05A02E 0 0

78286 0 0 0 2092 0 799

A8490071670150-09207-0411560014479774M/R BLADE TIP CAP

2092



REMARKS

ADMIN REMOVAL BASED ON HIST REVIEW AND DATA PROVIDED BY CCAD








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

26-Oct-2005 ET0732 746-5086 ed.thompson

3 W0H9AAD

0 0 0 4047

4047 0 0


A00705066

2 X

0 0 0 0

05A02E 0

78286 0 1746 1746 0 804

A8490228670150-09107-0411560011001702M/R BLADE TIP CAP

1746



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

20-Apr-2012 AF0603 961-6215 albert.flores

2 W0MUAAD

0 0 0 0 0 0 0 4470

4470 0 0


A00700388

0 0 0 0 0

05A02E 0 0

78286 0 0 0 891 0 799

A8491119870150-09207-0411560014479774M/R BLADE TIP CAP

891



REMARKS

INSTALLED WITH FAILCODE OF 804 DUE TO ACFT BEING TRANSFERRED TO BEST PROGRAM, HUNTSVILLE,AL








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H








44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

27-Jul-2016 OW0109 334-598-0670

1 W0U91TF

0 0 0 0 0 0 0 7620

7620 0


8724673

0 0 0 0 0

05B02 0 0

78286 0 0 4000 0 799

A0090489070101-31000-0431615011138188TAIL ROTOR BLADE ASSY

4000



REMARKS

COMPONENT IS UNSERVICEABLE AND IS BEING SHIPPED TO THE BEST PROGRAM IN HUNTSVILLE, AL.








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H








44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

27-Jul-2016 MJ0262 334-598-0670

1 W0U91TF

0 0 0 0 0 0 0 7620

7620 0


8724673

0 0 0 0 0

05B02 0 0

78286 0 0 4323 0 374

A0090172170101-31000-0431615011138188TAIL ROTOR BLADE ASSY

4323



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

12-Aug-2014 AG3612 252-464-5457 andrea.l.gariba

SPRRA110D0031

9 N65923D

0 0 0 0 1 0 5574 893

893 15 0

AUXILIARY POWER UNIT 2835013692818 116305-302

SPE041069

0 0 0 0 0

15B03 0

55820 0 0 0 0 0 799

S26345039912835013638089WHEEL, TURBINE

0



UNIT UNIQUE INVENTORY ITEMSEH-60A_BASELINE


8724673 EH-60A



Unt

UUUUUUnt

Unt

Un

Unt

Un

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





UNIT UNIQUE INVENTORY ITEMSEH-60A_BASELIN8724673 EH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c



a. ITEM NUMBER

Nomenclature


REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

12-Aug-2014 AG3612 252-464-5457 andrea.l.gariba

9 N65923D

0 0 0 0 1 0 5574 893

893 15 0

AUXILIARY POWER UNIT 2835013692818 116305-302

SPE041069

0 0 0 0 0

15B02B 0

99167 0 0 0 0 0 799

SIF474945029022835014596002WHEEL, COMPRESSOR

0



Documents

DA Form 2408-5 - Equipment Modification RecordNSN 1520-01-298-4532) MWO:1-1520-237-50-84 Priority Mnt Level 25-Jan-2007 R D USAACE 80 01-May-2012 MODIFICATION INSTRUCTIONS FOR THE