da form 2408-5 - equipment modification record · 19-may-2010 icmd, cmws modernization (p3i) on the...

PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN

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

8724615UH-60AHELICOPTER, UTILITY

3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE

Report Date: of 716-Sep-2016

OM27-Jun-2005

DYNCORPPROJECT OLRFTCKY (RB1876)

8101-Oct-2006

APU INLET BARRIER FILTER SYSTEMAFS-APU-IBF-IPMWO:Mnt LevelPriority

DR22-Sep-2006

DYNCORPPROJECT OLRFTCKY (RB1876)

3901-Oct-2006

INSTALLATION OF ELECTRONIC DATAMANAGEMENT [EDM] SYSTEM FORBLUE FORCE TRACKER.

1-1520-237-50-EMDMWO:

Mnt LevelPriority

DR04-Jun-2001

USAAVCN,FT.RUCKER, AL.(TB1027)

802-Mar-2002

INSTALLATION OF HFCOMMUNICATION SYSTEM AN/ARC-220(V) AND TSEC/KY-100 IN UH60/LHELICOPTER NSN 1520-01-035-0266UH-60A NSN 1520-01-298-4532 UH-60L

1-1520-237-50-76MWO:

Mnt LevelPriority

DR13-Apr-2001


13.202-Mar-2002

INSTALLATION OF SEALED LEAD-ACIDBATTERY (SLAB) SYSTEM ANDRELOCATION OF UTILITY LIGHTPOWER (UH-60A/L HELICOPTERS) UH-60A NSN 1520-01-035-0266 UH-60LNSN 1520-01-298-4532

1-1520-237-50-77MWO:

Mnt LevelPriority

DN01-May-1994


12802-Mar-2002

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

1-1520-237-50-66MWO:

Mnt LevelPriority

DN15-Sep-2000


5202-Mar-2002

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

1-1520-237-50-56 C4MWO:

Mnt LevelPriority

DR27-Apr-1998

FT RUCKER, FT.RUCKER, AL

8002-NOV-2001

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

DN30-Jun-2004

DYNCORP 9003-Apr-2008

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

1-1520-237-50-92MWO:

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-Mar-1988

USARMAVCEN,FT.RUCKER, AL.(JJ7093)

2003-May-1988

MODIFICATION OF WIRE STRIKEPROTECTION SYSTEM (WSPS) (UH/EH-60A HELICOPTER)

55-1520-237-50-47MWO:

Mnt LevelPriority

DR19-Mar-2007

PIF-REDSTONEARSWENALHUNTSVILLE, AL

12.503-NOV-2010

MODIFICATION INSTRUCTIONS FORINSTALLATION OF M4 MOUNTS ON UH-60A/L AIRCRAFT (NSN 1520-01-035-0266) UH-60A (NSN 1520-01-298-4532)UH-60L

1-1520-237-30-2MWO:

Mnt LevelPriority

DM15-Nov-1989

USARMAVCEN,FT.RUCKER, AL.(BM6188)

2204-May-1990

MODIFICATION OF DOWEL PINRETENTION MAIN GEARBOX

55-1520-237-50-43MWO:

Mnt LevelPriority

DN01-Aug-1991


2204-May-1990

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

DR25-Jan-2007

D CO, 1-131STAVN REGTBALAD, IRAQ

1005-Jul-2007

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

FN15-Mar-2010

YULISTAAVIATION

805-Nov-2010

M4 GUN MOUNT ON THE UH-60 A/LMODEL VERTICAL MOUNTSINSTALLATION (PILOT AND COPILOT)

1-1520-237-50-1008310MWO:

Mnt LevelPriority

DN17-Jun-1989

USARMAVCEN,FT.RUCKER, AL.(WG5804)

605-Oct-1989

INCOROPORATION OF EXHAUSTEXTENDER DOUBLERS

55-1520-237-50-51MWO:

Mnt LevelPriority

DR25-May-2000

L-3 CISLEXINGTON, KY(WW1514)

606-Oct-2005

FRIES W/ SAFETY RELEASE SYSTEMUH-60

N1162MWO:

Mnt LevelPriority

DM15-Nov-1989


2208-MAY-1990

MODIFICATION OF DOWEL PINRETENTION MAIN GEARBOX

1-1520-237-50-43MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN01-Oct-1989

WOU911(MB1851)

4809-Aug-1995

INSTALLATION OF GLOBAL POSITIONSYSTEM AN/ASN-149(V)1

55-1520-237-50-55MWO:

Mnt LevelPriority

DR02-Jun-2006

MOAVCRAD 509-Jul-2009

INSTALLATION OF PROVISIONS FOREXTERNAL ELECTRIC RESCUE HOISTCABLE GUARD DEFLECTOR

RSN 1001031MWO:

Mnt LevelPriority

DN02-Jun-2006

TASM-G MOSPRINGFIELD,MO

4010-JUL-2009

INSTALLATION OF RESCUE HOISTCABLE GUARD DEFLECTOR

1-1520-237-50-MEDMWO:

Mnt LevelPriority

DN15-Jan-1989

USAAVCN,FT.RUCKER, AL.(RS5598)

1210-Oct-1989

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

1-5945-237-50-1MWO:

Mnt LevelPriority

DR11-Aug-2000

USAAVCN,FT.RUCKER, AL.(RR4443)

1312-Aug-1999

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

1-1520-237-50-79MWO:

Mnt LevelPriority

DM15-Jun-1991


612-OCT-1989

INCOROPORATION OF EXHAUSTEXTENDER DOUBLERS

1-1520-237-50-51MWO:

Mnt LevelPriority

DN01-Mar-1989


512-OCT-1989

INCORPORATION OF IMPROVEDTIEDOWN FITTINGS

1-1520-237-50-53MWO:

Mnt LevelPriority

DN01-Oct-1991


413-DEC-1990

INCORPORATION OF STABILATORACTUATOR GROUNDING STRAP FORUH-60A/EH-60A HELICOPTERS

1-1520-237-50-54MWO:

Mnt LevelPriority

DN09-Jun-1988

USAAVNC,FT.RUCKER, AL.(BM6188)

12414-Dec-1990

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

55-1520-237-50-42MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN04-Mar-1999

WOU911(GR4425)

3514-Nov-1997

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

1-1520-237-50-74 C1MWO:

Mnt LevelPriority

DR08-Nov-1996

WOU911(DK1063)

17815-Apr-1998

INSTALLATION OF AN/ASN-128BDOPPLER/GPS NAVIGATION SYSTEMIN UH-60A/L HELICOPTER

1-1520-237-50-75MWO:

Mnt LevelPriority

DR21-Jun-2004

DYNCORP OLR,FTCKY (RB1876)

7515-Feb-2006

MODIFICATION 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

DM30-Jan-2003

DYNCORP OLR.FTCKY (RB1876)

30015-Feb-2006

INSTALLATION OF BLUE FORCETRACKER

1-1520-237-50-BFTMWO:

Mnt LevelPriority

DR22-Sep-2005


3715-Feb-2006

ELECTRONIC DATA MANAGEMENT(EDM) SYSTEM

RSN LSF 01-06MWO:

Mnt LevelPriority

DR27-Oct-2005


90015-Feb-2006

INSTALLATION OF AN/AAR-57[V]3COMMON MISSILE WARNING SYSTEMAND IMPROVED COUNTERMEASURE.

1-1520-237-50-53-CMWSMWO:

Mnt LevelPriority

DM08-Feb-2005

DYNCORP OLT,FTCKY (RB1876)

36115-Feb-2006

ENGINE INLET BARRIER FILTER1-1520-237-50-90MWO:Mnt LevelPriority

DM01-Sep-1991

USAAVNC,FT.RUCKER, AL.(MB1851)

215-Sep-1995

IMPROVED ENGINE COWLINGRELEASE HANDLE ASSEMBLY

1-1520-237-50-64MWO:

Mnt LevelPriority

DU31-May-1995

WOU911C, FT.RUCKER, AL.(MB1851)

2415-Sep-1995

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

1-1520-237-50-73MWO:

Mnt LevelPriority

DN14-Jun-1991

USAAVNC,FT.RUCKER,AL.(MB1851)

615-Sep-1995

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

1-1520-237-50-61 C1MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN14-Nov-1994

USAAVNC, FT.RUCKER, AL.(MB1851)

615-Sep-1995

DOE CHANGING OF TIE DOWN AT STA308.00 LEFT AND RIGHT

1-1520-237-50-61 CHG 1MWO:

Mnt LevelPriority

FR20-May-2006

DYNCORPINTERNATIONALFTCKY 42223

418-Apr-2008

FUEL CELL CORROSION INSPECTIONOF UH-60, EH-60, AND HH-60 SERIESHELICOPTERS.

1-1520-237-23-9MWO:

Mnt LevelPriority

OR20-Mar-2008

DYNCORPINTERNATIONALFTCKY 42223

518-Apr-2008

INSPECTION OF UH-60, EH-60, HH-60SERIES HELICOPTERS FOR BODYPLUG CORROSION INSPECTION

1-1520-237-23-10MWO:

Mnt LevelPriority

DN30-Sep-1987

SIKORSKY(EC7788)

118-Feb-1988

INSTALLATION OF FLIGHT DATARECORDER AND STATUS INDICATORLIGHT

55-1520-237-55-03MWO:

Mnt LevelPriority

DN05-Oct-1994


18419-Jun-2001

INSTALLATION OF HEADS UP DISPLAY(HUD) AN/AVS-7 FOR UH-60AHELICOPTERS AND UH-60LHELICOPTERS

1-1520-237-50-62MWO:

Mnt LevelPriority

DR07-Nov-2008

KILLEEN AFMA(CSC)

25019-May-2010

ICMD, CMWS MODERNIZATION (P3I)ON THE UH-60 A/L AIRCRAFT,STRUCTURE INSTALLATION ONLYWITH THE EXCEPTION OF HOLE CUTOUT AT AFT CENTER CONSOLE FORNVIS SAFE/ ARM SWITH ASSEMBLY

1-1520-237-50-97MWO:

Mnt LevelPriority

DM30-Sep-2003

KILLEEN AFMA(CSC)

1019-May-2010

INTERIM STATEMENT OFAIRWORTHINESS QUALIFICATIONS(ISAQ) FOR ALL UH-60A/LHELICOPTERS EQUIPPED WITHBALLISTIC PROTECTION SYSTEM(BPS)

ISAQ 108MWO:

Mnt LevelPriority

DM07-Jan-2008

KILLEEN AFMA(CSC)

7619-May-2010

INSTALLATION OF CMWS FIFTHSENSOR

1-1520-237-50-99MWO:

Mnt LevelPriority



PIDMWODATE HRS






DR30-Nov-2008

KILLEEN AFMA(CSC)

91219-May-2010

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF INTEGRATEDVEHICLE HEALTH MANAGEMENTSYSTEM (IVHUMS) ON UH-60A/LAIRCRAFT

1-1520-237-50-100MWO:

Mnt LevelPriority

DU15-Nov-1987


1620-Aug-1987

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

55-1520-237-50-46 C2MWO:

Mnt LevelPriority

DN15-Jan-1991

USAAVCN,FT.RUCKER, AL.(RS5598)

620-May-1993

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

55-1520-237-50-58MWO:

Mnt LevelPriority

DR28-Feb-2005

AMCOMPROJECT OLRKILLEEN TX(FL727205)

9421-Jun-2006

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE AIRWARRIOR MICROCLIMATE COOLINGSYSTEM AND MASK BLOWER WIRINGASSEMBLY ON THE UH-60A/LAIRCRAFT (NSN 1520-01-035-0266)(NSN 1520-01-298-4532)

1-1520-237-50-85MWO:

Mnt LevelPriority

OU31-Oct-2002

FT CAMPBELLFORTCAMPBELL, KY

222-APR-2003

UH-60 SERIES AIRCRAFT INSPECTAN/ARC-220 WIRING FOR CHAFING

1-1520-237-20-261MWO:

Mnt LevelPriority

DR21-Jun-2006

FT HOODKILLEEN,TX

21522-APR-2010

INSTALL BFT W/-301 ANTENNA (UH-60A/L)

BFT60-001MWO:

Mnt LevelPriority

DM22-Feb-1991

USAAVNC,FT.RUCKER, AL.(DS6547)

83222-Oct-1991

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

1-1520-237-50-59MWO:

Mnt LevelPriority

DR15-Mar-2004

FT. HOOD AFMFT. HOOD TX76544

10026-Sep-2013

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THECRASHWORTHY EXTERNAL FUELSYSTEM IN UH-60 SERIESHELICOPTERS

1-1520-237-50-86MWO:

Mnt LevelPriority

OM01-Feb-1993

WOU911(MB1851)

40028-Aug-1995

SINCGARS DIPLEXER REMOVAL ANDNEW COAX CABLE INST

1-1520-237-50-68MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN24-Jul-1995


4830-MAY-1995

DE-MODIFICATION OF THE GLOBALPOSITIONING SYSTEM AN/ASN-149 INTHE UH-60A

1-1520-237-50-55 DEMODMWO:

Mnt LevelPriority

DM18-Apr-1988

USARMAVCEN,FT.RUCKER, AL.(JS5144)

131-Aug-1988

INSTALLATION OF IMPROVEDCARTRIDGE ACTUATED DEVICE

55-4030-237-50-01MWO:

Mnt LevelPriority

DM18-Feb-2008

L3 VERTEXAEROSPACE

2031-May-2011

INSTALLATION OF T700-GE-701DENGINES AND SUPPORTCOMPONENTS ON UH-60A AND HH-60A AIRCRAFT

1-1520-237-20-3MWO:

Mnt LevelPriority

DM14-Apr-2008

L3 VERTEXAEROSPACE

2031-May-2011

INSTALLATION OF AUTO RELIGHTAND TRANSIENT DROOPIMPROVEMENT FOR T700-GE-701DENGINES ON UH-60A/HH60AAIRCRAFT

1-1520-237-30-3MWO:

Mnt LevelPriority



NUMBERLOCATIONPIDENTRYORGANIZATION

8.7.DATE

6.REMARKS

4. 5.

UH-60A 8724615HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL

Report Date: Page 1 of 4116-Sep-2016

SIKORSKY AIRCRAFTACFT M/R HEAD RIGGED I/A/W SA DWG 70400-00003 REV E. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD.A. ACFT CONTROLSERVO INPUT ROD HAS BEEN LENGTHENED1/2 TURN. B. LATERAL CONTROL SERVOINPUT ROD HAS BEEN LENGTHENED 1/8TURN. C. FORWARDCONTROL SERVO INPUTROD HAS BEEN SHORTENED 1/2 TURN. NOTE:WHEN AIRCRAFT RIGGING IS BIASEDRIGGING PIN HOLES ARE TEMPORARILYLOST AT THE ABOVE 3 POINTS. (SS0000)

29-May-1987 1

STRATFORD, CT.

QC000000

SIKORSKY AIRCRAFTUH-60-83-12(TB 55-1520-237-20-46)INSPECTION OF TAIL ROTOR ASSY FOR BENTSERVO VALVE INPUT STEM COMPLIED WITH.(SS0000)

20-Jun-1987 1

STRATFORD, CT.

QC000000

SIKORSKY AIRCRAFTUH-60-84-02 (TB 55-1520-237-20-48) ONE TIMEINSPECTION OF WIRE HARNESS ROUTINGFOR FEEDER HARNESS BETWEEN NO. 1 ANDNO. 2 JUNCTION BOXES COMPLIED WITH.(SS0000)

20-Jun-1987 2

STRATFORD, CT.

QC000000

SIKORSKY AIRCRAFTCOMPLIED WITH SOF MSG. UH-60A-86-21 (TB55-1520- 237-20-85) ONE TIME INSPECTION OFCREW SEATS FOR LONGITUDINALMOVEMENT OF LOCK PIN ADJUSTMENT.(SS0000)

20-Jun-1987 3

STRATFORD, CT.

QC000000

SIKORSKY AIRCRAFTCOMPLIED WITH SOF MSG. 242300Z MARCH87 (UH-60A- 87-04) UH-60A/EH-60A AIRCRAFT,REVISION TO INSPECTION OF EYEBOLT P/N70209-02136-102. (SS0000)

30-Jun-1987 1

STRATFORD, CT.

QC000000

SIKORSKY AIRCRAFTCOMPLIED WITH SOF MSG UH-60-87-08, UH-60/EH-60 AIRCRAFT, INSPECTION OFMIDSECTION BELLCRANK ASSEMBLIES.(JM0000)

10-Jul-1987 1

STRATFORD, CT.

QC000000

USARMAVCEN, FT.TWX 1113000Z AUG 87 (UH-60-87-09) CYCLICSTABILATOR SLEW SEITH C/W. (JA8930)

20-Aug-1987 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.STABILATOR PIVOT CHAFE REPAIR IAW 5244COMPLIED WITH. (DS1315)

24-Sep-1987 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TB 55-1520-237-20-92 ONE TIME INSPECTIONOF INPUT FLANGE ASSY C/W. (JA8930)

13-Oct-1987 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TWX 030100Z DEC 87 INSPECTION FORDEFECTIVE ENGINE POWER TURBINEMODULES COMPLETED 3 DEC 87. (MW5964)

03-Dec-1987 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TB 55-1520-237-20-93 (UH-60-87-XSOF-02) ONETIME INSP & RECURRING INSP OF ENGCOWLINGS C/W. (SL1657)

08-Jan-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.500 HR INSP #1 COMPLETED AT 500.0 ACFTHRS. PHASE INSP #2 DUE AT 1000.0 ACFTHRS. (SL1657)

12-Jan-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.ONE TIME FLOURESCENT PENETRANT INSPOF TAIL WHEEL FORK C/W. (SL1657)

29-Jan-1988 1

RUCKER, AL.

QC000000

AVSCOM OCM SECTIONOCM/ACE PERFORMED AT 588 A/C HRS AT FTRUCKER, AL.BY ACE TEAM MEMBER "W".(FS0000)

11-Feb-1988 1

ST. LOUIS MO.

QC000000

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.



USARMAVCEN, FT.TB 55-1520-237-20-95 (UH-60A-88-01) INSP FORCERTAIN SERIAL NUMBER TAIL ROTORBLADE ASSEMBLIES C/W. (SL1657)

17-Feb-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TB 55-1520-237-20-96 ONE TIME INSP OF T/RGEARBOX OUTPUT SHAFT C/W. (SL1657)

25-Mar-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TDR 49-88 ONE TIME INSP OF DESWIRL DUCTCLAMP C/W. (SL1657)

06-Apr-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TB 55-1520-237-20-97 (UH-60A-88-03) LIFEEXTENSION OF MAIN MODULE SHAFT C/W.(WC0759)

18-May-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TB 55-1520-237-20-98 (UH-60A-88-05)INITIATION OF APU MAXIMUM ALLOWABLEOPERATING TIME IN TERMS OF APU HOURSAND APU STARTS C/W 763 A/C HRS. 190 APUHRS. 922 STARTS. (WS6134)

01-Jul-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TB 55-1520-237-20-99 (TWX 112300Z JUL 88)OVERHAUL LIFE FOR THE TRANSMISSION OILCOOLER BLOWER (FAN AXIAL) C/W. (WS6134)

14-Jul-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TB 55-1520-237-20-100 UH-60A-88-09 ONE TIMEINSP OF ARA MFG CREW SEATS FOR LOOSECLEVIS SCREWS C/W. (WS6134)

03-Aug-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TB 1-1500-200-20-26 (GEN-88-03) INSP FORINSTL OF CORRECT INTERNAL PORTABLEFIRE EXT C/W. (WS6134)

23-Sep-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TWX 172230Z OCT 88 (UH-60-88-11) ACFTRESTRICTED FROM IMMEDIATE RAPELLINGOPERATIONS. (SL1657)

18-Oct-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TB 55-1520-237-20-101 (UH60-88-10) INSP OFTROOP/ GUNNER SEAT AND THREE MANMEDEVAC UPPER SUPPORT INSTL ASSY C/W.(SL1657)

28-Oct-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TB 55-1520-237-20-102 UH60-88-13 INSP OF M/RBLADE EXPANDABLE RETENTION PIN P/N70103-08107-101 FOR MISSING SEGMENTSC/W. (SL1657)

22-Nov-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.INSTL OF A GREASE FITTING ANDLUBRICATION OF THE WINDSHIELD WIPERCONVERTER IAW ENG STD A-17-87 C/W(FP7867)

05-Dec-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.APPLICATION OF EPOXY COATING ON M/RBLADE TIP CAPS IAW ENG STD A-5-87 C/W.(FP7867)

07-Dec-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.500 HR INSP & 2ND PHASE COMPLETED ATA/C HRS 999.2 (FP7867)

16-Dec-1988 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TB 55-2840-248-50-48 (UH-60-01) ONE TIMEINSPECTION OF ENGINE GAS GENERATORSTATOR SHROUD C/W. NA TO #1 ENGINE.(FP7867)

14-Feb-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.OCM/ACE PERFORMED AT 1059 A/C HRS ATFT. RUCKER, AL. BY ACE TEAM MEMBER M.ODOM. (MO0000)

03-Mar-1989 1

RUCKER, AL.

QC000000



8.7.DATE

6.REMARKS

4. 5.



USARMAVCEN, FT.PILOT WINDSHIELD BROKEN AT 1077.3 ACFTHRS FROM BIRD STRIKE. WINDOWREPLACED. WIRES DISCONNECTED &RECONNECTED PERT. TO WINDSHIELDREPLACEMENT. INSP COMPLETED. (FP7867)

08-Mar-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TWX 302100Z MAR 89 TB 55-1520-237-20-105(UH-60-03)INSPECTION OF ALL M/RSPINDLES ALL P/N'S C/W. (FP7867)

31-Mar-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TWX 121903Z JUNE 89 TB 55-1520-237-20-106(UH-60- 89-05) ONE TIME INSP OF WIRESTRIKE PROTECTION SYSTEM C/W. (FP7867)

16-Jun-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TWX 171600Z JUL 89 TB 55-1520-237-20-107(UH-60- 89-06) ONE TIME INSP OF THE RIGHTHAND & LEFT HAND RELAY PANELASSEMBLIES FOR SUSPECT GROUNDINGMODULES C/W. (FP7867)

18-Jul-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.INSTALLATION OF TAIL LANDING GEARLOWER PISTON ASSY C/W. IAW COR LTR DTD4 AUG 89. (FP7867)

21-Jul-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TWX 091705Z TB 55-1520-237-20-108 (UH-60-89-08) ONE TIME INSPECTION OF FUEL BOOSTPUMP HOSE ATTACHMENT C/W. (FP7867)

12-Aug-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TB 55-1520-237-20-104 (UH-60-89-09) CHANGE1 NEW OVERHAUL/RETIREMENT LIFESCHEDULE FOR UH-60 RETIREMENT LIFECOMPONENTS C/W. (FP7867)

22-Aug-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.INSPECTION OF T700 ENGINE ALTERNATORSTATOR C/W IAW COR LTR DTD 10 AUG 89.(FP7867)

22-Sep-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.REMOVAL OF HOOVER INFRAREDSUPPRESSORS SUBSYSTEM (HIRRS) INNERBAFFLE C/W. (FP7867)

10-Oct-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.MODIFICATION TO PITOT COVER IAW LTRFROM COR DTD 4 JAN 89 C/W. (FP7867)

13-Oct-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TAIL ROTOR DRIVESHAFT SUPPORTBEARINGS P/N SB1138101 REPLACED AT A/CHRS 1498.1 (FP7867)

20-Oct-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.500 HR INSP & 3RD PHASE COMPLETED ATA/C HRS 1498.1 (FP7867)

23-Oct-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TB 55-2840-248-50-48 (UH-60-89-10)INSPECTION OF GAS GENERATOR ROTOR &STATOR SHROUDS C/W. (FP7867)

24-Oct-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TWX 07110Z NOV 89, TB 55-1520-237-20-109ONE TIME INSPECTION OF OIL COOLER AXIALFAN C/W. (FP7867)

14-Nov-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TWX 222330Z TB 55-1520-237-20-110 (UH-60-89-12) ONE TIME INSPECTION OF OIL COOLERAXIAL FAN C/W. (FP7867)

29-Nov-1989 1

RUCKER, AL.

QC000000

USARMAVCEN, FT.TWX 051845Z DEC 89, TB 55-1520-237-20-112(UH-60- 89-13) RESTRICTIONS AGAINST USINGFITTING ASSY P/B70700-20433-45 FORRAPPELING, PARACHUTING, & TRANSPORTTIE DOWN OPERATIONS C/W. (FP7867)

08-Dec-1989 1

RUCKER, AL.

QC000000



8.7.DATE

6.REMARKS

4. 5.



USARMAVCEN, FT.TB 55-1520-237-20-111 ONE TIME INSPECTIONOF UPPER PRESSURE PLATE AND SPINDLETO HUB ATTACHMENT BOLTS C/W. (CW6383)

13-Jan-1990 1

RUCKER, AL.

QC000000

AVSCOM OCM SECTIONOCM/ACE PERFORMED AT 1756 A/C HRS ATFT. RUCKER, AL. BY ACE TEAM MEMBER 'P'.(RM5140)

23-Jan-1990 1

ST. LOUIS, MO

QC000000

USARMAVCEN, FT.TAIL ROTOR YOKE REPLACED DUE TO BEINGCRACKED AT A/C HRS 1764.1 (FP0000)

23-Jan-1990 2

ST, LOUIS, MO

QC000000

USAAVNC,TB 55-1520-237-20-115 (UH-60-90-01) ONE TIMEINSP & RECURRING INSP OF M/R BLADEEXPANDABLE PINS C/W. (FP7867)

11-Apr-1990 1

FT. RUCKER, AL.

QC000000

USAAVNC,TAIL ROTOR DRIVESHAFT SUPPORTBEARINGS P/N SB1138-101 REPLACED AT A/CHRS 1997.7 IAW TB 55-1520-237-20-104.(FP7867)

01-May-1990 1

FT. RUCKER, AL.

QC000000

USAAVNC,TWX 211108Z SEPT 89, ONE TIME INSPECTIONOF TRANSDUCERS, MOTIONAL P/N 322/A &322/Z C/W. (FP7867)

03-May-1990 1

FT. RUCKER, AL.

QC000000

USAAVNC,500 HR INSP & 4TH PHASE COMPLETED ATA/C HRS 1997.7 (FP7867)

11-May-1990 1

FT. RUCKER, AL.

QC000000

USAAVNC,TB 55-1520-237-20-113 INSP FOR DEFECTIVEROSEMOUNT ICE RATE INDICATORS C/W.(FP7867)

15-Jun-1990 1

FT. RUCKER, AL.

QC000000

USAAVNC,TB 55-1520-237-20-117 ONE TIME INSPECTIONOF M/R PITCH CONTROL HORNS C/W. (FP7867)

12-Jul-1990 1

FT. RUCKER, AL.

QC000000

USAAVNC,TB 55-1520-237-20-118 (UH-60-90-02) ONE TIMEINSPECTION OF T/R PITCH BEAM RETAININGWASHER & PITCH BEAM RETAINING NUT C/W.(FP7867)

14-Aug-1990 1

FT. RUCKER, AL.

QC000000

USAAVNC,INSTALLATION OF EMERGENCY LOCATORTRANSMITTER (ELT) IAW COR LTR DTD 17JAN 89 C/W. (FP7867)

25-Oct-1990 1

FT. RUCKER, AL.

QC000000

AVSCOM OCM SECTIONOCM/ACE PERFORMED AT 2493 A/C HRS ATFT. RUCKER, AL. BY ACE TEAM MEMBER 'C'.(JH0000)

29-Nov-1990 1

ST LOUIS, MO.

QC000000

USAAVNC,TB 55-1520-237-20-114 INSPECT & REWORK OFTHE MEDEVAC PROVISION POWERRECEPTACLE C/W. (FP7867)

04-Dec-1990 1

FT. RUCKER, AL.

QC000000


14-Dec-1990 1

FT. RUCKER, AL.

QC000000

USAAVNC,TB 55-1520-237-20-119 (UH-60-91-ASAM-01)INSP OF TAIL ROTOR PITCH BEAM RETAININGWASHER & PITCH BEAM ASSY C/W. (FP7867)

04-Jan-1991 1

FT. RUCKER, AL.

QC000000

USAAVNC,TB 55-1520-237-20-122 (UH-60-ASAM-05) INSPFOR FOUR UNSERVICEABLE SPINDLEASSEMBLIES C/W. (FP7867)

26-Feb-1991 1

FT. RUCKER, AL.

QC000000

USAAVNC,TB 1-1520-237-20-124 (UH-60-91-ASAM-06) ONETIME INSPECTION OF CARGO HOOKINTERNAL WIRE BUNDLE ROUTING C/W.(FP7867)

18-Mar-1991 1

FT. RUCKER, AL.

QC000000



8.7.DATE

6.REMARKS

4. 5.



USAAVNC,TB 1-1520-237-20-125 (UH-60-91-ASAM-08) ONETIME INSPECTION OF FIRE EXTINGUISHINGSYSTEM C/W. (FP7867)

02-Apr-1991 1

FT. RUCKER, AL.

QC000000

USAAVNC,T/R PITCH BEAM RETAINING WASHERREPLACED IAW TB 55-1520-237-20-119 (UH-60-ASAM-01). (FP7867)

16-Apr-1991 1

FT. RUCKER, AL.

QC000000

USAAVNC,TB 1-1520-237-20-126 UH-60-91-ASAM-09CHANGES TO INSPECTION PROCEDURES FORMAIN ROTOR ELASTOMERIC BEARINGS C/W.(FP7867)

15-May-1991 1

FT. RUCKER, AL.

QC000000

USAAVNC,TB 1-1520-237-20-127 (UH-60-91-ASAM-10) ONETIME INSPECTION AND REPLACEMENT OFMAIN LANDING GEAR BRAKE ASSY PISTONINSULATOR C/W. (FP7867)

05-Jul-1991 1

FT. RUCKER, AL.

QC000000


13-Nov-1991 1

FT. RUCKER, AL.

QC000000

USAAVNC,TB 1-1520-237-20-129 (UH-60-92-ASAM-01)INSPECTION FOR THREE UNSERVICEABLESPINDLE ASSEMBLIES C/W. (CW6383)

08-Jan-1992 1

FT. RUCKER, AL.

QC000000

AVSCOM OCM SECTIONOCM/ACE PERFORMED AT 3105 A/C HRS ATFT. RUCKER AL. BY ACE TEAM MEMBER 'R'.(RM5140)

22-Jan-1992 1

ST. LOUIS, MO

QC000000

USAAVNC,ONE TIME INSPECTION OF M/R SPINDLEELASTOMERIC THRUST BEARING FORSEPARATION OR DETERIORATION IAW INSPFROM ALMD C/W. (BE8533)

17-Apr-1992 1

FT. RUCKER, AL

QC000000

USAAVNC,ONE TIME INSPECTION OF TECH UH-60 CABINDOOR BEAM AS DIRECTED BY ALMD C/W.(BE8533)

01-May-1992 1

FT. RUCKER, AL

QC000000

USAAVNC,500 HR INSPECTION (7TH PE) COMPLETED AT3488.2 A/CHRS. 8TH PE DUE AT 3988.2 A/CHRS. (BE8533)

17-Jun-1992 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-134 (UH-60-92-ASAM-06) ONETIME INSPECTION FOR PROPER HARDWAREON THE PEDAL ADJUSTER ASSY C/W.(BE8533)

09-Sep-1992 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-135 (UH-60-93-ASAM-01) ONETIME OPERATIONAL CHECK OF THETRANSMISSION AND GEARBOX CHIPDETECTOR SYSTEM C/W. (BE8533)

16-Nov-1992 1

FT. RUCKER, AL

QC000000

USAAVNC,ONE TIME INSPECTION FOR CHAFFING OFFUEL MANIFOLD LINES ON LEFT AND RIGHTENGINES IAW COR LTR DTD 16NOV 92 C/W.(BE8533)

27-Nov-1992 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-136 (UH-60-93-ASAM-06) ONETIME INSPECTION TO REMOVE SUSPECT TAILROTOR PITCH BEAMS C/W. (BS8533)

12-Jan-1993 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-130 (UH-60-92-ASAM-05)INSPECTION AND REPLACEMENT OF MAINROTOR EXPANDABLE PINS C/W. (BS8533)

19-Feb-1993 1

FT. RUCKER, AL

QC000000

AVSCOM OCM SECTIONOCM/ACE PERFORMED AT 3925 A/C HRS ATFT. RUCKER, AL. BY ACE TEAM MEMBER N.EASTMAN. (NE0000)

11-Mar-1993 1

ST. LOUIS, MO.

QC000000



8.7.DATE

6.REMARKS

4. 5.



USAAVNC,TB 1-1520-237-20-142 (UH-60-93-ASAM-11)INSPECT AND REPLACE ARA CREWRESTRAINT BUCKLE/CROTCH ASSEMBLIES.(RS5598)

26-Apr-1993 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-140 (UH-60-93-ASAM-09) ONETIME INSPECTION TO DETERMINECOMPLIANCE WITH SYSTEM MWO'S. (WG5804)

04-May-1993 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-141 (UH-60-93-ASAM-10) ONETIME AND RECURRING INSP/CLEANING OFTHE ESSS VALVE AND PNEUMATIC LINES NATO THIS ACFT. (WG5804)

05-May-1993 1

FT. RUCKER, AL

QC000000

USAAVNC,TAIL ROTOR DRIVESHAFT SUPPORTBEARINGS P/N SB1138-101 REPLACED AT3987.6 ACFT HRS S/N #2 13495, #3 16118, #416093 I/A/W TB 1-1520-237-20-104 (WG5804)

11-May-1993 1

FT. RUCKER, AL

QC000000

USAAVNC,REPLACE ALL OLD CHICAGO RAWHIDE (CR)BEARINGS (P/N B40-80-9601) (WG5804)

11-May-1993 2

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-138 (UH-60-93-ASAM-08) TOBIAS TAIL ROTOR RIGGING THREE DEGREES.(WG5804)

17-May-1993 1

FT. RUCKER, AL

QC000000

USAAVNC,500 HR INSPECTION (8TH PE) COMPLETED AT3987.6 ACFT HRS 9TH PE DUR AT 4487.6 ACFTHRS. (WG5804)

18-May-1993 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-143 (UH-60-93-ASAM-12)ABRUPT CHANGE IN MAIN ROTOR TRACKVIBRATIONS. PILOT NOTIFICATION. (BS8533)

18-May-1993 2

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-146 (UH-60-93-ASAM-16) ONETIME INSP OF THE HYD PUMP MODULEKNURLED BLEED RELIEF KNOB SECURINGPIN COMPLETED AT 4202.7 ACFT HRS.(RS5598)

11-Aug-1993 1

FT. RUCKER, AL

QC000000

USAAVNC,PHASE INSP NO. 9 COMPLETED AT 4487.6ACFT HRS. (DK1315)

09-Dec-1993 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-250-20-2 (UH-60-95-ASAM-04)REDUCTION OF TORQUE OF SELFRESTRAINING BOLTS. (HW6012)

06-Jan-1994 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-139 (UH-60-94-ASAM-01) NVGCOMPATABILITY REWORK OF MASTERWARNING PANEL ASSY AT 4541 ACFT HRS.(RS5598)

10-Jan-1994 1

FT. RUCKER, AL

QC000000

AVSCOM OCM SECTIONOCM/ACE PERFORMED AT 4541 AC HRS ATFT. RUCKER, AL. BY 'A' (AB0000)

11-Jan-1994 1

ST. LOUIS, MO

QC000000

USAAVNC,TB 1-1520-237-20-149 (UH-60-94-ASAM-02)RETURN FOR EXCHANGE OF CERTAIN (ARA)MFG BUCKLE/CROTCH STRAP ASSY. (RB0303)

19-Jan-1994 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-151 (UH-60-94-ASAM-03) ONETIME REFURBISHMENT OF M/R SPINDLES &REPL OF CERTAIN M/R THRUST BEARINGS.(AL6539)

19-Jan-1994 2

FT. RUCKER, AL

QC000000

USAAVNC,UH-60-94-ASAM-04 REISSUE OF ONE TIMEINSP TO REMOVE SUSPECT TAIL ROTORPITCH BEAMS. ACFT HRS 4654. (DA0358)

14-Feb-1994 1

FT. RUCKER, AL

QC000000



8.7.DATE

6.REMARKS

4. 5.



USAAVNC,TB 1-1520-237-20-150 (UH-60-94-ASAM-06)COCKPIT STANDARDIZATION OF PILOT & CO-PILOT RESTRING RELEASE SYSTEM. ACFTHRS 4674. (NW6012)

15-Feb-1994 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-152 (UH-60-94-ASAM-05) ONETIME REMOVAL OF T/R GEARBOXES WITHOUTPUT SHAFT P/N 70358-06620-101 FORREWORK. ACFT HRS 4670. (DA0358)

15-Feb-1994 2

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-154 (UH-60-94-ASAM-07/08)CHANGE TO H-60 OVERHAUL RETIREMENTTABLE. (RS5598)

25-Mar-1994 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-155 (UH-60-94-ASAM-09)REMOVAL OF CERTAIN PRIMARY SERVOASSYS. (RS5598)

06-Apr-1994 1

FT. RUCKER, AL

QC000000

USAAVNC,500 HR PHASE 10 COMPLETED AT 4988 A/CHRS. (LS6188)

19-Aug-1994 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-159 (UH-60-95-ASAM-02)OPERATE WITH FUEL TANK SUBMERGEDBOOST PUMP ON AT ALL TIMES WITH ALLFUELS DURING GROUND & FLT OPERATIONS.(RS5598)

01-Nov-1994 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-158 (UH-60-95-ASAM-03)RESHIMMING OF T/R PIVOT BEARINGS.(HW6012)

26-Nov-1994 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-162 (UH-60-95-SOF-01)THREE PART INSP PROCEDURE FOR T/RGEARBOX OUTPUT SHAFTS. (CR0600)

07-Dec-1994 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-163 (UH-60-ASAM-05)CHANGE IN RETIREMENT LIFE FOR SERVOBEAM RAILINGS. (TF1038)

28-Jan-1995 1

FT. RUCKER, AL

QC000000

AVSCOM OCM SECTIONOCM/ACE PERFORMED AT 5278 AC HRS ATFT. RUCKER, AL BY 'C' (JH0000)

04-Feb-1995 1

ST. LOUIS, MO.

QC000000

USAAVNC,TB 1-1520-237-20-153 REISSUE OF ONE TIMEINSPECTION TO REMOVE SUSPECT T/R PITCHCHANGE SHAFTS. (GH0000)

31-Mar-1995 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-166 REISSUE OF ONE TIMEINSP TO REMOVE SUSPECT T/R PITCHCHANGE SHAFTS. NA DUE TO S/N 5487.8ACFT HRS. (MB1851)

17-Jul-1995 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-168 ONE TIME INSPCRACKED MAIN XMSN BEAMS, UPPER DECKSKIN CRACKS, FRAME CRACKS C/W AT 5487.8ACFT HRS. (MB1851)

08-Sep-1995 1

FT. RUCKER, AL

QC000000

USAAVNC,500 HR PHASE INSP #11 COMPLETED AT5487.8 ACFT HRS (MB1851)

20-Sep-1995 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-164 (UH-60-95-ASAM-07) ONETIME INSP OF TROOP/GUNNER SEATATTENUATION WIRES & ANNENUATORROLLERS C/W 5487.8 ACFT HRS. (MB1851)

21-Sep-1995 1

FT. RUCKER, AL

QC000000



8.7.DATE

6.REMARKS

4. 5.



USAAVNC,TB 1-1520-237-20-172 (SOF UH-60-96-01)CHANGE IN RETIREMENT LIFE AND REMOVALOF SPECIFIED SN SUPPORTS CW AT 5535.9ACFT HRS. (MB1851)

07-Nov-1995 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-173 (SOF UH-60-96-02) ONETIME INSP FOR SUSPECT T/R INBOARDRETENTION PLATES. (JA8930)

27-Nov-1995 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-174 (SOF UH-60-96-03)CHANGE IN RETIREMENT LIFE OF M/R BLADECUFFS. (SR1657)

05-Dec-1995 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-175 (SOF UH-60-96-04)REMOVAL OF SPECIFIC S/N AFT BELLCRANKSUPPORT ASSY'S PN 70400-08117-049(RB4443)

15-Dec-1995 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-171 (SOF UH-60-96-01) ONETIME INSP FOR SUSPECT M/R SHAFT NUTBOLTS. (SR1657)

06-Jan-1996 1

FT. RUCKER, AL

QC000000

USAAVNC,OCM/ACE PERFORMED AT 5700 AC HRS ATFT. RUCKER AL. BY 'D' (MQ0000)

15-Feb-1996 1

FT. RUCKER, AL

QC000000

USAAVNC,AWR DATED 12 OCT 95, VIBRATIONMANAGEMENT ENHANCEMENT PROGRAM(VMEP) INSTALLATION. (SR1657)

20-Feb-1996 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-172 (UH-60-ASAM-05)REVISED INCREASE IN FATIGUE LIFE OF THEFORWARD BELLCRANK SUPPORT ASSY PN70400-08116-048 (PP1803)

15-Jul-1996 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-178 (UH-60-96-ASAM-08)INCREASE IN FATIGUE LIFE OF CERTAIN T/RINBOARD RETENTION PLATES. AT 5986 ACFTHRS. (PP1803)

28-Aug-1996 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-180 (UH-60-96-ASAM-09)VISUAL INSP STABILATOR CLEVISES FORTHE APPLICATION OF EPOXY PRIMER C/W. AT5986.4 ACFT HRS. (PP1803)

16-Sep-1996 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-182 (UH-60-96-ASAM-10)ESTABLISH THE REQUIREMENTS FORREPLACEMENT OF THE TEFLON SLEEVE INTHE SHPERICAL ELASTOMERIC BEARINGASSY AT EVERY 500 HR PMS-2 INSPECTION.(PP1803)

17-Sep-1996 1

FT. RUCKER, AL

QC000000

CCADUH-60-97-ASAM-01/TB 1-1520-237-20-181 ASSYP/N 70103-08112-041/045 "SUPERCEDED BY UH-60-02-SOF-06" (DA7660)

15-Oct-1996 1

CORPC, TX. 78419-5260

QC000000

USAAVNC,500 HR INSP #12 COMPLETED AT 5986.4 ACFTHRS. (PP1803)

17-Oct-1996 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-184 (UH-60-97-ASAM-02) ONETIME INSP OF TAIL DRIVE FLEXIBLECOUPLING CONNECTIONS C/W AT 5986.4ACFT HRS. (PP1803)

26-Oct-1996 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-157 (UH-60-95-ASAM-01)HOISTING AND AERIAL RECOVERING OF UH-60/ESSS FIXED PROVISIONED HELICOPTER.(PP1803)

31-Oct-1996 1

FT. RUCKER, AL

QC000000



8.7.DATE

6.REMARKS

4. 5.



CCADUH-60-97-SOF-01/TB 1-1520-237-20-185REMOVAL OF CERTAIN REWORKED M/RSWASHPLATE ASSY'S (DA7660)

18-Dec-1996 1

CORPC, TX. 78419-5260

QC000000

USAAVNC,ACFT OPERATING UNDER AWR DATED 03 SEP96 SLAB BATTERY. (PP1803)

07-Jan-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-189 (UH-60-97-ASAM-06) INSPAND REMOVAL OF CERTAIN LATERALBELLCRANK ASSY'S MFG'D BY PURDY MFGCO. (PP1803)

08-Jan-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,GEN 97-ASAM-03, CHANGE OF PROCEDURESFOR LOADING THE CRYPTO KEYS INNAVSTAR AN/ASN-149 GLOBAL POSITIONINGSYSTEM RECEIVERS. (PP1803)

08-Jan-1997 2

FT. RUCKER, AL

QC000000

USAAVNC,ACFT OPERATING UNDER AWR DATED 20DEC 96 HAVE QUICK II RADIO. (PP1803)

08-Jan-1997 3

FT. RUCKER, AL

QC000000

USAAVNC,ACFT OPERATING UNDER AWR DATED 20DEC 96 ELT. (PP1803)

08-Jan-1997 4

FT. RUCKER, AL

QC000000

USAAVNC,ACFT OPERATING UNDER AWR DATED 09 FEB96 VMEP. (PP1803)

09-Jan-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-23-3 (UH-60-97-ASAM-05) ONETIME INSP FOR REMOVAL AND REWORK OFCERTAIN VISCOUS DAMPER BEARINGSUPPORT ASSY'S C/W. (PP1803)

09-Jan-1997 2

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-188 (UH-60-97-ASAM-07)INSP/ REPLACEMENT OF SPECIFIC S/N T/RSERVOCYLINDER UNDER ASSY'S P/N 2227000-9,13,17. (PP1803)

14-Jan-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-187 (UH-60-97-ASAM-08) INSPAND REMOVAL OF CERTAIN CONNECTINGLINK ASSY'S. (PP1803)

18-Jan-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-190 (UH-60-97-ASAM-09) INSPFOR CHANGE TO FINITE LIFE OF CERTAIN M/RSHAFT EXTENSION ASSY'S. C/W. (PP1803)

23-Jan-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-191 (UH-60-97-ASAM-10)ESTABLISHMENT OF FATIGUE LIFE FORCERTAIN MAIN SUPPORT BRIDGES. (PP1803)

13-Feb-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-192 (UH-60-97-ASAM-11)INCREASE IN FATIGUE LIFE FOR CERTAIN M/RBLADE CUFFS, PN: 70150-09109-041/043 C/WAT 6118.3 ACFT HRS. (RR4443)

03-Mar-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,J ACE PERFORMED AT 6237 A/C HRS AT FT.RUCKER, AL.BY TEAM MEMBER 'N' (DS5651)

04-Jun-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-194 (UH-60-97-ASAM-13) ONETIME INSP OF SPINDLE SPHERICALELASTOMERIC BEARINGS C.WAT 6237.1 ACFTHRS. (RR4443)

24-Jun-1997 1

FT. RUCKER, AL

QC000000

CCADUH-60-97-ASAM-16/TB 1-1520-237-20-198 INSPOF SWASHPLATE CLEVIS CONNECTOR P/N70400-08151-050, REPL ALL SWASHPLATELINKS MFG BY AIRBORNE APPAREL CAGE2A622 (DA7660)

08-Aug-1997 1

CORPC, TX. 78419-5260

QC000000



8.7.DATE

6.REMARKS

4. 5.



USAAVNC,TB 1-1520-237-20-195 (UH-60-97-ASAM-14) INSPOF BELLCRANK SUPPORT PN 70400-08158-101MANUFACTURED BY AMERICAN GENERAL1W160. (DK1063)

21-Aug-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-196 (UH-60-97-ASAM-15) INSPOF BRNG ROD END PN 70101-08202-101,MANUFACTURED BY ISLAND ENGINEERING40137. (DK1063)

21-Aug-1997 2

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-201 (UH-60-97-ASAM-18)REMOVAL OFCERTAIN REWORKED M/RSWASHPLATE ASSY'S. C/W AT 6406 ACFTHRS. (DK1063)

12-Sep-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-204 (UH-60-97-ASAM-19) ONETIME INSP OF ANVIS/HEAD POWER SUPPLYC/W AT 6428 ACFT HRS. (DK1063)

02-Oct-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-202 (UH-60-98-ASAM-01)REVISION TO THE SERVICE LIFE OF M/RSHAFT EXTENDERS MFG'D BY PURDY MFGCO. C/W AT 6447 ACFT HRS. (DK1063)

07-Oct-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-197 (UH-60-98-ASAM-02) INSPOF UH-60 ACFT WITH PUSHRODS MFG BYVERSATILE MACHINING, CAGE 65522 C/S AT6457 ACFT HRS. (DK1063)

15-Oct-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-203 (UH-60-98-ASAM-03) ALLUH-60 AIRCRAFT WITH THE SWASHPLATELINK ASSY P/N 70400-08110-054MANUFACTURED BY TEK (CAGE CODE 65780)C/W AT 6471.9 ACFT HRS. (RR4506)

04-Nov-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,500 HR PMS-2 INSP #13 COMPLETED AT 6471.9ACFT HRS (RR4506)

01-Dec-1997 1

FT. RUCKER, AL

QC000000

USAAVNC,500 HR INSP #13 COMPLETED AT 6471.9 ACFTHRS (RR4506)

01-Dec-1997 2

FT. RUCKER, AL

QC000000

USAAVNC,AIRCRAFT HISTORICAL RECORDSCONVERTED TO AUTOMATED SYSTEM.ENTERIES PRIOR TO 13 JAN 98 CAN BEFOUND IN HISTORICAL RECORDS ON FILE INRECORDS SECTION ON SITE. (TE1038)

13-Jan-1998 1

FT. RUCKER, AL

QC000000

CCADUH-60-98-SOF-01/TB 1-1520-237-20-228 RISKMANAGEMENT OF 230 GALLON EXTERNALTANK FLT OPS. (DA7660)

27-Jan-1998 1

CORPC, TX. 78419-5260

QC000000

USAAVNC,TB 1-1520-237-20-205 (UH-60-98-ASAM-04),INSP FOR LOOSE HUCK BOLTS ONOVERHAULED PRIMARY, YAWBOOST,COLLECTIVE BOOST, AND T/RSERVOS, C/W AT 6607 ACFTHRS. (DK1063)

16-Mar-1998 1

FT. RUCKER, AL

QC000000

USAAVNC,OCM/JACE PERFORMED AT 6616 A/C HR. ATFT RUCKER ALBY ACE MEMBER D AMCOM OCSEC, HUNTSVILLE, AL. (LS0000)

24-Mar-1998 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-203 (UH-60-98-ASAM-05),INSP OF UH60 ACFT WITH SWASHPLATE LINKPN 70400-08110-054/061 MFGD BY TEK (CAGE65780) C/W AT 6616 ACFT HRS. (DK1063)

01-May-1998 1

FT. RUCKER, AL

QC000000



8.7.DATE

6.REMARKS

4. 5.



USAAVNC,TB 1-1520-237-20-206 (UH-60-98-ASAM-07)LEFT TIE ROD P/N 70400-08115-043 MFG'D BYARGENCORD C/W AT 6762.2 ACFT HRS.(PP1803)

19-Sep-1998 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-208 (UH-60-99-ASAM-01)RESTORATION OF FULL SERVICE LIFE ONTHE SWASHPLATE LINK ASSY P/N: 70400-08110-054/061, MFG'D BY TEK (CAGE CODE65780) C/W AT 6819.3 ACFT HRS. (RR4443)

05-Nov-1998 1

FT. RUCKER, AL

QC000000

CCADUH-60-99-ASAM-06/TB 1-1520-237-20-210 INSP& REVISED RETIREMENT LIFE OF M/R HORNASSY P/N 70102-08111-047 (DA7660)

10-Dec-1998 1

CORPC, TX. 78419-5260

QC000000

USAAVNC,JACE/CPCE PERFORMED AT 6933 ACFT HRS.BY PROJECT OLR/DYNCORP (FTCKY)PROFILER GG. (SR4681)

19-Feb-1999 1

FT. RUCKER, AL

QC000000

USAAVNC,JACE/CPCE PERFORMED AT 6933 ACFT HRS.BY PROJECT OLR/DYNCORP (FTCKY)PROFILER GG. (SR4681)

19-Feb-1999 2

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-167 ONE TIME INSP OFSTA.635 FRAME ASSY. FOR TAIL STRUTINSTL. CLEARANCE C/W AT 6971.8 ACFT HRS.(RR4443)

08-Apr-1999 1

FT. RUCKER, AL

QC000000

USAAVNC,500 PHASE INSPECTION PMS-2 #14COMPLETED AT 6971.8ACFT HRS. PMS-2 #15DUE AT 7471.8 ACFT HRS. (RR4443)

07-May-1999 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-213 (UH-60-99-ASAM-10)INSP. AND PREVENTIVE MAINT. ON THENUMBER TWO CROSSFEED BREAKAWAYVALVE (P/N 70307-0306-103) C/W AT7165.0ACFT. HRS. (MA4187)

31-Jul-1999 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-2840-248-20-23 (UH-60-99-ASAM-11) ONETIME INSP OF T700-GE-700/701/701C ENGINESC/W AT 7167.9ACFT. HRS. ON ENG.#1: GE-E-307349 & ENG.#2: GE-E- 207478. (MA4187)

03-Aug-1999 1

FT. RUCKER, AL

QC000000

USAAVNC,#2 CROSSFEED BREAKAWAY VALVEREPLACED I/A/W TB 1- 1520-237-20-213 THISDATE AT 7170.1 ACFT. HRS. (RR4443)

04-Aug-1999 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-216 (UH-60-99-ASAM-02)CYCLIC STICK WIRING BUNDLE RELOCATIONC/W AT 7401.7 ACFT HRS. (RR4443)

15-Dec-1999 1

FT. RUCKER, AL

QC000000

CCADUH-60-00-ASAM-03/TB 1-1520-237-20-217 INSP& REMOVAL OF SUSPECT PRIMARY SERVOASSY'S (DA7660)

29-Dec-1999 1

CORPC, TX. 78419-5260

QC000000

USAAVNC,TB 1-1520-237-20-218 (UH-60-00-ASAM-04)INSPECTION OF TAIL LANDING GEAR STRUTASSY FOR MISSING BEARING RETENTION PINC/W AT 7472.0 ACFT HRS. TAILSTRUT SN:C002-00145 (RR4443)

15-Mar-2000 1

FT. RUCKER, AL

QC000000



8.7.DATE

6.REMARKS

4. 5.



USAAVNC,ACFT M/R HEAD RIGGED IAW SA DWG 70400-0003 REV. E SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A. AFT CONTROL SERVOINPUT ROD HAS BEEN LENGTHENED 3/4TURNS. B. LATERAL CONTROL SERVO INPUTROD NO CHANGES. C. FORWARD CONTROLSERVO INPUT ROD HAS BEEN SHORTENED3/4 TURNS. C/W AT 7472.0 ACFT HRS. (RR4443)

16-Mar-2000 1

FT. RUCKER, AL

QC000000

USAAVNC,500 HOUR PHASE INSPECTION PMS-2 #15COMPLETED AT 7472.0 ACFT HRS; NEXT PMS-2 #16 DUE AT 7972.0 ACFTHRS. (RR4443)

17-Mar-2000 1

FT. RUCKER, AL

QC000000

USAAVNC,OCM/ACE PERFORMED AT 7488 ACFT HRS BYTEAM MEMBER (J) AMCOM/OLR FTCKY.(RR4443)

13-Apr-2000 1

FT. RUCKER, AL

QC000000

USAAVNC,ACFT M/R HEAD RIGGED IAW SA DWG 70400-00003 REV E.SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A. AFT CONTROL SERVOINPUT ROD HAS BEEN SHORTENED 3/4 TURN.B. LATERAL CONTROL SERVO INPUT RODHAS BEEN SHORTENED 1/4 TURN. C.FORWARD CONTROL SERVO INPUT ROD HASBEEN LENGTHENED 3/4 TURN. C/W AT 7487.6ACFT HRS. (RR4443)

24-Apr-2000 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-219 (UH-60-00-ASAM-05)INSPECTION OF FIRE EXTINGUISHER WIRINGC/W AT 7508.8 ACFT HRS. (N/A THIS ACFT)(RR4443)

18-May-2000 1

FT. RUCKER, AL

QC000000

USAAVNC,ONE TIME AND RECURRING INSPECTION OFBOOST SERVO AND PILOT ASSIST MODULEMANIFOLD BASE PLATE I/A/W DYN PROCESSCONTROL #UH60-00-01 COMPLETED AT 7576.6ACFT HRS. (RR4443)

07-Jun-2000 1

FT. RUCKER, AL

QC000000

CCADUH-60-00-SOF-02/TB 1-1520-237-20-222REMOVAL OF INPUT MODULE GEARBOXASSY'S WIYH POTENTIALLY CRACKED BEVELGEARS (DA7660)

02-Aug-2000 1

CORPC, TX. 78419-5260

QC000000

USAAVNC,TB 1-1520-237-20-224 (UH-60-00-ASAM-07) ONETIME INSPECTION OF WIRE HARNESSESCONNECTING THE #1 & #2 JUNCTION BOXESC/W AT 7812.8 ACFT HRS. (N/A FOR THISACFT) (RR4443)

01-Sep-2000 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-225 (SOF UH-60-01-01)INITIAL AND RECURRING INSP OF THE MLGDRAG BEAM ASSY AND DECREASE TORQUEON THE JACKPAD NUT C/W AT 7897.0 ACFTHRS. (RR4443)

06-Nov-2000 1

FT. RUCKER, AL

QC000000

CCADUH-60-01-SOF-03/TB 1-1520-237-20-229REMOVAL OF SPECIFIC LATERAL SERVOBELLCRANK ASSY P/N 70400-08150-045 MFGBY PURDY CORP CAGE 15152 (DA7660)

05-Jan-2001 1

CORPC, TX. 78419-5260

QC000000

USAAVNC,SOF UH-60-01-04 (TB 1-1520-237-20-228) RISKMANAGEMENT OF 230 GALLON EXTERNALTANK FLIGHT OPERATIONS C/W AT 7971.1ACFT HRS. (RR4443)

09-Jan-2001 1

FT. RUCKER, AL

QC000000



8.7.DATE

6.REMARKS

4. 5.



USAAVNC,UH-60-01-02 (TB 1-1520-237-20-225) REVISIONTO SOF UH-60-01-01 (TB 1-1520-237-20-225)INITIAL AND RECURRING INSPECTION OF THEMAIN LANDING GEAR DRAG BEAM ASSY. ANDDECREASE TORQUE ON THE JACKPAD NUTC/W AT 7971.1 ACFT HRS. (RR4443)

10-Jan-2001 1

FT. RUCKER, AL

QC000000

CCADUH-60-01-SOF-05/TB 1-1520-237-20-230INSPECTION OF M/R SPINDLE "REVISION TOUH-60-00-SOF-01" (DA7660)

05-Mar-2001 1

CORPC, TX. 78419-5260

QC000000

USAAVNC,TB 55-2840-248-50-48 (UH-60-01) ONE TIMEINSPECTION OF ENGINE GAS GENERATORSTATOR SHROUD C/W ON #2 ENGINE.(FP7867)

17-May-2001 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-232 (SOF UH-60-01-07), INSPOF MAIN ROTOR FLIGHT CONTROL SELFLOCKING BOLTS C/W AT 7971.1 ACFT HRS.(BA2721)

07-Jun-2001 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-232 (SOF UH-60-01-08), INSPOF MAIN ROTOR FLIGHT CONTROL SELFLOCKING BOLTS C/W AT 7971.1 ACFT HRS.(BA2721)

07-Jun-2001 2

FT. RUCKER, AL

QC000000

USAAVNC,ACFT M/R HEAD RIGGED I/A/W WITH SA DWG70400-00003REV. E. SYSTEM CONTROLS HAVEBEEN BIASED IN ACCORDA. PRIMARY SERVOCONTROL ROD BIAS FWD: 1 TURN SHORTENAFT: 1 TURN LENGTHEN, LATERAL: 1/2 TURNSHORTEN. PITCH/TRIM 0 ADJUSTMENTS. T/RCABLE TENSION LEFT: 162 LBS AT 20DEGREES C. RIGHT 161 LBS. (TB1027)

13-Jun-2001 1

FT. RUCKER, AL

QC000000

USAAVNC,PMS-2 PHASE INSPECTION #16 COMPLETEDAT 7971.1 ACFT HRS PMS-2 PHASEINSPECTION #17 DUE AT 8471.1 ACFT HRS.(TB1027)

19-Jun-2001 1

FT. RUCKER, AL

QC000000

USAAVNC,GEN-MIM-01-005 INSPECTION ANDIDENTIFICATION OF ACFT WITH RECEIVERTRANSMITTERS (RT) WHICH REQUIREUPGRADES. COMPLETED AT 7975.6 ACFTHRS. (TB1027)

11-Jul-2001 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-241 (SOF UH-60-02-03) ONETIME INSP OF FLIGHT CONTROL SYSTEMPITCH TRIM ASSY COMPLETED AT 8002.1ACFT HRS. (TB1027)

11-Dec-2001 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-242 (SOF UH-60-02-04) INSPOF APU FUEL LINES FOR PROPER GROMMETAT APU SHROUD ASSY COMPLETED AT 8002.1ACFT HRS. (TB1027)

24-Jan-2002 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-246 (UH-60-02-ASAM-02)INITIAL AND RECURRING INSPECTION OF THECONTROL ROD JAMNUT COMPLETED AT8002.1 ACFT HRS. (TB1027)

08-Feb-2002 1

FT. RUCKER, AL

QC000000

CCADUH-60-02-ASAM-03/TB 1-1520-237-20-245 INSPOF ENGINE CONTROL QUADRANT POWERCONTROL LEVER (PCL) WIRING (DA7660)

12-Feb-2002 1

CORPC, TX. 78419-5260

QC000000



8.7.DATE

6.REMARKS

4. 5.



USAAVNC,TB 1-1520-237-20-244 (UH-60-02-ASAM-04)RESTRAINT SYSTEM INSPECTION, C/W @8002.1 ACFT HRS (JB2761)

23-Mar-2002 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-252 (UH-60-02-ASAM-06)COLLECTIVE AND YAW BOOST SERVOASSEMBLIES SWAGE PIN COLLARSCOMPLETED AT 8030.2 ACFT HRS. (TB1027)

18-Apr-2002 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-256 (UH-60-02-ASAM-08) INSPOF AN/ARC-220 WIRING FOR CHAFING C/W @8119 ACFT HRS. (RM5140)

13-Jun-2002 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-257 (UH-60-02-ASAM-09) INSPOF T/R QUADRANT HARDWAREINSTALLATION C/W @ 8122.9 ACFT. HRS.(RM5140)

16-Jun-2002 1

FT. RUCKER, AL

QC000000

USAAVNC,OCM/ACE PERFORMED AT 8174 ACFT. HRS.BY TEAM MEMBER R AMCOM PROJECT OLRFT.C.KY. (TS0568)

01-Jul-2002 1

FT. RUCKER, AL

QC000000

USAAVNC,TB 1-1520-237-20-261 (UH-60-02-ASAM-11)INSPECT AN/ARC-220 WIRING FOR CHAFINGC/W AT 8368.7 ACFT HRS. (RM5140)

24-Sep-2002 1

FT. RUCKER, AL

QC000000

USAAVNC,UH-60-03-ASAM-01 FWD BELLCRANKSUPPORT ASSY RETIREMENT LIFE C/W AT8471 ACFT HRS. (RM5140)

09-Dec-2002 1

FT. RUCKER, AL

QC000000

USAAVNC,UH-60-03-ASAM-02 TAIL ROTOR SERVO ASSYRETIREMENT LIFE C/W AT 8471 ACFT HRS.(RM5140)

09-Dec-2002 2

FT. RUCKER, AL

QC000000

USAAVNC,GEN-03-ASAM-01 (SINGARS) ARC-201BATTERY BOX AT 8470.7 ACFT HRS. (RM5140)

17-Dec-2002 1

FT. RUCKER, AL

QC000000

USAAVNC,PMS-2 #17 COMPLETED @ 8470.7 ACFT. HRS.NEXT PMS #18 DUE @ 8970.7 ACFT. HRS.(GA0000)

24-Jan-2003 1

FT. RUCKER, AL

QC000000

USAAVNC,OCM/ACE PERFROM AT 8774 ACFT HRS BYTEAM MEMBER J AMCOM/OLR FT.C KY(FS6922)

23-Jun-2003 1

FT. RUCKER, AL

QC000000

CCADACFT INDUCTED INTORECAPITALIZATION/REBUILD PROGRAM ONTHIS DATE AT 8961.7 ACFT HRS @ CCAD. ALLXFER CRITERIA MET IAW TM 1-1500-228-23.(EC7788)

31-Oct-2003 1

CORPUS CHRISTI,TX.

QC000000

CCADAIRCRAFT STRIPPED AND PAINTED IAW TM 1-1500-345-23 EXTERIOR PAINTED CARC, MIL-L-46168, CREW COMPART. PAINTEDLUSTERLESS BLACK (CARC MIL-L-46168,TROOP/CARGO AREA LUSTERLESS GRAY,CARC, MIL-L-46168. (GC2172)

08-Nov-2004 1

CORPUS CHRISTI, TX.78412

QC000000

CCADACFT COMPLETEDRECAPITALIZATION/REBUILD PROGRAM ONTHIS DATE AT 8961.7 ACFT HRS IAW SOW01OCT03 & TM 1-1500-328-32,COMBATOPERATIONS. (EC7788)

16-Nov-2004 1

CORPUS CHRISTI,TX.

QC000000

CCADJACE/ACE PERFORMED AT 8961.7 ACFT HRSAT CCAD, COPRUS CHRISTI,TX. (EC7788)

16-Nov-2004 2

CORPUS CHRISTI,TX.

QC000000



8.7.DATE

6.REMARKS

4. 5.



CCADALL PHASE INSP CRITERIA C/W IAW T 1-1500-328-23 @ 8961.7 ACFT HRS. NEXT PMS-2PHASE INSP DUE AT 9461.7 ACFT HRS.(EC7788)

16-Nov-2004 3

CORPUS CHRISTI,TX.

QC000000

CCADALL H-60 ACFT INCORPORATION OFCORROSION RESISTANCE ENHANCEMENTMODIFICATIONS IN CORROSION PRONEATEAS. (EC7788)

16-Nov-2004 4

CORPUS CHRISTI,TX.

QC000000

CCADAWR FOR FM IMMUNE AN/ARN-147 VOR/ILSRECEIVERS P/NAN/ARN-147 VOR/ILSRECEIVERS P/N 622-6376-020 IN THESTANDARD CONFIGURATION AND FM IMMUNEAN/ARN- 147 VOR/ILS RECEIVERS P/N 622-6376-020 WITH THE VIM-123 ADAPTER TRAYMOUNT IN AN/ARN-123 CONFIG- URED UH-60A/L & EH-60A AND CINC HAWKHELICOPTERS (AWR 917)(DTD 21DEC01)(EC7788)

16-Nov-2004 5

CORPUS CHRISTI,TX.

QC000000

CCADUH-60-04-ASAM-01 GLARE SHIELD LIGHTINGCIRCUIT BREAKER REPLACEMENT C/W(EC7788)

16-Nov-2004 6

CORPUS CHRISTI,TX.

QC000000

CCADUH-60-04-SOF-01 FWD BELLCRANK SUPPORTINSTALLATION HARDWARE C/W. (EC7788)

16-Nov-2004 7

CORPUS CHRISTI,TX.

QC000000

CCADUH-60-04-SOF-02 DISABLING OF COCKPITAIRBAG SYS. (CABS) C/W. (EC7788)

16-Nov-2004 8

CORPUS CHRISTI,TX.

QC000000

CCADISAQ FOR UH-60A & EH-60A HELICOPTERSWITH MAIN MODASSYS(P/N 70351-08100-075 &70351-08100-076)EQUIPPED WITH THEIMPROVED PLANETARY CARRIER ASSY,P/N70351-08175-046(ISAQ 106)(DTD06JAN04)(EC7788)

16-Nov-2004 9

CORPUS CHRISTI,TX.

QC000000

CCADUH-60-04-ASAM-02 TAIL ROTOR D/S FLANGENUT C/W (EC7788)

16-Nov-2004 10

CORPUS CHRISTI,TX.

QC000000

CCADUH-60-04-ASAM-03 FUEL SYS INTEGRITYCHECKS C/W (EC7788)

16-Nov-2004 11

CORPUS CHRISTI,TX.

QC000000

CCADUH-60-04-SOF-04 MR/HUB SUB ASSY REWORKC/W (EC7788)

16-Nov-2004 12

CORPUS CHRISTI,TX.

QC000000

CCADUH-60-04-ASAM-04 FUEL SYS INTEGRITYCHECKS C/W (EC7788)

16-Nov-2004 13

CORPUS CHRISTI,TX.

QC000000

CCADUH-60-04-ASAM-05 RESTRAINT SYSTEMINSPECTION C/W (EC7788)

16-Nov-2004 14

CORPUS CHRISTI,TX.

QC000000

AR AASFUH-60-05-ASAM-02 BLUE FORCE TRACKERCOMPLIED WITH,MWO 1-1520-237-50-BFT2/AWR 1206 NOT APPLIED (WW1514)

02-Mar-2005 1

CJTR, NLR, AR 72199-9600

QC000000

AR AASFUH-60-05-01 REACTIVEACTION OF COCKPITAIRBAG SYSTEM COMPLIED WITH. CABS NOTINSTALLED @ THIS LOCATION. (WW1514)

14-Mar-2005 1

CJTR, NLR, AR 72199-9600

QC000000

AR AASFAIRCRAFT PLACED ON ESM 04/15/2005 @9024.7 ACFT HRS, PMI #1 DUE @9311.7 ACFTHRS. (MB9758)

14-Apr-2005 1

CJTR, NLR, AR 72199-9600

QC000000



8.7.DATE

6.REMARKS

4. 5.



AR AASFUH-60-05-ASAM-03 AIRCREW RESTRAINTSYSTEM COMPATIBILITY COMPLIED WITH(WW1514)

21-Apr-2005 1

CJTR, NLR, AR 72199-9600

QC000000

AR AASFUH-60-05-ASAM-04 TAIL LANDING GEAR YOKEASSY. COMPLIED WITH (WW1514)

21-Apr-2005 2

CJTR, NLR, AR 72199-9600

QC000000

AR AASFUH-60-05-ASAM-06 TROOP SEAT RESTRAINTBUCKLES COMPLIED WITH @ 9041.2 ACFTHRS (WW1514)

03-Jun-2005 1

CJTR, NLR, AR 72199-9600

QC000000

AR AASFUH-60-05-ASAM-07 AIR INTRUSION OFHYDRAULIC SYSTEM COMPLIED WITH @9043.7 ACFT HRS (WW1514)

05-Jun-2005 1

CJTR, NLR, AR 72199-9600

QC000000

AR AASFUH-60-05-ASAM-09 CEFS INSTALLATIONBOLTS COMPLIED WITH MWO'S NOT APPLIEDAT THIS TIME. (WW1514)

03-Aug-2005 1

CJTR, NLR, AR 72199-9600

QC000000

AR AASFUH-60-05-ASAM-10 ENGINE OUTPUT SHAFTCOMPLETED N/A BY SERIAL NUMBERS(WW1514)

09-Aug-2005 1

CJTR, NLR, AR 72199-9600

QC000000

D CO 1-131 AVN BNMILES INSTALLATION COMPLETE PER AWRDTD 2APR04 SUCESSFUL COMPLETION OFEMC CHECK ON 17AUG05 THIS IS ATEMPORARY INSTALLATION (MF3926)

17-Aug-2005 1

POE

QC000000

DYNCORPINTERNATIONAL

ACE/CPCE PERFORMED AT 9213 ACFT HRSBY TEAM MEMBERS K & W AMCOM PROJECTOLR (JP2527)

30-Sep-2005 1

CJTR,NLR,AR 72199-9600

QC000000

AR AASFUH-60-06-ASAM-01 TAIL LANDING GEARSHOCK STRUT INSPECTION COMPLETED @9213.4 ACFT HRS. (WW1514)

15-Dec-2005 1

CJTR NLR, AR 72199-9600

QC000000

AR AASFUPDATED ENTRY FOR AWR'S: THEFOLLOWING AWR'S APPLY TO THISAIRFRAME, ELT R4 DTD 1 APR 92, AWR 913 R3DTD 1 AUG 03, AWR 1076 R3 DTD 12 DEC03,AWR 1097 R4 DTD 29 JUN 05, AWR 1270DTD 26 MAY 05, AWR 1299 R1 DTD 30 SEP 05AND AWR 1300 R3 DTD 22 DEC 05 (WW1514)

01-Jan-2006 1

CAMP ROBINSON NLR,AR 72199

QC000000


UH-60-05-ASAM-11 ANTI CHAFF GROMMETINSPECTION C/W @ 9255.6 ACFT HRS.(RH4356)

29-Mar-2006 1

FT. CAMPBELL KY42223

QC000000


UH-60-05-ASAM-01 FUEL SYSTEM INTERGRITYCK COMPLIED WITH THIS DATE.

25-Apr-2006 1

FT. HOOD TX 76542

QC000000

AR AASFAIRCRAFT ENTERED INTO SCP-6 AUTO.RECORDS PROGRAM

09-May-2006 1

CJTR,NLR,AR

QC000000


ACE/CPCE PERFORMED AT 9263 ACFT HRSBY TEAM MEMBER S C & W AMCOM PROJECTOLR

19-May-2006 1

WEST FORT HOOD,TX

QC000000



8.7.DATE

6.REMARKS

4. 5.




PMI #1 COMPLETED @ AT 9262.9 HRS NEXTDUE PMI2 @ 9622.9 ACFT HRS

30-May-2006 1

WEST FORT HOOD, TX

QC000000


UH-60-06-ASAM-02 M/R PITCH CONTROL RODJAMNUTS INSPECTED AND TREATED FORCORROSION COMPLETED 30 MAY 2006 @9262.9 ACFT HRS.

30-May-2006 2

WEST FORT HOOD,TX

QC000000


INTERIM STATEMENT OR AIRWORTHNESSQUALIFICATION APPLIED FOR ALL UH-60A/LACFT EQUIPPED WITH THE AIR WERRIORMICROCLIMATE COOLING SYSTEM IAW (ISAQ114) DATED 28 JAN 05

21-Jun-2006 1

KILLEEN TX 76543

QC000000

D CO 1-131 AVN BNUH-60-06-ASAM-04 DISABLING COCKPITAIRBAG SYSTEM C/W 25 JUN 2006 @ 9278.9ACFT HRS. CAB NOT INSTALLED ( CR199703 )

25-Jun-2006 1

FORT HOOD, TX

QC000000

D CO 1-131 AVN BNUH-60-06-SOF-02 DISABLING COCKPITAIRBAG SYSTEM C/W 25 JUN 2006 @ 9278.9ACFT HRS. CAB NOT INSTALLED ( CR199703)

25-Jun-2006 2

FORT HOOD, TX

QC000000

D CO 1-131 AVN BNACFT FOLDED AND RECONFIGURED FORTRANSPORTATION ON SHIP TO KUWAIT INSUPPORT OF OIF.

29-Aug-2006 1

UDARI ARMY AIRFIELD,KUWAIT

QC000000

D CO 1-131 AVN BNEMC CHECKS FOR INSTALLATION OF DESERTMODS COMPLETED ON A/C 8524405

01-Sep-2006 1

UAAF

QC000000

D CO 1-131 AVN BNUH-60-06-ASAM-05 BLUE FORCE TRACKERHARDWARE INSTALLATION C/W 29 AUG 2006@ 9299.1 ACFT HRS

08-Sep-2006 1

UAAF, KUWAIT

QC000000

D CO 1-131 AVN BNUH-60-06-ASAM-03, SWASHPLATE DUPLEXBEARING C/W 12 OCT 06 @ 9368.0 ACFT HRS.READING WAS .05.

13-Oct-2006 1

BALAD, IRAQ

QC000000

D CO 1-131 AVN BNT/R INBOARD RETENTION PLATEREPLACEMENT AND RIG CHECK AT 9396.9ACFT HRS. RED W/O BIAS 4.5W/BIAS4.8DIFF.0.3 YELLOW W/O BIAS 4.199 W/BIAS 4.509DIFF. 0.31 BLACK W/O BIAS 4.839 W/ BIAS5.129DIFF. 0.29 BLUE W/O BIAS 4.798 W/ BIAS5.128 DIFF. 0.33 (PT721546)

25-Oct-2006 1

BALAD IRAQ

QC000000

D CO 1-131 AVN BNUH-60-07-ASAM-01 #1 AND #2 ENG WHITEHARNESS INSP C/W @ 9474.1 ACFT HRS

02-Dec-2006 1

BALAD IRAQ

QC000000

D CO 1-131 AVN BNUH-60-07-ASAM-03 INSP OF COLL AND YAWBOOST SERVO INPUT ARMS FOR PRESENCEOF ROLL PIN INSTALLED C/W @ 9522.5 ACFTHRS.

23-Dec-2006 1

BALAD, IRAQ

QC000000

D CO 1-131 AVN BNUH-60-07-ASAM-02 ADMENDMENT TO UH-60-07-ASAM-01 COMPLIED WITH @ 9526.7 ACFTHRS.

27-Dec-2006 1

BALAD, IRAQ

QC000000

D CO 1-131 AVN BNCOMPLIED WITH UH-60-07-ASAM-04 30-Dec-2006 1

BALAD IRAQ

QC000000



8.7.DATE

6.REMARKS

4. 5.



D CO 1-131 AVN BNTEMPORARY REPAIR TO R/H LOWER CARGODOOR TRACK PER MEC LE-BAL014-0446 @9556 ACFT HRS. PERMANENT REPAIR TO BEACCOMPLISHED AT THE NEXT PMI @ 10225ACFT HRS.

01-Jan-2007 1

BALAD,IRAQ

QC000000

D CO 1-131 AVN BNR/H CARGO DOOR HAS BULLET HOLE-REPAIRED PER MEC LE-BAL014-0449

02-Jan-2007 1

BALAD,IRAQ

QC000000

D CO 1-131 AVN BNUH-60-07-ASAM-05 ARC-220 POWER UPPROCEDURES COMPLIED WITH @ 9596.9ACFT HRS.

23-Jan-2007 1

LSA ANACONDA,BALAD, IRAQ

QC000000

D CO 1-131 AVN BNMAIN ROTOR RIG COMPLETED DURING PMI-2@ 9596.9 LATERAL PRIMARY SERVO SHORT1/3 TURN. L3 VERTEX BALAD, IRAQ 20070205MT5955

06-Feb-2007 1

BALAD, IRAQ APO AE09391

QC000000

D CO 1-131 AVN BNT/R BIAS SET: RED 4.110 4.440 = 0.33BLUE 4.770 5.100 = 0.33YELLOW 4.090 4.420 = 0.33BLACK 4.760 5.090 = 0.33L3 VERTEX BALAD,IRAQ 20070205 MT5955

06-Feb-2007 2


QC000000

D CO 1-131 AVN BNPMI-2 COMPLETED AT 9596.9 ACFT HRS.NEXTPMI-1 DUE AT 9956.9 ACFT HRS.L3 VERTEXBALAD, IRAQ 20070205 MT5955

06-Feb-2007 3


QC000000

D CO 1-131 AVN BNUH-60-06-ASAM-02 M/R PITCH CONTROL RODJAMNUTS REPLACED @ PMI-2. 9596.9 ACFTHRS.

06-Feb-2007 4

BALAD, IRAQ

QC000000

D CO 1-131 AVN BNUH-60-07-ASAM-06 - EXTERNAL RESCUEHOIST - CABLE GUARD DEFLECTOR.COMPLIED WITH @ 9596.9 ACFT HRS. NOTINSTALLED ON THIS AIRCRAFT.

08-Feb-2007 1


QC000000



8.7.DATE

6.REMARKS

4. 5.



D CO 1-131 AVN BNMEC LETTER: LE-BAL014-0738 13 FEB 2007MAIN TRANSMISSION HOUSINGASSEMBLYSERIAL NUMBER: E211-00169 ISEXTENDED 40 HOURS TO ALIGN WITH THEPMI-1 @ 9956.9 ACFT HRS.AVIATIONENGINEERING DIRECTORATE HAS REVIEWEDREQUEST AND IT IS GRANTED. ONE FACTORIN DETERMINING A HOUSING LIFE EXTENSIONIS CONSIDERING HOW MUCH TIME THE MAINMODULE WAS OPERATED WHILE ESSS WASINSTALLED ON THE AIRCRAFT. THE UH60PROGRAM MANAGEMENT OFFICE PROVIDEDTHE INFORMATION: TIME ON HOUSING IS2682.0 HRS, OPERATED WITH ESSS 500 HRS(MAX). BASED UPON THE NUMBER OFHOURS THE MAIN MODULE OPERATED WHILEESSS WAS INSTALLED ON THE AIRCRAFT,THIS OFFICE IS ABLE TO GRANT THEREQUESTED EXTENSION OF 40 HOURS.ESSS/ERFS MAY NOT BE USED. THIS IS AONE TIME EXTENSION FOR THIS AIRCRAFTSERIAL NUMBER ONLY. EXTENSION IS TO BEANNOTATED IN APPROPRIATE PERMANENTA/C RECORD.REPAIR COORDINATEDTHROUGH AED, REFERENCE TTS41084.//ORIGINAL SIGNED//BILLMCCANDLESS, DB3 AEROSPACE ENGINEER,US ARMY RDECOM, AMSRD-AMR-AE-M DSN:312-992-3986, X7830, COM'L: 732-532-3986,X7380, TASM, APO AE 09391 [email protected]

16-Feb-2007 1

BALAD, IRAQ

QC000000

D CO 1-131 AVN BNUH-60-07-AMAM-01, COMMON MISSILEWARNING SYSTEM, COMPLIED WITH @ 9653.0ACFT HRS, 28 MARCH 2007. INSP A-895ENTERED INTO 2408-18.

28-Mar-2007 1

BALAD, IRAQ

QC000000

D CO 1-131 AVN BNACFT WIRING MOD TO ACCEPT THE PDMME-367-3 DIGITAL ELECTRONIC CLOCKSPREVIOUSLY C/W.

29-Mar-2007 1

BALAD, IRAQ

QC000000

D CO 1-131 AVN BNUH-60-07-ASAM-07, CEFS BONDING JUMPER,COMPLIED WITH @ 9765.1 ACFT HRS. N/ATHIS ACFT.

09-May-2007 1

BALAD, IRAQ

QC000000

D CO 1-131 AVN BNSTA 360.1 BL 16.4 FOUND CRACKED DURINGMAIN MODULE REPLACEMENT. 360 BEAMREPLACED BY CCAD IAW DMWR 1-1520-237-2, PG 4-326, TASK 2-2-03. REFERENCE LE-BAL015-0666

28-May-2007 1

BALAD IRAQ

QC000000

L3 VERTEXAEROSPACE

ACFT COMP RIG FOR REPL OF M/M AND T/RRIG AND BAIS COMP FOR PMI-1, @ACFT HRS9789.3 ACFT HRS NO ADJUSTMENTS MADEON FLTCONTROLS,RED=4.801=5.132=.331BLK=4.136=4.465=.329YEL=4.766=5.102=.338BLU=4.124=4.455=.331

07-Jun-2007 1

LAS ANACONDA BALADIRAQ

QC000000

L3 VERTEXAEROSPACE

PMI-1 COMP @9789.3 ACFT HRS NEXT PMI-2DUE @ 10149.3 ACFT HRS

08-Jun-2007 1

LAS ANACONDA BALADIRAQ

QC000000



8.7.DATE

6.REMARKS

4. 5.



D CO 1-131 AVN BNT/R BIAS CHECK. RED-W/O-BIAS-4.8, W/BIAS-5.16, DIFF-.331, YELLOW-W/OBIAS-4.81-W-BIAS-5.15-DIFF-.339, BLACK-W/O 4.19, W/BAIS-4.50,DIFF- .316, BLUE- W/O BIAS-4.20-W/BIAS 4.54-DIFF .344

14-Jun-2007 1

BALAD IRAQ

QC000000

D CO 1-131 AVN BNUH-60-07-ASAM-08, COMPLIED WITH 19 JULY2007 @ 9911.3 ACFT HRS. DISCREPANT HMUPART NUMBERS NOT INSTALLED ON THISAIRCRAFT.

19-Jul-2007 1

BALAD, IRAQ

QC000000

AR AASFH-60-08-AMAM-01 MAIN LANDING GEARSHOCK STRUTS COMPLIED WITH AT ACFTHOURS 9970.1

08-Oct-2007 1

CJTR, AR

QC000000

AR AASFH-60-08-ASAM-02 POWER AVAILABLECONTROL CABLE COMPLIED WITH AT ACFTHOURS 9970.1

13-Nov-2007 1

CJTR, AR

QC000000

AR AASFH-60-08-ASAM-04 PILOT'S LOWER SEAT RAILCHAFING ELECTRICAL HARNESS COMPLIEDWITH AT ACFT HOURS 9971.1

26-Nov-2007 1

RBM, N. LITTLE ROCK,AR

QC000000

AR AASFH-60-08-AMAM-02 COMPLIED WITH AT 9971.1ACFT HRS. T/R OUTBOARD RETENTIONPLATE S/N A257-03002

27-Nov-2007 1

CJTR, NLR, AR 72199-9600

QC000000

AR AASFCOMPLIED WITH REQUIREMENTS OF H-60-08-ASAM-05 TAIL ROTOR QUARDANT SPRINGASSEMBLY AT AIR CRAFT HOURS: 9971.1

12-Dec-2007 1

RBM CJTR, AR

QC000000


ANNUAL ACE EVALUATION COMPLETED AT9971 ACFT HRS AT NO LITTLE ROCK, AR BYTEAM MEMBERS RR & W

14-Dec-2007 1

KILLEEN, TX

QC000000

AR AASFH-60-08-AMAM-05 GOODRICH INTERNALRESCUE HOISTS COMPLY WITH

29-Jan-2008 1

NORTH LITTLE ROCK,AR 72199

QC000000

AR AASFH-60-08-SOF-01 (MAIN ROTOR BALDEEXPANDABLE PIN INSPECTION CHANGE)COMLIED WITH AT 9972.1 ACFT HRS.

30-Jan-2008 1

RBM, CJTR, NLR, AR72199

QC000000


OCM/ACE PERFORMED AT 9975.1 ACFT HRSBY TEAM MEMBER N, AMCOM PROJECT OLR.

07-Mar-2008 1


QC000000


UH-60-07-ASAM-10, MAIN FUEL MANIFOLDFUEL LINE INSP C/W AT 9975.1 ACFT HRS

09-Apr-2008 1

FTCKY, 42223

QC000000


H-60-08-ASAM-01, TROOP/GUNNERS SEATATTENTUATING WIRES C/W AT 9975.1 ACFTHRS

09-Apr-2008 2

FTCKY, 42223

QC000000


H-60-08-ASAM-03, CHANGES TO FUEL SYSINTEGRITY CHKS C/W AT 9975.1 ACFT HRS

09-Apr-2008 3

FTCKY, 42223

QC000000


H-60-08-ASAM-06, M/R PYLON SLIDING COVERC/W AT 9975.1 ACFT HRS

09-Apr-2008 4

FTCKY,42223

QC000000



8.7.DATE

6.REMARKS

4. 5.




H-60-08-AMAM-04, COCKPIT DOORJETTISONABLE WINDOWS C/W AT 9975.1ACFT HRS

09-Apr-2008 8

FTCKY, 42223

QC000000


H-60-08-AMAM-06, CMWS SEQUENCERS C/WAT 9975.1 ACFT HRS

09-Apr-2008 9

FTCKY, 42223

QC000000


H-60-08-AMAM-07, DOPPLER 128D SOFTWAREC/W AT 9975.1 ACFT HRS

09-Apr-2008 10

FTCKY, 42223

QC000000


M/R RIG COMPLETE: PRIMARY SERVO BIASADJUSTMENTS FWD-SHORTENED .5 FLAT,AFT-LENGTHENED .5 FLAT, LAT-LENGTHENED2.5 FLATS.

10-Apr-2008 1

FTCKY, 42223

QC000000


T/R RIG COMPLETE: BIAS RED 4.723 - 5.040 =.317, BLUE 4.000 - 4.330 = .330, YEL 4.860 -5.150 = .290, BLK 4.000 - 4.340 = .340.

10-Apr-2008 2

FTCKY, 42223

QC000000


TB 1-1500-200-20-31, AIRCRAFT DESERTOPERATIONS CLEANING REQUIREMENTCOMPLETED AT 9975.1 ACFT HRS

18-Apr-2008 2

FTCKY, 42223

QC000000


TB 1-1520-237-30-1, RESET INSPECTIONCOMPLETED AT 9975.1 ACFT HRS, NEXT PMI-1DUE AT 10335.1 ACFT HRS.

18-Apr-2008 3

FTCKY, 42223

QC000000


H-60-08-AMAM-08, FLIGHT CONTROL RIGGINGUPDATE C/W AT 9980.3 ACFT HRS

25-Jun-2008 1


QC000000


H-60-08=ASAM-10, ELECTRICAL WIRE CHAFEISSUES, COMPLIED WITH DURING RESET @9980.3 ACFT HRS

14-Jul-2008 1


QC000000

AR AASFH-60-08-ASAM-11 (FLIGHT CONTROLINSPECTION) COMPLIED WITH @ 9991.0 ACFTHRS.

16-Sep-2008 1


QC000000

AR AASFH-60-08-ASAM-12 ( PARKER AT STARTERS)COMPLIED WITH @ 9991.0 ACFT HRS.

26-Sep-2008 1


QC000000

AR AASFT/R RIG CHECK COMPLETED FOR T/R G/BINBOARD RET. PLATE TQ CHECK @ 9995.0ACFT HRS: RED A-4.845 B-5.178= 0.333, BLUEA-4.110 B-4.463= 0.353, YELLOW A-4.860 B-5.192= 0.332, BLACK A-4.105 B-4.463=0.361.

03-Oct-2008 2


QC000000

AR AASFH-60-08-ASAM-13 (FIRE EXTINGUISHER TUBE)COMPLIED WITH @ 10002.5 ACFT HRS.

10-Oct-2008 1


QC000000

AR AASFH-60-09-SOF-01 (SUSPECTED HMU'S)COMPLIED WITH @ 10007.5 ACFT HRS.

27-Oct-2008 1


QC000000



8.7.DATE

6.REMARKS

4. 5.



AR AASFH-60-09-SOF-02 (ALQ 144/CMWS) COMPLIEDWITH @ 10025.7 ACFT HRS.

12-Nov-2008 1


QC000000

AR AASFH-60-09-SOF-03 (POSSIBLE RETIREMENT LIFEOVERFLIGHT) COMPLIED WITH @ 10027.9ACFT HRS

20-Nov-2008 1


QC000000

AR AASFH-60-09-ASAM-04 (RESCUE HOIST (CAD)COMPLIED WITH @ 10062.1 ACFT HRS.

02-Mar-2009 1


QC000000

AR AASFH-60-09-ASAM-05 (T/R QUADRANT SPRINGCAPSULES LIFE LIMIT CHANGE) COMPLIEDWITH @ 10062.1 ACFT HRS.

06-Mar-2009 1


QC000000

AR AASF(ELT EBC-406HM) INSTALLED @ 10063.1 ACFTHRS (ELT ID #) ADCC09CC8040775 (ELT S/N#)400968

11-Mar-2009 1


QC000000

AR AASFH-60-09-ASAM-07 (FIRE EXTINGUISHERWIRING) COMPLIED WITH @ 10092.9 ACFTHRS.

22-Apr-2009 1


QC000000

AR AASFH-60-09-ASAM-08 (ENGINE COWLINGS)COMPLIED WITH @ 10101.5 ACFT HRS.

22-Apr-2009 2


QC000000

AR AASFOPERATE WITHIN THE LIMITATIONSPRESCRIBED IN THE ENCLOSED ISAQ'SDATED: 127(M/R SOLID BLADE PINS)24OCT06,104R1(AFCC)04OCT02, 116R2(APX-118)22NOV06, 128(FOGS)02MAR07, 105R3(ARC-220)31OCT02, 130(DOPPLERGPS)07MAR07.(ENTRY ENTERED USING GEN-MIM-2004-002 ULLS-A UNITS UTILIZING THELESS PAPER METHOD)

27-Apr-2009 1


QC000000

AR AASFOPERATE WITHIN THE LIMITATIONSPRESCRIBED IN THE ENCLOSED AWR'SDATED: 1479(IMP MAIN MOD)04JAN08,1455(BATT CAUTION ADVIS PANEL)20NOV07,1310(ARC-164 HQ II)04NOV05, 1120R5(M-240HMACHINE GUN)10OCT07, 1516(ELT)20JUN08,1127R1(HELIBASKET)22SEP06, 1386(PPCSOFTWARE)31MAY07, 1466(GARMINGPS)18APR08, 917(ARN-147)21DEC01,1444R1(FOGS)14NOV07, 1467R2(ASN 128DDOPPLER GPS)27FEB08, 1578(IMP DRAGBEAMS)05JAN09, 1054R8(BAMBIBUCKETS)31OCT08, 1292R3(ASN 128DDOPPLER GPS)27APR07, 1452(LC-6 DIGCHRON)09JAN08, 1467R2(DOPPLERGPS)27FEB08. (ENTRY ENTERED USING GEN-MIM-2004-002 ULLS-A UNITS UTILIZING THE PA

27-Apr-2009 2


QC000000

AR AASFH-60-09-ASAM-09 (FIRE EXTINGUISHERWIRING REV.) COMPLIED WITH @ 10095.1ACFT HRS.

07-May-2009 1


QC000000



8.7.DATE

6.REMARKS

4. 5.



AR AASFH-60-09-ASAM-11 (CARGO DOOR WINDOWS)COMPLIED WITH @ 10117.0 ACFT HRS.

29-Jun-2009 1


QC000000

AR AASFMAINTENANCE ENGINEERING CALL (MECF87066) AND MAINTENANCE ENGINEERINGORDER (MEO A5908) INSTALLATION OFRESCUE HOIST CABLE GUARD IAW RSN1001031 COMPLIED WITH BY MOAVCRAD @10119.0 ACFT HRS.

09-Jul-2009 1


QC000000

AR AASFH-60-09-AMAM-06 (CARGO HOOK CART. LIFEREDUCTION) COMPLIED WITH @ 10147.6 ACFTHRS.

26-Aug-2009 1


QC000000

AR AASFH-60-09-AMAM-04 (CO-PILOTS SEATINTERFERENCE W/ A2C2S) COMPLIED WITH @10145.5 ACFT HRS.

04-Sep-2009 1


QC000000

AR AASFGEN-09-AMAM-03 (ULLS-A(E) INTERGRATEDMATERIAL MANAGEMENT CENTER (LCF)CHANGE 60) COMPLIED WITH @ 10168.7 ACFTHRS.

15-Sep-2009 1


QC000000

AR AASFH-60-09-AMAM-07 (HALON HAND-HELD FIREEXTINGUISHERS HHFE) COMPLIED WITH @10169.9 ACFT HRS.

23-Sep-2009 1


QC000000

AR AASFB.F.T. UPDATED WITH VERSION 6.5INSTALLED SEPTEMBER 2009 BY PATRICBAYLESS FROM WEST STAR.

01-Oct-2009 1


QC000000

AR AASFH-60-10-AMAM-04 (ASN-128 B/C DOPPLER GPSNAV SET) COMPLIED WITH @ 10194.4 ACFTHRS.

16-Nov-2009 1


QC000000

AR AASFH-60-10-ASAM-03 (FIRE BOTTLE DISCHARGELINES AND NOZZLES) COMPLIED WITH @10194.4 ACFT HRS.

17-Nov-2009 1


QC000000


AIRCRAFT 8724615 ACE COMPLETED AT10215 ACFT HRS AT LITTLE ROCK, AR BYTEAM MEMBERS RR & W

15-Dec-2009 1


QC000000

AR AASFH-60-10-AMAM-05 (ULLS-A (E) LEGITIMATECODE FILE CHANGE 60B) COMPLIED WITH @10214.9 ACFT HRS

18-Dec-2009 1


QC000000

AR AASFH-60-10-ASAM-04 (SAS) COMPLIED WITH @10214.9 ACFT HRS.

23-Dec-2009 1


QC000000

AR AASFH-60-10-AMAM-11 (OIL SAMPLING SCHEDULECHG) COMPLIED WITH @ 10243.8 ACFT HRS.

05-Feb-2010 1


QC000000

AR AASFUH-60-10-ASAM-06 (AUTO-IGN & DROOPIMPROVEMENT (TDI) MOD) COMPLIED WITH @10243.8 ACFT HRS.

12-Feb-2010 1


QC000000



8.7.DATE

6.REMARKS

4. 5.



AR AASFH-60-10-ASAM-07 (STAB HINGE FITTING)COMPLIED WITH @ 10321.9

29-Apr-2010 1


QC000000


AIRWORTHINESS RELEASE (AWR) FOR ALLUH-60A/L/M AND HH-60A/L HELICOPTERSEQUIPPED WITH THE PROTECTIVEMATERIALS COMPANY BALLISTIC ARMORPROTECTION SYSTEM (BAPS)(AWR 1524),ENTERED AT 10,321.9 HRS

19-May-2010 1


QC000000


AIRWORTHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS WITH INTEGRATEDVEHICLE HEALTH MANAGEMENT SYSTEM(IVHMS) HEALTH USAGE MANAGEMENTSYSTEM (HUMS) INSTALLED (AWR 1346),ENTERED AT 10,321.9 HRS

19-May-2010 2


QC000000


AIRWORTHINESS RELEASE (AWR) FOR THEOPERATION OF COMMON MISSILE WARNINGSYSTEM (CMWS), IMPROVEDCOUNTERMEASURES DISPENSER (ICMD),AND PRE-PLANNED PRODUCT IMPROVEMENT(P3I), ON UH-60A/L HELICOPTER (AWR 1425),ENTERED AT 10,321.9 HRS

19-May-2010 3


QC000000


AIRWORTHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS EQUIPPED WITH THECOMMON MISSILE WARNING SYSTEM (CMWS)5TH SENSOR A AND B KIT (AWR 1494),ENTERED AT 10,321.9

19-May-2010 4


QC000000

AR AASFH-60-10-AMAM-12(IMPROVED DRAG BEAMS)COMPLIED WITH @ 10321.9

19-May-2010 5


QC000000

AR AASFH-60-10-ASAM-08 (APU & APU FIREWALLCLEARANCE CHECK) COMPLIED WITH @10321.9 ACFT HRS.

01-Jun-2010 1


QC000000

AR AASFH-60-10-SOF-02 (SPINDLE LUG NDI ANDRETIREMENT LIFE CHANGE) COMPLIED WITH@ 10321.9 ACFT HRS.

30-Jun-2010 1


QC000000

AR AASFH-60-10-AMAM-16 (CMWS GUARD SIDPENSESWITCH) COMPLIED WITH @ 10321.9 ACFTHRS.

06-Jul-2010 1


QC000000

AR AASFH-60-10-ASAM-11 (COMMON COMPONENTRETIREMENT CHANGE TIMES UPDATE)COMPLIED WITH @ 10321.9 ACFT HRS.

27-Jul-2010 1


QC000000

AR AASFH-60-10-ASAM-12 (T700 SERIES ENGINECOMMON COMP RC TIMES) COMPLIED WITH@ 10321.9 ACFT HRS.

30-Jul-2010 1


QC000000

AR AASFMR/ & T/R RIG CHECK COMPLETED FOR RMVLOF T/R PITCH BEAM COMPLETED @ 10321.9ACFT HRS. SEE HISTORICAL RECORDS FORWORKSHEET. TAIL ROTOR BIAS ASFOLLOWS: RED (A)4.893 (B)5.230= 0.338, BLUE(A)4.156 (B)4.488= 0.332, YELLOW (A)4.795(B)5.128= 0.333, BLACK (A)4.135 (B)4.468=0.333

30-Jul-2010 2


QC000000



8.7.DATE

6.REMARKS

4. 5.



AR AASFPMI-1 COMPLETED AT 10321.9 ACFT HOURS.NEXT PMI-2 DUE AT 10681.9 ACFT HOURS.

11-Aug-2010 1


QC000000


ACE PERFORMED AT 10352 AIRCRAFT HOURSAT LITTLE ROCK, AR BY TEAM MEMBERS K &Q.

16-Sep-2010 1


QC000000

AR AASFH-60-11-AMAM-03(OIL COOLER FAN AXIALBEARINGS) COMPLIED WITH @ 10364.8 ACFTHRS.

01-Nov-2010 1


QC000000

AR AASFMWO 1-1520-237-50-1008310 REV F (M4VERTICAL GUN MOUNT) DATED 28 JUN 2010INSTALLED.

05-Nov-2010 1


QC000000

AR AASFM/R RIG COMPLETE: PRIMARY SERVO BIASADJUSTMENTS FWD-SHORTENED 2 FLAT,AFT-LENGTHENED 2 FLAT, LAT-LENGTHENED2 FLATS. (SEE RIG SHEET DATED 6 NOV 10)

08-Nov-2010 1


QC000000

AR AASFT/R RIG COMPLETE: BIAS RED 5.13 - 4.80=0.33, BLUE 4.58 - 4.25 = 0.33, YEL 5.13 - 4.79= 0.34, BLK 4.55 - 4.22 = 0.33 . (SEE RIG SHEETDATED 6 NOV 10)

08-Nov-2010 2


QC000000

AR AASFH-60-11-ASAM-03 (HMU- UH-60A ONLY )COMPLIED WITH @ 10380.8 ACFT HRS

29-Nov-2010 1


QC000000

AR AASFH-60-11-AMAM-04 (AMCOM CHANGE 61)COMPLIED WITH THIS DATE

10-Dec-2010 1

NORTH LITTLEROCK,AR

QC000000

AR AASFH-60-11-ASAM-04 (AN/ARN-153 TCN-500TACAN RECEIVER BEARING ERROR)COMPLIED WITH @ 10386.0 ACFT HRS

10-Dec-2010 2

NORTH LITTLEROCK,AR

QC000000

1-185THCOMPLIED WITH REQUIREMENTS OF H-60-11-ASAM-06 AS OF THIS DATE (CYCLIC STICKSTOP BOLTS)

12-Jan-2011 1

NORTH FORT HOOD, TX

QC000000

1-185THAWR 1270, REV7, DATED 27NOV 2010, EIBF BKIT TEMP INSTALLED @ CAMP BUEHRING,KUWAIT 31JAN 2011

31-Jan-2011 1

CAMP BUEHRING,KUWAIT

QC000000

1-185THAWR 1223, REV 5, DATED 15 MAY 2009, IRANTI-COLLISION LIGHT, TEMP INSTALLED @CAMP BUEHRING, KUWAIT 31 JAN 2011

31-Jan-2011 2


QC000000

1-185THAWR 1524 REV 3, DATED 4 JAN 2011, BAPS,TEMP INSTALLED @ CAMP BUEHRING,KUWAIT 31 JAN 2011

31-Jan-2011 3


QC000000

1-185THH-60-11-ASAM-08, IFF/LOS ANTENNA,COMPLIED WITH. INSP OK

20-Feb-2011 1

COB SPEICHER, IRAQ

QC000000

1-185THH-60-11-AMAM-06, MEDEVAC CAROUSELREFURBISHMENT, COMPLIED WITH

27-Feb-2011 1

COB SPEICHER, IRAQ

QC000000



8.7.DATE

6.REMARKS

4. 5.



1-185THCOMPLIED WITH H-60-11-ASAM-09, INTERNALAUXILIARY FUEL TRANSFER SYSTEMS(IAFTS), DOES NOT APPLY TO THISAIRFRAME.

31-Mar-2011 1

COB SPEICHER, IRAQ

QC000000

1-185THH-60-11-AMAM-09 (AWR UPDATE) COMPLIEDWITH

25-Apr-2011 1

COB SPEICHER, IRAQ

QC000000

1-185THH-60-11-AMAM-11 (AWR UPDATE) COMPLIEDWITH

25-Apr-2011 2

COB SPEICHER, IRAQ

QC000000

1-185THH-60-10-ASAM-15 ESSS FUEL VENT LINEELBOW COMPLIED WITH.

25-Apr-2011 3

COB SPEICHER, IRAQ

QC000000

L3 VERTEXAEROSPACE

AWR 1682 DATED 1 OCT 10, (701D ENGINEMOD) COMPLETED @ 10665.9 ACFT HRS FOR#1 & #2 ENGINES

31-May-2011 1

BALAD, IRAQ

QC000000

L3 VERTEXAEROSPACE

M/R RIG CHECK COMPLETED FOR [email protected] ACFT HRS. LOW COLL: 90=9.4, 180=-2.2, 270=-10, 0=2.3, TOT=-.05 AVG=-.01, HIGHCOLL: 90=20.2, 180=11.1, 270=10.9, 0=20.3,TOTAL=62.5, AVG=15.62, FWD TOT=34.2, AFTTOTAL=20, LEFT TOTAL=15.2, RIGHTTOTAL=14.1.

31-May-2011 2

COB SPEICHER, IRAQ

QC000000

L3 VERTEXAEROSPACE

PMI-2 COMPLETED 31/MAY/11 @ 10665.9 ACFTHRS. NEXT PMI-2 DUE @ 11385.9 ACFTHRS.ACFT RELEASED FOR MOC / MTF.

31-May-2011 3

BALAD, IRAQ

QC000000

L3 VERTEXAEROSPACE

T/R RIG COMPLETED DURING PMI-2. CABLETENSION READINGS : R/S 176LBS L/S 176LBS@31C

31-May-2011 4

BALAD AB, IRAQ

QC000000

1-185THApplied Airworthiness Release (AWR) forUH/HH-60A/L/M Operations with CockpitDoors/Windows and or Cabin Doors /windowsRemoved (AWR1279), Quick release pins havebeen temporarily installed in the L/R CockpitDoors for the duration of operations withCockpit Doors removed I/A/W THIS AWR

06-Jun-2011 1

COB SPEICHER, IRAQ

QC000000

1-185THH-60-11-AMAM-13, EXTERNAL RESCUE HOISTMOUNT FITTING, COMPLIED WITH. (ACFT NOTEQUIPPED WITH EXTERNAL RESCUE HOIST,DOES NOT APPLY TO THIS AIRFRAME).

17-Jun-2011 1

COB SPEICHER, IRAQ

QC000000

1-185THH-60-11-AMAM-14 COMPLIED WITH. AMAMDOES NOT APPLY TO THIS ACFT

21-Jun-2011 1

COB SPEICHER, IRAQ

QC000000

1-185THT/R CABLE TENSION CHECKED ANDADJUSTED. CABLE TENSION READINGS ASOF THIS DATE: R/S-189 L/S 190 @ 40C

27-Jun-2011 1

COB SPEICHER, IRAQ

QC000000

1-185THH-60-11-ASAM-13, ENGINE AIR INLET ANTI-ICING/MODULATING VALVE, COMPLIED WITH.INSP FAILED. #1 ENG P/N: 3214072-4(INCORRECT VALVE), #2 ENG P/N IS 3214072-3(CORRECT VALVE), (FOR T-701D'S)

02-Jul-2011 1

COB SPEICHER, IRAQ

QC000000

1-185THH-60-11-SOF-01, DISCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS, COMPLIED WITH.INSP OK, NO SUSPECT NUTS FOUND.

08-Jul-2011 1

COB SPEICHER, IRAQ

QC000000



8.7.DATE

6.REMARKS

4. 5.



1-185THH-60-11-ASAM-14, ENGINE COWLING REPAIRRESTRICTIONS COMPLIED WITH @ 10698.6ACFT HRS. L/H PART NUMBER: 70070-30308-041 (PASS); R/H PART NUMBER: 70070-30308-041 (PASS). INSPECTION COMPLETE.

18-Jul-2011 1

COB SPEICHER, IRAQ

QC000000

1-185THH-60-11-ASAM-13, ENGINE AIR INLET ANTI-ICING/MODULATING VALVE, COMPLIEDWITH.REPLACED #1 INLET ANTI ICE VALVE(SEE -15 ENTRY 2 JUL 11 #1) W/ PN3214072-3.(ORIGINAL VALVE WAS FOUND TO BECORRECT PN 3214072-3) BOTH VALVES ARENOW IN COMPLIANCE.

21-Jul-2011 1

COB SPEICHER, IRAQ

QC000000

L3 VERTEXAEROSPACE

H-60-11-AMAM-15, INTEGRATED VEHICLEHEALTH MANAGEMENT SYSTEM, COMPLIEDWITH (L-3 VERTEX). INSP OK. ALL SENSORSIN CORRECT POSITION, AND IVHMU (P/N:30279-0302, S/N: 00701) ADDED TO 2408-16.

20-Aug-2011 1

COB SPEICHER, IRAQ

QC000000

1-185THT/R BIAS COMPLETED FOR T/R BLADEREPLACEMENT: YEL: 5-4.66=.340 BLUE: 4.34-4.01=.330 RED:5.04-4.71=.330 BLACK:4.36-4.02=.340

20-Aug-2011 2

COB SPEICHER, IRAQ

QC000000

1-185THH-60-11-AMAM-20, AN/ASN-128D DOPPLER &AVIATION MISSION PLANNING SYSTEMSOFTWARE UPGRADE, COMPLIED WITH. P/N:P320A002-03; S/N: 1059; SOFTWAREUPGRADED ON 20AUG11.

25-Sep-2011 1

COB SPEICHER, IRAQ

QC000000

1-185THCOMPLYED WITH H-60-12-AMAM-01, FUELMOMENT CHART ERRORS, DOES NOT APPLY,H-60-M ONLY.

08-Oct-2011 1

COB SPEICHER, IRAQ

QC000000

1-185THH-60-12-SOF-01, TAIL ROTOR INTERMEDIATEGEARBOX, COMPLIED WITH. SUSPECTGEARBOX NOT INSTALLED.

08-Oct-2011 2

COB SPEICHER, IRAQ

QC000000

1-185THH-60-11-AMAM-19, LCF CHANGE 62, COMPLIEDWITH 8 OCT 2011

08-Oct-2011 3

COB SPEICHER, IRAQ

QC000000

1-185THH-60-12-SOF-02, TAIL ROTOR INTERMEDIATEGEARBOX, COMPLIED WITH. SUSPECTGEARBOX NOT INSTALLED.

11-Oct-2011 1

COB SPEICHER, IRAQ

QC000000

D CO 1-131 AVN BNH-60-12-SOF-03, TAIL ROTOR INTERMEDIATEGEARBOX, COMPLIED WITH. SUSPECTGEARBOX NOT INSTALLED.

22-Oct-2011 1

AL ASAD, IRAQ

QC000000

AR AASFACFT RETURNED FROM DEPLOYMENTTRANSFERED BACK TO AR AASF @1089.5ACFT HRS

09-Feb-2012 1


QC000000

AR AASFH-60-12-SOF-04 (EXTERNAL RESUCUE HOISTOPS) COMPLIED WITH @ 10895.5 AIRCRAFTHOURS.

22-Feb-2012 1


QC000000

AR AASFH-60-12-ASAM-06 COMPLIED WITH @10895.5ACFT HRS: ( UPPER BULKHEAD FUEL SYSBREAKAWAY VALVE AND FIRE EXT SYSDIRECTIONAL VALVE)

23-Feb-2012 1


QC000000



8.7.DATE

6.REMARKS

4. 5.



AR AASFH-60-12-AMAM-03 (TRANSPONDER ANDCOMMON MISSILE WARNING SYSTEMINSTALLATION) COMPLIED WITH @ 10895.5AIRCRAFT HOURS.

13-Mar-2012 1


QC000000

AR AASFCOMPLETE MAIN ROTOR RIG COMPLETEDFOR FLIGHT CONTROL ROD INSP @ 10918.8AIRCRAFT HOURS.SEE ATTACHED RIG SHEETDATED 17-APR-2012.PRIMARY SERVO BIAS /FWD - SHORTEN 1 FLAT / AFT - LENGTHEN 1FLAT / LAT - SHORTEN 2/3 FLAT

17-Apr-2012 1


QC000000

AR AASFTAIL ROTOR RIG COMPLETED @10918.8AIRCRAFT HOURS.SEE ATTACHED RIGSHEET. CABLE TENSION: L/H 164 R/H 165TEMP 20 DEG CT/R BIAS: INITIAL BIASDIFFRED 4.794 5.106 0.312BLU 4.0584.398 0.340YEL 4.773 5.106 0.333BLK4.055 4.388 0.333

17-Apr-2012 2


QC000000

AR AASFH-60-12-SOF-05 (LEGACY MAIN ROTORBLADES) COMPLIED WITH @ 10918.8AIRCRAFT HOURS.

23-Apr-2012 1


QC000000


ACE/CPCE PERFORMED AT 10954 ACFT HRS.BY TEAM MEMBER "K"

16-May-2012 1

FT. HOOD, TX

QC000000

DEFENSE SUPPORTSERVICES (DS2)

(LATE ENTRY) H-60-10-ASAM-16, ALL H-60AND UH-1 SERIES AIRCRAFT, RESCUE HOISTCABLE CUT HARNESS CONNECTOR. HOISTNOT INSTALLED THIS DATE AT 10953.6AIRCRAFT HOURS DURING RESETINSPECTION.

17-May-2012 1

FT. HOOD TEXAS

QC000000


(LATE ENTRY) H-60-12-ASAM-02, ALL H-60A/K/L SERIES AIRCRAFT, DRAG BEAMREPLACEMENT COMPLETED ENTERED THISDATE 10953.6 AIRCRAFT HOURS DURINGRESET INSPECTION.

17-May-2012 2

FT. HOOD TEXAS

QC000000


H-60-11-AMAM-17, ALL H-60 SERIES AIRCRAFT, TAIL ROTOR INBOARD/OUTBOARDRETENTION PLATE SHIMS.COMPLETED THISDATE AT 10953.6 AIRCRAFT HOURS DURINGRESET INSPECTION.

18-May-2012 1

FT. HOOD TEXAS

QC000000


H-60-12-ASAM-06, ALL H-60 SERIESAIRCRAFT, UPPER BULKHEAD FUEL SYSTEMBREAKAWAY VALVE AND FIREEXTINGUISHING SYSTEM DIRECTIONALVALVE. COMPLETED THIS DATE AT 10953.6AIRCRAFT HOURS DURING RESETINSPECTION.

21-May-2012 1

FT. HOOD TEXAS

QC000000


MAINTENANCE ENGINEERING CALL (MECF146550) 360 DEGREE LIGHT SCORING ATINSIDE DIAMETER OF LOWER MATINGSURFACE BY LOWER SPLIT CONE SEATAPPROXIMATELY .125 IN. WIDE BY .00025 IN.DEEPCOMPLIED WITH BY (DS 2 ) FT HOODTEXAS.

22-May-2012 1

FT HOOD TEXAS

QC000000



8.7.DATE

6.REMARKS

4. 5.




H-60-12-AMAM-09, ALL H-60 SERIESAIRCRAFT, HYDRAULIC LINE CHAFE DUE TOMISSING CLAMPS COMPLETED THIS DATE AT10953.6 AIRCRAFT HOURS. DURING RESETINSPECTION.

30-May-2012 1

FT. HOOD TEXAS

QC000000


H-60-12-ASAM-01, ALL H-60 SERIESAIRCRAFT, TAIL ROTOR OUTPUT BEVELGEAR NON-DESTRUCTIVE INSPECTIONCOMPLTED THIS DATE AT 10953.4 AIRCRAFTHOURS ON TAIL ROTOR GEARBOX P/N 70358-06600-046, S/N A006-02186. DURING RESETINSPECTION.

05-Jun-2012 1

FT. HOOD TEXAS

QC000000


SAQ-105 DATED 18 APR 08 FINAL STATEMENTOF AIRWORTHINESS QUALIFICATION (SAQ)FOR THE UH-60A/L HELICOPTERS EQUIPPEDWITH THE STANDARD INSTALLATIONINSTALLATION AN/ARC-220 (V) 1/ (V) 2 HIGHFREQUENCY (HF) RADIO ENTERED THIS DATEAT 10953.6 AIRCRAFT HOURS. DURING RESETINSPECTION.

29-Jun-2012 1

FT. HOOD TEXAS

QC000000


SAQ-107 DATED 7 MAY 08 FINAL STATEMENTOF AIRWORTHINESS QUALIFICATION (SAQ)FOR UH-60A/L/M AND HH-60A/L/MHELICOPTERS EQUIPPED WITH THEIMPROVED ENGINE DRIVESHAFT (ECP-310)ENTERED THIS DATE AT 10953.6 AIRCRAFTHOURS. DURING RESET INSPECTION.

29-Jun-2012 2

FT. HOOD TEXAS

QC000000


SAQ-120 DATED 23 DEC 08, STATEMENT OFAIRWORTHINESS QUALIFICATION (SAQ) FORUH/HH-60A/L HELICOPTERS EQUIPPED WITHTHE IMPROVED DRAG BEAM ENTERED THISDATE AT 10953.6 AIRCRAFT HOURS. DURINGRESET INSPECTION.

29-Jun-2012 3

FT. HOOD TEXAS

QC000000


SAQ-127 DATED 20 OCT 08, FINALSTATEMENT OF AIRWORTHINESSQUALIFICATION (SAQ) FOR UH/HH-60A/L/MHELICOPTERS EQUIPPED WITH THE SOLIDBLADE PIN ENTERED THIS DATTE AT 10953.6AIRCRAFT HOURS. DURING RESETINSPECTION.

29-Jun-2012 4

FT. HOOD TEXAS

QC000000


MAIN ROTOR SYSTEM RIG COMPLETED I/A/WTM 1-1520-BLACKHAWK CHAPTER 9, W/P1049.00 AT 10953.6 AIRCRAFT HOURS FORTHE COMPLETED OF RESET INSPECTION ANDTHE FOLLOWING ADJUSTMENT WHEREMADE.FWD PRIMARY SERVO CONTROL ROD 0FLAT.AFT PRIMARY SERVO CONTROL ROD 0FLAT.LAT PRIMARY SERVO CONTROL RODSHORTEND 1 FLAT.

05-Jul-2012 1

FT. HOOD TEXAS

QC000000



8.7.DATE

6.REMARKS

4. 5.




TAIL ROTOR SYSTEM RIG COMPLETED I/A/WTM 1-1520-BLACKHAWK CHAPTER 9, WP 105100 AT 10953.6 AIRCRAFT HOURS FOR THECOMPLETION OF RESET INSPECTION ANDTHE FOLLOWING ADJUSTMENT WHEREMADE. BLADE INITIAL BIAS DIFFRED4.900 5.250 0.350BLUE 4.250 4.6000.350YELLOW 4.900 5.250 0.350BLACK4.200 4.520 0.320BASELINE CABLETENSION TEMP 31 DEGREE (C), RIGHT HANDCABLE 174 LBS, LEFT HAND CABLE 172 LBS.

05-Jul-2012 2

FT. HOOD TEXAS

QC000000


MAIN ROTOR SHAFT EXTENSION S/N A286-01094 REPAIRED I/A/W MEC F146550 DATED 22MAY 2012 AUTHORIZED BY RONALD DMEDLOCK COMPETED THIS DATE AT 10953.6AIRCRAFT HOURS DURING RESETINSPECTION.

05-Jul-2012 3

FT. HOOD TEXAS

QC000000


AWR 1120 DATED 30 NOV 10 (R-8)AIRWORTHINESS RELEASE (AWR) FOROPERATION OF UH-60A/L/M HELICOPTERSWITH THE M-240H MACHINE GUN INSTALLEDENTERED THIS DATE AT 10953.6 AIRCRAFTHOURS. DURING RESET INSPECTION.

07-Jul-2012 1

FT. HOOD TEXAS

QC000000


AWR 1309 DATED 10 FEB 12 (R-7)AIRWORTHINESS RELEASE (AWR) FOR EH-60A AND UH/HH-60A/L/M HELICOPTERSEQUIPPED WITH OREGON AERO SEATCUSHIONS ENTERED THIS DATE AT 10953.6AIRCRAFT HOURS. DURING RESETINSPECTION.

07-Jul-2012 2

FT. HOOD TEXAS

QC000000


AWR 1310 DATED 4 NOV 05 AIRWORTHINESSRELEASE (AWR) FOR ALL UH-60A/L AND EH-60A HELICOPTERS EQUIPPED WITH RT-1518C/ARC-164 HAVE QUICK II (HQII) UHF/AMRADIOS ENTERED THIS DATE AT 10953.6AIRCRAFT HOURS DURING RESET INSPECTION.

07-Jul-2012 3

FT. HOOD TEXAS

QC000000


AWR 1346 DATED 31 JAN 12 (R-20)AIRWORTHINESS RELEASE (AWR) FOR UH/HH-60A/L HELICOPTERS WITH INTERGRATEDVEHICLE HEALTH MANAGEMENT SYSTEM(IVHMS) HEALTH USAGE MANAGEMENTSYSTEMS (HUMS) INSTALLED ENTERED THISDATE AT 10953.6 AIRCRAFT HOURS. DURINGRESET INSPECTION.

07-Jul-2012 4

FT. HOOD TEXAS

QC000000


AWR 1425 DATED 29 JUN 12 (R-16)AIRWORTHINESS RELEASE (AWR) FOR THEOPERATION OF COMMON MISSILE WARNINGSYSTEM (CMWS), IMPROVEDCOUNTERMEASURES DISPENSER (ICMD),AND PRE-PLANNED PRODUCT IMPROVEMENT(P3I), ON UH-60A/L HELICOPTERS ENTEREDTHIS DATE AT 10953.6 AIRCRAFT HOURS.DURING RESET INSPECTION.

07-Jul-2012 5

FT. HOOD TEXAS

QC000000



8.7.DATE

6.REMARKS

4. 5.




AWR 1452 DATED 20 JAN 12 (R-2)AIRWORTHINESS RELEASE FOR ALL UH/HH-60A/L HELICOPTERS EQUIPPED WITH THE LC-6 DIGITAL CHRONOMETER ENTERED THISDATE AT 10953.6 AIRCRAFT HOURS. DURINGRESET INSPECTION.

07-Jul-2012 6

FT. HOOD TEXAS

QC000000


AWR 1455 DATED 10 NOV 11 (R-3)AIRWORTHINESS RELEASE FOR ALL UH/EH-60A/L HELICOPTERS EQUIPPED WITH THEBATTELLE CAUTION ADVISORY PANEL (CAP)ENTERED THIS DATE AT 10953.6 AIRCRAFTHOURS. DURING RESET INSPECTION.

07-Jul-2012 7

FT. HOOD TEXAS

QC000000


AWR 1479 DATED 13 JAN 12 (R-2)AIRWORTHINESS RELEASE (AWR) FOR UH-60A AND EH-60A HELICOPTERS WITH MAINMODULE ASSEMBLIES (PART NUMBER 70351-08100-075 AND 70351-08100-076) EQUIPPEDWITH THE IMPROVED PLANETARY CARRIERASSEMBLY, PART NUMBER 70351-08175-046ENTERED THIS DATE AT 10953.6 AIRCRAFTHOURS DURING RESET INSPECTION.

07-Jul-2012 8

FT. HOOD TEXAS

QC000000


AWR 1494 DATED 29 JUN 12 (R-7)AIRWORTHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS EQUIPPED WITH THECOMMON MISSLE WARNING SYSTEM (CWMS)5TH SENSOE A AND B KIT ENTERED THISDATE AT 10953.6 AIRCRAFT HOURS. DURINGRESET INSPECTION.

07-Jul-2012 9

FT. HOOD TEXAS

QC000000


AWR 1529 DATED 7 OCT 11 (R-2)AIRWORTHINESS RELEASE (AWR) FOR UH/HH-60A/L HELICOPTERS EQUIPPED WITH THEATTITUDE HEADING REFERENCE SET (AHRS),DUAL ATTITUDE HEADING REFERENCE UNIT(AHRU) ENTERED THIS DATE AT 10953.6AIRCRAFT HOURS DURING RESETINSPECTION.

07-Jul-2012 10

FT. HOOD TEXAS

QC000000


AWR 1566 DATED 18 MAR 11 (R-2)AIRWORTHINESS RELEASE (AWR) FOR ALLUH/HH-60A/L/M HELICOPTERS EQUIPPEDWITH THE TITANIUM (1000997-001(S7020-12008-043) OR STAINLESS STEEL RESCUE HOISTCABLE (GUARD) DEFLECTOR ENTERED THISDATE AT 10953.6 AIRCRAFT HOURS. DURINGRESET INSPECTION.

07-Jul-2012 11

FT. HOOD TEXAS

QC000000


AWR 1590 DATED 20 APR 12 (R-4)AIRWORTHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS WITH AN/ARN-147VOR/ILS RECEIVER/ELECTRONIC MOUNTINGBASE ENTERED THIS DATE AT 10953.6AIRCRAFT HOURS . DURING RESETINSPECTION.

07-Jul-2012 12

FT. HOOD TEXAS

QC000000


AWR 1648 DATED 9 MAR 12 (R-2)AIRWORTHINESS RELEASE (AWR) FOR UH/HH-60A/L/M WITH A NCS MAGNUS MODELRNM101 LAPTOP ONBOARD AND OPERATINGENTERED THIS DATE AT 10953.6 AIRCRAFTHOURS. DURING RESET INSPECTION.

07-Jul-2012 13

FT. HOOD TEXAS

QC000000



8.7.DATE

6.REMARKS

4. 5.




AWR 1667 DATED 3 MAY 12 (R-5)AIRWORTHINESS RELEASE (AWR) FOR THEVERTICAL PILOT AND COPILOT M4 CARBINEMOUNT SYSTEM INSTALLED ON UH-60A/LHELICOPTERS ENTERED THIS DATE AT10953.6 AIRCRAFT HOURS. DURING RESETINSPECTION.

07-Jul-2012 14

FT. HOOD TEXAS

QC000000


AWR 1682 DATED 13 MAR 12 (R-9)AIRWORTHINESS RELEASE (AWR) FORSPECIFIED UH-60A HELICOPTERS TOOPERATE WITH T700-GE-701D/CC AND ORT700-GE-701C ENGINES WITH AUTO-RELIGHTAND TRANSIENT DROOP IMPROVEMENT (TDI)INSTALLED ENTERED THIS DATE AT 10953.6AIRCRAFT HOURS. DURING RESETINSPECTION.

07-Jul-2012 15

FT. HOOD TEXAS

QC000000


AWR 1753 DATED 31 AUG 11 (R-1)AIRWORTHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS EQUIPPED WITH THEDOPPLER GLOBAL POSITIONING SYSTEMNAVIGATION SYSTEM (DGNS), AN/ASN-128B/DENTERED THIS DATE AT 10953.6 AIRCRAFTHOURS. DURING RESET INSPECTION.

07-Jul-2012 16

FT. HOOD TEXAS

QC000000


AWR 1788 DATED 11 JAN 12 (R-3) FM IMMUNEAN/ARN-147 VOR/ILS RECEIVERES (P/N 622-6376-020 IN THE STANDARD CONFIGURATIONAND FM IMMUNE AN/ARN-147 VOR/ILSRECEIVERS P/N 622-6376-020 WITH THE VIM-123 ADAPTER TRAY MOUNT IN AN/ARN-123CONFIGURED UH-60A/L, EH-60A AND CINCHAWK HELICOPTERS ENTERED THIS DATE AT10953.6 AIRCRAFT HOURS ENTERE THIS DATEAT 10953.6 AIRCRAFT HOURS. DURING RESETINSPECTION.

07-Jul-2012 17

FT. HOOD TEXAS

QC000000


AWR 1800 DATED 30 NOV 11 AIRWORTHINESSRELEASE (AWR) FOR THE ELECTRONIC DATAMANAGER (EDM) AND/OR BLUE FORCETRACKING SYSTEM (BFT) ON UH/EH/HH-60A/LHELICOPTERS ENTERED THIS DATE AT10953.6 AIRCRAFT HOURS. DURING RESETINSPECTION.

07-Jul-2012 18

FT. HOOD TEXAS

QC000000


H-60-12-AMAM-12, ALL H-60A/K/L SERIESAIRCRAFT, RESCINDER CONNONCOMPONENT REMOVAL DATES COMPLETEDTHIS DATE AT 10953.6 AIRCRAFT HOURSDURING RESET INSPECTION.

10-Jul-2012 1

FT. HOOD TEXAS

QC000000


H-60-12-ASAM-07, ALL H-60 SERIESAIRCRAFT, ELECTRICAL WIRING CHAFE.COMPLETED THIS DATE AT 10953.6 AIRCRAFTHOURS. DURING RESET INSPECTION.

11-Jul-2012 1

FT. HOOD TEXAS

QC000000


A-665, 48 MONTH INSPECTION REPLACE FUELCELL O-RINGS SEALS COMPLETED THISDATE AT 10953.6 AIRCRAFT HOURS DURINGRESET INSPECTION NEXT DUE 11 JULY 2012.

11-Jul-2012 2

FT. HOOD TEXAS

QC000000



8.7.DATE

6.REMARKS

4. 5.




A-670, 48 MONTH INSPECTION CABIN TUBEINSPECTION COMPLETED THIS DATE AT10953.6 AIRCRAFT HOURS DURING RESETINSPECTION NEXT DUE 11 JULY 2012..

11-Jul-2012 3

FT. HOOD TEXAS

QC000000


A-673, 48 MONTH INSPECTION FUEL CELLCORROSION INSPECTION COMPLETED THISDATE AT 10953.6 AIRCRAFT HOURS DURINGRESET INSPECTION NEXT DUE 11 JULY 2016.

11-Jul-2012 4

FT. HOOD TEXAS

QC000000


A-675, 48 MONTH INSPECTION FLIGHTCONTROL ROD INSPECTION COMPLETEDTHIS DATE AT 10953.6 AIRCRAFT HOURSDURING RESET INSPECTION NEXT DUE 11JULY 2016.

11-Jul-2012 5

FT. HOOD TEXAS

QC000000


TB 1-1520-237-30-1 DATED 09 JANUARY 2009,HH-60L/UH-60A/L AIRCRAFT DESERTOPERATIONS SPECIAL INSPECTION ANDCLEANING REQUIREMENT (RESETINSPECTION) COMPLETED THIS DATE AT10953.6 AIRCRAFT HOURS NEXT PMI-1 DUE AT11313.6 AIRCRAFT HOURS.

11-Jul-2012 6

FT. HOOD TEXAS

QC000000


LOW LEVEL FUELFUNCTIONAL CHECK DUECOMPLETED THIS DATE AT 10953.6 AIRCRAFTHOURS FOR COMPLETION OF RESETINSPECTION.

13-Jul-2012 1

FT. HOOD TEXAS

QC000000


TAIL ROTOR SYSTEM RIG COMPLETED I/A/WTM 1-1520-BLACKHAWK CHAPTER 9, WP 105100 AT 10955.6 AIRCRAFT HOURS THEFOLLOWING ADJUSTMENT WHERE MADE.BLADE INITIAL BIAS DIFFRED 4.8005.100 0.300BLUE 4.200 4.5200.320YELLOW 4.800 5.110 0.310BLACK4.200 4.510 0.310BASELINE CABLETENSION TEMP 33 DEGREE (C), RIGHT HANDCABLE 181 LBS, LEFT HAND CABLE 182 LBS.

17-Jul-2012 1

FT. HOOD TEXAS

QC000000


H-60-12-ASAM-08, ALL H-60 SERIESAIRCRAFT, CARGO HOOK MANUAL RELEASESPRING ASSEMBLY COMPLETED THIS DATEAT 10955.6 AIRCRAFT HOURS.

18-Jul-2012 1

FT. HOOD TEXAS

QC000000


AWR 1800, DATED 20 JUL 12 (R-1)AIRWORTHINESS RELEASE (AWR) FOR THEELECTRONIC DATA MANAGER (EDM) AND /OR BLUE FORCE TRACKING SYSTEM (BFT)UH/EH/HH-60A/L HELICOPTERS. ENTEREDTHIS DATE AT 10956.1 AIRCRAFT HOURS.

26-Jul-2012 1

FT. HOOD TEXAS

QC000000


H-60-12-AMAM-14, ALL UH-60L SERIESAIRCRAFT, AN/ARN-149 LOW FREQUENCY(LF) AUTOMATIC DIRECTION FINDER (ADF)N/A THIS AIRCRAFT AT 10956.1 AIRCRAFTHOURS.

30-Jul-2012 1

FT. HOOD TEXAS

QC000000


MAIN ROTOR RIG CHECK COMPLETED PERUNIT REQUEST NO ADJUSTMENT MADE THISDATE AT 10958.1 AIRCRAFT HOURS.

02-Aug-2012 1

FT. HOOD TEXAS

QC000000



8.7.DATE

6.REMARKS

4. 5.



AR AASFMAIN ROTOR RIG CHECK COMPLETED @10963.9 ACFT HRS.LOW COLL ANGLE -.6HIGHCOLL ANGLE 15.2FWD CYCLIC 33.1AFTCYCLIC 19.3LEFT CYCLIC 16.0RIGHT CYCLIC14.2PRIAMARY SERVO ADJUSTMENT.FWD 11/2 FLT SHORTAFT 1 1/2 FLT LONGLAT 1/2FLT LONG

21-Aug-2012 1


QC000000

AR AASFTAIL ROTOR RIG COMPLETED: @ ACFT HRS.10963.9RED 5.158BLUE: 4.505YELLOW:5.169BLACK: 4.544

22-Aug-2012 1


QC000000

AR AASFH-60- 12- ASAM-09 (BREEZE EASTERNEXTERNAL RESCURE HOIST CARTRIDGEACTUTED DEVICE (CAD) ELECTRICALCONNECTOR. COMPLIED WITH @ 10963.9ACFT HRS

11-Sep-2012 1


QC000000

AR AASFH-60-12-AMAM-15 (TRIM ACTUATOR)COMPLYED WITH @ 10963.0 ACFT HRS

25-Sep-2012 1


QC000000

AR AASFH-60-12-AMAM-16 (M/R SPINDLE SUB-COMPONENT TRACKING REQUIREMENTS)COMPLIED WITH @ 10974.3 ACFT HRS.

05-Oct-2012 1


QC000000

AR AASFH-60-13-AMAM-02(ATTITUDE HEADINGREFERENCE SYSTEM (AHRS) WIRINGHARNESSES) COMPLYED WITH @11002.2ACFT HRS .

13-Nov-2012 1


QC000000

AR AASFH-60-13-ASAM-01 (ANTI- COLLISION LIGHTPOWER SUPPLY) COMPLIED WITH @ 11016.8ACFT HRS.

28-Nov-2012 1


QC000000

AR AASFH-60-13-AMAM-03(DECU/EDECU TURBINE GASTEMPERATURE (TGT) BIAS) COMPLIED [email protected] ACFT HRS.

30-Nov-2012 1


QC000000

AR AASFH-60-13-AMAM-04(ULLSA-E LCF CHANGE 63)COMPLIED WITH @ 11056.5 ACFT HRS

11-Jan-2013 1


QC000000

AR AASFH-60-13-AMAM-05 ( MAIN LANDING GEARWHEEL BRAKE ASSEMBLY ) COMPLIED WITHAT 11047.4 ACFT HRS

25-Jan-2013 1


QC000000

AR AASFGEN-13-AMAM-02 (COUNTERMEASURE(CMWS) AND (ATIRCM) COMPONENTTRACKING) COMPLIED WITH @ 11065.1 ACFTHRS.

11-Feb-2013 1


QC000000

AR AASFH-60-13-ASAM-04, PLASTIC MEDIA BLAST(PMB) AND OXIDE RESIDUE, COMPLIED WITHAT 11065.1 ACFT HRS

26-Mar-2013 1


QC000000

AR AASFMAIN ROTOR RIG COMPLETED @ 11065.1ACFTHRS: LOW COLL ANGLE: .7HIGH COLLANGLE: 15.1FWD CYC ANGLE: 33.1AFT CYCANGLE: 19.6LEFT CYC ANGLE: 15.2RIGHT CYCANGLE: 15.3TAIL ROTOR FINAL ANGLE: RED3.05; BLK 3.07; YEL 2.99: BLU 3.03:

02-Apr-2013 1


QC000000



8.7.DATE

6.REMARKS

4. 5.



AR AASFH-60-13-AMAM-01 (FLIGHT CONTROL RIGGINGPROCEDURES) COMPLIED WITH @ 11065.1ACFT HRS

05-Apr-2013 1


QC000000

AR AASFH-60-13-ASAM-05 (BREEZE EASTERNVARIABLE SPEED ELECTRIC RESCUE HOIST)COMPLIED WITH AT 11065.1 ACFT HRS. THISHOIST NOT INSTALLED ON THIS AIRCRAFT.

09-Apr-2013 1


QC000000

AR AASFH-60-13-AMAM-07 (LOAD DEMAND SPINDLE(LDS) CABLE CLEARANCE) COMPLIED WITHAT 11065.1 ACFT HRS .

12-Apr-2013 1


QC000000

AR AASFMAIN ROTOR COMPLETED @ 11066.4 ACFTHRS: LOW COLL ANGLE: -.55, HIGH COLLANGEL: 15.05, FWD CYCLIC ANGLE: 33.2, AFTCYCLIC ANGLE: 20.2, LEFT CYCLIC ANGLE:15.6, RIGHT CYCLIC ANGLE: 14.7, PRIMARYSERVO CONTROL ROD BIAS: FWD SHT 3 1/2FLATS, AFT LNGTH 3 1/2 FLATS, LAT SHT 1FLATS, T/R CABLE TENSION: L/H 160, R/H 160 ,AT 74.5 F, T/R BIAS MEASURMENTS REDANGLE 3.0, BLK 3.0, YEL 3.0, BLU 3.0, T/RSERVO PISTON TRAVEL: EXTENDED 3.52INITIAL, HIGH COLL FULL LEFT YAW 3.50,RETRACTED 0, LOW COLL FULL RIGHT YAW.025, ACFT RIGGED BY JN268702, AM430570.

24-Apr-2013 1


QC000000

AR AASFCOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-06(PHASE MAINTENANCE INSPECTIONCHECKLIST CHANGE)

17-May-2013 1


QC000000

AR AASFH-60-13-SOF-01 (ATTITUDE HEADINGREFERENCE SET AHRS) COMPLIED WITH AT11076.9 ACFT HRS. DUAL FOGS INSTALLEDON THIS ACFT.

01-Jun-2013 1


QC000000


ACE COMPLETED AT 11109 AIRCRAFT HOURSAT LITTLE ROCK, AR BY TEAM MEMBERS W &Q.

21-Jun-2013 1


QC000000

AR AASFH-60-13-AMAM-10(LCF CHANGE 64) COMPLIEDWITH @ 11152.4 ACFT HRS

26-Aug-2013 1


QC000000


AIRWORTHINESS RELEASE (AWR) FOR THECRASHWORTHY EXTERNAL FUEL TANKSYSTEMS (CEFS) ON UH/HH-60A/LHELICOPTERS (AWR 1451 DATED 15OCT12 R4)INSTALLED AT 11197.6 ACFT HRS.

26-Sep-2013 1


QC000000

AR AASFGEN-13-AMAM-04 (AN / APN-209 RADARALTIMETER SET COMPONENT TRACKING)COMPLIED WITH @ 11152.4

17-Oct-2013 1

NORTH LITTLE ROCK,ARKANSAS

QC000000

AR AASFH-60-14-SOF-01 (BREEZE EASTERN EXTERNALRESCUE HOIST INSTALLATION) COMPLIEDWITH @ 11206.9 ACFT HRS. HOIST NOTINSTALLED.

01-Nov-2013 1


QC000000



8.7.DATE

6.REMARKS

4. 5.



AR AASFH-60-13-AMAM-11 (MAIN XMSN BOWLATTACHMENT HARDWARE REPLACEMENT)COMPLIED WITH AT 11227.4 ACFT HRS.

13-Nov-2013 1


QC000000

AR AASFH-60-14-ASAM-02 (HEALTH USAGEMONITORING SYSTEM (HUMS)ACCELEROMETERS) COMPLIED WITH @11231.4 ACFT HRS

26-Nov-2013 1


QC000000

AR AASFH-60-14-ASAM-04 (MAIN ROTOR HUB NDI)COMPLIED WITH @ 11235.8 AIRCRAFT HOURS

03-Jan-2014 1


QC000000

AR AASFH-60-14-AMAM-03 (DISCREPANT CONNECTINGLINK) COMPLIED WITH @ 11235.8 ACFT HRS.

09-Jan-2014 1


QC000000

AR AASFH-60-14-ASAM-03 (ENGINE INLET BARRIERFILTER (EIBF) BRACKET REMOVAL) @ 11240.8ACFT HRS.

21-Jan-2014 1


QC000000

AR AASFTAIL ROTOR BIAS SET: READINGS ARE ASFOLLOWS : RED- 0.00,3.01,3.01, FINAL DEG-3.01, BLACK-0.01,3.01,3.01,FINAL DEG-3.01,YELLOW- 0.00, 3.01,3.01, FINAL DEG-3.01,BLUE- 0.01, 3.02, 3.02, FINAL DEG-3.02,DIMENSION CHECK READINGS ARE ASFOLLOWS: RED-4.855,5.181,DIFF-.326, BLACK-4.166, 4.509, DIFF-.343, YELLOW-4.862, 5.200,DIFF-.338, BLUE- 4.136,4.470, DIFF-.334, TAILROTOR BIAS SET AT 11244.3 ACFT HRS.

24-Jan-2014 1


QC000000

AR AASFH-60-14-SOF-02 (TAIL ROTOR PITCH CHANGESHAFT ASSY) COMPLIED WITH @ 11244.5ACFT HRS.

28-Jan-2014 1


QC000000

AR AASFH-60-14-AMAM-08 (COMMUNICATIONCONSOLE CIRCUIT BREAKER PROTECTION)COMPLIED WITH @ AIRCRAFT HOURS11270.4CONSOLE NOT INSTALLED

05-Mar-2014 1


KL415170

AR AASFH-60-14-AMAM-09 (MAIN TRANSMISSIONFILTER BOWL AND CHIP DETECTORATTACHMENT HARDWARE) COMPLIED WITH@ 11287.7 ACFT HRS

15-Mar-2014 1


JJ638123

AR AASFH-60-14-AMAM-10 (HONTEK COATED MAINROTOR BLADE REMOVAL) COMPLIED WITH @11287.7 ACFT HRS.

11-Apr-2014 1


KL415170

AR AASFH-60-14-ASAM-06 (FLIGHT CONTROL MIXER)COMPLIED WITH @ 11287.7 ACFT HRS.

17-Apr-2014 1


KL415170

AR AASFH-60-14-AMAM-12 (MAIN ROTOR SPINDLE NUTRETIREMENT LIFE EXTENSION) COMPLIEDWITH @ 11287.7 ACFT HRS.

01-May-2014 1


JJ638123

AR AASFH-60-14-AMAM-05 (LCF CHANGE 65)COMPLIED WITH @ 11287.7 ACFT HRS.

17-May-2014 1


JJ638123



8.7.DATE

6.REMARKS

4. 5.



AR AASFH-60-14-AMAM-05 ULLS-A(E) ALC LEGITIMATECODE FILE (LCF) CHANGE 65 REQUIREMENTS@ 1125.0 ACFT HRS.

17-May-2014 2


CS452504

AR AASFH-60-13-AMAM-15 (CEFS RIGHT HAND FUELCELL COVER PLATE) COMPLIED WITH @11287.7 ACFT HRS.

22-May-2014 1


KL415170

AR AASFMAIN ROTOR RIG COMPLETED @ 11287.7ACFT HRS, READING ARE AS FOLLOWS: LOWCOLLECTIVE: -0.605, HIGH COLLECTIVE:15.8975, FWD CYCLIC ANGLE: 33.36, AFTCYCLIC ANGLE: 19.35, LEFT CYCLIC ANGLE:15.41, RIGHT CYCLIC ANGLE: 15.52, PRIMARYSERVO CONTROL ROD BIAS: FWDSHORTENED 2 FLATS, AFT LENGTHENED 2FLATS. LAT NOT ADDJUSTMENT, T/R CABLETENSION L/H: 168, R/H : 165 AT 83.9 DEG F,T/R SERVO PISTON TRAVEL EXTENEDE:INITIAL: 3.52 HIGH COLL FULL LEFT: 3.48,RETRACTED: INITIAL: 0, LOW COLLECTIVEFULL RIGHT: 0.02, T/R BIAS MEASUREMENTS:RED DIFF: .353 FINAL ANGLE 2.94, BLK DIFF:.36 FINAL ANGLE: 3.05, YELLOW DIFF:.371FINAL ANGLE 3.05, BLUE DIFF: .339 FINALANGLE: 2.97. ACFT RIGGED BY EL437658,RB577886, JH756451.

03-Jun-2014 1


JJ638123

AR AASFH-60-14-AMAM-14 (IVHMS CABLING)COMPLIED WITH @ 11287.7 ACFT HRS.

10-Jun-2014 1


KL415170

AR AASFPMI 1 COMPLETED @ 11287.7 ACFT HRS, NEXTPMI 2 DUE @ 11647.7 ACFT HRS.

23-Jun-2014 1


JJ638123

AR AASFH-60-14-AMAM-09 (MAIN TRANSMISSIONFILTER BOWL AND CHIP DETECTOR HDW)COMPLIED WITH @ 11287.7 ACFT HRS.

23-Jun-2014 2


JJ638123

AR AASFGEN-12-AMAM-07 (GENERAL,AIRCRAFT FIRSTAID KIT MODERNIZATION) COMPLETED @11287.7 ACFT HRS.

23-Jun-2014 3


JJ638123

AR AASFH-60-14-SOF-03 (DISCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS) COMPLIED WITHAT 11291.7 ACFT HRS.

08-Jul-2014 1


JJ638123

AR AASFMEC 184703 ONE TIME FLT AUTHORIZEDFROM CAMP ROBINSON AR TO SPRINGFIELDMO. FOR REPAIR TO TAILCONE STA. 485

09-Jul-2014 1


CS452504


ACE COMPLETED AT 11294 AIRCRAFT HOURSAT SPRINGFIELD MO BY TEAM MEMBERS RR& K

29-Jul-2014 1

SPRINGFIELD, MO 65803

AS425855

MO TASMGCOMPLIED WITH H-60-14-ASAM-10 MAINTRANSMISSION PLANETARY CARRIERASSEMBLY AT 11293.7 ACFT HOURS.

02-Sep-2014 1


KH848355

MO TASMGCOMPLIED WITH H-60-14-ASAM-09 ENGINEOUTPUT SHAFT AT 11293.7 ACFT HOURS.

02-Sep-2014 2


KH848355



8.7.DATE

6.REMARKS

4. 5.



MO TASMGH-60-14-ASAM-08 (HMU QUICK DISCONNECTPINS) COMPLIED WITH AT 11293.7 ACFT HRS.

02-Sep-2014 3


KH848355

MO-TASMGLOWER TAIL CONE FRAME STA. 485REPLACED I/A/W MEC F186776 AT 11293.7ACFT HOURS.

09-Sep-2014 1


SK948291

MO-TASMGR/H TAIL CONE FRAME AT STA. 485REPLACED I/A/W MEC F187132 AT 11293.7ACFT HOURS.

09-Sep-2014 2


SK948291

MO TASMGCOMPLIED WITH H-60-14-AMAM-16 ATTITUDEHEADING REFERENCE UNIT 2410 TRACKINGAT 11293.7 ACFT HOURS.

23-Sep-2014 1


KH848355

MO TASMGCOMPLIED WITH H-60-14-SOF-04 OPERATORSAND CREWMEMBERS CHECKLIST AT 11293.7ACFT HOURS.

26-Sep-2014 1


KH848355

AR AASFH-60-14-AMAM-19 (LCF CHANGE 66)COMPLIED WITH @ 11297.2 ACFT HRS.

02-Oct-2014 1


JJ638123

AR AASFH-60-15-SOF-01 (OIL COOLER FAN AXIALBEARING) COMPLIED WITH @ 11297.2 ACFTHRS.

30-Oct-2014 1


KL415170

AASF / W895AAH-60-15-AMAM-02 (IVHMS FIRE DETECTION)COMPLIED WITH @ 11302.9 ACFT HRS.

05-Nov-2014 1


KL415170

AR AASFH-60-15-ASAM-01 (LED CAUTION ADVISORYPANEL (CAP) COMPLIED WITH @ 11320.0ACFT HRS.

02-Dec-2014 1


JJ638123

AASF / W895AAH-60-15-AMAM-05 (AHRS EMERGENCYPROCEDURES) COMPLIED WITH @ 11324.0ACFT HRS.

15-Dec-2014 1


KL415170

AR AASFH-60-15-AMAM-06 (ASE EQUIPTMENT)COMPLIED WITH @ 11364.8 ACFT HRS.

06-Mar-2015 1


JJ638123

AR AASFH-60-15-AMAM-10 (AV-DEC GASKETINSPECTION) COMPLIED WITH @ 11404.4ACFT HRS.

28-May-2015 1


CG450464



8.7.DATE

6.REMARKS

4. 5.



AR AASFUPDATED AWRS: 1054 R15 06 APR 15 (BAMBIBUCKET );1120 R10 29OCT14 (M-240H WITHTATICAL LASER INSTALLED);1279 R5 13JUN14(COCKPIT DOORS AND CABIN DOORS);1309R8 14APR14 (OREGON AERO SEATCUSHIONS); 1310 04NOV05 (RT-1518C ARC-164HQII RADIO);1346 R22 15 DEC 2014(IVHMS ANDHUMS); 1407 R3 28MAY14(EFW & ELBIT WITHHUD);1425 R18 18 SEP 14 (CMWS, ICMD, P3I,OFP AND TIE INSTALLED); 1451 R6 26SEP14(CEFS);1466 R6 27AUG13(GARMIN GPSMAP);1477 R8 2 MAR 15 (FRIES R100297 FASTROAP INSERTION EXTRACTION SYSTEM);1479R2 13JAN12(MAIN MOD WITH IMPROVEDPLANETARY CARRIER);1494 R8 26SEP14(CMWS AND 5TH SENSOR);1513 R8 1DEC14(INTEGRATED PERFORMANCE AND AIRCRAFTCONFIGURATION (IPAC); 1516 R815SEP14(ELT EBC-406 HM);1529 R4 22JAN2015(FOGS DUAL CONFIG);1566 R4 13 MAR15(TITANIUM OR STAINLESS STEEL HOISTCABLE GUARD);1590 R5 04APR14 (AN-ARN-147 VOR-ILS REC ELEC MOUNT BASE);1682R18 15 APR 15 (UH60A WITH 701D CC OR 701CENGINE WITH AUTO RELIGHT & TDI);1753 R530JAN15 (DOPPLER GPS AN ASN 128B &D);1788 R5 23DEC15(FM IMMUNE ARN 147 VORILS);1800 R3 16JUL14 (EDM AND BFT);1913250CT13 (MSD-V3 LAPTOP); 1939 1 APR14( M4

02-Jun-2015 1


JJ638123

AR AASFH-60-15-ASAM-03 (TROOP/GUNNER SEATENTRGY ATTENUATORS) COMPLIED WITH @11416.9 ACFT HRS.

12-Jun-2015 1


JJ638123

AR AASFH-60-15-AMAM-11 (MODE-S TRANSPONDERADDRESS REVIEW) COMPLIED WITH AT11421.4 ACFT HRS. (MODE S ADDRESS53407344)

24-Jun-2015 1


CG450464

AFM, RASM-WACE COMPLETED AT 11453 AIRCRAFT HOURSAT NORTH LITTLE ROCK, ARKANSAS BY ACETEAM 2, W & BB

04-Sep-2015 1


DD459579

AR AASFCOMPLIED WITH H-60-15-AMAM-14 (ULLS-A(E)LCF CHG 67 REQUIREMENTS AT 11460.7 ACFTHRS.

22-Sep-2015 1


CG450464

AR AASFCOMPLIED WITH H-60-15-SOF-02 (FRIESRELEASE CABLE) AT 11466.7 ACFT HRS.

24-Sep-2015 1


CG450464

AR AASFCOMPLIED WITH REQUIREMENTS OF H-60-15-AMAM-18 (MEDEVAC CAROUSEL) @ 11466.7ACFT HRS.

30-Sep-2015 1


JJ638123

AR AASFCOMPLIED WITH H-60-16-AMAM-01 (ENGINEINLET BARRIER FILTER) @ 11486.0 ACFT HRS.

27-Oct-2015 1


JJ638123

AR AASFCOMPLIED WITH H-60-16-AMAM-03(PERSONNEL LOCATOR SET - PLS) REMOVAL@ 11497.0 ACFT HRS, NOT INSTALLED

24-Nov-2015 1


CG450464



8.7.DATE

6.REMARKS

4. 5.



AR AASFCOMPLIED WITH H-60-16-ASAM-02(DEFECTIVE FUEL HOSES) @ 11511.8 ACFTHRS.

06-Jan-2016 1


ES708572

AR AASFH-60-16-ASAM-01 (INBOARD RETENTIONPLATE TQ CHECK) COPLIED WITH @ 11511.8ACFT HRS.

08-Jan-2016 1


JJ638123

AR AASFM/R AND T/R RIG COMPLETED @ 11511.8 ACFTHRS. READINGS ARE AS FOLLOWS; LOWCOLL ANGLE: -0.625, HIGH COLL ANGLE:15.125, FWD CYCLIC ANGLE: 33.8, AFT CYCLICANGLE: 20.1, LEFT CYCLIC ANGLE: 15.6,RIGHT CYCLIC ANGLE: 15.4. PRIMARY SERVOCONTROL ROD DIAS: FWD: +2 FLATS, AFT -2FLATS, LAT: +1 FLAT. T/R SERVO PISTONTRAVEL IS AS FOLLOWS: INITIAL: 3.51, HIGHCOLL: 3.47, RETRACTED: INITIAL; 0, LOWCOLLECTIVE: 0.044. T/R CABLE TENSION ISSET AS FOLLOWS; L/H 158, R/H 159 24°C . T/RBIAS AS FOLLOWS RED DIAS : 2.99, BLACK:2.99, YELLOW: 3.01, BLUE: 3.00, VERIFY BIASRED: 2.98, BLACK: 2.99, YELLOW: 3.07, BLUE:3.05, COLLECTIVE FULL UP PEDAL FULLLEFT: RED 19.8, BLACK: 19.6, YELLOW: 19.8,BLUE: 19.6.

14-Jan-2016 1


JJ638123

AR AASFAMAM-UH60-16-06 T-CLIP INSTALLATION CW19 APR 16 @ 11546.2 ACFT HRS

20-Apr-2016 1


ES708572

AR AASFCOMPLIED WITH REQUIREMENTS OF GEN-16-AMAM-04 (TRANSPONDER BATTERYREPLACEMENT) @11568.7 ACFT HRS.

02-Jun-2016 1


JJ638123

AR AASFH-60-16-SOF-01 (UPPER CABIN STATION 379FRAME CRACKING) COMPLIED WITH @11596.9 ACFT HRS.

22-Jun-2016 1


JJ638123

AR AASFH-60-16-AMAM-09 (ULLS-A(E) COMPONENTSN/PN DUPLICATION COMPLIED WITH @11596.9 ACFT HRS.

23-Jun-2016 1


JJ638123

FT HOOD AFMA RASMW

ACE COMPLETED AT 11601 AIRCRAFT HOURSAT N LITTLE ROCK, AR BY TEAM MEMBERSRR & K

28-Jun-2016 1


AS425855

ARAASFH-60-16-AMAM-10 (PHASE LCF UPDATES)COMPLIED WITH THIS DATE @ 11600.9 ACFTHRS

22-Jul-2016 1


ES708572

AR AASFCOMPLIED WITH REQUIREMENTS OF H-60-16-SOF-02 (RESCUE HOIST OPERATIONALRESTRICTIONS @ 11600.9 ACFT HRS.

17-Aug-2016 1


JJ638123

AR AASFAIRCRAFT TRANSFERRED TO BESTPROGRAM ON 24 AUGUST 2016 FORARMY/BEST PROGRAM BY B CO 2-285TH AVNREG AT 11600.9 ACFT HOURS DATA PLATEREMAINED INSTALLED.

24-Aug-2016 1


JJ638123



8.7.DATE

6.REMARKS

4. 5.



SCIENCE &ENGINEERINGSERVICES LLC

H-60-AMAM-04 NOT COMPLIED WITH 07-Sep-2016 1

HUNTSVILLE

JP901591

SCIENCE &ENGINEERINGSERVICES LLC

H-60-16-AMAM-07 NOT COMPLIED WITH 07-Sep-2016 2

HUNTSVILLE

JP901591

SCIENCE ANDENGINEERINGSERVICES LLC

H-60-16-ASAM-06 NOT COMPLIED WITH 16-Sep-2016 1

HUNTSVILLE

JH902419


DATE AC HRS SHAFT VERTICAL REASON FOR VIB CHECKLONGITUDINALLATERAL

IPS READINGS4.

8724615HELICOPTER, UTILITYUH-60A3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Report Date: 16-Sep-2016 1/4

COMPLETEION OF PMS-202-Nov-2004 TAIL ROTOR 0.01008961.7

COMPLETEION OF PMS-202-Nov-2004 #1 ENG 0.06008961.7

COMPLETEION OF PMS-202-Nov-2004 #2 ENG 0.26008961.7

COMPLETETION OF PMS-202-Nov-2004 OIL COOLER 0.060.1708961.7

COMPLETEION OF RETORQUES15-Nov-2004 TAIL ROTOR 0.04008964.7

REPLACEMENT OF #2 ENGINE16-Mar-2005 @ ENGINE 0.3008982.1

COMPLETION 120 HR. INSP14-Jun-2005 TAIL ROTOR 0.13009081.7

COMPLETION 120 HR INSP14-Jun-2005 OIL COOLER 0.060.2309081.7

COMPLETION 120 HR INSP14-Jun-2005 #1 ENG SHF 0.35009081.7

COMPLETION 120 HR. INSP14-Jun-2005 #2 ENG SHA 0.48009081.7

120 HR INSP08-Sep-2005 OIL COOLER 0.070.2809184.9

120 HR INSP08-Sep-2005 #1 ENGINE 0.17009184.9

120 HR INSP08-Sep-2005 #2 ENGINE 0.25009184.9

120 HR INSP08-Sep-2005 TAIL ROTOR 0.06009184.9

INBOARD RETENTION TQ CHK25-Oct-2006 TAIL ROTOR 0.03009397.9

120HR INSP09-Dec-2006 #1 ENG HSS 0.11009499.9

120 HR INSP09-Dec-2006 #2 ENG HSS 0.18009499.9

120 HR INSP09-Dec-2006 OIL COOLER 0.080.209499.9

120 HR INSP09-Dec-2006 T/R 0.05009499.9

POST PMI 208-Feb-2007 #1 ENG 0.13009596.9

POST PMI 208-Feb-2007 #2 ENG 0.08009596.9

POST PMI 208-Feb-2007 TAIL ROTOR 0.05009596.9

POST PMI 208-Feb-2007 OIL COOLER 0.150.4109596.9

120 HR INSP26-Apr-2007 #1 ENG 0.23009716.4

120 HR INSP26-Apr-2007 #2 ENG 0.39009716.4

120 HR INSP26-Apr-2007 OIL COOLER 0.160.3209716.4

120 HR INSP26-Apr-2007 TAIL ROTOR 0.07009716.4

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.



POST PMI-109-Jun-2007 T/R 0.03009789.3

POST PMI-109-Jun-2007 OIL COOLER 0.070.4209789.3

POST PMI-109-Jun-2007 #1 ENG 0.35009789.3

POST PMI-109-Jun-2007 #2 ENG 0.22009789.3

INBRD RETENTION PLATE RETORQUE14-Jun-2007 T/R 0.03009798.3

T/R PADDLE BOOT REPLACEMENT30-Jun-2007 T/R 0.18009848

120 HR INSP15-Jul-2007 T/R 0.07009906

120 HR INSP15-Jul-2007 OIL COOLER 00.0609906

120 HR INSP15-Jul-2007 # 1 ENG 0.35009906

120 HR INSP15-Jul-2007 # 2 ENG 0.18009906

POST RESET16-Apr-2008 #1 ENG 0.29009975.1

POST RESET16-Apr-2008 #2 ENG 0.21009975.1

POST RESET16-Apr-2008 T/R 0.07009975.1

POST RESET16-Apr-2008 OIL COOLER 00.1809975.1

#1 ENG INSTALL04-Mar-2009 #1 ENG 0.140010062.1

120 HR INSP30-Apr-2009 #1 ENG 0.050010095.1

120 HR INSP30-Apr-2009 #2 ENG 0.110010095.1

120 HR INSP30-Apr-2009 OIL COOLER 00.09010095.1

120 HR INSP30-Apr-2009 TAIL ROTOR 0.110010095.1

REINT OF #2 ENG23-Sep-2009 #2 ENG 0.240010172.7

120 HR INSP09-Jan-2010 T/R 0.170010214.9

120 HR INSP09-Jan-2010 #1ENG 0.160010214.9

120 HR INSP09-Jan-2010 OIL COOLER 00.269010214.9

120 HR INSP09-Jan-2010 #2 ENG 0.210010214.9

T/R BOOT REPLACEMENT17-Feb-2010 TAIL ROTOR 0.020010250.3

POST PHASE TEST FLT13-Aug-2010 #1 ENG 0.040010325.3

POST PHASE TEST FLT13-Aug-2010 #2 ENG 0.270010325.3




IPS READINGS4.



POST PHASE TEST FLT13-Aug-2010 OIL COOLER 00.1010325.3

POST PHASE TEST FLT13-Aug-2010 TAIL ROTOR 0.080010325.3

STRAT AIR RECONFIGURE28-Jan-2011 TAIL ROTOR 0.030010426.5

120 HR INSP07-Apr-2011 #1 ENG 0.080010557.9

120 HR INSP07-Apr-2011 #2 ENG 0.370010557.9

120 HR INSP07-Apr-2011 OIL COOLER 00.06010557.9

120 HR INSP07-Apr-2011 T/R 0.080010557.9

120 HR/POST PMI-205-Jun-2011 #1 ENG 0.170010665.9

120 HR/POST PMI-205-Jun-2011 #2 ENG 0.290010665.9

120HR/POST PMI II05-Jun-2011 OIL COOLER 0.130.32010665.9

120HR/ POST PMI II05-Jun-2011 TAIL ROTOR 0.040010665.9

REPLACED TORN BOOT06-Jun-2011 TAILROTOR 0.090010665.9

120 HR INSP26-Mar-2012 #1 ENG 0.240010897.5

120 HR INSP26-Mar-2012 #2 ENG 0.050010897.5

120 HR INSP26-Mar-2012 OIL COOLER 0.060.2010897.5

120 HR INSP26-Mar-2012 TAIL ROTOR 0.020010897.5

COMPLETION OF RESET INSPECTION.13-Jul-2012 # 1 ENGINE 0.360010953.6

COMPLETION OF RESET INSPECTION.13-Jul-2012 # 2 ENGINE 0.210010953.6

COMPLETION OF RESET INSPECTION.13-Jul-2012 TAIL ROTOR 0.010010953.6

COMPLETION OF RESET INSPECTION.13-Jul-2012 OIL COOLER 0.040.16010953.6

MAIN TRANSMISSION REPLACEMENT11-Apr-2013 #1 ENGINE 0.270011065.1

MAIN TRANSMISSION REPLACEMENT11-Apr-2013 #2 ENGINE 0.020011065.1

MAIN TRANSMISSION REPLACEMENT11-Apr-2013 OIL COOLER 0.10.25011065.1

MAIN TRANSMISSION REPLACEMENT11-Apr-2013 TAIL ROTOR 0.060011065.1

MAIN AND TAIL ROTOR RIG30-Apr-2013 TAIL ROTOR 0.060011066.4

120HR INSP28-May-2013 #1 ENGINE 0.350011073.6

120HR INSP28-May-2013 #2 ENGINE 0.190011073.6




IPS READINGS4.



120HR INSP28-May-2013 OIL COOLER 0.030.12011073.6

120HR INSP28-May-2013 TAIL ROTOR 0.080011073.6

#1 DRIVESHAFT REMOVAL / RE-INSTALL26-Sep-2014 OIL COOLER 00.22011294.7

120 HR07-Jun-2015 #1 ENG 0.120011408.7

120 HR07-Jun-2015 #2 ENG 0.090011408.7

120 HR07-Jun-2015 TAIL ROTOR 0.050011408.7

120 HR07-Jun-2015 OIL COOLER 0.050.18011408.7

ENGINE REINSTALL02-Sep-2015 #2 ENG 0.040011451.6

OIL COOLER REPLACEMENT02-Sep-2015 OIL COOLER 0.070.22011451.6

RMV AND REINSTALL OF T/R BLADES26-Jan-2016 TAIL ROTOR 0.130011514.8

120 HR12-Feb-2016 #1 ENG 0.190011527.2

120 HR12-Feb-2016 #2 ENG 0.070011527.2

120 HR12-Feb-2016 TAIL ROTOR 0.050011527.2

120 HR12-Feb-2016 OIL COOLER 0.120.43011527.2

06-May-2016 TAIL ROTOR 0.090011554.2

6. Remarks




8724615HELICOPTER, UTILITY UH-60A

7. FREQUENCY 4.

5. ITEMS TO BE INSPECTED

2. MODEL 3. SERIAL NUMBER 1. NOMENCLATURE

8. NEXTNO DUE 6. REFERENCE 9. COMPLETED AT

INSP

A020 11610.910TM 1-1520-237-PMDPERFORM M/R SPINDLE LUGS,M/R CUFF, TIP CAPSINSPECTION

11600.9H

A022 07 Jul 201614TM 1-1520-237-23-914 DAY FLYABLE STORAGEENGINE RUN UP

23 Jun 2016D

A092 18 Jul 201630TM 11-6140-203-23&P30 DAY SLAB BATTERYINSPECTION (D8565/11-1)

18 Jun 2016D

A100 18 Sep 201630DA PAM 738-751#1 ENGINE HISTORY RECORDERREADING DUE

19 Aug 2016D

A101 18 Sep 201630DA PAM 738-751#2 ENGINE HISTORY RECORDERREADING DUE

19 Aug 2016D

A103 24 Jul 201630TM 1-1500-344-23AIRCRAFT WASH DUE 24 Jun 2016D

A110 11608.740TM 1-1520-237-PMSPMS 40 HOUR INSPECTION 11568.7H

A115 24 Jul 201630TM 1-1520-237-23-12LUBE REQUIRMENTS 24 Jun 2016D

A115 11640.940TM 1-1520-237-23-12LUBE REQUIRMENTS 11600.9H

A116 11960.9360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

11600.9H

A116 23 Jun 201712H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

23 Jun 2016M

A117 11960.9360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 11600.9H

A117 23 Jun 201712H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 23 Jun 2016M

A140 11647.7120AWR 1346R16, IVHMSIN ACF

DOWNLOAD AND REVIEW IVHMSDATA

11527.7H

A160 14 Sep 201690TM 1-1520-237-23-1290 DAY CORROSIONINSPECTION

16 Jun 2016D

A177 16 Sep 201690AR 95-190 DAY REVIEW/UPDATE OF 365-4 ENTRIES

18 Jun 2016D

A210 11647.2120TM 1-1520-237-23-12120 HOUR INSPECTIONREQUIREMENTS

11527.2H

A211 11960.9360H-60-10-AMAM-11APU OIL SAMPLE 11600.9H

A211 23 Jun 201712H-60-10-AMAM-11APU OIL SAMPLE 23 Jun 2016M

A213 11647.7120TM 1-2840-248-23ENGINE COMPRESSORCLEANING

11527.7H

A214 11647.7120TM 1-1520-237-23-12CLEAN TAIL WHEEL ADAPTER 11527.7H

A222 06 Mar 2017360TM 1-1680-377-13&PAMSS SURVIVAL KITINSPECTION

11 Mar 2016D

A230 25 Sep 2016120MWO 1-1520-237-50-77INSPECT BATTERYCOMPARTMENT FORCORROSION (SLAB)

28 May 2016D

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

A295 11647.7360TM 1-1520-237-23-12STABILATOR ACTUATOR ASSYLUBE

11287.7H

A296 11647.7360TM 1-1520-237-23-12STABILATOR INSPECTION 11287.7H

A298 11960.9360TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 11600.9H

A298 23 Jun 201712TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 23 Jun 2016M

A299 11956.9360TM 1-1520-237-23-12SWASHPLATE LUBE 11596.9H

A299 23 Jun 201712TM 1-1520-237-23-12SWASHPLATE LUBE 23 Jun 2016M

A320 11647.7360TM 1-2840-248-23ENGINE INSPECTION &CLEANING

11287.7H

A400 12007.7720TM 1-1520-237-PMIPMI-1 11287.7H

A401 11647.7720TM 1-1520-237-PMIPMI-2 10927.7H

A408 11647.7720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-2, AREA 5 AND 6)

10927.7H

A410 12007.7720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-1, AREA 1 THRU 4)

11287.7H

A415 11647.7720H-60-10-AMAM-11MAIN GEARBOX OIL SAMPLE-PART # 073, 074, 076

10927.7H

A440 11647.7720TM 1-1520-237-23-12CLEAN TAIL WHEEL LOCKPIN 10927.7H

A470 12165.91500TM 1-1520-237-23-12REPLACE NUMBER TWOCROSSFEED VALVE

10665.9H

A471 13113.62160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

10953.6H

A472 13113.62160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

10953.6H

A473 13113.62160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

10953.6H

A476 15953.65000TM 1-1520-237-23-12REPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

10953.6H

A477 14975.15000TM 1-1520-237-23-12REPLACEMENT OF STABILATORACTUATOR BOLTS

9975.1H

A480 14255.65000TM 1-1520-237-23-12REPLACE PIVOT BOLT 70400-08159-101,102,103,104

9255.6H

A485 14255.65000TM 1-1520-237-23-12REPLACE BELLCRANK BOLT70400-08159-105,106,107,108

9255.6H

A496 29 Oct 20166TM 1-1500-204-23-1CF3BR FIRE EXTINGUISHERWEIGHT TEST & INSPECTION

29 Apr 2016M

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

23 Jun 2016M

A502 23 Dec 20166TM 1-1520-237-23-12INSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

23 Jun 2016M






7. FREQUENCY 4.




INSP

A530 04 Nov 201612DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

04 Nov 2015M

A532 26 Sep 201612TM 1-1500-204-23-4COMPASS SWING / RMI 26 Sep 2015M

A533 17 Dec 201612TM 1-1520-237-23-12PITOT STATIC SYSTEMINSPECTION

17 Dec 2015M

A534 20 Apr 201824TM 1-1500-204-23-1FIRST AID KIT INSPECTION 20 Apr 2016M

A538 01 Jul 201712TM 1-1520-237-23-12FAT/OAT GAUGEINSPECTION/TEST

01 Jul 2016M

A541 08 Jul 201712TM 1-1520-237-23, C4REPLACE DIGITAL CLOCKBATTERY

08 Jul 2016M

A550 26 Jun 201712AWR1346R16IVHUMS BATTERYREPLACEMENT

26 Jun 2016M

A553 24 Sep 201612AR 95-1AIRCRAFT WEIGHINGINVENTORY (365-1)

24 Sep 2015M

A580 10 Jun 201724TM 11-6140-203-23&PRETURN SLAB TO AVIM FORCAPACITY CHECK (VEREY 24MONTH)

10 Jun 2015M

A621 25 Sep 201624AR 95-1AIRCRAFT WEIGHING CLASS 2 25 Sep 2014M

A625 10 Jun 201860TM 11-6140-203-23&PREPLACEMENT OF SLABBATTERY (SLAB)

10 Jun 2013M

A630 01 Nov 2019114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 May 2010M

A633 01 Nov 2019114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 May 2010M

A638 01 Nov 2019114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

01 May 2010M

A640 01 Nov 2019114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

01 May 2010M

A648 21 Mar 2023180TM 1-1520-237-23REPLACE T/R SPRING CAPSULEASSY

21 Mar 2008M

A660 01 Jun 201672TB 9-1300-385REPLACE THRUSTEREMERGENCY RELEASE CARGOHOOK, MJ20

01 Jun 2010M

A665 11 Jul 201648H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

11 Jul 2012M

A670 11 Jul 201648TM 1-1520-237-23-1CABIN TUB INSPECTION 11 Jul 2012M

A673 11 Jul 201648TM 1-1520-237-23-12FUEL CELL CORROSIONINSPECTION

11 Jul 2012M

A675 11 Jul 201648TM 1-1520-237-23-12FLIGHT CONTROL ROD INSP 11 Jul 2012M

A695 11647.7720H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

10927.7H

A695 17 Apr 201848H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

17 Apr 2014M






7. FREQUENCY 4.




INSP

A755 17961.79000H-60-10-ASAM-11PC LINK TO SWASHPLATEBOLTS REPLACEMENT

8961.7H

E015 02 Oct 2016180MWO 1-1520-237-50-92ASN 128D DOPPLER GPSBATTERY REPLACEMENT

05 Apr 2016D

E040 14 Sep 201690TM 11-5841-294-12APR-39 RADAR/LASERWARNING OPNL CHECK, 5841-01-236-8951

16 Jun 2016D

E125 16 Aug 201690TM 11-5810-262-23KY-58 PMCS/OPNL CHECK 18 May 2016D

E145 25 Sep 20166TM 11-5821-333-12AN/ARC-201 A(V) SINCGARS HUBBATT REPL

25 Mar 2016M

E155 22 Aug 20166TM 11-5810-262-23KY-58 BATTERY REPLACEMENT 22 Feb 2016M

E222 10 Oct 201612AWR 1516 (EBC-406HM)

ELT FUNCTIONAL SELF TEST 10 Oct 2015M

E300 20 Jul 201630AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

20 Jun 2016D

E300 11716.9120AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

11596.9H

E320 01 Dec 2016360AWR 1516 FOR ELTEMERGENCY LOCATORTRANSMITTER G-SWITCH (EBC-406HM)

07 Dec 2015D

E325 23 May 201860AWR 1516R2 FOR ELTREPLACEMENT OF ELTBATTERY PN GS-46

23 May 2013M

E330 05 May 20166AWR1346R16UNDER WATER ACOUSTICBEACON BATTERYREPLACEMENT

05 May 2010Y

E331 11680.2120AWR1346R16TEST ** UNDERWATERACCOUSTIC BECON BATTERYREPLACEMENT ** TEST

11560.2H

E331 06 Oct 20166AWR1346R16TEST ** UNDERWATERACCOUSTIC BECON BATTERYREPLACEMENT ** TEST

06 Apr 2016M

E351 30 Dec 20166TM 11-5895-1841-13PREPLACE APX-118TRANSPONDER BATTERY

30 Jun 2016M




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: 1/1216-Sep-2016

87246151520010350266 00HELICOPTER, UTILITY

156001095713502C12D

79718962B4970035170219-05001-042TAIL CONE FITTING CCCC COND COND

162001231183103A01

011188BEM148370250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001231183103A01

28810954BEM200670250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001421089003B01

010958BMC48170250-13101-044TAIL SHOCK STRUT ASSY CCCC COND COND

165001285302405A01Z RED

85710954A106-0178770106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z BLACK


165001285302405A01Z YELLOW


165001285302405A01Z BLUE


531501537465205A02H

85910954B941-1292070103-08108-041SOLID BLADE PIN CCCC COND COND

531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


161501199764605A03A

534910954A107-0129970104-08000-050SWASHPLATE ASSY CCCC COND COND

161501383899206A11

357711065A2580080370351-08080-045ACCESSORY MODULE CCCC COND COND

161501383899206A11

476011065A2580231070351-08080-045ACCESSORY 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

420211065A2250006370351-08100-076MAIN TRANSMISSIONMODULE

CCCC COND COND

161501353382506E

269811065A2640604770351-08001-049INPUT MODULE CCCC COND COND

161501353382506E

110711065A2640756070351-08001-049INPUT MODULE CCCC COND COND

168001074515206F

438910954A005-0179470357-06300-042INTERMEDIATE GEARBOX CCCC COND COND

161501376508906G01

369210954A006-0218670358-06600-046TAIL ROTOR GEARBOXASSY

CCCC COND COND

161501524780506H04

97910954C845-0254270361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501524780506H04

97910954C845-0364870361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501081277506H06

19921095433149-10770361-03001-045SHAFT ASSY, T/R DRV SEC1

CCCC COND COND

161501158951706H08

142311452A2700359270361-03009-047SHAFT ASSY, T/R DRV SEC2

CCCC COND COND

161501158952206H09 FORWARD

010954WG30049-00268

70361-05001-051SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501158952206H09 CENTER

010954WG30049-00377

70361-05001-051SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501158952206H09 AFT

010954WG30050-00012

70361-05001-051SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501083295306H11

590210954A273-0106770361-05002-045SHAFT ASSY, T/R DRV SEC6

CCCC COND COND

161501158578806H12

188110954354302970361-06002-047SHAFT ASSY, T/R DRV SEC7

CCCC COND COND

432001207722807A01

147711065239087ABR70652-02300-050PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01

3919995K0723ABR70652-02300-050PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01

92911065K4395ABR70652-02300-050PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

481001102247307B05A # 1

97910954122203213850-3-1VALVE, SOLENIOD CCCC COND COND

481001102247307B05A # 2

24710954170563213850-3-1VALVE, SOLENIOD CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






165001250376707B11

9219975C401-020190204-0004ACCUMULATOR CCCC COND COND

168001342049608B20 COPILOT'S

199210954065100-601561-000PANEL INDICATOR (PDU) CCCC COND COND

168001342049608B20 PILOT'S

1992109541245100-601561-000PANEL INDICATOR (PDU) CCCC COND COND

611501114969609A01

216811065544128B302-8-DMGENERATOR CCCC COND COND

611501114969609A01

214511065617328B302-8-DMGENERATOR CCCC COND COND

168001310225911C21

011288TMD0484374859

70400-02300-048MIXER ASSEMBLY CCCC COND COND

156001411515111D17

08962UNK4615 #270209-22103-065SERVO BEAM FITTING CCCC COND COND

156001411515611D17

08962UNK4615#370209-22103-067SERVO BEAM FITTING CCCC COND COND

156001411515011D17


156001411514811D17


168001261204411D25

83710954829270400-06641-117STABILATOR ACTUATOR CCCC COND COND

168001261204411D25

402210954B292-0456570400-06641-117STABILATOR ACTUATOR CCCC COND COND

599601316274311D26 R/H

2952109542535A70902-02001-048STABILATOR AMPLIFIER CCCC COND COND

599601316274311D26 L/H

63210954R930-0054670902-02001-048STABILATOR AMPLIFIER CCCC COND COND

299501169529115A04

1309112887584-1353163290-100ENGINE SEQUENCINGUNIT

CCCC COND COND

NSN PENDING19E04B VER 1.15

167113282985P320A002-03SIGNAL DATACONVERTER

CCCC COND COND

584101421416219E05A

011198340HHHG7209AD01RECEIVER-TRANSMITTER,RADAR

CCCC COND COND

584101245909319E05C

011198967AAA3060591INDICATOR HEIGHT CCCC COND COND

660501503528419E06A

011294719765100-20ATTITUDE HEADINGREFERENCE UNIT

CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






589501504040719F02 VER 5.20

01142114351008939G-5RECEIVER-TRANSMITTERRADAR RT-1

CCCC COND COND

661001490516852A VER 002

89710954501096670901-01802-101AUTOMAT FLT CONTCOMPUTER

CCCC COND COND

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 COMPONENTS5/1216-Sep-2016

00

156001081924402C15J20000

A496-00846 8962896270209-06051-043TAIL PYLON FITTING RCRC20000

161501450483405A01A16054

B308-00091 01095470103-08112-047HUB, M/R ROTOR ASSY RCRC5100

161501442692605A01I RED15415

A001-02064 19391095470102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501442692605A01I BLUE15801

A001-02435 15531095470102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501442692605A01I YELLOW17239

E001-00495 1151095470102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501442692605A01I BLACK17031

E001-00695 3231095470102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501074515105A01L22962

A286-01094 19921095470351-08186-043MAIN ROTOR SHAFTEXTENDER

RCRC14000

161501127738805A01T13000

015152-00300 109541095470107-08400-046BIFILAR, M/R ROTORASSY

RCRC13000

161501106190305A0218927

A007-09656 22741160170150-09100-043MAIN ROTOR BLADEASSY

RCRC9600

161501106190305A0215425

A00700240 57761160170150-09100-043MAIN ROTOR BLADEASSY

RCRC9600

161501106190305A0218728


RCRC9600

161501106190305A0219488


RCRC9600

161501113818805B0216049

A00905509 52391128870101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501113818805B0219285

A00907494 19591124470101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501083681206G01B20962

A257-03002 19921095470102-11101-042O/B RETENTION PLATE(T/R)

RCRC12000

414001329342806H2313972

1019 01145252E15-1FAN AXIAL 002520

156001129125607A24 PITCH14868

B112-01210 90861095470410-02500-049SAS ACTUATOR RCRC13000

156001129125607A24 YAW18529

B112-08538 54251095470410-02500-049SAS ACTUATOR RCRC13000

156001129125607A24 ROLL23954

C112-04202 01095470410-02500-049SAS ACTUATOR RCRC13000

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

161501141753211C2313114

233-03246 18571095470400-06100-042TAIL ROTOR PITCHCHANGE SHAFT

022160

165001305695411C2522437B300-00123 3517109542227000-17TAIL ROTOR SERVO

ASSYRCRC

15000

165001143122611D01 AFT34654

B303-13202 010254274000-1031MAIN ROTOR PRIMARYSERVO

RCRC24400

165001143122611D01 LATERAL35255

B303-15978 010855274000-1031MAIN ROTOR PRIMARYSERVO

RCRC24400

165001143122611D01 FORWARD30083B303-01400B 49831066670410-02820-054MAIN ROTOR PRIMARY

SERVORCRC

24400

156001158968511D0413000B345-01833 103221032270400-08102-045AFT BELLCRANK RCRC

13000

156001164416111D0525962

A391-01977 0896270400-08112-045AFT TIE ROD SUPTFITTING

RCRC17000

168001164416011D0613154

M392-10519 01095470400-08111-042AFT TIE ROD ASSY RCRC2200

156001286887011D0713362

390-01512 0896270400-08117-049AFT BELLCRANK SPTASSY

RCRC4400

304001287243811D0821666015152-02056 2881095470400-08151-061LATERAL SWASHPLATE

LINKRCRC

11000

168001221286311D0928962F337-01846 19921095470400-08166-041LATERAL SERVO

BELLCRANKRCRC

20000

168001158965311D1118954346-00871 30001095470400-08104-048AFT WALKING BEAM RCRC

11000

156001289269711D1324954

344-02330 01095470400-08115-046LEFT TIE ROD RCRC14000

156001296948611D141427128801118 2941106570400-08114-051RIGHT TIE ROD ASSY RCRC

3500

168001158965211D152396266936-00728 19921095470400-08101-046FORWARD BELLCRANK RCRC

15000

156001221261911D1616554

B367-04879 01095470400-08162-042FWD BELLCRANK SPTASSY

RCRC5600













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.

1520010350266HELICOPTER,UTILITY

UH-60A 8724615 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 8 of 12

16-Sep-2016

COND COND

156001095713502C12D

79718962TAIL CONE FITTING B4970035170219-05001-042 CCCC

20000 20000

156001081924402C15J

89628962TAIL PYLON FITTING A496-0084670209-06051-043 RCRC

COND COND

162001231183103A01

011188FWD FIXED GEARSHOCK

BEM148370250-12051-045 CCCC

COND COND

162001231183103A01


BEM200670250-12051-045 CCCC

COND COND

162001421089003B01

010958TAIL SHOCK STRUTASSY

BMC48170250-13101-044 CCCC

5100 16054

161501450483405A01A

010954HUB, M/R ROTOR ASSY B308-0009170103-08112-047 RCRC

6400 15415

1615014426926 RED05A01I

193910954MAIN ROTOR SPINDLEASSY

A001-0206470102-08200-069 RCRC

6400 15801

1615014426926 BLUE05A01I


A001-0243570102-08200-069 RCRC

6400 17239

1615014426926 YELLOW05A01I


E001-0049570102-08200-069 RCRC

6400 17031

1615014426926 BLACK05A01I


E001-0069570102-08200-069 RCRC

14000 22962

161501074515105A01L

199210954MAIN ROTOR SHAFTEXTENDER

A286-0109470351-08186-043 RCRC

13000 13000

161501127738805A01T

1095410954BIFILAR, M/R ROTORASSY

015152-0030070107-08400-046 RCRC

COND COND

1650012853024 RED05A01Z

85710954DAMPER ASSY, M/R A106-0178770106-08100-046 CCCC

COND COND

1650012853024 BLACK05A01Z


COND COND

1650012853024 YELLOW05A01Z


COND COND

1650012853024 BLUE05A01Z


9600 18927

161501106190305A02

227411601MAIN ROTOR BLADEASSY

A007-0965670150-09100-043 RCRC

9600 15425

161501106190305A02


A0070024070150-09100-043 RCRC

9600 18728

161501106190305A02


A0070908770150-09100-043 RCRC

9600 19488

161501106190305A02


A0071405570150-09100-043 RCRC

COND COND

531501537465205A02H

85910954SOLID BLADE PIN B941-1292070103-08108-041 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

16-Sep-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

534910954SWASHPLATE ASSY A107-0129970104-08000-050 CCCC

10000 16049

161501113818805B02

523911288TAIL ROTOR BLADEASSY

A0090550970101-31000-043 RCRC

10000 19285

161501113818805B02

195911244TAIL ROTOR BLADEASSY

A0090749470101-31000-043 RCRC

COND COND

161501383899206A11

357711065ACCESSORY MODULE A2580080370351-08080-045 CCCC

COND COND

161501383899206A11

476011065ACCESSORY MODULE A2580231070351-08080-045 CCCC

COND COND

161501503311506A

420211065MAIN TRANSMISSIONMODULE

A2250006370351-08100-076 CCCC

COND COND

161501353382506E

269811065INPUT MODULE A2640604770351-08001-049 CCCC

COND COND

161501353382506E

110711065INPUT MODULE A2640756070351-08001-049 CCCC

COND COND

168001074515206F

438910954INTERMEDIATEGEARBOX

A005-0179470357-06300-042 CCCC

COND COND

161501376508906G01

369210954TAIL ROTOR GEARBOXASSY

A006-0218670358-06600-046 CCCC

12000 20962

161501083681206G01B

199210954O/B RETENTION PLATE(T/R)

A257-0300270102-11101-042 RCRC

COND COND

161501524780506H04

97910954DRIVESHAFT ASSYENGINE

C845-0254270361-08014-041 CCCC

COND COND

161501524780506H04

97910954DRIVESHAFT ASSYENGINE

C845-0364870361-08014-041 CCCC

COND COND

161501081277506H06

199210954SHAFT ASSY, T/R DRVSEC 1

33149-10770361-03001-045 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 10 of 12

16-Sep-2016

COND COND

161501158951706H08


A2700359270361-03009-047 CCCC

COND COND

1615011589522 FORWARD06H09

010954SHAFT ASSY, T/R SEC3,4,5

WG30049-0026870361-05001-051 CCCC

COND COND

1615011589522 CENTER06H09


WG30049-0037770361-05001-051 CCCC

COND COND

1615011589522 AFT06H09


WG30050-0001270361-05001-051 CCCC

COND COND

161501083295306H11


A273-0106770361-05002-045 CCCC

COND COND

161501158578806H12


354302970361-06002-047 CCCC

2520 13972

414001329342806H23

011452FAN AXIAL 101952E15-1 00

COND COND

432001207722807A01

147711065PUMP MODULE ASSY,HYDRAUL

239087ABR70652-02300-050 CCCC

COND COND

432001207722807A01


K0723ABR70652-02300-050 CCCC

COND COND

432001207722807A01


K4395ABR70652-02300-050 CCCC

13000 14868

1560011291256 PITCH07A24

908610954SAS ACTUATOR B112-0121070410-02500-049 RCRC

13000 18529

1560011291256 YAW07A24

542510954SAS ACTUATOR B112-0853870410-02500-049 RCRC

13000 23954

1560011291256 ROLL07A24

010954SAS ACTUATOR C112-0420270410-02500-049 RCRC

COND COND

4810011022473 # 107B05A

97910954VALVE, SOLENIOD 122203213850-3-1 CCCC

COND COND

4810011022473 # 207B05A

24710954VALVE, SOLENIOD 170563213850-3-1 CCCC

COND COND

165001250376707B11

9219975ACCUMULATOR C401-020190204-0004 CCCC

COND COND

1680013420496 COPILOT'S08B20

199210954PANEL INDICATOR (PDU) 065100-601561-000 CCCC

COND COND

1680013420496 PILOT'S08B20

199210954PANEL INDICATOR (PDU) 1245100-601561-000 CCCC

COND COND

611501114969609A01

216811065GENERATOR 544128B302-8-DM CCCC

COND COND

611501114969609A01

214511065GENERATOR 617328B302-8-DM CCCC

COND COND

168001310225911C21

011288MIXER ASSEMBLY TMD048437485970400-02300-048 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 11 of 12

16-Sep-2016

2160 13114

161501141753211C23

185710954TAIL ROTOR PITCHCHANGE SHAFT

233-0324670400-06100-042 02

15000 22437165001305695411C25

351710954TAIL ROTOR SERVOASSY

B300-001232227000-17 RCRC

24400 34654

1650011431226 AFT11D01

010254MAIN ROTOR PRIMARYSERVO

B303-13202274000-1031 RCRC

24400 35255

1650011431226 LATERAL11D01


B303-15978274000-1031 RCRC

24400 300831650011431226 FORWARD11D01


B303-01400B70410-02820-054 RCRC

13000 13000156001158968511D04

1032210322AFT BELLCRANK B345-0183370400-08102-045 RCRC

17000 25962

156001164416111D05

08962AFT TIE ROD SUPTFITTING

A391-0197770400-08112-045 RCRC

2200 13154

168001164416011D06

010954AFT TIE ROD ASSY M392-1051970400-08111-042 RCRC

4400 13362

156001286887011D07

08962AFT BELLCRANK SPTASSY

390-0151270400-08117-049 RCRC

11000 21666304001287243811D08

28810954LATERAL SWASHPLATELINK

015152-0205670400-08151-061 RCRC

20000 28962168001221286311D09

199210954LATERAL SERVOBELLCRANK

F337-0184670400-08166-041 RCRC

11000 18954168001158965311D11

300010954AFT WALKING BEAM 346-0087170400-08104-048 RCRC

14000 24954

156001289269711D13

010954LEFT TIE ROD 344-0233070400-08115-046 RCRC

3500 14271156001296948611D14

29411065RIGHT TIE ROD ASSY 2880111870400-08114-051 RCRC

15000 23962168001158965211D15

199210954FORWARD BELLCRANK 66936-0072870400-08101-046 RCRC

5600 16554

156001221261911D16

010954FWD BELLCRANK SPTASSY

B367-0487970400-08162-042 RCRC

COND COND

156001411515111D17

08962SERVO BEAM FITTING UNK4615 #270209-22103-065 CCCC

COND COND

156001411515611D17

08962SERVO BEAM FITTING UNK4615#370209-22103-067 CCCC

COND COND

156001411515011D17


COND COND

156001411514811D17


COND COND

168001261204411D25

83710954STABILATOR ACTUATOR 829270400-06641-117 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 12 of 12

16-Sep-2016

COND COND

168001261204411D25

402210954STABILATOR ACTUATOR B292-0456570400-06641-117 CCCC

COND COND

5996013162743 R/H11D26

295210954STABILATOR AMPLIFIER 2535A70902-02001-048 CCCC

COND COND

5996013162743 L/H11D26

63210954STABILATOR AMPLIFIER R930-0054670902-02001-048 CCCC

COND COND

299501169529115A04

130911288ENGINE SEQUENCINGUNIT

7584-1353163290-100 CCCC

COND COND

NSN PENDING VER 1.1519E04B

16711328SIGNAL DATACONVERTER

2985P320A002-03 CCCC

COND COND

584101421416219E05A

011198RECEIVER-TRANSMITTER, RADAR

340HHHG7209AD01 CCCC

COND COND

584101245909319E05C

011198INDICATOR HEIGHT 967AAA3060591 CCCC

COND COND

660501503528419E06A

011294ATTITUDE HEADINGREFERENCE UNIT

719765100-20 CCCC

COND COND

5895015040407 VER 5.2019F02

011421RECEIVER-TRANSMITTER RADAR R

14351008939G-5 CCCC

COND COND

6610014905168 VER 00252A

89710954AUTOMAT FLT CONTCOMPUTER

501096670901-01802-101 CCCC

7. SIGNIFICANT HISTORICAL DATA




HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM1483 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

16-Sep-2016

9000 20188

165001125090703A01A

00PISTON, MAIN L/GEARSTR

BEM148370250-12067-102 RCRC


