DA Form 2408-5 - Equipment Modification Record

PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN

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

7923340UH-60AHELICOPTER, UTILITY

3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE

Report Date: Page 1 of 916-Sep-2016

OU16-Nov-1993

PCW -ASF 157ER5987

201-Feb-1994

ALL UH/EH/MH-60 SERIES AIRCRAFT,NIGHT VISION GOGGLE (NVG)COMPATIBILITY REWORK OF MASTERWARNING PANEL ASSEMBLY

1-1520-237-20-139MWO:

Mnt LevelPriority

DN01-Mar-1989

PCW -DYNCORP,FTHOOD,TXER5987

501-Jun-1990

INCORPORATION OF IMPROVEDTIEDOWN FITTINGS

1-1520-237-50-53MWO:

Mnt LevelPriority

DN16-Oct-1989


2401-Jun-1990

MODIFICATION OF FLIGHT CONTROLMIXER ASSEMBLY (UH-60A/EH-60AHELICOPTERS)

55-1520-237-50-49MWO:

Mnt LevelPriority

DM15-Nov-1989


2201-Jun-1990

MODIFICATION OF DOWEL PINRETENTION MAIN GEARBOX

55-1520-237-50-43MWO:

Mnt LevelPriority

DN01-Oct-1990

PCW -DYNCORP, FTHOOD,TX(ER5987)

1201-Jun-1990

INCORPORATION OF ENGINEQUADRANT SECONDARY STOP TONO. 1 AND NO. 2 ENGINE POWERCONTROL LEVERS (UH-60AHELICOPTERS)

55-1520-237-50-39MWO:

Mnt LevelPriority

DM30-Jan-2003

DYNCORPPROJECT OLRFTCKY(WT524342)

25001-Oct-2006

INSTALLATION OF BLUE FORCETRACKER

1-1520-237-50-BFTMWO:

Mnt LevelPriority

OM27-Jun-2005


8001-Oct-2006

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

DR22-Sep-2005


3901-Oct-2006

ELECTRONIC DATA MANAGEMENT(EDM) SYSTEM

RSN LSF 01-06MWO:

Mnt LevelPriority

DU31-May-1995

PCW -DYNCORP,FTHOOD,TX(ER5987)

3601-Sep-1995

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

1-1520-237-50-73MWO:

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






DN30-Jun-2004

DYNCORP OLRFTCKY

9003-Jan-2008

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

1-1520-237-50-92MWO:

Mnt LevelPriority

DM22-Feb-1991

PCW -DYNCORP,FTHOOD, TX(ER5987)

83204-Nov-1993

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

1-1520-237-50-59MWO:

Mnt LevelPriority

DN01-Aug-1991


3.505-Nov-1990

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

DR15-Jul-1985

PCW -LSI MSDER5987

4005-Oct-1986

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

55-1520-237-50-34MWO:

Mnt LevelPriority

DU30-Mar-1987

PCW -LSI MSD(ER5987)

406-Mar-1987

MODIFICATION OF MAIN ROTORBLADE DE-ICE DISRUPTOR HARNESSAND TAIL ROTOR SLIP RINGHARNESS (UH-60A HELICOPTERS)

55-1520-237-50-36MWO:

Mnt LevelPriority

OT01-May-2002

AR ARNGJG1139

0.506-May-2002

MAIN MODULE PLANETARY CARRIERASSEMBLY, UH-60A/EH-60A/UH-60QSERIES AIRCRAFT

UH-60-02-07MWO:

Mnt LevelPriority

DN01-Jan-1988

PCW -MODSIKORSKY ACFTER5987

0.308-Jul-1985

IMPROVED RETAINING NUTS, CLEVISAND RESTRAINT SYSTEM ONCRASHWORTHY ARMOR CREWSEATS

55-1520-237-50-1MWO:

Mnt LevelPriority

DM18-Jun-1993

C/W -CCAD,CORPC,TX (ER5987)

296908-Oct-1998

INCORPORATION OF UH-60AREFURBISHMENT/STANDARDIZATIONPROGRAM

1-1520-237-55-07MWO:

Mnt LevelPriority

DN30-Apr-1987

PCW -CCAD,CORPC,TX (ER5987)

6708-Oct-1998

INCORPORATION OF WIRE STRIKEPROTECTION SYSTEM (WSPS) (UH-60A HELICOPTER)

55-1520-237-50-24MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN29-Jul-1994


18608-Oct-1998

INSTALLATION OF ELECTRICALLYHEATED GLASS CENTER WINDSHIELD(UH-60A HELICOPTER)

1-1520-237-50-70MWO:

Mnt LevelPriority

DN05-Oct-1994


18408-Oct-1998

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

1-1520-237-50-62MWO:

Mnt LevelPriority

DN01-May-1994


15208-Oct-1998

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

1-1520-237-50-66MWO:

Mnt LevelPriority

DN17-Jun-1989

PCW -CCAD,CORPC,TX ER5987

608-Oct-1998

INCOROPORATION OF EXHAUSTEXTENDER DOUBLERS

55-1520-237-50-51MWO:

Mnt LevelPriority

DN30-Apr-1997


5208-Oct-1998

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

1-1520-237-50-56MWO:

Mnt LevelPriority

DN01-Jun-1988

C/W -CCAD,CORPC,TX ER5987

308-Oct-1998

CRASHWORTHY ARMORED CREWSEATS/IMPROVED SEATINGRESTRAINT SYSTEM

55-1680-237-50-01MWO:

Mnt LevelPriority

DN07-Mar-1995


61.508-Oct-1998

INCORPORATION OF IMPROVEDAIRSPEED SYSTEM (UH-60AHELICOPTERS)

1-1520-237-50-22MWO:

Mnt LevelPriority

DN09-Jan-2004

AR AASF 10009-Apr-2010

INSTALLATION OF CABIN HEATINGSYSTEM 70TH001-1

1001029MWO:

Mnt LevelPriority

DN26-Mar-1984

PCW -FLMDSOBASER5987

16810-Dec-1982

MODIFICATION TO INSTALL ROTORBLADE DE-ICE KIT (UH-60AHELICOPTERS)

55-1520-237-50-5MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN26-Mar-1984

PCW -FLMDSOBAS(ER5987)

1210-Dec-1982

BLADE DE-ICE CHECKOUT APU (UH-60A HELICOPTERS)

55-1520-237-50-4MWO:

Mnt LevelPriority

DN26-Mar-1984


410-Dec-1982

IMPROVED ANTI-ICING MODULATINGVALVE SENSE LINE INSTALLATION(UH-60A HELICOPTERS)

55-1520-237-50-3MWO:

Mnt LevelPriority

DN26-Mar-1984


610-Dec-1982

INCORPORATION OF IMPROVEDDROOP STOP CAM ASSEMBLIES (UH-60A HELICOPTERS)

55-1520-237-50-16MWO:

Mnt LevelPriority

DR27-Oct-2005

DYNCORPFTCKY

90010-Jun-2006

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

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

Mnt LevelPriority

DR21-Jun-2004

DYNCORPFTCKY

7510-Jun-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

DR28-Feb-2005

DYNCORPFTCKY

9410-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

OR10-Jan-2006

DYNCORPFTCKY

30010-Jun-2006

INSTALLATION OF BLUE FORCETRACKING

1-1520-237-50-85BFT60-001MWO:

Mnt LevelPriority

DM08-Feb-2005

DYNCORPFTCKY

36110-Jun-2006

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

DR22-Sep-2006

DYNCORPFTCKY

3710-Jun-2006

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

1-1520-237-50-EMDMWO:

Mnt LevelPriority



PIDMWODATE HRS






DM01-Sep-1991


212-Mar-1993

IMPROVED ENGINE COWLINGRELEASE HANDLE ASSEMBLY

1-1520-237-50-64MWO:

Mnt LevelPriority

OT07-Jan-2003

3-4 AHB FHTX 113-Jul-2005

ALL H-60 SERIES AIRCRAFT,INSPECTION OF MAIN ROTOR BLADECUFF ASSEMBLY

UH-60-03-02MWO:

Mnt LevelPriority

OT13-Feb-1995


ALL EH/UH/MH-60A/L AIRCRAFT,CHANGE TO RETIREMENT LIFE FORCERTAIN MAIN ROTOR BLADE CUFFS

UH-60-95-02MWO:

Mnt LevelPriority

OT01-Dec-1995


ALL UH/EH/MH-60A/L/K AIRCRAFT,CHANGE IN RETIREMENT LIFE OFMAIN ROTOR BLADE CUFF, P/N 70150-09109-041, MANUFACTURED BY FENNMANUFACTURING

UH-60-96-03MWO:

Mnt LevelPriority

DN25-May-1983

PCW -LSI(ER5987)

213-Jun-1983

MODIFICATION OF MAIN ROTORSERVO INPUT PUSHROD ASSEMBLY(UH-60A HELICOPTERS)

55-1520-237-50-13MWO:

Mnt LevelPriority

DN15-Jan-1989


1213-Nov-1989

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

1-5945-237-50-1MWO:

Mnt LevelPriority

DN09-Jun-1988


9213-Nov-1989

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

55-1520-237-50-42MWO:

Mnt LevelPriority

DN23-Jan-1989


3013-Nov-1989

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

55-1520-237-50-44MWO:

Mnt LevelPriority

DN17-Jan-1989


213-Nov-1989

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

55-1520-237-50-52MWO:

Mnt LevelPriority



PIDMWODATE HRS






DM18-Apr-1988

PCW -DYNCORP,FTHOOD, TXER5987

513-Oct-1993

INSTALLATION OF IMPROVEDCARTRIDGE ACTUATED DEVICE

55-4030-237-50-01MWO:

Mnt LevelPriority

DN01-Feb-1993


43613-Oct-1994

INSTALLATION OF DUAL AN/ARC-186/ARC-201 (V) FM RADIO SYSTEMSAND HARDWIRING OF TSEC KY-58 (UH-60A HELICOPTERS) NATIONALSTOCK NUMBER (NSN) 1520-01-035-0266

1-1520-237-50-69MWO:

Mnt LevelPriority

DN15-May-1984

PCW -LSI MSDER5987

26614-Dec-1984

INCORPORATION OF WATERINTEGRITY IMPROVEMENTS (UH-60AHELICOPTERS)

55-1520-237-50-18MWO:

Mnt LevelPriority

DM01-Apr-1985


10614-Dec-1984

INCORPORATION OF FUEL BOOSTPUMP SYSTEM

55-1520-237-50-25MWO:

Mnt LevelPriority

DN01-Oct-1982


814-Dec-1984

INCORPORATION OF A ENGINEPRIME/BOOST SYSTEM (UH-60AHELICOPTERS)

55-1520-237-50-7MWO:

Mnt LevelPriority

OU31-Oct-2002

DYNCORP @NLR,AR 72199DM5698

214-Jul-2003

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

1-1520-237-20-261MWO:

Mnt LevelPriority

OM12-Jun-2002

DCSAVN,CJTR,NLR,AR 72199BM3659

0.514-Jun-2002

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

UH-60-02-ASAM-08MWO:

Mnt LevelPriority

FN13-Jun-2013

DET 2 CO B638TH ASB

814-Sep-2013

INSTRUCTIONS FOR THE REMOVALOF THE #1 (CO-PILOTS) AHRU ANDINSTALLATION OF NAV SYS : CN-1313(VG), TRU-2A/A (RG)

1-1520-237-20-2MWO:

Mnt LevelPriority

DR25-Jan-2007

449TH AVUM 1015-Sep-2011

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



PIDMWODATE HRS






DU30-Nov-1983

PCW -LSI(ER5987)

116-Dec-1983

CARGO HOOK EXTERNAL SPRINGRETROFIT KIT

55-1520-237-50-28MWO:

Mnt LevelPriority

DU13-Jun-1985


416-Jul-1985

MODIFICATION OF IMPROVED MAINROTOR-TAIL ROTOR PITCH CONTROLROD BOLTS (UH-60A HELICOPTERS)

55-1520-237-50-31MWO:

Mnt LevelPriority

DN24-Mar-1988


117-Nov-1988

INSTALLATION OF SELF-SEALINGADAPTERS

55-2840-248-50-28MWO:

Mnt LevelPriority

DN15-Jan-1991


818-Jul-1991

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

55-1520-237-50-58MWO:

Mnt LevelPriority

DN15-Nov-1990


418-Jul-1991

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

1-1520-237-50-61MWO:

Mnt LevelPriority

DU10-Aug-1987

PCW -LSI MSDER5987

618-Nov-1987

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

55-1520-237-50-46MWO:

Mnt LevelPriority

DM12-Aug-1983

PCW -LSI(ER5987)

4819-Dec-1983

UPPER CARGO TRACK ASSEMBLY55-1520-237-50-12MWO:Mnt LevelPriority

DR13-Apr-2001

DYNCORPKILLEEN TX(JC5677)

8019-May-2004

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-Sep-1986

PCW -LSI MSD 85021-May-1987

INCORPORATION OF ANVISCOMPATIBLE LIGHTING SYSTEM

55-1520-237-50-20MWO:

Mnt LevelPriority



PIDMWODATE HRS






DR07-Nov-2008

CSC/RASM-E 27023-Feb-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

DR01-Jul-2008

CSC/RASM-E 7623-Feb-2010

MODIFICATION INSTRUCTION FORTHE INSTALLATION OF CMWS FIFTHSENSOR ON UH-60A AND UH-60LHELICOPTERS

1-1520-237-50-99 (D)MWO:

Mnt LevelPriority

DN24-Mar-1988

PCW -LSI MSC(ER5987)

6723-Jun-1988

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

55-1520-237-50-47MWO:

Mnt LevelPriority

DN15-Dec-1984


223-May-1985

MODIFICATION OF MAIN ROTORSLIDING COVER (UH-60AHELICOPTERS)

55-1520-237-50-32MWO:

Mnt LevelPriority

OM05-Sep-2012

AASF#1 124-FEB-2015

HYDRO-MECHANICAL UNIT(HMU)H-60-12-ASAM-11MWO:Mnt LevelPriority

OM06-Feb-2007

MOAVCRAD(MEC F82152)

4026-Sep-2008

HOIST CABLE (GUARD) DEFLECTORUH-60-07-ASAM-06MWO:Mnt LevelPriority

DR21-Aug-2008

DYN CORPTASM-EUROPE

7427-Jun-2010

INSTALLATION OF THE AIRCRAFTWIRELESS INTERCOM SYSTEM (AWIS)ON THE UH-60A/L HELICOPTERS.

1-1520-237-50-96MWO:

Mnt LevelPriority

OM24-Sep-2002

DCSAVN,CJTR,NLR,AR 72199BM3659

0.527-Sep-2002

UH-60 SERIES AIRCRAFT, REVISIONTO UH-60-02-ASAM-08 (TB 1-1520-237-20-256) INSPECT AN/ARC-220 WIRINGFOR CHAFING


Mnt LevelPriority

DM11-Oct-1983

PCW -LSI(ER5987)

128-Jul-1989

IMPROVED CARGO HOOK KEEPERINSTALLATION FOR UH-60AHELICOPTERS

55-1520-237-50-15MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN31-Oct-1996


3528-Oct-1993

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

1-1520-237-50-74MWO:

Mnt LevelPriority

DR08-Nov-1996


17828-Oct-1993

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

1-1520-237-50-75MWO:

Mnt LevelPriority

DR30-Apr-1991


13228-Oct-1993

MODIFICATION OF THE HOVERINFERRED SUPPRESSION SYSTEM(UH-60A HELICOPTERS) NATIONALSTOCK NUMBER (NSN) 1520-01-035-0266

1-1520-237-50-63MWO:

Mnt LevelPriority



NUMBERLOCATIONPIDENTRYORGANIZATION

8.7.DATE

6.REMARKS

4. 5.

UH-60A 7923340HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL


UNKOWNACFT M/R HEAD RIGGED IAW DWG 70400-00003 REV B SYS CONTROLS HAVE BEENBIASED IN ACCORD.(A)LATERAL CONTROLSERVO INPUT ROD PN70400-02258-046 HASBEEN SHORTENED 1/4 TURN.(B)ACFTCONTROL SERVO INPUT ROD PN70400-02258-045 HAS BEEN LENGTHED 1/2 TURN.(C)FORWARD CONTROL SERVO INPUT RODPN70400-02258-047 HAS BEEN SHORTNED 1/2TURN. NOTE:WHEN ACFT RIGGINGIS BIASEDRIGGING PIN HOLES ARE TEMPORARILYLOST AT THE ABOVE 3 POINTS. (ER5987)

08-May-1981 1

UNKOWN

QC000000

UNKOWNONE TIME INSPECTION OF AIRCRAFT INLETANTI-ICING VALVE PER MSG. UH-60A-79-2. /S/JAMES KRETZ (ER5987)

25-May-1981 1

UNKOWN

QC000000

CO 9TH AVN BNUH-60A-81-12/TB55-1520-237-20-18, ONE TIMEINSPECTION OF SHAFT ASSY, ENGINEOUTPUT. C/W /S/ MERRILL (ER5987)

01-Jul-1981 1

UNKOWN

QC000000

CO 9TH AVN BNUH-60A-81-14/TB55-1520-237-20-20, ONE TIMEINSPECTION OF SWASHPLATE ASSY, MAINROTOR HEAD. C/W /S/ MERRILL (ER5987)

01-Jul-1981 2

UNKOWN

QC000000

CO 9TH AVN BNACAB SOF MSG AH60A081-18, ONE TIMEINSPECTION OF MAIN MODULE INTERNALSHAFT. /S/ UNKOWN (ER5987)

24-Jul-1981 1

UNKOWN

QC000000

CO 9TH AVN BNUH-60A-81-23, ONE TIME INSPECTION OFSTABILATOR ACTUATOR INSPREQUIREMENTS DELETED. /S/ R.E.KELLY(ER5987)

01-Aug-1981 1

UNKOWN

QC000000

CO 9TH AVN BNUH-60A-81-20/TB1-1520-237-20-24, RECURRINGINSPECTION OF BLADE ASSY MAIN ROTORTIP CAP. /S/ J. LEWIS,TI (ER5987)

13-Aug-1981 1

FT LEWIS,WA 98433

QC000000

CO 9TH AVN BNUH-60A-81-27, ONE TIME INSPECTIN OF UH-60A SHAFT ASSEMBLY ENGINE OUTPUT. /S/C.L.CARLO (ER5987)

01-Oct-1981 1

FT LEWIS,WA 98433

QC000000

CO 9TH AVN BNUH-60A-81-28, ONE TIME INSPECTION OFENGINE DESUARL DUCT COMPLETED. /S/ J.JORDAN (ER5987)

27-Oct-1981 1

FT LEWIS,WA 98433

QC000000

CO 9TH AVN BNAPPLIED PART 1 OF ECO #81192 SPRINGCLIPS TO T/R SERVO. /S/ J. JORDAN (ER5987)

09-Dec-1981 1

FT LEWIS,WA 98433

QC000000

CO 9TH AVN BNUH-60A-82-06, ONE TIME INSPECTION OFPILOTS/COPILOTS SEAT RUBBING BAR. /S/ J.CROTEHETT (ER5987)

01-May-1982 1

FT LEWIS,WA 98433

QC000000

SIKORSKY ACFTQUALITY ASSURANCE

REPLACED ANTI-ICE VALVE D/N 70306-10012-107,P-131 WITH SAME PN, S/N P-107 NEW. /S/UNKOWN (ER5987)

04-Jul-1982 1

UNKOWN

QC000000

B CO 9TH ACABUH-60A-82-13, ONE TIME INSPECTION OF MAINROTOR SERVO INPUT LINK BEARINGSCOMPLETED. /S/ TONY LEWIS (ER5987)

06-Aug-1982 1

FT LEWIS, WA 98433

QC000000

B CO 9TH ACABUH-60A-82-11, ONE TIME INSPECTION OF MAINROTOR SERVO PRESSURE SWITCHMANIFOLD SCREWS COMPLETED. /S/UNKOWN (ER5987)

10-Aug-1982 1

FT LEWIS, WA 98433

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.



B CO 9TH ACAB#1 ENG S/N 207636 HAD ALL MOUNTSCHANGED DUE TO EXCESSIVE WEAR. /S/ CCART (ER5987)

17-Aug-1982 1

FT LEWIS, WA 98433

QC000000

B CO 9TH ACABUH-60A-82-17, ONE TIME INSPECTIN OFTAILROTOR SERVO COMPLETED. /S/ C CART(ER5987)

01-Sep-1982 1

FT LEWIS, WA 98433

QC000000

B CO 9TH ACABUH-60A-82-17, ONE TIME INSPECTIN OFFLIGHT CONTROL MIXER LIMITED BEARINGSAND MIXER LIMITER ROLLER COMPLETED. /S/C. CART (ER5987)

01-Sep-1982 2

FT LEWIS, WA 98433

QC000000

B CO 9TH ACABUH-60A-82-19, ONE TIME INSPECTIN OF YAWTRIM AND ROLL TRIM SERVOS FORIMPROVED SEAL COMPLETED. /S/ G. HURT(ER5987)

27-Oct-1982 1

FT LEWIS, WA 98433

QC000000

B CO 9TH ACABUH-60A-82-22/TB55-1520-237-20-37, ONE TIMEINSPECTION OF UPPER CARGO DOORTRACKS COMPLETED. /S/ C. CART (ER5987)

02-Dec-1982 1

FT LEWIS, WA 98433

QC000000

FLMDSOBASBLADE DE-ICE ANTI ICE KIT INSTALLED. /S/UNKOWN (ER5987)

10-Dec-1982 1

FT LEWIS, WA 98433

QC000000

B CO 9TH BNUH-60A-83-04/TB55-1520-237-30-1, ONE TIMEINSPECTION ON UH-60A ACFT INLET DUCTASSY COMPLETED. /S/ G. HURT (ER5987)

01-Apr-1983 1

FT LEWIS, WA 98433

QC000000

B TRP 2/17 CAVUH-60A-83-02/TB55-1520-237-20-40,ONE TIMEINSPECTION OF FLIGHT CONTROLDIRECTIONAL CONTROL LEVER /S/ T.THOMPSON (ER5987)

01-Apr-1983 2

FT CKY 42223

QC000000

ACE TEAMOCM/ACE PERFORMED AT 417 A/C HRS, AT FTLEWIS BY ACE TEAM MEMBER D KEYSERTSARCOM OCM SEC.ST LOUIS MO. /S/ DKEYSER (ER5987)

01-Sep-1983 1

FT LEWIS

QC000000

B TRP 2/17 CAVUH-60A-83-09/TB55-1520-237-20-43, ONE TIMEINSP OF STABILATOR AMPLIFIER. /S/UNKOWN (ER5987)

11-Oct-1983 1

FT CKY 42223

QC000000

B CO 9TH AVN BNUH-60A-83-12/TB55-1520-237-20-46, ONE TIMEINSP OF TAIL ROTOR SERVO ASSYCOMPLETED. /S/ G. HURT (ER5987)

07-Nov-1983 1

FT LEWIS, WA 98433

QC000000

B CO 9TH AVN BNUH-60A-83-12/TB55-1520-237-20-46, ONE TIMEINSP OF TAIL ROTOR SERVO ASSYCOMPLETED. /S/ G. HURT (ER5987)

10-Nov-1983 1

FT LEWIS, WA 98433

QC000000

B CO 9TH AVN BNUH-60A-83-11/TB55-1520-237-20-47,INSPECTION OF ACCESSORY MODULES OILSCREENS COMPLETED. /S/ C. CART (ER5987)

12-Dec-1983 1

FT LEWIS, WA 98433

QC000000

B CO 9TH AVN BNUH-60A-84-01/TB55-1520-237-50-1, ONE TIMEINSPECTION OF MAIN ROTOR SHAFTCOMPLETED. /S/ M. GODFREY (ER5987)

26-Jan-1984 1

FT LEWIS, WA 98433

QC000000

B CO 9TH AVN BNUH-60A-84-02/TB55-1520-237-20-48, ONE TIMEINSPECTION OF WIRING HARNESS BETWEEN#1 AND #2 JUNCTION BOXES COMPLETED. /S/UNKNOWN (ER5987)

20-Mar-1984 1

FT LEWIS, WA 98433

QC000000

B TRP 2/17 CAVNUH-60A-84-03/TB55-1520-237-20-49, ONE TIMEINSPECTION OF TAIL ROTOR PYLON COVERHINGE BRACKET. C/W /S/ UNKNOWN (ER5987)

06-Apr-1984 1

FT CKY 42223

QC000000



8.7.DATE

6.REMARKS

4. 5.



BCO OHH AVN BN FTUH-60A-84-04/TB55-1520-237-50-2, ONE TIMEINSPECTION OF STABILATOR AMPLIFIERSCOMPLETED. /S/ UNKNOWN (ER5987)

16-Apr-1984 1

FT LEWIS, WA 98433

QC000000

B CO 9TH AVN BNFTUH-60A-84-06/TB55-1520-237-20-52, ONE TIMEINSPECTION OF TAIL ROTOR GEARBOX ANDINTERMEDIATE GEARBOX OIL LEVELCOMPLETED. /S/ (ER5987)

08-May-1984 1

FT LEWIS, WA 98433

QC000000

B CO 9TH AVN BNFT#1 ENGINE S/N 206636 HAD ALL MOUNTSCHANGED DUE TO EXCESSIVE WEAR. /S/KNOWN (ER5987)

24-May-1984 1

FT LEWIS, WA 98433

QC000000

B CO 9TH AVN BNFTUH-60A-84-07/TB55-1520-237-20-53, ONE TIMEINSPECTION OF ENG OUTPUT SHAFT BOLTSCOMPLETED SHAFTS HAVE MS9724-08 BOLTSINSTALLED. /S/ KNOWN (ER5987)

04-Jun-1984 1

FT LEWIS, WA 98433

QC000000

B CO 9TH AVN BNFTUH-60A-84-08/TB55-1520-237-20-50, ONE TIMEINSPECTION OF CARGO HOOK ACCEESSURECARTRIDGE ASSY COMPLETED. /S/ C. CART(ER5987)

11-Jun-1984 1

FT LEWIS, WA 98433

QC000000

B CO 9TH AVN BNFTUH-60A-84-11/TB55-1520-237-20-56, INSP OFLONGITUDINAL LATERAL LINK ASSY FORCRACKED BEARING INNER RACECOMPLETED. /S/ L. COOK (ER5987)

10-Jul-1984 1

FT LEWIS, WA 98433

QC000000

B CO 9TH AVN BNFTUH-60A-84-12/TB55-1520-237-20-55,INSPECTION OF M/R SPINDLE ASSY P/C ARMATTACHING BOLTS COMPLETED. /S/UNKNOWN (ER5987)

30-Jul-1984 1

FT LEWIS, WA 98433

QC000000

B CO 9TH AVN BNFTUH-60A-84-10/TB55-1520-237-20-55, ONE TIMEINSPECTION OF TAIL CONE CANTAL HINGEBULKHEAD RAIUS BLKS COMPLETED. /S/ L.COOK,TI (ER5987)

05-Sep-1984 1

FT LEWIS, WA 98433

QC000000

ACE TEAMOCM/ACE PERFORMED AT 0561 A/C HRS ATFT LEWIS WA BY ACE TEAM MEMBER DGOSETT AVSCOM OCM/SEC ST LOUIS MO.. /S/D. GOSSETT (ER5987)

12-Oct-1984 1

FT LEWIS, WA 98433

QC000000

B CO 9TH AVN BNFTUH-60A-84-13/TB55-1520-237-20-57, ONE TIMEINSPECTION OF TAIL ROTOR CONTROLCABLES COMPLETED AT 592.1 ACFT HRS. /S/J. MOLLAUN (ER5987)

08-Nov-1984 1

FT LEWIS, WA 98433

QC000000

UNKNOWNCOMPLIED WITH ECPNOS.92,183,184,196,210,223, AND 239SIKORSKY. /S/ GREG WATERS (ER5987)

30-Nov-1984 1

UNKNOWN

QC000000

B CO 9TH AVN BNUH-60A-84-17/TB55-1520-237-20-59, ONE TIMEINSPECTION TO CHANGE THE AUTOMATIONRPM LIMITS. /S/ UNKNOWN (ER5987)

03-Jan-1985 1

FT LEWIS,WA 98433

QC000000

UNKNOWNUH-60A-85-03, ONE TIME INSPECTION & REPLOF STABILATOR AMPLIFIER PN60902-02001044. /S/ UNKNOWN (ER5987)

24-Feb-1985 1

FT RUCKER,AL

QC000000

B CO 9TH AVN BNUH-60A-85-02, MAINTENANCE MANDATORYTO CHANGE THE AUTOROTATION RPM LIMITSON THE UH-60A. B. MOLLAUN (ER5987)

27-Feb-1985 1

FT LEWIS,WA

QC000000



8.7.DATE

6.REMARKS

4. 5.



B CO 9TH AVN BNUH-60A-86-01/TB55-1520-237-28-1, ONE TIMEINSPECTION OF REPLACEMENT OF T/RDRIVEHSAFT BEARINGS PNSB1138-101COMPLETED 11MAR86 @ 709.0 ACFT HRS. /S/E. LEWIS JR (ER5987)

03-Mar-1985 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-85-06/TB55-1520-237-20-61, ONE TIMEINSPECTION OF PRIMARY SERVOS ANDCONTROL RODS COMPLETED @ 615.0 ACFTHRS. /S/ J. MOLLAUN (ER5987)

07-Mar-1985 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-85-07, IMMEDIATE GROUNDING &INSPECTION OF FLIGHT CONTROLSCOMPLETED. /S/ J. MOLLAUN (ER5987)

11-Apr-1985 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-85-10/TB55-1520-237-20-64, ONE TIMEINSPECTION OF FLIGHT CONTROLSCOMPLETED AT 961 ACFT HRS. L. CAMPBELL(ER5987)

02-May-1985 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-85-12, ONE TIME AND REPETETIVEINSPECTION ON THE T700-GE-700 ENGINE OFTHE AIR NOZZLE FLANGE ON THE POWERTURBINE CASING COMPLETED @ 627 ACFTHRS. /S/ J. MOLLAUN (ER5987)

06-May-1985 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-85-13/TB55-1520-237-20-66, ONE TIMEMODIFIED FLYABLE STORAGE PROCEDURESOF THE UH60A AIRCRAFT COMPLETED17MAY85 @ 631 ACFT HRS. /S/ E.G.LEWIS(ER5987)

24-May-1985 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-85-14/TB55-1520-237-20-68, ONE TIMERECORDS INSPECTION OF MAIN ROTORSHAFT COMPLETE 03JUN85 @ 631.6 ACFTHRS. /S/ J. MOLLAUN (ER5987)

03-Jun-1985 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-85-14/TB55-1520-237-20-68, ONE TIMERECORDS INSPECTION OF MAIN ROTORSHAFT COMPLETE 03JUN85 @ 631.6 ACFTHRS. /S/ J. MOLLAUN (ER5987)

03-Jun-1985 2

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-85-15/TB55-1520-237-20-69, ONE TIMEMAINTENANCE MANDATORY. /S/ J. MOLLAUN(ER5987)

03-Jun-1985 3

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-85-13/TB55-1520-237-20-71, ONE TIMEINSPECTION OF TAIL ROTOR DRIVE SHAFTBEARINGS COMPLETED. /S/ J. MOLLAUN(ER5987)

26-Jun-1985 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNSUPPLEMENT OF INSPECTION OF TAILROTOR DRIVE SHAFTBEARINGS PNSB1135-101 COMPLETED. /S/ THOMAS BOOTH(ER5987)

02-Aug-1985 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-85-18, UNGROUNDINGREQUIREMENTS FOR UH60A, EH-60A ACFTSCOMPLETED 09OCT85. /S/ THOMAS BOOTH(ER5987)

15-Oct-1985 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNOCM/ACE PERFORMED AT 636 A/C HRS AT FTLEWIS BY ACE TEAM MEMBER 5 AVSCOMOCM/SEC ST LOUIS MO. /S/ UNKNOWN(ER5987)

30-Oct-1985 1

FT LEWIS,WA

QC000000



8.7.DATE

6.REMARKS

4. 5.



B CO 9TH AVN BNUH-60A-86-01/TB55-1520-237-28-1, ONE TIMEINSPECTION OF REPLACEMENT OF T/RDRIVEHSAFT BEARINGS PNSB1138-101COMPLETED 11MAR86 @ 709.0 ACFT HRS. /S/E. LEWIS JR (ER5987)

03-Mar-1986 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-86-02/TB55-1520-237-20-74, ONE TIMEINSPECTION OF T/R DRIVESHAFT NUTSCOMPLETED 11MAR86 @ 709.0 ACFT HRS. /S/E. LEWIS JR (ER5987)

03-Mar-1986 2

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-86-03, REVISION OF ONE TIMEINSPECTION OF T/R DRIVESHAFT NUTSCOMPLETED 15MAR86 @ 715.0 ACFT HRS. /S/UNKNOWN (ER5987)

13-Mar-1986 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-86-06, RETROFIT OFSTABILATOR/AFCS CONTROL PANELCOMPLETED 21APR86. N/A THIS ACFT. /S/ I.THOMPSON (ER5987)

12-May-1986 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-86-07, UNGROUNDING OF UH60A/EH-60 ACFTS REQUIREMENTS COMPLETED17MAY86 @ 719.0 ACFT HRS. /S/ I. THOMPSON(ER5987)

12-May-1986 2

FT LEWIS,WA

QC000000

507TH TRANS COUH-60A-86-09, ONE TIME INSPECTION OFENGINE OIL COOLERS. C/W /S/ UNKNOWN(ER5987)

02-Jul-1986 1

FT CKY 42223-5000

QC000000

B CO 9TH AVN BNUH-60A-86-08, REPL OF STAB ACTUATORS PN70400-06614-1100 COMPLETED 10MAY86. /S/ I.THOMPSON (ER5987)

08-Jul-1986 1

FT LEWIS,WA

QC000000

ACE TEAMUH-60A-86-11, REVISIONS OF REQUIREMENTSFOR REPORTING INGROUNDING OF UH60AACFT. C/W 862.8 ACFT HRS./S/ F. EVANS(ER5987)

16-Jul-1986 1

FT CAMPBELL KY

QC000000

B CO 9TH AVN BNUH-60A-86-10, ONE TIME STAKING OFBEARINGS ON LEVER ASSY, PN 70400-02623-041 COMPLETED 15JUL86. /S/ I.THOMPSON(ER5987)

17-Jul-1986 1

FT LEWIS,WA

QC000000

ACE TEAMOCM/ACE PERFORMED AT 0852 A/C HRS ATFT LEWIS,WA BY ACE TEAM MEMBER JAVSCOM OCM/SEC ST LOUIS MO. /S/UNKNOWN (ER5987)

10-Oct-1986 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-86-12, ONE TIME INSPECTION FORUH60A ACFT LOCATION OF HANGE OUT OFSERIAL NUMBRED YAW & COLLECTIVEBOOST SERVOS COMPLETED 30JUL86 @791.0 ACFTHRS. /S/ E.G.LEWIS (ER5987)

05-Dec-1986 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-86-14, REVISION TO 86-10PREVIOUSLY COMPLIED WITH. /S/ E.G.LEWIS(ER5987)

05-Dec-1986 2

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-86-16, COMPLIED WITH 17OCT86 @857.0 ACFT HRS. /S/ E.G.LEWIS (ER5987)

05-Dec-1986 3

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-86-17, COMPLIED WITH NOTAPPLICABLE TO THIS ACFT /S/ E.G.LEWIS(ER5987)

05-Dec-1986 4

FT LEWIS,WA

QC000000



8.7.DATE

6.REMARKS

4. 5.



B CO 9TH AVN BNUH-60A-86-19, COMPLIED WITH 31OCT86 @872.0 ACFT HRS. /S/ E.G.LEWIS (ER5987)

05-Dec-1986 5

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-86-20, COMPLIED WITH 17NOV86 @907.6 ACFT HRS. /S/ E.G.LEWIS (ER5987)

05-Dec-1986 6

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-86-21, COMPLIED WITH 02DEC86 @907.6 ACFT HRS. /S/ E.G.LEWIS (ER5987)

05-Dec-1986 7

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-86-15, COMPLIED WITH /S/ UNKNOWN(ER5987)

05-Dec-1986 8

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-86-22, MANDATORY REVISION TO 86-17. C/W /S/ R.T.MARTIN (ER5987)

29-Dec-1986 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-87-03, ONE TIME & RECURRINGINSPECTION OF T/R DRIVESHAFT SPLINECOUPLINGS COMPLETED 14MAR87 @ 938.4ACFT HRS. /S/ UNKNWON (ER5987)

04-Mar-1987 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-87-04, REVISION TO INSPECTION OFEYEBOLT P/N 70209-02136-102 COMPLETED06APR87 @ 944.9 ACFT HRS. /S/ E.G.LEWIS(ER5987)

01-Apr-1987 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-87-06, ONE TIME OF RECURRINGINSPECTION OF OIL COOLER DRVESHAFTSPLINES COMPLETED 21MAY87 @ 962.5 ACFTHRS. /S/ E.G.LEWIS (ER5987)

22-May-1987 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-87-07, ONE TIME & RECURRINGINSPECTION OF TWO LONGITUDINAL LINKASSYS AND ONE LATERAL CLEVIS ASSY FORCRACKED BEARING INNER RACE,COMPLETED /S/ THOMAS BOOTH (ER5987)

01-Jun-1987 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNGEN-87-02, ALL US ARMY OWNED ACFTLOCAL PURCHASE OF TBO ITEMS,COMPLETED 10JUL87 @ 998.3 ACFT HRS. /S/JAMES WALKER (ER5987)

10-Jul-1987 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-87-08, ALL H60 SERIES HELICOPTERSONE TIME INSPECTION OF MIDSECTIONBELLCRANK ASSY DUE NLT 1001.9 ACFT HRSOR 15JUL87 COMPLETED 14JUL87 AT 998.3ACFT HRS. /S/ JAMES WALKER (ER5987)

14-Jul-1987 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNPMS-2 COMPLETED AT 998.3 ACFT HRS. /S/JAMES WALKER (ER5987)

25-Aug-1987 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNOCM/ACE PERFORMED AT 1025 A/C HRS FTLEWIS WA BY ACE TEAM MEMBER L. AVSCOMOCM/SEC ST LOUIS MO. /S/ UNKNOWN(ER5987)

01-Oct-1987 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-87-10, INSPECTION OF INPUT FLANGEASSY'S COMPLETED 16OCT87 AT 1028.9 ACFTHRS. /S/ JAMES WALKER (ER5987)

17-Oct-1987 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-87-11, ONE TIME INSPECTION OFCARGO DOOR UPPER AND LOWER ROLLERASSY, COMPLETED AT 1049.8 ACFT HRS. /S/JAMES WALKER (ER5987)

02-Nov-1987 1

FT LEWIS,WA

QC000000



8.7.DATE

6.REMARKS

4. 5.



B CO 9TH AVN BNTB55-1520-237-20-93, ONE TIME ANDSUBSEQUENT CONDITIONAL INSPECTION OFENG COWLING COMPLETED AT 1075.3 ACFTHRS. /S/ S. SALLEY (ER5987)

06-Dec-1987 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-87-09, CYCLIC STABILATOR SLEWSWITCH COMPLETED 18NOV87 AT 1062.4ACFT HRS. /S/ S. SALLEY (ER5987)

02-Feb-1988 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-88-01/TB55-1520-237-20-95,INSPECTION FOR CERTAIN S/N T/R BLADEASSY COMPLETED 16FEB88 AT 1114.3 ACFTHRS. /S/ UNKNOWN (ER5987)

16-Feb-1988 1

FT LEWIS,WA

QC000000

B CO 9TH AVN BNUH-60A-88-02, ONE TIME INSPECTION OF THET/R G/B OUTPUT COMPLETED AT 1114.3 ACFTHRS. /S/ JAMES WALKER (ER5987)

20-Mar-1988 1

FT LEWIS,WA

QC000000

B CO 2/9TH AVN REGTUH-60A-88-05/TB55-1520-237-20-98, INITIATIONOF APU MOAT-TERMS OF OPN HRS AND APUSTARTS COMPLETED AT 1190.7 ACFT HRS. /S/E. HAYWOOD (ER5987)

05-May-1988 1

FT LEWIS,WA

QC000000

B CO 2/9TH AVN REGTUH-60A-88-03, DTG 112100Z NAT 88 RECORDSCH OF MAIN MODULE SHAFT AND TBOCORRECTION AND ADDITION OF ON MAINMODULE WITH STORES OR VOLLANDSYSTEMS INSTALL AN ANYTIME /S/ WELLS(ER5987)

05-May-1988 2

FT LEWIS,WA

QC000000

B CO 2/9TH AVN REGTUH-60A-88-04, DTG 121720ZMAY88 REVISIONTO SOF MSG88-02 CHANGING BEARINGLIMITS AND LUG AREA WEAR NOTED. /S/UNKNOWN (ER5987)

05-May-1988 3

FT LEWIS,WA

QC000000

B CO 2/9TH AVN REGTUH-60A-88-05/TB55-1520-237-20-98, INITIATIONOF APU MOAT-TERMS OF OPN HRS AND APUSTARTS COMPLETED AT 1190.7 ACFT HRS. /S/E. HAYWOOD (ER5987)

09-Jul-1988 1

FT LEWIS,WA

QC000000

B CO 2/9TH AVN REGTUH-60A-88-06,OIL COOLER BLOWEROVERHAUL TO 2000HRS COMPLETED AT1192.7 ACFT HRS. /S/ WELLS (ER5987)

12-Jul-1988 1

FT LEWIS,WA

QC000000

B CO 2/9TH AVN REGTUH-60A-88-07, COMPLETED 19JUL88 AT 1192.7ACFT HRS/S/ E. OWSLEY (ER5987)

19-Jul-1988 1

FT LEWIS,WA

QC000000

B CO 2/9TH AVN REGTUH-60A-88-08, COMPLETED 29JUL88 AT 1192.7ACFT HRS/S/ JAMES WALKER (ER5987)

29-Jul-1988 1

FT LEWIS,WA

QC000000

ASF 127UH-60A-88-09, ONE TIME INSPECTION OF ARACREW SEAT C/W AT 1492.8 ACFT HRS. /S/ J.JONES,WG-11 (ER5987)

08-Aug-1988 1

FT RUCKER,AL 36362

QC000000

ASF 127GEN-88-02, INSPECTION FOR INSTALLATIONOF CORECT PORTABLE FIRE EXTINGUISHER.C/W AT 1492.8 HRS. /S/ J. YORK, WG-11(ER5987)

26-Sep-1988 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-88-11, IMMEDIATE RESTRICTION OFRAPELLING OPERATION. C/W AT 1215.2 ACFTHRS. /S/ C.YOHN, WG-11 (ER5987)

27-Oct-1988 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-88-10, ONE TIME INSPECTION OFTROOP/GUNNER SEAT SUPPORT UPPERINSTALLATION C/W AT 1228.9 ACFT HRS. /S/C. YOGN,WG-11 (ER5987)

07-Nov-1988 1

FT RUCKER,AL 36362

QC000000



8.7.DATE

6.REMARKS

4. 5.



ASF 157UH-60-88-10, ONE TIME INSPECTION OFTROOP/GUNNER SEAT SUPPORT UPPERINSTALLATION C/W AT 1228.9 ACFT HRS. /S/C. YOGN,WG-11 (ER5987)

07-Nov-1988 2

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-88-12, REVISION TO UH-60-88-10 C/W AT1228.9ACFT HRS. /S/ C. YOHN,WG-11 (ER5987)

07-Nov-1988 3

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-88-13, ONE TIME INSPECTION OF M/RBLADE PINS C/W AT 1236 ACFT HRS. /S/ C.YOHN,WG-11 (ER5987)

18-Nov-1988 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-89-01, ONE TIME INSPECTION OF ALL T-700 ENGS FOR SUSPECT GAS GEN STATORSHROUDS C/W AT 1272.8 ACFT HRS. /S/ C.YOHN,WG-11 (ER5987)

15-Feb-1989 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-89-02, CORRECTION OF 89-01 C/W AT1272.8 ACFT HRS. /S/ C. YOHN,WG-11 (ER5987)

21-Feb-1989 1

FT RUCKER,AL 36362

QC000000

AVSCOM/OCMOCM/ACE PERFORMED AT 1292 A/C HRS ATFT RUCKER,AL.BY ACE TEAM MEMBER NAVSCOM OCM/SEC ST LOUIS MO. /S/ D.SHROEDER (ER5987)

01-Mar-1989 1

ST LOUIS MO.

QC000000

ASF 157UH-60-89-03, ONE TIME INSPECTION OF M/RSPINDLE RETAINING NUT C/W AT 1323.8 ACFTHRS. /S/ L. MEDLEY,WG-11 (ER5987)

03-Apr-1989 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-89-04, REVISION TO 89-03 C/W AT 1323.8ACFT HRS. /S/ C. YOHN,WG-11 (ER5987)

03-Apr-1989 2

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-89-05, ONE TIME INSPECTION OF WIRESTRIKE PROTECTION SYSTEM C/W AT 1326.1ACFT HRS. /S/ L. MEDLEY,WG-11 (ER5987)

15-Jun-1989 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-89-06, ONE TIME INSPECTION OF L/HAND R/H RELAY PANEL C/W AT 1327.9 ACFTHRS. /S/ J. JONES, WG-11 (ER5987)

18-Jul-1989 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-89-07, REVISION TO 89-06 C/W AT 1328.9ACFT HRS. /S/ L.MEDLEY, WG-11 (ER5987)

07-Aug-1989 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-89-08, ONE TIME INSPECTION OF FUELBOOST PUMP HOSE ATTACHMENT C/W AT1330.5 ACFT HRS. /S/ L.MEDLEY, WG-11(ER5987)

14-Aug-1989 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-89-09, CORRECTION OF RETIREMENTLIFE COMPONENT SCHEDULE C/W AT 1330.5ACFT HRS. /S/ C. YOHN,WG-11 (ER5987)

17-Aug-1989 1

FT RUCKER,AL 36362

QC000000

ASF 157TB55-1520-237-20-104, NEWOVELRHAUL/RETIREMENT LIFE SCHEDULEFOR H-60 RETIREMENT LIFE COMPONENT C/WAT 1332.5 ACFT HRS. /S/ T. ELSBERND(ER5987)

24-Aug-1989 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-89-10,ONE TIME INSPECTION OF T700-GE-700 ENG GAS GEN ROTOR AND STATORHISTORICAL RECORDS C/W AT1332.5 ACFTHRS. /S/ C. YOHN,WG-11 (ER5987)

20-Sep-1989 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-89-11, ONE TIME INSPECTION OF OILCOOLER AXIAL FAN C/W AT 1368 ACFT HRS/S/ C. YOHN,WG-11 (ER5987)

07-Nov-1989 1

FT RUCKER,AL 36362

QC000000



8.7.DATE

6.REMARKS

4. 5.



ASF 157OCM/ACE PERFORMED BY AVSCOM OCM/SECST LOUIS,MO AT1368 ACFT HRS. /S/ C.YOHN,WG-11 (ER5987)

14-Nov-1989 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-89-12, ONE TIME INSPECTION OF OILCOOLER AXIAL FAN C/W AT 1368 ACFT HRS./S/ C. YOHN,WG-11 (ER5987)

22-Nov-1989 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-89-13, ACFT RESTRICTED FROM USINGFITTING ASSY PN70700-20433-045 FORRAPPELLING,PARACHUTING ANDTRANSPORTABILTIY TIEDOWN OPERATIONSC/W AT 1368 ACFT HRS. /S/ C.YOHN,WG-11(ER5987)

08-Dec-1989 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-90-01, ONE TIME AND RECURRINGINSPECTION OF M/R BLADE EXP PIN C/W AT1438.0 ACFT HRS. /S/ L. MEDLEY,WG-11(ER5987)

13-Apr-1990 1

FT RUCKER,AL 36362

QC000000

ASF 157TB55-1520-237-20-111, ONE TIME INSPECTINOOF UPPERPRESSURE PLATE AND SPINDLETO HUB ATTACHMENT BOLT C/W AT 1463.5ACFT HRS. /S/ C.YOHN,WG-11 (ER5987)

02-Aug-1990 1

FT RUCKER,AL 36362

QC000000

ASF 157TB55-1520-237-20-117, ONE TIME INSPECTINOOF M/R PITCH CONTROL HORNS C/W AT14634.5 ACFT HRS. /S/ C.YOHN,WG-11(ER5987)

02-Aug-1990 2

FT RUCKER,AL 36362

QC000000

ASF 157TB55-1520-237-20-113, INSPECTION FORDEFECTIVE ROSEMOUNT ICED RATE METERSC/W 1463.5 ACFT HRS. /S/ C.YOHN,WG-11(ER5987)

02-Aug-1990 3

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-90-02, ONE TIME AND RECURRINGINSPECTION OF T/R P/C BEAM RETAININGNUT AND WASHER C/W AT 1481.3 ACFT HRS./S/ L. MEDLEY,WG-11 (ER5987)

16-Aug-1990 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-91-01, ONE TIME REPLACEMENT AND30 HR SPECIAL INSPECTION OF T/R P/C BEAMRETAINING NUT WASHER C/W AT 1496 ACFTHRS. /S/ C.YOHN, WG-11 (ER5987)

09-Jan-1991 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-91-02, N/A TO THIS ACFT. /S/ C.YOHN,WG-11 (ER5987)

09-Jan-1991 2

FT RUCKER,AL 36362

QC000000

AVSCOM/OCMOCM/ACE COMPLETED AT 1486 ACFT HRS. /S/D. EASLEY (ER5987)

14-Jan-1991 1

ST LOUIS MO

QC000000

ASF 157PERIODIC INSPECTION #3 COMPLETED AT1496.4 ACFT HRS PERIODIC INSP #4 DUE AT1996.4 ACFT HRS. /S/ C. YOHN,WG-11 (ER5987)

05-Mar-1991 1

FT RUCKER,AL 36362

QC000000

6TH BN 159TH REGUH-60-91-ASAM-05, INSPECTION OF M/RSPINDLE SN C/W AT 1506.5 ACFT HRS. /S/ J.HALL,SGT (ER5987)

08-Mar-1991 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-91-ASAM-03, EXTENDED TBO HRS FORMAIN TRANSMODULE N/A FOR THIS ACFT /S/C. YOHN,WG-11 (ER5987)

11-Apr-1991 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-91-ASAM-06, ONE TIME INSPECTION OFCARGO HOOK INTERNAL WIRE BUNDLE C/WAT 1531.9 ACFT HRS. /S/ C. YOHN,WG-11(ER5987)

11-Apr-1991 2

FT RUCKER,AL 36362

QC000000



8.7.DATE

6.REMARKS

4. 5.



ASF 157UH-60-91-ASAM-07, ADVANCE NOTIFIACTIONOF MANUAL CHANGE FOR MAINTRANSMISSION MODULE C/W AT 1531.9 ACFTHRS. /S/ C.YOHN,WG-11 (ER5987)

11-Apr-1991 3

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-91-ASAM-08, ONE TIME INSPECTION OFFIRE EXTINGUISHING SYSTEM C/W AT 1531.9ACFT HRS. /S/ C. YOHN,WG-11 (ER5987)

11-Apr-1991 4

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-91-ASAM-09, CHANGE TO INSPECTIONPROCEDURES FOR M/R SPINDLEELASTOMERIC BEARINGS C/W AT 1607.9ACFT HRS. /S/ C.YOHN,WG-11 (ER5987)

08-Aug-1991 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-91-ASAM-10, ONE TIME INSPECTIONAND REPLACEMENT OF M/L/G BRAKE ASSYPISTON INSULATORS C/W AT 1607.9 ACFTHRS. /S/ C.YOHN,WG-11 (ER5987)

08-Aug-1991 2

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-91-ASAM-04, N/A FOR THIS ACFT. /S/ C.YOHN,WG-11 (ER5987)

13-Aug-1991 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-92-ASAM-01, INSPECTION FOR THREE 3UNSERVICEABLE SPINDLES C/W AT 1744ACFT HRS. /S/ C.YOHN,WG-11 (ER5987)

10-Jan-1992 1

FT RUCKER,AL 36362

QC000000

ASF 157OCM/ACE COMPLETED AT 1799 ACFT HRS.BYAVSCOM OCM/ SEC ST LOUIS MO. /S/ J.FOWLER (ER5987)

11-Mar-1992 1

FT RUCKER,AL 36362

QC000000

ASF 157TB1-1520-237-20-128, DISCONNECTINO OF THEPITCH BIAS ACTUATOR C/W AT 1842.7 ACFTHRS. /S/ C. YOHN,WG-11 (ER5987)

28-Apr-1992 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-92-ASAM-02, ONE TIME INSPECTION ONALL EVEN S/N ACFT FOR ENG OUTPUT SHAFTBOLT TORQUE AND VIB CH AT 1843 ACFTHRS. /S/ L. MEDLEY,WG-11 (ER5987)

21-May-1992 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-92-ASAM-03,, T700 GAS GEN TURBINEBLADE FAILURES/ENGINE CLEANINGPROCEDURES C/W AT 1837 ACFT HRS. /S/ C.YOHN,WG-11 (ER5987)

15-Jun-1992 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-92-ASAM-04, N/A FOR THIS ACFT. /S/C.YOHN,WG-11 (ER5987)

27-Jul-1992 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-92-ASAM-06, ONE TIME INSPECTIONFOR PROPER HARDWARE ON T/R PEDALADJUSTER ASSY C/W AT 1892 ACFT HRS. /S/C.YOHN,WG-11 (ER5987)

28-Sep-1992 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-92-ASAM-05, INSPECTION ANDREPLACEMENT OF M/R BLADE EXPANDABLEPINS C/W AT 1892 ACFT HRS. /S/ C. YOHN,WG-11 (ER5987)

29-Sep-1992 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-93-ASAM-01, ONE TIME OPERATIONALCHECK OF MAIN MODULE AND GEARGOXCHIP DETECTOR SYSTEMS C/W AT 1920.9ACFT HRS. /S/ C.YOHN,WG-11 (ER5987)

17-Nov-1992 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-93-ASAM-02, GAS GEN TURBINE ROTORBLADE FAILURES ENGINE CLEANING ANDSINGLE ENGINE FLIGHT PLANNING C/W AT1920.9 ACFT HRS. /S/ C.YOHN,WG-11 (ER5987)

17-Nov-1992 2

FT RUCKER,AL 36362

QC000000



8.7.DATE

6.REMARKS

4. 5.



ASF 157UH-60-93-ASAM-03, REVISION TO ASAM 92-05C/W AT 1920.9 ACFT HRS. /S/ C. YOHN,WG-11(ER5987)

19-Nov-1992 1

FT RUCKER,AL 36362

QC000000

ASF 157GEN-93-01, PROHIBIT USE OF BRAYCO 599CORROSION PREVENTIVE COMPOUND C/W AT1930 ACFT HRS. /S/ C. YOHN,WG-11 (ER5987)

04-Dec-1992 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-93-ASAM-04, REVISION TO 92-ASAM-06ONE TIME INSPECTION FOR PROPERHARDWARE ON THE T/R PEDAL ADJUSTERASSY C/W AT 1930 ACFT HRS. /S/ C.YOHN,WG-11 (ER5987)

07-Dec-1992 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-93-ASAM-05, ONE TIME INSPECTIONFOR T/R DRIVE SHAFT VISCOUS DAMPERBEARINGS C/W AT 1934.2 ACFT HRS. /S/C.YOHN,WG-11 (ER5987)

22-Dec-1992 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-93-ASAM-06, ONE TIME INSPECTION TOREMOVE SUSPECT T/R PITCH BEAMS C/W AT1934.2 ACFT HRS. /S/ C.YOHN,WG-11 (ER5987)

22-Dec-1992 2

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-93-ASAM-07, REVISION OF CORROSIONLIMITS FOR T/R G/B C/W. /S/ L. MEDLEY,WG-11(ER5987)

23-Dec-1992 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-93-ASAM-08, ALL UH60A,EH-60L HELOSBUILT PRIOR TO S/N 91-26345 TO BIAS T/RRIGGING THREE DEGREES C/W AT 1930 ACFTHRS. /S/ L. MEDLEY, WG-11 (ER5987)

12-Jan-1993 1

FT RUCKER,AL 36362

QC000000

AVSCOM/OCMOCM/ACE INSPECTION COMPLETED AT 1942ACFT HRS. /S/ MEDLEY,WG-11 (ER5987)

14-Jan-1993 1

ST LOUIS MO.

QC000000

ASF 157UH-60-93-ASAM-09, ONE TIME INSPECTION TOCOMPLY WITH SYSTEM MWO'S C/W AT 1993.5ACFT HRS. /S/ C.YOHN,WG-11 (ER5987)

14-Apr-1993 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-93-ASAM-10, N/A FOR THIS ACFT. /S/ C.YOHN,WG-11 (ER5987)

14-Apr-1993 2

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-93-ASAM-11, INSPECTION/REPLACEARA CREW RESTRAINT SYSTEMS C/W AT1993.5 ACFT HRS. /S/ C. YOHN,WG-11 (ER5987)

14-Apr-1993 3

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-93-ASAM-12, ABRUPT CHANGE M/RTRACK/VIBRATIONS C/W AT 1992 ACFT HRS./S/ C. YOHN,WG-11 (ER5987)

30-Apr-1993 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-93-ASAM-13, N/A FOR THIS ACFT. /S/C.YOHN, WG-11 (ER5987)

02-Jun-1993 1

FT RUCKER,AL 36362

QC000000


03-Jun-1993 1

FT RUCKER,AL 36362

QC000000


12-Jul-1993 1

FT RUCKER,AL 36362

QC000000



8.7.DATE

6.REMARKS

4. 5.



USAATCOM,MAINTENGINEER

FT RUCKER NOTED DURING PHASEINSPECTION THREE SOLID RIVETS HAD BEENREPLACED WITH CHERRYLOCKS, ONE RIVETIS NEAR BL 0 AND THE OTHER TWO NEARLEFT ANDRIGHT SIDES IN THE SERVO BEAMRAILS. DISPOSITION: THE BLIND RIVETS ARESECURE AND DO NOT REQUIREREPLACEMENT DURING PHASE INSPECTION#4. /S/ K. CLANCY (ER5987)

06-Aug-1993 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-93-ASAM-16, ONE TIME INSPECTION OFTHE HYD PUMP KNURLED BLEED/RELIEFVALVE C/W AT 1992 ACFT HRS. /S/ C.YOHN,WG-11 (ER5987)

13-Aug-1993 1

FT RUCKER,AL 36362

QC000000

ASF 157PERIODIC INSPECTION #4 COMPLETED AT1992 ACFT HRS PERIODIC INSPECTION #5 DUEAT 2492 ACFT HRS. /S/ C. YOHN,WG-11(ER5987)

19-Aug-1993 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-94-ASAM-01,MSTER WARNGPANELREWORK FOR NVG COMPATABLITY C/W AT2001.5 ACFT HRS. /S/ C. YOHN,WG-11 (ER5987)

19-Nov-1993 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-94-ASAM-02, RETURN FOR XCH OFCERTAIN ARA MFG BUCKLE/CROTCH STRAPASSYS PN4495-29 IN ALL H60SERIES ACFTC/W AT 2016.1 ACFT HRS. /S/ C. YOHN,WG-11(ER5987)

26-Jan-1994 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-94-ASAM-03,TIME REFURBISHMENT OFM/R SPINDLE AND REPLACEMENT OFCERTAIN M/R THRUST BEARING C/W 2016.1ACFT HRS. /S/ C. YOHN,WG-11 (ER5987)

01-Feb-1994 1

FT RUCKER,AL 36362

QC000000

ASF 157UH-60-94-ASAM-04, ONE TIME INSPECTION TOREMOVE SUSPECT T/R PITCH BEAMS C/W AT2016.1 ACFT HRS. /S/ C. YOHN,WG-11 (ER5987)

02-Feb-1994 1

FT RUCKER,AL 36362

QC000000

ATCOM/OCMACE/AACE PERFORMED AT 2016.5 ACFT HRS.BY ACE TEAM MEMBER B. /S/ C. MAUSER(ER5987)

18-Feb-1994 1

ST LOUIS MO.

QC000000

ASF 157UH-60-94-ASAM-05, ONE TIME REMOVAL OFT/R GEARBOX WITH OUTPUT SHAFT PN 70358-06620-101 C/W AT 2016.5ACFT HRS. /S/ C.LYOHN,WG-11 (ER5987)

23-Feb-1994 1

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-94-ASAM-06, COCKPITSTANDARIZAITON OF PILOT/COPILOTRESTRAINT RELEASE SYSTEMS C/W AT2016.5 ACFT HRS. /S/ C. LYOHN,WG-11(ER5987)

23-Feb-1994 2

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-94-ASAM-07, CHANGE TOOVERHAUL/RETIRMENT TABLE C/W AT 2018.0ACFT HRS. /S/ C. YOHN,WG-11 (ER5987)

17-Mar-1994 1

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-94-ASAM-08, CHANGE TO ASAM 94-ASAM-07 C/W AT 2018.0 ACF HRS. /S/ C.YOHN,WG-11 (ER5987)

17-Mar-1994 2

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-94-ASAM-09 REMOVAL OF CERTAIN S/NPRIMARY SERVO ASSYS C/W AT 2020.8 ACFTHRS. /S/ C. YOHN,WG-11 (ER5987)

07-Apr-1994 1

FT RUCKER, AL 36362

QC000000



8.7.DATE

6.REMARKS

4. 5.



ASF 157UH-60-94-ASAM-10, REVISION TO 94-ASAM-03ONE TIME REFURBISHMENT OF M/R SPINDLESAND REPLACEMENT OF M/R THRUSTBEARING (ADD -046 THRUST BEARING) C/WAT 2021.6 ACFT HRS. /S/ C. YOHN,WG-11(ER5987)

26-Apr-1994 1

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-94-ASAM-11, M/R BLADE DE-ICEHEATER MAT RESISTANCE MEARSUREMENTSTESTS METHOD C/W AT 2021.6 ACFT HRS. /S/C.YOHN,WG-11 (ER5987)

26-Apr-1994 2

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-94-ASAM-12, N/A FOR UH-60A ACFT. /S/C. LYOHN,WG-11 (ER5987)

13-Jul-1994 1

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-95-ASAM-01, HOISTING AND AERIALRECOVERY OF UH60/EH-60 ESSS FIXEDPROVISIONED HELOS C/W AT 2108.6 ACFTHRS. /S/ C. YOHN,WG-11 (ER5987)

17-Oct-1994 1

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-95-ASAM-02, ALL H60 ACFTREQUIREMENT TO OPERATE THE FUEL TANKSUBMERGED BOOST PUMPS ON AT ALLTIMES WITH ALL FUELS DURING GROUNDAND FLIGHT OPERATIONS C/W AT 2108.6ACFT HRS. /S/ C. YOHN,WG-11 (ER5987)

25-Oct-1994 1

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-95-ASAM-03, ALL H60 ACFT SHALLREQUIRE RESHIMMING OF T/R PIVOTBEARINGS PERREVISED PROCEDURES ANDCERTAIN BLADE ASSYS WILL BE INSPECTIONFOR SPECIFIED SERIAL NUMBERS WHICHCONTAIN COMPOSITE PIVOT BEARINGSRETAINERS C/W AT 2108.6 ACFT HRS. /S/ C.YOHN,WG-11 (ER5987)

01-Nov-1994 1

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-95-ASAM-04, REDUCTION OF TORQUEOF SELF RETAINING PIVOT BOLTS ANDRECURRING INSPECTION AT 500HRS PMS-2CW/ AT 2114. ACFT HRS. /S/ R. MICHAELS(ER5987)

23-Nov-1994 1

FT RUCKER, AL 36362

QC000000

ASF 157TB1-2840-248-20-2, ONE TIME INSPECTIONAND CONVERSION OF T700 ENG RECORDSC/W AT 2114.9 ACFT HRS. /S/ C. YOHN,WG-11(ER5987)

29-Nov-1994 1

FT RUCKER, AL 36362

QC000000

ASF 157TB1-2835-214-20-1, ONE TIME NSPECTION OFFORMS AND RECORDS FOR H60 ACFT APUC/W AT 2114.9 ACFT HRS. /S/ C. YOHN,WG-11(ER5987)

29-Nov-1994 2

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-95-SOF-01, THREE PART INSPECTIONPROCEDURES AND REPLACEMENT OF TAILROTOR GEARBOX X/W AT 2119 ACFT HRS. /S/R. MICHAELS (ER5987)

09-Dec-1994 1

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-95-ASAM05, CHANGE IN RETIREMENTLIFE FOR SERVO BEAM RAILS AND PMS #2INSPECTION OF PN70209-22103-050/052/054/056 RAILS. C/W AT 2140 ACFTHRS. /S/ R. MICHAELS (ER5987)

28-Feb-1995 1

FT RUCKER, AL 36362

QC000000



8.7.DATE

6.REMARKS

4. 5.



ASF 157UH-60-95-SOF-02, CHANGE IN RETIREMENTLIFE FOR CERTAIN M/R BALDESCUFFS(8LUGS) C/W AT 2148 ACFT HRS./S/ R.MICHAELS (ER5987)

09-Mar-1995 1

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-95-ASAM-06, ONE TIME INSPECTIONFOR CRACKED MAIN XMSN BEAM, UPPERDECK SKIN CRACKS, FRAME CRACKS, C/W AT2178 ACFT HRS. /S/ R. MICHAELS (ER5987)

29-Jun-1995 1

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-95-ASAM-07, CRITERIA FORTROOP/GUNNER SEAT ATTENUATION WIREEXPLICIT SHIMMING PROCEDURES FORATTENUATIN ROLLERS C/W /S/ R. MICHAELS(ER5987)

12-Aug-1995 1

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-95-ASAM-08, INFORMATIONAL ACFTWITH T700-GE-700 AND T700-GE-701 ENGINES,GAS GEN TURBINES ROTOR BLADEINFORMATIONS. /S/ D.L.5818 (ER5987)

02-Oct-1995 1

FT RUCKER, AL 36362

QC000000

ASF 157UH-60-96-ASAM-01, ONE TIME REPLACEMENTOF SPECIFIC FLIGHT CONTROL PIVOT BOLTSNUTS ON CERTAIN SERIES ACFT DOES NOTAPPLY TO THIS ACFT. /S/ D.L.5818 (ER5987)

19-Oct-1995 1

FT RUCKER, AL 36362

QC000000

AASF #1ACFT RECEIVED FROM THE 6TH, BN, 159THREG. USAR,AT2194.6 ACFT HRS. AT AASF #1MGM-AL FOR TNE 1/131 AVN BN.MONTGOMERY, AL. /S/ D.L.5818 (ER5987)

26-Oct-1995 1

MONTGOMERY, AL

QC000000

AASF #1UH-60-96-01, CHANGE IN RETIREMENT LIFE OFCERTAIN SERIAL NUMBERED BELLCRANKSUPPORT ASSY. /S/ D.L.5818 (ER5987)

08-Nov-1995 1

MONTGOMERY, AL

QC000000

AASF #1UH-60-96-02, ONE TIME INSPECTION FORSUSPECT T/R INBOARD RETENTION PLATES./S/ WN4759 (ER5987)

29-Nov-1995 1

MONTGOMERY, AL

QC000000

AASF #1UH-60-96-ASAM-02,ONE TIME INSPECTIONFOR SUSPECT MAIN ROTOR SHAFT NUTBOLTS. /S/ WN4759 (ER5987)

29-Nov-1995 2

MONTGOMERY, AL

QC000000

AASF #1UH-60-96-03, ACFT CHANGE IN RETIREMENTLIFE OF CERTAIN MAIN ROTOR BLADE CUFF/S/ WN4759 (ER5987)

11-Dec-1995 1

MONTGOMERY, AL

QC000000

AASF #1UH-60-96-04, REMOVAL OF SPECIFIC S/N AFTBELLCRANK SUPPORT ASSYS, PN 70400-08117-049. /S/ WN4759 (ER5987)

19-Dec-1995 1

MONTGOMERY, AL

QC000000

AASF #1UH-60-96-ASAM-03, REVISION TO UH60-96-ASAM-02 FOR NON-STANDARD M/R SHAFTNUT BOLTS. /S/ WN4759 (ER5987)

18-Jan-1996 1

MONTGOMERY, AL

QC000000

AASF #1UH-60-96-ASAM-04/TB1-1520-237-20-176, ONETIME INSPECTION AND REVISION OF FRIESSYSTEM AIRWORTHINESS RELEASE TOREFLECT MAXIMUM OPERATIONAL WEIGHTLIMITS. /S/ DL5818 (ER5987)

30-Jan-1996 1

MONTGOMERY, AL

QC000000

1108TH AVCRADACFT STRIPPED USING PLASTIC MEDIABLAST, AND PAINTED WITH LOW REFLECTIVEPOLYURETHANE ACFT GREEN,MILC-46168IAW TM55-1500-345-23. /S/ DL5818 (ER5987)

14-May-1996 1

GULFPORT,MS

QC000000



8.7.DATE

6.REMARKS

4. 5.



AASF #1UH-60-96-ASAM-05/TB1-1520-237-20-172,INCREASE IN FATIGUE LIFE OF CERTAINSERIAL NUMBERED FORWARD BELLCRANKSUPPORT ASSYS. /S/ DL5818 (ER5987)

22-Jul-1996 1

MONTGOMERY,AL

QC000000

AASF #1UH-60-96-ASAM-06, REITERATE ASAM-93-12ABRUPT CHANGES IN M/R TRACK ABNORMALVIBRATIONS. /S/ DL5818 (ER5987)

20-Aug-1996 1

MONTGOMERY,AL

QC000000

AASF #1UH-60-96-ASAM-07, REPLACEMENT OF M/RSPINDLE ASSYS WITH CERTAIN SERIALNUMBER RETAINING RODS. /S/ DL5818(ER5987)

20-Aug-1996 2

MONTGOMERY,AL

QC000000

AASF #1ACFT FORMS AND RECORDS CONVERTED TOULLS-A AUTOMATED SYSTEM IAWUSAATCOM DIRECTIVES DATED 08AUG96,SYSTEM IMPLEMENTED AT 0900:00 ON THE22AUG96. /S/ DL5818 (ER5987)

25-Aug-1996 1

MONTGOMERY,AL

QC000000

AASF #1UH-60-96-ASAM-08, INCREASE IN FATIGUELIFE OF CERTAIN T/R INBOARD RETENTIONPLATE ASSY. /S/ DL5818 (ER5987)

30-Aug-1996 1

MONTGOMERY,AL

QC000000

AASF #1UH-60-96-ASAM-09, ONE TIME INSPECTION OFTHE STABILATOR ACTUATOR CLEVISES FORCORROSION. /S/ DL5818 (ER5987)

30-Aug-1996 2

MONTGOMERY,AL

QC000000

AASF #1UH-60-96-ASAM-10, ESTABLISHMENT OF A500HR AND RECURRING INSPECTION ANDREPLACEMENT OF THE M/R SPINDLE SLEEVEBEARINGS. /S/ DL5818 (ER5987)

12-Sep-1996 1

MONTGOMERY,AL

QC000000

AASF #1ACE/AACE INSPECTION PERFORMED BYDYNCORP OLR TEAM FOR HOOK,TX AT 2256ACFT HRS. BY TEAM MEMBER PROFILER "N"/S/ DL5818 (ER5987)

19-Sep-1996 1

MONTGOMERY,AL

QC000000

AASF #1UH-60-06-ASAM-11, ONE TIME INSPECTION OFM/R BLADE ASSY, FOR CERTAIN SERIALNUMBERED BLADE CUFFS. /S/ DL5818(ER5987)

04-Oct-1996 1

MONTGOMERY,AL

QC000000

AASF #1UH-60-97-ASAM-01, ONE TIME INSPECTION TOIDENTIFY M/R HUBS WITH IMPROPER MFGPROCESS USED IN THE DAMPENERATTACHMENT HOLES. /S/ DL5818 (ER5987)

16-Oct-1996 1

MONTGOMERY,AL

QC000000

AASF #1UH-60-97-ASAM-02, ONE TIME INSPECTION OFFLEXIBLE COUPLING ON TAIL ROTOR DRIVESHAFTS FOR INCORRECT ATTACHMENT TOTHE MAIN TRANSMISSION FLANGE. /S/ DL5818(ER5987)

31-Oct-1996 1

MONTGOMERY,AL

QC000000

AASF #1UH-60-97-ASAM-03, ONE TIME INSPECTION OFT700-GE- 700 ENGINE RECORDS FORUNDAMPED TRUBINE ROTORS OR DAMPENEDROTORS WITH USED BLADES INSTALLED. /S/DL5818 (ER5987)

31-Oct-1996 2

MONTGOMERY,AL

QC000000

AASF #1UH-60-97-SOF-01, ONE TIME INSPECTION OFMAIN ROTOR SWASHPLATE FOR CERTAINSERIAL NUMBEREED ASSYS. /S/ DL5818(ER5987)

05-Dec-1996 1

MONTGOMERY,AL

QC000000



8.7.DATE

6.REMARKS

4. 5.



AASF #1UH-60-97-ASAM-04, ONE TIME INSPECTIONFOR RECORDS ON CERTAIN M/R BLADECUFFS PRODUCED BY THE FENN CORP. TOREVISE AND EXTEND THE CURRENT TBOHOURS. /S/ DL5818 (ER5987)

31-Dec-1996 1

MONTGOMERY,AL

QC000000

AASF #1UH-60-97-ASAM-05, ONE TIME INSPECTIONFOR REMOVAL AND REWORK OF CERTAINVISCOUS DAMPER BEARING SUPPORTSASSYS MFG BY THE LAUMANN CO. /S/ DL5818(ER5987)

08-Jan-1997 1

MONTGOMERY,AL

QC000000

AASF #1UH-60-97-ASAM-06, ONE TIME INSPECTION OFACFT RECORDS FOR INSTALLATION OFCERTAIN LATERAL SERVO BELLCRANKS MFGBY PURDY MACH CO. /S/ DL5818 (ER5987)

08-Jan-1997 2

MONTGOMERY,AL

QC000000

AASF #1UH-60-97-ASAM-07, ONE TIME ACFT RECORDSINSPECTION TO IDENTIFY CERTAIN TAILROTOR SERVO ASSYS WITH SUSPECTS NONCOMPATIBLE SEALS INSTALLED. /S/ DL5818(ER5987)

18-Jan-1997 1

MONTGOMERY,AL

QC000000

AASF #1UH-60-97-ASAM-08, ONE TIME ACFT VISUALINSPECTIONS OF THE LONGITUDINALCONNECTING LINK TO IDENTIFY ANDREMOVE CERTAIN MFG SUSPECT LINKS. /S/DL5818 (ER5987)

18-Jan-1997 2

MONTGOMERY,AL

QC000000

AASF #1UH-60-97-ASAM-09, IDENTIFY AND CHANGERETIREMENT LIFE OF CERTAIN MAIN ROTORMST EXTENSIONS. /S/ DL5818 (ER5987)

18-Jan-1997 3

MONTGOMERY,AL

QC000000

AASF #1UH-60-97-ASAM-10, ONE TIME INSPECTION OFTHE MAIN ROTOR BELLCRANK SUPPORTBRIDGE TO IDENTIFY ASSYS MFG BY AIR INDCORP. FOR REDUCED FINITE LIFE. /S/ DL5818(ER5987)

21-Feb-1997 1

MONTGOMERY,AL

QC000000

AASF #1UH-60-97-ASAM-11, INCREASED OR REVISEDRETIREMENT LIFE OF CERTAINCONFIGURATION,(SIX LUG) MAIN ROTORBLADES CUFFS. /S/ DL5818 (ER5987)

06-Mar-1997 1

MONTGOMERY,AL

QC000000

AASF #1UH-60-97-ASAM-12, RESTORATION OFSERVICE LIFE OF CERTAIN TAIL ROTORINBOARD RETENTION PLATES N/A BY PARTNUMBER AND OR SERIAL NUMBER. /S/ DL5818(ER5987)

16-Apr-1997 1

MONTGOMERY,AL

QC000000

AASF #1JACE INSPECTION PERFORMED BY DYNCORPINSPECTIONS TEAM MEMBER "N" ATCOMOLR/MWO BRANCH, AT 2259.0 ACFT HRS. STLOUIS,MO /S/ DL5818 (ER5987)

27-May-1997 1

MONTGOMERY,AL

QC000000

AASF #1UH-60-97-ASAM-13, ONE TIME INSPECTION OFTHE MAIN ROTOR SPINDLE ELASTOMERICSPHERICAL BEARINGS FOR THE CORRECTINSTALLATION OF OR EXCESSIVE WEAR INTHE TEFON SLEEVE BEARINGS PN SB5203-202. (ER5987)

08-Jun-1997 1

MONTGOMERY,AL

QC000000



8.7.DATE

6.REMARKS

4. 5.



CCADACFT COMPLETEDREFURBISHMENT/STANDARDIZATIONPROGRAM 08OCT98 BY CCAD AT 2258.8 ACFTHRS IAW ATCOM SOW DTD 05AUG93 WHICHINCLUDED MWO1-1520-23755/7 AND PMS-2.(ER5987)

08-Oct-1998 1

CORPC,TX 78419

QC000000

CCADNEXT PMS-2 DUE AT 2758.8 ACFT HRS.(ER5987)

08-Oct-1998 2

CORPC,TX 78419

QC000000

CCADACFT EXTERIOR PAINTED WITH LOWREFLECTIVE POLYURETHANE ACFT GREEN,MIL-C-46168 IAW TM55-1500-345-23DTD12JUN86, AND ECP #0245. (ER5987)

08-Oct-1998 3

CORPC,TX 78419

QC000000

CCADACFT SIX-MONTHS FILE WILL BE RETAINEDAT CCAD, IAW TDS NO. AGEN-X0363, CHG 1DTD 13JAN84. (ER5987)

08-Oct-1998 4

CORPC,TX 78419

QC000000

CCADALL ENTRIES CONVERTED TO ULLS-A ATCCAD 08OCT98, AT 2258.8 ACFT HRS.(ER5987)

08-Oct-1998 5

CORPC,TX 78419

QC000000

CCADTB1-1520-237-20-193, INCORPORATION OFCORROSION RESISTANCE ENHANCEMENTMODIFICATION IN CORROSION PRONEAREAS. CW (ER5987)

08-Oct-1998 6

CORPC,TX 78419

QC000000

CCADUH-60-97-ASAM-15/TB1-1520-237-20-196,INSPECTION FOR BEARING ROD END,PN70101-08202-101,MFG BY ISLAND ENG(CAGE CODE 40137). C/W (ER5987)

08-Oct-1998 7

CORPC,TX 78419

QC000000

CCADUH-60-97-ASAM-19/TB1-1520-237-20-204, ONETIME INSPECTION OF ANVIS/HUD POWERSUPPLY. N/A EQUIP NOT INSTALLED. (ER5987)

08-Oct-1998 8

CORPC,TX 78419

QC000000

CCADUH-60-98-ASAM-02/TB1-1520-237-20-197,REMOVE & DISPOSE ALL PUSHRODS PN70400-08155-050/-051 MFG BY VERSATILE MACHINC.(CAGE CODE 6S522). C/W (ER5987)

08-Oct-1998 9

CORPC,TX 78419

QC000000

CCADUH-60-98-ASAM-03/TB1-1520-237-20-203,SWASHPLATE LINK, PN70400-08110-054, MFGBY TEK(CAGE CODE 657 80). C/W (ER5987)

08-Oct-1998 10

CORPC,TX 78419

QC000000

CCADUH-60-98-ASAM-04/TB1-1520-237-20-205,LOOSE HUCK BOLTS ON OVERHAULEDPRIMARY, YAW BOOST,COLLECTIVE ANDTAIL ROTOR SERVOS. C/W (ER5987)

08-Oct-1998 11

CORPC,TX 78419

QC000000

CCADUH-60-99-ASAM-02/TB1-1520-237-20-207,INSPECTION OF ALL EXTERNAL RESCUEHOISTS MFG BY BREEZE EASTERN TOENSURE THAT THE CORRECT TENSIONROLLERS ARE INSTALLED. N/A THIS ACFT.(ER5987)

08-Oct-1998 12

CORPC,TX 78419

QC000000

CCADUH-60-99-ASAM-01/TB1-1520-237-20-208,INSPECTION RESTORATION FULL SERVICELIFE ON SWASHPLATE LINK ASSY P/N 70400-08110-054/-061, MFG BY TEK(CAGE CODE65780). C/W (ER5987)

08-Oct-1998 13

CORPC,TX 78419

QC000000

AR AASFUH-60-99-ASAM-07/TB1-1520-237-20-212 INSPM/R HUB ASSY C.W. 2258.8 ACFT HRS(JG1139)

25-Mar-1999 1

CJTR AR

QC000000



8.7.DATE

6.REMARKS

4. 5.



AR AASFASAM UH-60-99-ASAM-08 TB1-1520-237-20-211INSP BELLCRANK SUPPORT ASSY (JG1139)

17-Jun-1999 1

CJTR AR

QC000000

AR AASFUH-60-99-ASAM-11 ONE TIME INSP OF ALLT700 ENG RECORDS (JG1139)

12-Aug-1999 1

CJTR AR

QC000000

AR AASF CJTRAIRCRAFT FORMS AND RECORDSCONVERETED TO ULLS-A (WW1514)

26-Aug-1999 1

NO. LITTLE ROCK, AR72199-9600

QC000000

AR AASFUH-60-99-ASAM-10 REPLACEMENT OF #2CROSSFEED LINE (JG1139)

27-Aug-1999 1

CJTR AR

QC000000

AR AASFUH-60-99-ASAM-12 INSP OF HMU P-3 LINE GE3078804046T52G06/#2 GEE 307010 4046T52G04(JG1139)

27-Aug-1999 2

CJTR AR

QC000000

AR AASFUH-60-99-ASAM-09 ONE TIME INSP OF M/REXPANDABLE PINS (JG1139)

01-Sep-1999 1

CJTR AR

QC000000

AR AASFUH-60-00-ASAM-02 CYCLIC STICK WIRINGBUNDLE (JG1139)

15-Dec-1999 1

CJTR AR

QC000000

AR AASFUH-60-00-ASAM-03 MAIN PRIMARY SERVO(JG1139)

13-Jan-2000 1

CJTR AR

QC000000

AR AASFUH-60-00-ASAM-04 INSP TAIL LANDING GEARSHOCK STRUT NSP TAIL LANDING GEARSHOCK STRUT (JG1139)

20-Mar-2000 1

CJTR AR

QC000000

AR AASFACE/CPCE PERFORMED AT 2390 ACFT HRS.BY TEAM MEMBER "W" AMCOM OLR/MWOBRANCH KILLEEN, TX. JERRY D.PARKSADABLE (JP2527)

28-Apr-2000 1

CJTR NLR AR

QC000000

AR AASF CJTRUH-60-00-ASAM-05/TB1-1520-237-20-219.INSPFIRE EXTINGUISHER WIRING (BM9758)

16-May-2000 1

NO.LITTLEROCK,AR.72119-9600

QC000000

AR AASF CJTRUH-60-00-01/TB1-1520-237-20-221.INSP OF M/RSPINDLE LUGSES WITH POTENTIALLYCRACKED BEVEL GEAR (BM9758)

12-Jul-2000 1


QC000000

AR AASF CJTRYH-60-00-02/TB1-1520-237-20-222.INPUTMODULE GEAR BOX ASSEMBLIES WITHPOTENTIALLY CRACKED BEVEL GEARGEAR(BM9758)

03-Aug-2000 1


QC000000

AR AASFUH-60-00-ASAM-07 ONE TIME INSP OFWIREING HARNESSES BETWEEN NO.1 ANDNO.2 JUNCTION BOX. BOXES (JG1139)

16-Sep-2000 1

N.L.R. AR

QC000000

AR AASFSOF UH-60-01-01/TB1-1520-237-20-225.INITIAL& RECURRING INSP.OF THE MAIN LANDINGGEAR DRAG BEAM ASSY.& DECREASE TQ.ONTHE JACKPAD NUT. (BM9758)

10-Dec-2000 1

NORTH LITTLE ROCKAR

QC000000

AR AASFSOF UH-60-01-02/TB1-1520-237-225.INSP.MAINLANDING GEAR DRAG BEAM ASSY.IAW UH-60-01-02 (BM9758)

05-Jan-2001 1

NORTH LITTLE ROCKAR

QC000000

AR AASFINSP FOR INSTALLATION OF JUELMONITORING SYS IAW UH-60-01-04 (TB 1-1520-237-20-228) (JG1139)

18-Jan-2001 1

CJTR N. LITTLE ROCKAR

QC000000



8.7.DATE

6.REMARKS

4. 5.



AR AASFINSP LATERAL SERVO BELLCRANKASSEMBLY IAW UH-60-01-03 ( TB 1-1520-237-20-229) (JG1139)

19-Jan-2001 1


QC000000

AR AASFSOF UH-60-01-06 (TB 1-1520-237-20-231) INSPOF ALL SAS ACTUATORS (BM3659)

26-Mar-2001 1

CJTR, N. LITTLE ROCK,AR

QC000000

AR AASFSOF UH-60-01-07/ (TB 1-1520-237-20-232) INSPOF MAIN ROTOR FLIGHT CONTROL SELF-LOCKING BOLTS (BM3659)

02-Jun-2001 1

CJTR, N. LITTLE ROCK,AR 72199

QC000000

AR AASFINSPECTION OF MAIN ROTOR FLIGHTCONTROL SELF-LOCKING BOLTS UH-60-01-08/ TB1-1520-237-20-232 (BP8008)

02-Jun-2001 2

CAMP JOE T.ROBINSON

QC000000

AR AASFSOF UH-60-01-09 (TB1-1520-237-20-233) INSPOF M/R BLADE EXPANDABLE PINS. (BM3659)

12-Jun-2001 1

CJTR N.L.R. AR

QC000000

AR AASFINSPECTION OF MAIN ROTOR SPINDLE UH-60-01-05/ TB 1-1520-237-20-230 (NDI) (BP8008)

25-Jun-2001 1

CAMP JOE T.ROBINSON

QC000000

AR AASFUH-60-02-01/TB 1-1520-237-20-240 INSP FORIMPROPER OR UNINSTALLED HARDWARE ONTHE OIL COOLER SHAFT ASSY FWD MOUNT(BP8008)

18-Nov-2001 1

N. LITTLE ROCK AR

QC000000

AR AASFINSP FOR IMPROPER OU UNINSTALLEDHARDWARE ON THE OIL COOLER FAN SHAFTASSY. FWD MOUNT. (JG1139)

19-Nov-2001 1

CJTR N.L.R. AR

QC000000

AR AASFUH-60-02-ASAM-01 / TB 1-1520-237-20-239INSP. OF T/R BLADE FARING ASSY. P/N 70104-11104-044 COMPLETED (BP8008)

27-Nov-2001 1

RBM N. LITTLE ROCKAR 72199

QC000000

AR AASFMAIN ROTOR HUB SUBASSEMBLY REWORK(JG1139)

07-Dec-2001 1

CJTR N.L.R AR

QC000000

AR AASFACE/CPCE PERFORMED AT 2626 ACFT HRS.BY TEAM MEMBERS W &TT. AMCOM PROJECTOLR. KILLEEN, TX (JG1139)

11-Dec-2001 1

N.L.R. AR CJTR

QC000000

AR AASFUH-60-02-03 ONE TIME VISUAL INSPECTIONOF PITCH TRIM ACTUATOR ROD CLEVIS PINAND WASHER ASSY (BP8008)

12-Dec-2001 1


QC000000

AR AASF NLR ARUH-60-02-04 (TB 1-1520-237-20-242) INSPECTAPU FUEL LINES (JG1139)

29-Jan-2002 1

CAMP ROBINSON AR

QC000000

AR ARNGINSP OF M/R BLADE EXP. PINS UH-60-02-05C/W (JG1139)

04-Feb-2002 1

CJTR N.R. AR

QC000000

AR ARNGUH-60-02-ASAM-02 TB1-1520-237-20-246INITIAL AND RECURRING INSP OF CONTROLROD JAMNUT C/W (JG1139)

08-Feb-2002 1

CJTR N.L.R. AR

QC000000

AR ARNGINSP RESTRAINT SYSTEM UH-60-02-ASAM-04C/W (JG1139)

15-Mar-2002 1

CJTR N.L.R AR

QC000000

AR ARNGUH-60-02-ASAM-06 INSP SWAGEPINS/COLLARS ON BOOST SERVO ASSY.(JG1139)

01-May-2002 1

CJTR N.L.AR

QC000000



8.7.DATE

6.REMARKS

4. 5.



AR ARNGMAIN MODULE PLANETARY CARRIER ASSYUH-60-02-08 TB 1-1520-237-20-255 (JG1139)

06-May-2002 1

CJTR N.L. ROCK AR

QC000000

AR AASFUH-60-02-ASAM-08 INSPECT ARC-220 POWERAMPLIFIER/ COUPLER (JG1139)

17-Jun-2002 1

CJTR N.LITTLE ROCKAR

QC000000

AR AASFUH-60-02-ASAM-09 INSP TAIL ROTORQUADRANT HARDWARE INSTALLATION(JG1139)

17-Jun-2002 2

CJTR N.LITTLE ROCKAR

QC000000

DYNCORPACE/CPCE PERFORMED AT 2656 ACFT HRSBY TEAM MEMBERS K&W. AM COM PROJECTOLR. KILLEEN,TX (JP2527)

23-Jul-2002 1

KILLEEN,TX

QC000000

DCSAVN-QCUH-60-02-ASAM-11 (TB 1-1520-237-20-261) C/W@ 2657 ACFT. HRS. INSP. OF ARC-220 WIRING(BM3659)

01-Oct-2002 1

CJTR, NLR, AR 72199-9600

QC000000

AR AASF CAMP J. T.ROB. N LITTLE AR

ACFT RIGGED IAW TM 1-1520-237-23-6PRIMARY SERVO CONTROL ROD BIASSETTINGS ARE AS FOLLOWS: FWD:LENGTHEN 1 TURN AFT: SHORTEN 1 TURNLAT: NONE (BP8008)

11-Oct-2002 1

N. LITTLE ROCK AR72199-9600

QC000000

DCSAVN CJTRUH-60-03-ASAM-01, BELLCRANK SUPPORTASSY. RETIREMENT LIFE, COMPLETED @2680.3 ACFT. HRS. (WW1514)

10-Dec-2002 1

N.L.R., AR 72199-9600

QC000000

DCSAVN CJTRUH-60-03-ASAM-02, TAIL ROTOR SERVORETIREMENT LIFE, COMPLETED @ 2680.3ACFT. HRS. (WW1514)

10-Dec-2002 2

N.L.R., AR 72199-9600

QC000000

AR AASFGEN-03-ASAM-01 C/W ( BATTERY BON ONSINCGARS ) (JG1139)

03-Jan-2003 1

CJTR N LITTLE ROCKAR

QC000000

AR AASFUH-60-02-ASAM-03 (TB 1-1520-237-20-245)ENGINE PCL QUADRANT INSP COMP. (JG1139)

23-Apr-2003 1

CJTR N LITTLE ROCKAR

QC000000

DYNCORPACE/OPCE PERFORMED AT 2733 ACFT HRSBY TEAM MEMBERS K & I AMCOM PROJECTOLR KILLEEN TX (JL7296)

18-Jul-2003 1

KILLEEN TX.

QC000000

DYNCORPMODIFICATION OF ARC-220 POWERAMPLIFIER CANNON PLUG BACKSHELL UH-60-02-ASAM-11 COMPLIED WITH @ 2733 ACFTHRS. (DM5698)

18-Jul-2003 2

KILLEEN TX.

QC000000

DCSAVN AR ARNGUH-60-04-01 FORWARD BELLCRANKSUPPORT HARDWARE INSPECTIONCOMPLIED WITH @ 2733.2 ACFT HRS(WW1514)

02-Oct-2003 1

NORTH LITTLE ROCK,AR 72199

QC000000



8.7.DATE

6.REMARKS

4. 5.



AR ARMY NAT GUARDACFT M/R HEAD RIGGED IAW DWG 70400-00003 REV B SYSCONTROLS HAVE BEENBIASED IN ACCORD.(A)LATERAL CONTROLSERVO INPUT ROD PN70400-02258-046 HASBEEN LENGTHENED 1/2. (LONG MIXERRIGGING PIN WILL NOT GO IN NOW.) LATCONT ROD SHORTED 3/4 TURN. RWDCONT.ROD SHORTENED 2 1/2 TURNS. AFTCONT ROD LENGTHED 2 1/2 TURNS. .NOTE:WHEN ACFT RIGGING IS BIASEDRIGGING PIN HOLES ARE TEMPORARILYLOST AT THE ABOVE 3 POINTS. (JG1139)

16-Jan-2004 1

AR AASF N.L.R. AR

QC000000

DCSAVN AR ARNGARDUH-60-04-ASAM-01 GLARE SHIELD LIGHTINGCIRCUT BREAKER REPLACEMENT (WW1514)

26-Feb-2004 1

CJTR N.L.R. AR 72199-9600

QC000000

DCSAVN AR ARNGPMS-2 COMPLETED @ 2733.2 ACFT.HRS. NEXTINSPECTION DUE IS @ 3233.2 ACFT. HRS.(WW1514)

26-Feb-2004 2

CJTR N.L.R. AR 72199-9600

QC000000

DCSAVN AR ARNGUH-60-04-ASAM-02 TAIL ROTOR DRIVESHAFTFLANGE NUT INSPECTION COMPLIED WITH @2757.3 ACFT HRS. (WW1514)

02-Apr-2004 1

CJTR, N.L.R., AR 72199-9600

QC000000

DCSAVN AR ARNGEMC CHECK COMPLETED IAW AWR 1054 (SEIBAMBI WATER BUCKETS) DTD 16 APR 04 ONAIRCRAFT UH-60A 8023435 FOR ALL UH-60AAIRCRAFT LOCATED @ CJTR NLR, AR 72199-9600 (WW1514)

05-May-2004 1

CJTR NLR, AR 72199-9600

QC000000

DYNCORP OLRACE/CPCE PERFORMED AT 2772 ACFT. HRS.BY TEAM MEMBERS K & W. AMCOM PROJECTOLR LITTLE ROCK, AR (JP2527)

02-Jun-2004 1

KILLEEN, TX

QC000000

DCSAVN AR ARNGSAFETY OF FLIGHT UH-60-04-02 DISABLINGOF COCKPIT AIRBAG SYSTEM COMPLIED.MWO NOT APPLIED AT 2780.1 ACFT HRS.(MF3926)

24-Jun-2004 1

CJTR NLR, AR 72199-9600

QC000000

DCSAVN AR ARNGUH-60-04-04 MAIN ROTOR HUB SUBASSY.REWORK COMPLIED WITH @ 2831.4 ACFT HRS(WW1514)

23-Aug-2004 1

CJTR N.L.R., AR 72199-9600

QC000000

DCSAVN AR ARNGUH-60-04-ASAM-04 FUEL SYS. INTEGRITYCHECK REVISION COMPLIED WITH. (WW1514)

27-Aug-2004 1

CJTR N.L.R., AR 72199-9600

QC000000

DCSAVN AR ARNGMAVEN OPTIONAL II HEATER INSTALLED(IMPROVED HEATING SYSTEM) (WW1514)

27-Jan-2005 1

CJTR, NLR, AR 72199-9600

QC000000

DCSAVN ARA ARNGLATE ENTRY: UH-60-04-ASAM-05 COMPLIEDWITH. RESTRAINT SYSTEM INSPECTION(WW1514)

27-Jan-2005 2

CJTR, NLR, AR 72199-9600

QC000000

DCSAVN AR ARNGUH-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

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

14-Mar-2005 1

CJTR, NLR, AR 72199-9600

QC000000



8.7.DATE

6.REMARKS

4. 5.



DCSAVN AR ARNGUH-60-05-SOF-02 AIRCRAFT PLACED ON ESM04/15/2005 @ 2931.1 ACFT HRS, PMI #1 DUE @3083.2ACFT HRS. (MB9758)

14-Apr-2005 1

CJTR, NLR, AR 72199-9600

QC000000

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

21-Apr-2005 1

CJTR, NLR, AR 72199-9600

QC000000

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

21-Apr-2005 2

CJTR, NLR, AR 72199-9600

QC000000

DCSAVN AR ARNGUH-60-05-ASAM-06 TROOP SEAT RESTRAINTBUCKLES COMPLIED WITH @ 2931.1 ACFTHRS (WW1514)

03-Jun-2005 1

CJTR, NLR, AR 72199-9600

QC000000

DCSAVN AR ARNGUH-60-05-ASAM-07 AIR INTRUSION OFHYDRAULIC SYSTEM COMPLIED WITH @2931.1 ACFT HRS (WW1514)

05-Jun-2005 1

CJTR, NLR, AR 72199-9600

QC000000

DCSAVN AR ARNGUH-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

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

09-Aug-2005 1

CJTR, NLR, AR 72199-9600

QC000000

DET 1 B CO 777THASB

UH-60-05-ASAM-11 WIRE HARNESS CHAFINGCOMPLIED WITH (PCW)

22-Sep-2005 1

CAMP BONDSTEEL

QC000000

DYNCORPACE/CPCE PERFORMED AT 3066 ACFT HRSBY TEAM MEMBERS K & W AMCOM PROJECTOLR (JP2527)

30-Sep-2005 1

CJTR,NLR,AR 72199-9600

QC000000

DET 1 B CO 777THASB

UH-60-06-ASM-01 INSPECT TAIL SHOCKSTRUT FOR CERTAIN P/N'S COMPLIED WITH

14-Dec-2005 1

CAMP BONDSTEEL

QC000000

D CO 1/131 AVN BNPMI 2 COMPLETED AT 3074.4 ACFT HRS. PMI1 DUE AT 3434.4 ACFT HRS.

04-Apr-2006 1

FT HOOD TX

PT721546

DCSAVN AR ARNGAIRCRAFT ENTERED INTO SCP-6 AUTO.RECORDS PROGRAM

25-Apr-2006 1

CJTR,NLR,AR

QC000000

D CO, 1-131ST AVN BNUH-60-06-ASAM-02 M/R PITCH CONTROL RODJAMNUTS INSPECTED AND TREATED FORCORROSION COMPLETED 05 MAY 2006 @4155.1 ACFT HRS.

05-May-2006 1

FT. HOOD, TX

CH961897

D CO, 1-131ST AVNUH-60-06-ASAM-03, SWASHPLATE BEARINGINSPECTION, C/W 15 JUN 2006 @ 3116.6 ACFTHRS, 21 JUN 2006.

21-Jun-2006 1

FT. HOOD, TX

CH961897

D CO 1/131 AVNUH-60-06-ASAM-04 DISABLING COCKPITAIRBAG SYSTEM C/W 25 JUN 2006 @ 3113.6ACFT HRS. CAB NOT INSTALLED ( CR199703)

25-Jun-2006 1

FORT HOOD, TX

CR199703

D CO 1/131 AVNUH-60-06-SOF-02 DISABLING COCKPITAIRBAG SYSTEM C/W 25 JUN 2006 @ 3113.6ACFT HRS. CAB NOT INSTALLED ( CR199703)

25-Jun-2006 2

FORT HOOD, TX

CR199703



8.7.DATE

6.REMARKS

4. 5.



D CO, 1-131ST AVNACFT FOLDED AND RECONFIGURED FORTRANSPORTATION ON SHIP TO KUWAIT INSUPPORT OF OIF.

29-Aug-2006 1

UDARI ARMY AIRFIELD,KUWAIT

CH961897

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

01-Sep-2006 1

UAAF

PT721546

D CO 1-131 AVN BNUH-60-06-ASAM-05 BLUE FORCE TRACKERHARDWARE INSTALLATION C/W 30 AUG 2006@ 3117.5 ACFT HRS

08-Sep-2006 1

UAAF, KUWAIT

WT524342

D CO 1/131 AVNINSP A 110-PMS 40 HOUR (ESM) +/- 2 HOURWINDOW EXTENDED TO +/- 3 HOURS WHILEACFT ARE DEPLOYED IN SUPPORT OF OIF.ENTENSION VOID WHEN ACFT ARE RE-DEPLOYED TO HOME STATION. PER AMCOMMEC LE-BAL013-2128

23-Sep-2006 1

LSA ANACONDA

BW860588

D CO 1-131 AVN BNUH-60-07-ASAM-01 #1 AND #2 ENG WHITEHARNESS INSP C/W @ 3301.6 ACFT HRS

02-Dec-2006 1

BALAD IRAQ

WT524342

D CO. 1-131 AVNUH-60-06-ASAM-01 REMOVAL AND REPLACEMENT OF ALL 70250-13101-041, 042, AND 043TAIL LANDING GEAR SHOCK STRUTS DUE ATNEXT PMI,PMS-2, PREVIOUSLY COMPLIEDWITH AT 3074.4 ACFT HRS. INFORMATIONVERIFIED BY 2410 HOTLINE.

04-Dec-2006 1

LSA, ANACONDA

RG414089

D CO. 1-131 AVN REGTUH-60-07-ASAM-03 INSP OF COLL AND YAWBOOST SERVO INPUT ARMS FOR PRESENCEOF ROLL PIN INSTALLED C/W @ 3377.1 ACFTHRS.

23-Dec-2006 1

BALAD, IRAQ

RG414089

D CO 1-131 AVN REGTUH-60-07-ASAM-02 ADMENDMENT TO UH-60-07-ASAM-01 COMPLIED WITH @ 3379.6 ACFTHRS.

27-Dec-2006 1

BALAD, IRAQ

RG414089

D CO 1/131 AVNCOMPLIED WITH UH-60-07-ASAM-04 30-Dec-2006 1

BALAD IRAQ

PT721546



8.7.DATE

6.REMARKS

4. 5.



D CO, 1-131ST AVNREGT

MEC: LE-BAL014-0517 14 JAN 07.PERMISSION IS GRANTED TO REPLACE THEBL 34.5L FLOOR WEB AS REQUESTED IAW TM1-1500-204-23 STANDARD SHEET METALPRACTICES. ORIGINAL MATERIAL, TITANIUM6AL-4V 0.020' THICK, IS NOT AVAILABLE;AUTHORIZATION IS GIVEN TO USE 301 CRES1/2 HARD 0.020' THICK AS A SUBSTITUTE.CAREFULLY, REMOVE RIVETS TO ENSURENODAMAGE OCCURS TO UNDERLYINGSTRUCTURE. FABRICATE NEW WEBACCORDING TO THE ORIGINAL WEBDIMENSIONS. DEBURR FABRICATED WEBAND APPLY 2 COATS OF EPOXY PRIMER TOBOTH SIDES OF WEB. UTILIZE EXISTINGHOLES. USE ORIGINAL RIVET TYPE ANDINSTALL RIVETS WET WITH EPOXY PRIMER.TOUCH-UP PAINT AS NEEDED. REPAIRSHALL BE RE-EVALUATED AT RESET DUE TOMATERIAL SUBSTITUTION. ANNOTATEREPAIR AND RE-EVALUATION AT RESET INTHE APPROPRIATE AIRCRAFT HISTORICALRECORDS AND LOGBOOK.//ORIGINALSIGNED//TRAVIS W. MASSA, GS-09AEROSPACE ENGINEER, US ARMY RDECOM,AMSRD-AMR-AE-M DSN: 312-992-3986 X7830,COM'L: 732-532-3986 X7830, TASM, APO AE09391 [email protected]

14-Jan-2007 1

BALAD, IRAQ

CH961897

D CO 1-131 AVN REGTUH-60-07-ASAM-05 ARC-220 POWER UPPROCEDURES COMPLIED WITH @ 3410.1ACFT HRS.

23-Jan-2007 1

LSA ANACONDA,BALAD, IRAQ

RG414089


CO-PILOT DOOR BEAM CRACKED; MECNUMBER LE-BAL014-0477; AUTHORIZATIONFOR REPAIR BY L3 VERTEX IAW SIKORSKYREPAIR PROCEDURE CDP-24022-1. L3VERTEX AEROSPACE BALAD, IRAQ APO AE09391 08 JAN 2007 JM139643. ACFT HRS3410.0

26-Jan-2007 1

BALAD, IRAQ

CH961897


PILOT DOOR BEAM CRACKED; MEC NUMBERLE-BAL014-0478: AUTHORIZATION FORREPAIR BY L3 VERTEX IAW SIKORSKYREPAIR PROCEDURE CDP-24022-1. L3VERTEX AEROSPACE BALAD, IRAQ APO AE0939108 JAN 2007 JM139543. 3410.0 ACFTHRS

26-Jan-2007 2

BALAD, IRAQ

CH961897



8.7.DATE

6.REMARKS

4. 5.




CABIN STRAP AT STA. 363 REPAIR; MECNUMBER LE-BAL014-0517: AUTHORIZATIONFOR SUBSTITUTE MATERIAL TO BE USED. RE-EVALUATION DUE AT RESET PER MEC. L3VERTEX BALAD, IRAQ APO AE 09391.JM139543. 3410.0 ACFT HRS.PERMISSION ISGRANTED TO REPLACE THE BL 34.5L FLOORWEB AS REQUESTED IAW TM 1-1500-204-23STANDARD SHEET METAL PRACTICES.ORIGINAL MATERIAL, TITANIUM 6AL-4V 0.020"THICK, IS NOT AVAILABLE; AUTHORIZATIONIS GIVEN TO USE 301 CRES 1/2 HARD 0.020"THICK AS A SUBSTITUTE. CAREFULLYREMOVE RIVETS TO ENSURE NO DAMAGEOCCURS TO UNDERLYING STRUCTURE.FABRICATE NEW WEB ACCORDING TO THEORIGINAL WEB DIMENSIONS. DEBURRFABRICATED WEB AND APPLY 2 COATS OFEPOXY PRIMER TO BOTH SIDES OF WEB.UTILIZE EXISTING HOLES. USE ORIGINALRIVET TYPE AND INSTALL RIVETS WET WITHEPOXY PRIMER. TOUCH-UP PAINT ASNEEDED. REPAIR SHALL BE RE-EVALUATIONAT RESET IN THE APPROPRIATE AIRCRAFTHISTORICAL RECORDS ANDLOGBOOK.//ORIGINAL SIGNED//TRAVIS W.MASSA, GS-09 AEROSPACE ENGINEER, USARMY RDECOM, AMSRD-AMR-AE-M DSN: 312-992-3986 X7830, COM'L 732-532-3986 X7830,TASM, APO AE 09391 [email protected]

26-Jan-2007 3

BALAD, IRAQ

CH961897


PMI-1 COMPLETED @ 3410.1 20070126. PMI-2DUE @ 3770.1 ACFT HRS. L3 VERTEXAEROSPACE BALAD, IRAQ APO AE 09391.JM139543

26-Jan-2007 4

BALAD, IRAQ

CH961897

D CO,1-131ST AVNREGT

UH-60-06-ASAM-02 M/R PITCH CONTROL RODJAMNUTS REPLACED @ PMI-1. 3410.1 ACFTHRS.

26-Jan-2007 5

BALAD, IRAQ

CH961897



8.7.DATE

6.REMARKS

4. 5.



D CO, 1-131ST AVIATIONREGIMENT

MAIN ROTOR RIG COMPLETED 23 JAN2007CONTL POSITIONS: 90 DEG RT/ 180DEG FWD/ 270 DEG LFT/ 0 DEG AFT/TOTAL/AVERAGE/REQD TOLERANCELOWCOL ANGLE #1 8.8 / -1 / -10/ -1.3 / -2.1 / -0.525 /-0.6 +OR- 0.125#2 #3#4HIGH COL ANGLE 20.6 / 12.8 / 9.7 / 17.4/ 60.5 / 15.125 /+15 TO +16FWD CYCLICANGLE -3.2 / /30.6/ / 33.8 //DIFF BETWEEN 270 & 90 DEG POSITIONS+33.0 MINAFT CYCLIC ANGLE 23.8 / / 4.5/ / 19.3 / /DIFF BETWEEN 90 & 270POS. NOT LESS THAN +19 DEGLEFT CYCLICANGLE / -8.7 / / 6.4 / 15.1/ /SUM OF180 & 0 POS TO BE 15 TO 17 DEG, AVG RANGE+7.5 TO 8.5 DEGRIGHT CYCLIC ANGLE / 7.3// 6.9/ 14.2/ /SUM OF 180 TO 0 POS TO BE 14TO 17 DEG, AVE RANGE+7.0 TO 8.0 DEG PRIMARY SERVO CONTROLROD BIAS: FWD: 1/2 TURN EXTRASHORTENED/AFT: 1/2 TURN EXTRALENGTHENED/LAT: 1 TURN LENGTHENEDT/RCABLE TENSION CHECK: TEMP (C) 16 DEG,CABLE TENSION LEFT 130 FT LBS, RIGHT 130FT LBSM/R RIG, PRIM SERVO BIAS, T/R CABLETENSION CHECKS COMPLETED BY: L-3VERTEX AEROSPACE, INBALAD, IRAQ 09391

27-Jan-2007 1

BALAD, IRAQ

RH170527

D CO 1-131 AVN BNT/R RIG AND BAIS CK COMP FOR INBOARDRETENTION PLATE RETORQUE @ 3419.2 ACFTHRSRED=4.999=5.33=.331YEL=4.708=5.04=.332BLK=4.141=4.454=.313BLU-4.226=4.566=.340

01-Feb-2007 1

BALAD IRAQ

WT524342


UH-60-07-ASAM-06 - EXTERNAL RESCUEHOIST - CABLE GUARD DEFLECTOR.COMPLIED WITH @ 3422.8 ACFT HRS. NOTINSTALLED ON THIS AIRCRAFT.

08-Feb-2007 1

BALAD, IRAQ APO AE09391

CH961897


UH-60-07-AMAM-01, COMMON MISSILEWARNING SYSTEM (CMWS) INSPECTIONCOMPLIED WITH. 28 MARCH 2007 @ 3504.8ACFT HRS. INSP A-895 ENTERED ON 2408-18.

28-Mar-2007 1

BALAD, IRAQ

CH961897


ACFT WIRING MOD TO ACCEPT THE PDMME-367-3 DIGITAL ELECTRONIC CLOCKS C/W @3530.6 ACFT HOURS.

02-Apr-2007 1

BALAD, IRAQ

CH961897


UH-60-07-ASAM-07, CEFS BONDING JUMPER,COMPLIED WITH @ 3639.6 ACFT HRS. N/ATHIS ACFT.

09-May-2007 1

BALAD, IRAQ

CH961897



8.7.DATE

6.REMARKS

4. 5.




MEC LETTER: LE-BAL015-0820 DATED: 21JUNE 2007 TAIL CONE SHEAR DECKCRACKACFT 7923340; 3766.8 ACFT HRS,CURRENTLY IN PMI-2 PHASE MAINTENANCE.PERSONNEL DISCOVERED AN APPROX. 1"CRACK IN THE WEB ON THE RIGHT REARCORNER OF THE TAIL CONE SHEAR DECK.REQ. AUTHORIZATION FOR REPAIR. RE: LE-BA008-0830AUTHORIZATION GRANTED TOREPAIR IAW SIKORSKY REPAIR PROCEDURE(SE-0871T021) REPAIR SCHEME 01 FORCRACKS LESS THAN 3" IN LENGTH. THE UNITHAS A COPY OF SE-0871T021. REF.: MEC LE-BAL015-0619, MEC LE-BAL015-0818.ANNOTATE REPAIR IN ACFT HISTORICALRECORDS.//ORIGINAL SIGNED// GARRY A.MERCALDI, DB3, ELECTRONICS ENGINEER,US ARMY RDECOM, AMSRD-AMR-AE-S DSN:312-992-3986 X7830, COM'L: 732-532-3986X7830, TASM, APO AE 09391 [email protected]

21-Jun-2007 1

BALAD, IRAQ

CH961897

L-3 VERTEXAEROSPACE APO AE09391

T/R RIG COMPLETED FOR PMI-2. BIAS SET @RED: .335, BLACK: .336, YELLOW: .333, BLUE:.331. T/R CABLE TENSION CHECK: L/H: 195,R/H: 194, TEMP: 42CCOMPLETED @ 3766.8ACFT HRS.

28-Jun-2007 1

BALAD, IRAQ

DL920021


M/R RIG COMPLETED FOR PMI-2 @ 3766.8ACFT HRS. LOW COLL: 90=9.1, 180=-2.4, 270=-9.8, 0=2.3, TOT=-0.8 AVG=-0.2, HIGH COLL:90=19.9, 180=10.8, 270=10.9, 0=20.4, TOTAL=62,AVG=15.5, FWD TOT=34, AFT TOTAL=19.2,LEFT TOTAL=16.1, RIGHT TOTAL=14.3.

28-Jun-2007 2

BALAD, IRAQ

DL920021


PMI-2 COMPLETED 1 JULY 2007 @ 3766.8ACFT HRS. NEXT PMI-1 DUE @ 4126.9 ACFTHRS.

01-Jul-2007 1

BALAD, IRAQ

DL920021


UH-60-07-ASAM-08, COMPLIED WITH 19 JULY2007 @ 3809.4 ACFT HRS. DISCREPANT HMUPART NUMBERS NOT INSTALLED ON THISAIRCRAFT.

19-Jul-2007 1

BALAD, IRAQ

CH961897


EIBF "B" KIT REMOVED. 04-Aug-2007 1

BALAD, IRAQ

CH961897


UH-60-07-ASAM-09, N/A THIS ACFT. DECU. 04-Aug-2007 2

BALAD, IRAQ

CH961897

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

08-Oct-2007 1

CJTR, AR

JP118008

AR AASFH-60-08-ASAM-02, POWER AVAILABLECONTROL CABLE, C/W AT 3872.4 ACFT HRS.

07-Nov-2007 1


CG450464

AR AASFH-60-08-ASAM-02 POWER AVAILABLECONTROL CABLE COMPLIED WITH AT ACFTHOURS 3872.4

13-Nov-2007 1

CJTR, AR

JP118008



8.7.DATE

6.REMARKS

4. 5.



DYNCORP OLROCM/ACE PERFORMED AT 3775 ACFT HRS BYTEAM MEMBER R. AMCOM PROJECT OLR.

28-Nov-2007 1

FTCKY 42223

TS640568

DYNCORP RESETUH-60-05-ASAM-01, REVISION OF FUELSYSTEM INTEGRITY CHECKS, PREVIOUSLYCOMPLIED WITH.

29-Nov-2007 1

FTCKY, 42223

TK005995

DYNCORP RESETUH-60-05-ASAM-05, TIE ROD ASSEMBLIES,PREVIOUSLY COMPLIED WITH.

29-Nov-2007 2

FTCKY 42223

TK005995

DYNCORP RESETUH-60-05-ASAM-08, TIE ROD ASSEMBLYREINSPECTION, PREVIOUSLY COMPLIEDWITH.

29-Nov-2007 3

FTCKY, 42223

TK005995

DYNCORP RESETUH-60-05-ASAM-11, WIRING HARNESSCHAFING, PREVIOUSLY COMPLIED WITH.

29-Nov-2007 4

FTCKY, 42223

TK005995

DYNCORP RESETUH-60-04-03 (SOF), CRASHWORTHYEXTERNAL FUEL SYSTEM (CEFS), NOTAPPLIED AT THIS TIME ESSS HARD POINTSNOT INSTALLED.

29-Nov-2007 5

FTCKY, 42223

TK005995

DYNCORP RESETUH-60-05-SOF-02, ENHANCED SCHEDULEDMAINTENANCE (ESM) PROGRAMIMPLEMENTATION, PREVIOUSLY COMPLIEDWITH.

29-Nov-2007 6

FTCKY, 42223

TK005995

DYNCORP RESETUH-60-06-SOF-01, MAIN ROTOR (M/R) HUBASSEMBLY, PREVIOUSLY COMPLIED WITH.

29-Nov-2007 7

FTCKY, 42223

TK005995

DYNCORP RESETH-60-08-AMAM-01, MAIN LANDING GEARSHOCK STRUTS INSPECTION, COMPLETED AT3874.9 AIRCRAFT HOURS.

12-Dec-2007 1

FTCKY, 42223

TK005995

DYNCORP RESETH-60-08-AMAM-02, TAIL ROTOR OUTBOARDRETENTION PLATE SHIMS INSPECTION,COMPLETED AT 3874.9 AIRCRAFT HOURS.

12-Dec-2007 2

FTCKY, 42223

TK005995

DYNCORP RESETH-60-08-ASAM-01, TROOP/GUNNERS SEATUPPER ENERGY ATTENUATING WIRESINSPECTION, COMPLETED AT 3874.9AIRCRAFT HOURS.

12-Dec-2007 3

FTCKY, 42223

TK005995

DYNCORP RESETH-60-08-ASAM-03, CHANGES TO CURRENTFUEL SYSTEM INTEGRITY CHECKSCOMPLETED AT 3874.9 AIRCRAFT HOURS.

12-Dec-2007 4

FTCKY, 42223

TK005995

DYNCORP RESETH-60-08-ASAM-04, PILOT'S LOWER SEAT RAILCHAFING ELECTRICAL HARNESSINSPECTION, COMPLETED AT 3874.9AIRCRAFT HOURS.

12-Dec-2007 5

FTCKY, 42223

TK005995

DYNCORP RESETH-60-08-ASAM-05, TAIL ROTOR QUADRANTSPRING CAPSULE ASSEMBLY INSPECTION,COMPLETED AT 3874.9 AIRCRAFT HOURS.

12-Dec-2007 6

FTCKY, 42223

TK005995

DYNCORP OLRMWO 1-1520-237-50-92MODIFICATIONINSTRUCTIONS FOR THE INSTALLATION OFTHE DOPPLER NAVIGATION SETPREPLANNED IMPROVEMENT (DGNS P31)

03-Jan-2008 1

FTCKY

QC000000

DYNCORP RESETH-60-08-AMAM-04, COCKPIT DOORJETTISONABLE WINDOWS, COMPLETED AT3874.9 AIRCRAFT HOURS.

14-Jan-2008 1

FTCKY, 42223

TK005995



8.7.DATE

6.REMARKS

4. 5.



DYNCORP RESETMAIN ROTOR RIG COMPLETED @ 3874.9 ACFTHRS, 15 JAN 2008 (RESET).LOW COLL ANGLE:90 RT +8.2, 180 FWD -1.1, 270 LFT -9.3, 0 AFT -0.1, TOTAL -2.3, AVG -0.575.HIGH COLLANGLE: 90 RT 18.8, 180 FWD 12.1, 270 LFT11.2, 0 AFT 18.1, TOTAL 60.2, AVG -15.05.FWDCYCLIC ANGLE: 90 RT -2.3, 270 LFT 31.2,TOTAL 33.5.AFT CYCLIC ANGLE: 90 RT 24.5,270 LFT 5.3, TOTAL 19.2.LEFT CYCLIC ANGLE:180 FWD 8.7, 0 AFT 6.6, TOTAL 15.3, AVG7.65.RT CYCLIC ANGLE: 180 FWD 6.9, 0 AFT7.5, TOTAL 14.4, AVG 7.2.PRIMARY SERVOCONTROL ROD BIASFWD: MINUS 6FLATS.AFT: PLUS 6 FLATS.LAT: MINUS 3FLATS.

15-Jan-2008 1

FTCKY, 42223

TK005995

DYNCORP RESETTAIL ROTOR COMPLETE RIG COMPLETED @3874.9 ACFT HRS, 15 JAN 2008 (RESET).T/RCABLE TENSIONL/H: 165R/H: 165TEMP: 21 C

15-Jan-2008 2

FTCKY, 42223

TK005995

DYNCORP RESETCABIN STRAP REPAIR AT STA.363, BL 34.5LRE-EVALUATED/INSPECTED OK. INSPECTIONCONDUCTED DURING RESET @ 3874.9 ACFTHRS PER MEC NUMBER LE-BAL014-0517,BALAD IRAQ.

18-Jan-2008 1

FTCKY, 42223

TK005995

DYNCORP RESETTB 1-1520-237-30-1, 21 SEP 2007, (RESET)AIRCRAFT DESERT OPERATIONS SPECIALINSPECTION AND CLEANING REQUIREMENTCOMPLETED @ 3874.9 AIRCRAFT HOURS.

28-Jan-2008 1

FTCKY, 42223

TK005995

DYNCORP RESETCOMPLIED WITH THE REQUIREMENTS OF TB 1-1500-200-20-31 DATED 23 NOV 06, AIRCRAFTDESERT OPERATIONS CLEANINGREQUIREMENT @ 3874.9 AIRCRAFT HOURS.

28-Jan-2008 2

FTCKY, 42223

TK005995

DYNCORP RESETH-60-08-SOF-01, MAIN ROTOR BLADEEXPANDABLE PIN INSPECTION CHANGECOMPLETED AT 3874.9 AIRCRAFT HOURS.

29-Jan-2008 1

FTCKY, 42223

TK005995

DYNCORP RESETH-60-08-AMAM-05, GOODRICH INTERNALRESCUE HOISTS, NOT APPLICABLE TO THISAIRCRAFT @ 3874.9 ACFT HRS.

29-Jan-2008 2

FTCKY, 42223

TK005995

DYNCORP RESETH-60-08-AMAM-06, COMMON MISSILEWARNING SYSTEM (CMWS) SEQUENCERS,INSPECTION COMPLETED AT 3882.7AIRCRAFT HOURS.

11-Feb-2008 1

FTCKY, 42223

TK005995

DYNCORP RESETTAIL ROTOR COMPLETE RE-RIG COMPLETED(9-11 RE-TORQUES) @ 3884.5 AIRCRAFTHOURS.BIAS:BLUE 4.000 - 4.340 = 0.340RED4.700 - 5.040 = 0.340BLK 4.000 - 4.340 =0.340YEL 4.750 - 5.080 = 0.330CABLETENSION: R180 L179 TEMP 30C

15-Feb-2008 1

FTCKY, 42223

TK005995

DYNCORP RESETH-60-08-ASAM-06, MAIN ROTOR PYLONSLIDING FORWARD FAIRING INSPECTIONCOMPLETED 27 FEB 2008 @ 3885.4 ACFT HRS.

27-Feb-2008 1

FTCKY, 42223

TK005995

FT CAMPELL KYRESET/PMI COMPLETED @ 3874.9 ACFT HRSWITH ALL MAINT. LOGGED IN AMDSCOMPUTER SYSTEM, NEXT PMI-1 DUE AT4234.9 ACFT HRS.

10-Apr-2008 1


TK005995



8.7.DATE

6.REMARKS

4. 5.



AR AASFH-60-08-AMAM-08 COMPLIED WITH ON 20 MAY2008 @ 3924.6 ACFT HRS. (70400-02252-133CABIN OVERHEAD PITCH FIXED LINKINSTALLED), (NO PITCH BIAS ACTUATORINSTALLED)

28-May-2008 1


MB173659

AR. AASFH-60-08-AMAM-07 (ASN-128B/D) COMPLIEDWITH @ 3952.2 ACFT HRS.

12-Jun-2008 1


CG450464

AR AASFH-60-08-ASAM-11 (FLIGHT CONTROLINSPECTION) COMPLIED WITH @ 4011.9 ACFTHRS.

16-Sep-2008 1


KL415170

AR. AASFH-60-08-ASAM-12 ( PARKER AT STARTERS)COMPLIED WITH @ 4017.8 ACFT HRS.

26-Sep-2008 1


CG450464

AR. AASFH-60-08-ASAM-13 (FIRE EXTINGUISHERTUBES) COMPLIED WITH @ 4017.8 ACFT HRS.

26-Sep-2008 2


CG450464

AMCOM FT HOODPROJECT OLR

ACE/CPCE PERFORMED AT 4037 AIRCRAFTHOURS BY TEAM MEMBERS K & Q.

08-Oct-2008 1


WS244328

AR AASFH-60-09-SOF-01 (SUSPECTED HMU'S)COMPLIED WITH @ 4036.7 ACFT HRS.

27-Oct-2008 1


CG450464

AR AASFRESCUE HOIST CABLE (GUARD) DELFECTORINSTALLED BY MOAVCRAD I/A/W MEC(F82152) @ 4036.7 ACFT HRS.

30-Oct-2008 1


CG450464

AR AASFMAINTENANCE ENGINEERING CALL (MECF83224) R/H 34.5 BEAM (ATTACHMENT BEAMFOR RESCUE HOIST ATTACHMENT BRACKET)REPLACEMENT COMPLETED BY MOAVCRAD@ 4036.7 ACFT HRS.

30-Oct-2008 2


CG450464

AR AASFH-60-09-SOF-02 (ALQ 144/CMWS) COMPLIEDWITH @ 4036.7 ACFT HRS.

18-Nov-2008 1


CG450464

AR AASFH-60-09-SOF-03 (POSSIBLE RETIREMENT LIFEOVERFLIGHT) COMPLIED WITH @ 4036.7 ACFTHRS

20-Nov-2008 1


KL415170

AR AASFM/R & T/R RIG COMPLETED FOR RMVL/REINSTOF MAIN XMSN @ 4036.7 ACFT HRS. PRIMARYSERVO SETTINGS AS FOLLOWS: (FWD)SHORT 1/2 TURN (AFT) LENGTH 1/2 TURN((LAT) SHORT 4 FLATS. T/R BIAS ASFOLLOWS : (RED) A-4.79 B-5.13 =0.34 (BLUE) A-4.02 B-4.38 =0.36 (YELLOW) A-4.76 B-5.11=0.35 (BLACK) A-4.04 B-4.39 =0.35

21-Nov-2008 1


CG450464

AR AASFH-60-08-ASAM-10 (ELECTRICAL WIRECHAFING) COMPLIED WITH @ 4036.7 ACFTHRS.

15-Dec-2008 1


CG450464



8.7.DATE

6.REMARKS

4. 5.



AR AASFH-60-09-ASAM-04 (RESCUE HOIST (CAD)COMPLIED WITH @ 4082.6 ACFT HRS.

02-Mar-2009 1


CG450464

AR AASFH-60-09-ASAM-05 (T/R QUADRANT SPRINGCAPSULES LIFE LIMIT CHANGE) COMPLIEDWITH @ 4082.6 ACFT HRS.

06-Mar-2009 1


KL415170

ARAASFH-60-09-ASAM-07 (FIRE EXTINGUISHERWIRING) COMPLIED WITH @ 4107.7 ACFTHRS.

22-Apr-2009 1


CS452504

AR AASF(ELT EBC-406HM) INSTALLED IN ACFT @4135.7 ACFT HRS. (ELT ID #)ADCC09CC7040775 ELT S/N # ) 400964

08-Jun-2009 1


CS452504

AR AASFH-60-09-ASAM-11 (CARGO DOOR WINDOWS)COMPLIED WITH @4453.4 ACFT HRS

30-Jun-2009 1


CB636828

AR AASFH-60-09-ASAM-08 ENGINE COWLING WEIGHTRESTRICTIONS COMPLIED WITH @ 4129.2ACFT HRS.

06-Aug-2009 1


CG450464

AR AASFH-60-09-ASAM-09 (FIRE EXTINGUISHERWIRING REV.) COMPLIED WITH @ 4116.4 ACFTHRS.

06-Aug-2009 2


CG450464

AR AASFH-60-09-AMAM-06 (CARGO HOOK CART. LIFEREDUCTION) COMPLIED WITH @ 4207.1 ACFTHRS.

26-Aug-2009 1


CG450464

AR AASFH-60-09-AMAM-04 (CO-PILOTS SEATINTERFERENCE W/ A2C2S) COMPLIED WITH @4207.1 ACFT HRS.

04-Sep-2009 1


CG450464

AR AASFGEN-09-AMAM-03 (ULLS-A(E) INTERGRATEDMATERIAL MANAGEMENT CENTER (LCF)CHANGE 60) COMPLIED WITH @ 4207.1 ACFTHRS.

15-Sep-2009 1


KL415170

AR AASFH-60-09-AMAM-07 (HALON HAND-HELD FIREEXTINGUISHERS HHFE) COMPLIED WITH @4207.1 ACFT HRS.

23-Sep-2009 1


CG450464

AR AASFM/R AMD T/R RIG CHECK FOR REPLACEMENTOF T/R PADDLES.LOW COLL -.3175, HIGHCOLL 15.3375 COLL DIFF 15.655FWD CYCLIC33.27, AFT CYCLIC 20.01, LEFT CYCLIC 15.19,RIGHT CYCLIC 14.80.T/R BIAS: RED 5.261-7.929=.332, BLUE 4.427-4.095=.332, YELLOW5.264-4.925=.339, BLACK 4.446-4.108=.338.CABLE TENSION TEMP 31C LEFT186 AND RIGHT 186.

30-Sep-2009 1


CB636828

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

01-Oct-2009 1


CS452504

DET 1 B CO 777THASB

H-60-10-AMAM-03 COCKPIT AIRBAG SYSTEMDEACTIVATION N/A (PCW)

10-Nov-2009 1

CAMP BONDSTEEL

JR238301



8.7.DATE

6.REMARKS

4. 5.



AR AASFH-60-10-AMAM-04 (ASN-128 B/C DOPPLER GPSNAV SET) COMPLIED WITH @ 4210.1 ACFTHRS.

16-Nov-2009 1


CG450464

AR AASFH-60-10-ASAM-03 (FIRE BOTTLE DISCHARGELINES AND NOZZLES) COMPLIED WITH @4210.1 ACFT HRS.

17-Nov-2009 1


CG450464

URS MOAVCRADT/R RIG CHECK COMPLETED AT 4216.1 ACFTHOURS. T/R BIAS COMPLETED AT 4216.1ACFT HOURS. BLACK 4.092/4.435=.343YELLOW 4.793/5.121=.328 BLUE4.120/4.455=.335 RED 4.775/5.105=.330

15-Dec-2009 1

SPRINGFIELD MO

MM413003

URS MOAVCRADPMI-1 COMPLETED AT 4221.3 ACFT HOURS 05-Jan-2010 1

SPRINGFIELD MO

MM413003

URS MOAVCRADH-60-10-ASAM-04 ( SAS LINKS) COMPLIEDWITH AT 4221.3 ACFT HOURS

11-Jan-2010 1

SPRINGFIELD MO

MM413003

URS MO AVCRADH-60-10-AMAM-05 (LCF CHANGE 60B)COMPLIED WITH AT 4221.3 ACFT HOURS

13-Jan-2010 1

SPRINGFIELD MO

MM413003

URS MOAVCRADH-60-10-AMAM-11 COMPLIED WITH AT 4226ACFT HRS

02-Feb-2010 1

SPRINGFIELD MO

MM413003

AR AASFENTRY DATED 05 JAN 2010 ENTERED INERROR, PMI-1 COMPLETED @ 4216.1 ACFTHRS. @ MOAVCRAD, NEXT PMI-2 DUE @4576.1 ACFT HRS. FUEL INTEGRITY TESTCOMPLETED DURING PMI, SEE WORKSHEETFOR TEST RESULTS.

05-Feb-2010 1


CG450464

AR AASFH-60-10-ASAM-06 (AUTO-IGN & DROOPIMPROVEMENT (TDI) MOD) COMPLIED WITH @4238.0 ACFT HRS.

12-Feb-2010 1

CAMP ROBINSON,ARKANSAS

CS452504

CSC/RASM-E MWO 1-1520-237-50-97 (P3I) COMPLETED @4242.6 ACFT HOURS

23-Feb-2010 1


TS272708

CSC/RASM-E MWO 1-1520-237-50-99 (5TH SENSOR)COMPLETED @ 4242.6 ACFT HOURS

23-Feb-2010 2


TS272708

AR AASFBFT VERSION 6.5 UPGRADE COMPLETED @4242.6 ACFT HRS. BY JASON GRADY,BFTFIELD SERVICE REP, QINETIQ N AMERICANSYSD ENGINEERING GROUP, MOAVCRAD.

06-Apr-2010 1


CG450464

AR AASFOPTION II CABIN HEATER SYSTEM (MAVEN)PN: 70070-95123-011 RMVD FORINSTALLATION OF ENVIRO SYSTEM, INC.HEATER PN: 70TH001-1. MWO RSN 1001029COMPLIED WITH @ 4242.6 ACFT HRS.

09-Apr-2010 1


CG450464

AR AASFCOMPLIED WITH H-60-10-ASAM-07 @ 4242.6 28-Apr-2010 1


CB636828

DET 2 D CO 2/147THAVN

COMPLIED WITH H-60-10-AMAM-12 (IMPROVEDDRAG BEAM)

07-May-2010 1

BOONE, IA

RM235107



8.7.DATE

6.REMARKS

4. 5.



DET 1 B CO 777TH ASBC/W REQUIREMENTS OF H-60-10-ASAM-08(AUX POWER UNIT (APU) AND APU FIREWALL)

18-Jun-2010 1

HOHENFELS, GERMANY

RM235107


H-60-10-AMAM-16 (COMMON MISSILEWARNING GUARDED DISPENSE SWITCH)COMPLIED WITH

25-Jun-2010 1

MNBG-E TF AVIATIONKOSOVO

BS084804


H-60-10-SOF-02(SPINDLE LUG NON-DESTRUCTIVE INSPECTION AND RETIREMENTLIFE CHANGES) COMPLIED WITH

26-Jun-2010 2


BS084804

DET 1 B CO 77TH ASBC/W REQUIREMENTS OF H-60-10-ASAM-11(ALL H-60 A/C COMMON COMPONENT R/CTIMES UPDATE)

07-Aug-2010 1


RM235107

DET 1 777TH AVNH-60-10-ASAM-12 (T700 SERIES ENGINESCOMMON COMPONENT RETIREMENT CHANGETIMES) COMPIED WITH.

28-Aug-2010 1


BS084804

DET 1 B CO. 777THASB

H-60-10-ASAM-15 (ESSS-FUEL SYSTEM VENTELBOW) COMPLIED WITH

10-Sep-2010 1

APO AE 09340

JR238301

DET1 B CO. 777TH ASBH-60-10-ASAM-16 (RESCUE HOIST CABLE CUTHARNESS CONNECTOR) COMPLIED WITH

22-Sep-2010 1

CAMP BONDSTEEL

JR238301

DET 1 B CO 777TH AVNH-60-11-ASAM-02 (TAIL ROTORSERVOCYLINDER ASSEMBLYHARDWARE)COMPLIED WITH.

14-Oct-2010 1

APO AE 09340

BS084804

DET 1 B CO 777TH ASBH-60-11-AMAM-03 (OIL COOLER FAN AXIALBEARING) COMPLIED WITH

26-Oct-2010 1

APO AE 09340

BS084804

DET 1 B CO 777 ASBH-60-11-ASAM-04 (TACAN RECEIVER)COMPLIED WITH

02-Dec-2010 1

APO AE 09340

RM235107

WUAUC0H-60-11-AMAM-04 (LCF CHANGE 61)COMPLIED WITH.

17-Dec-2010 1

APO AE 09340

BS084804

DET 1 B CO 777TH ASBH-60-11-ASAM-08 (LINE OFSIGHT(LOS)/IDENTIFY FRIEND OR FOE(IFF)ANTENNA AND INTREGRATED VEHICLEHEALTH AND MONITORING SYSTEM(IVHMS)ACCELEROMETER CONNECTORS SAFETYWIRE)COMPLIED WITH.

23-Feb-2011 1

APO AE 09340

BS084804

DET 1 B CO 777TH ASBH-60-11-AMAM-06 (MEDEVAC CAROUSELREFURBISHMENT) COMPLIED WITH.

02-Mar-2011 1

APO AE 09340

BS084804

DET 1 CO B 449TH ASBCOMPLIED WITH H-60-11-ASAM-09 (INTERNALAUXILIARY FUEL TRANSFER SYSTEM) @4459.8 ACFT HRS

07-Apr-2011 1

APO AE 09340

CB636828

DYNCORP KOSOVOCOMPLIED WITH REQUIREMENTS OF H-60-11-ASAM-06; CYCLIC WIRING HARNESS @ 4561.5ACFT HOURS ON 03-MAY-2011. INSTALLEDMARKER SLEEVES ON PILOT AND CO-PILOTSCYCLIC STICK WIRING HARNESSES

03-May-2011 1

CAMP BONDSTEEL

RS784200

DET 1 CO B 449THCOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-11 (AWR UPDATE)

20-May-2011 1

CBS

JH430868



8.7.DATE

6.REMARKS

4. 5.



DYNCORP KOSOVOCOMPLETED MAIN ROTOR RIG @ 4561.5 ACFTHOURS ON THIS DATE. LCA= 90RT: 8.3,180FWD: -2.6, 270LFT: 0AFT: 1.8, TOTAL: -2.4,AVG: -0.6E. HCA= 90RT: 20.1, 180FWD: 12.6,270LFT: 9.8, 0AFT: 17.6, TOTAL: 60.1, AVG:15.025. FCA= 90RT: -2.0, 270LFT: 31.4, TOTAL:33.4. ACA= 90RT: 25.7, 270LFT: 4.3, TOTAL:21.4. LCA= 180FWD: 8.7, 0AFT: 15.5. RCA=180FWD: 6.7, 0AFT: 7.5, TOTAL: 14.2.PROTRACTOR SN: PT-03.

23-May-2011 1

CAMP BONDSTEEL

RS784200

DYNCORP KOSOVOCOMPLETED TAIL ROTOR RIG @ 4561.5 ACFTHOURS. RED: INT-4.793, BIAS-5.130, DIFF-0.337; BLUE: INT-4.125, BIAS-4.470, DIFF-0.345;YELLOW: INT-4.770, BIAS-5.102, DIFF-0.332;BLACK: INT-4.110, BIAS-4.450, DIFF-0.340. TAILROTOR PISTON TRAVEL: OUT-3.48, IN-0.035

23-May-2011 2

CAMP BONDSTEEL

RS784200

DYNCORP KOSOVOCOMPLETED TAIL ROTOR CABLE TENSIONCHECK @ 4561.5 ACFT HOURS. L/H: 165 LBS,R/H: 163 LBS, AVG: 164 LBS, DIFF: 2 LBS.TEMP: 80`F. THERMOMETER SN:UF791,TENSIONOMETER SN: 21464.

23-May-2011 3

CAMP BONDSTEEL

RS784200

DYNCORP KOSOVOCOMPLETED PMI-2 REQUIREMENTS @ 4561.5ACFT HOURS. NEXT PMI-1 DUE @ 4921.5 ACFTHOURS

26-May-2011 1

CAMP BONDSTEEL

RS784200

DET 1 CO.B 449TH ASBCOMPLY WITH REQUIREMENTS OF H-60-11-AMAM-13 (EXTERNAL RESCUE HOIST MOUNTFITTING)@ACFT HRS. 4566.0

11-Jun-2011 1

CBS

TS659739

449TH AVUMH-60-11-SOF-01, ALL H-60 SERIES AIRCRAFT,DISCREPANT SELF LOCKING DOUBLEHEXAGON NUTS COMPLIED WITH

11-Jul-2011 1

CBS

DN337516

449TH AVUMH-60-11-ASAM-13, ALL H-60A/L SERIESAIRCRAFT, ENGINE AIR INLET ANIT-ICING/MODULATING VALVE COMPLIED WITH

11-Jul-2011 2

CBS

DN337516

DET 1 CO B 449THAVUM

H-60-11-AMAM-15-INTERGRATED VEHICLEHEALTH MANAGEMENT SYSTEM-N/A THISAIRCRAFT-IVHMS NOT INSTALLED

11-Jul-2011 3

CBS

JH430868

449TH AVUMH-60-11-ASAM-14, ALL H-60 SERIESAIRCRAFT, ENGINE COWLING REPAIRRESTRICTION COMPLIED WITH

15-Jul-2011 1

CBS

DN337516

449TH AVUMTAIL ROTOR RIG COMPLETED @ 4679.8AIRCRAFT HOURS, TAIL ROTOR BIAS SET TO:RED 5.184-4.854=.330; BLUE 4.446-4.109= .337;YELLOW 5.120-4.786= .334; BLACK 4.452-4.117= .335, TAIL ROTOR CABLE TENSION L/HCABLE 171, R/H CABLE 173 @ 30 DEG C, T/RPISTON TRAVEL (INITIAL) OUT 3.53 IN 0 -(AFTER) OUT 3.47 IN .049

16-Sep-2011 1

CBS

DN337516

449TH AVUMH-60-11-AMAM-20, AN/ASN-128D DOPPLERAND AVIATION MISSION PLANNING SYSTEM(AMPS) SOFTWARE UPGRADE COMPLIEDWITH

26-Sep-2011 1

CBS

DN337516

DET 1 C0 B 449TH ASBH-60-12-AMAM-01 FUEL MOMENT UPDATE TOOPERATORS MANUAL FOR H-60M N/A THISAIRCRAFT

07-Oct-2011 1

CBS

JH430868



8.7.DATE

6.REMARKS

4. 5.



DET 1 CO B 449TH ASBCOMPLIED WITH H-60-12-SOF-01- ONE TIMEINSPECTION OF INTERMEDIATE GEARBOXESFOR SUSPECTED INTERNAL LUBIRICATIONFAILURE WITH 100 HOURS OR LESS TSN, AND/OR TSO

08-Oct-2011 1

CBS

JH430868

DET 1 CO B 449THLATE ENTRY- COMPLIED WITH H-60-SOF-02-REDUCTION OF TSN &TSO HOURS FROM100HRS TO 50 HRS ON T/R GEARBOXES

15-Oct-2011 1

CBS

JH430868

DET 1 CO B 449THCOMPLY WITH REQUIREMENTS OF H-60-12-SOF-03-AUTHORIZE THE USE OF GEARBOXES70357-06300-042 OR 70357-06300-044 ON ALL H-60 A/K/L/M AIRCRAFT

15-Oct-2011 2

CBS

JH430868

CO B, 777TH ASBCOMPLIED WITH THE REQUIREMENTS OF H-60-11-AMAM-19, ULLS-A (E) LCF CHANGE 62

13-Nov-2011 1

CBS

DM649028

CO B 777 ASBH-60-12-ASAM-02, ALL H-60A/K/L SERIESAIRCRAFT, DRAG BEAM REPLACEMENTCOMPLIED WITH

09-Dec-2011 1

CAMP BONDSTEEL

AL727224

CO B 777 ASBH-60-12-AMAM-04 INFORMATIONAL, ALL H-60M SERIES AIRCRAFT, AN/APX-118TRANSPONDER (H-60 M ONLY)

20-Dec-2011 1

CAMP BONDSTEEL

AL727224

TASM-E MANNHEIM,GERMANY

PERFORMED ACE/CPCE EVALUATION I/A/WTB 1-1520-237-50-6 AT 4808.1 ACFT HRS BYACE TEAM MEMBER "Z".

20-Dec-2011 2

CAMP BONDSTEEL

BD883896

CO B, 777TH ASBH-60-12-ASAM-03: UH-60L/M SERIESAIRCRAFT, FIRE SUPPRESSION SYSTEMPLUMBING INSPECTION, N/A THIS MDS

11-Jan-2012 1

CAMP BONDSTEEL

DM649028

DYNCORP KOSOVOCOMPLETED MAIN AND TAIL ROTOR RIG FORCOMPLETION OF 48 MONTH CONTROL RODINSPECTION. LOW COL ANGLE AVG -.575,HIGH COL 15.1, FWD CYC 33.2, AFT CYC 20.8,LEFT CYC 7.85, RT CYC 7.05. T/R BIAS RED .31,BLU .34, YEL .326, BLK .340. CABLE TENSIONL 160, R 160 @ 70F.

14-Jan-2012 1

CAMP BONDSTEEL

AL727224

DYNCORP KOSOVO48 MO CONTROL ROD INSP COMPLETED BYDYNCORP KOSOVO AT 4820.7 ACFT HOURS.

14-Jan-2012 2

CAMP BONDSTEEL

AL727224

DYNCORP KOSOVO48 MO CABIN TUB INSPECTION COMPLETEDBY DYNCORP KOSOVO AT 4820.7 ACFTHOURS.

14-Jan-2012 3

CAMP BONDSTEEL

AL727224

CO B, 777TH ASBH-60-12-AMAM-05: IMPROPERLY INSTALLEDLITTER LIFT CONNECTOR, HH-60 AIRCRAFTONLY

20-Jan-2012 1

CAMP BONDSTEEL

DM649028

CO B 777 ASBH-60-12-ASAM-04: H-60M SERIES AIRCRAFT,AN/ARC-231 OPERATION WITH MOD 10SOFTWARE (N/A THIS MDS)

25-Jan-2012 1

CAMP BONDSTEEL

AL727224

CO B 777 ASBCABLE TENSION ADJUSTED DURING 9-11 HRCABLE TENSION CHECK. NEW TENSION L/H:126, R/H: 125 @ +14 DEGREES CELCIUS.

29-Jan-2012 1

CAMP BONDSTEEL

AL727224

CO B 777 ASBH-60-12-ASAM-05: MAINTENANCEMANDATORY, ALL H-60M SERIES AIRCRAFT,FM #2 ANTENNA CONNECTOR BRACKET (H-60M AIRCRAFT ONLY)

16-Feb-2012 1

CAMP BONDSTEEL

AL727224



8.7.DATE

6.REMARKS

4. 5.



CO B, 777TH ASBH=60-12-SOF-04: BREEZE EASTERNEXTERNAL RESCUE HOIST OPERATIONSCOMPLIED WITH. NO BREEZE EASTERNEXTERNAL HOIST INSTALLED IN THISAIRCRAFT

17-Feb-2012 1

CAMP BONDSTEEL

DM649028

CO B, 777TH ASBH-60-12-AMAM-06: INTERCOMMUNICATIONSYSTEM (ICS) CABLE ROUTING ANDCLAMPING, N/A THIS AIRCRAFT, UH-60M MDSONLY

22-Feb-2012 1

CAMP BONDSTEEL

DM649028

CO B, 777TH ASBCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-06, UPPER BULKHEAD FUEL SYSTEMBREAKAWAY VALVE AND FIREEXTINGUISHING SYSTEM DIRECTIONALVALVE

23-Feb-2012 1

CAMP BONDSTEEL

DM649028

CO B, 777TH ASBCOMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-03 @ 4855.9 ACFT HOURS ON 23 FEB 12( TRANSPONDER AND COMMON MISSILEWARNING SYSTEM INSTALLATION )

23-Feb-2012 2

CAMP BONDSTEEL

DM649028

CO B 777 ASBH-60-12-AMAM-07: MAINTENANCEMANDATORY, ALL H-60M SERIES AIRCRAFT,MAIN ROTOR BLADE WATER INTRUSIONINSPECTION.(H-60M AIRCRAFT ONLY)

09-Mar-2012 1

CAMP BONDSTEEL

AL727224

DYNCORP INT LLCCOMPLIED WITH REQUIREMENTS OF H-60-12-SOF-05 (CHANGE TO DEPOT REPAIREDLEGACY MAIN ROTOR BLADES COMPLIANCEDATE) COMPLETED @ 4917.3 ACFT HOURS ON11-APR-2012

11-Apr-2012 1

CAMP BONDSTEEL

RS784200

DYNCORP INT LLCCOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-17 (TAIL ROTOR RETENTION PLATESHIMS) COMPLETED @ 4917.3 ACFT HOURSON 12-APR-2012

12-Apr-2012 1

CAMP BONDSTEEL

RS784200

DYNCORP INT LLCCOMPLETED CABIN ROOF AIRFRAME REPAIRAT STA-368; WL-265,-BL-35R BY APPLING AFORMED PATCH OVER CRACKED AREAAFTER STOP DRILLING CRACK.

16-Apr-2012 1

CAMP BONDSTEEL

RS784200

DYNCORP INT LLCCOMPLETED 2 CABIN BEADED PANELAIRFRAME REPAIRS AT STA-293 THRU 308;WL-232 & WL-242,-BL-35R BY APPLING AFORMED PATCH OVER CRACKED AREAAFTER CUTTING OUT CRACKED AREAS.

16-Apr-2012 2

CAMP BONDSTEEL

RS784200

DYNCORP INT LLCCOMPLETED MAIN & TAIL ROTOR RIGCHECKS; NO ADJUSTMENTS NEEDED.

25-Apr-2012 1

CAMP BONDSTEEL

RS784200

DYNCORP INT LLCCOMPLETED TAIL ROTOR BIAS ADJUSTMENT.RED: INT=4.755, BIAS=5.089, DIFF=.334; BLUE:INT=4.032, BIAS=4.370, DIFF=.338; YELLOW:INT=4.697, BIAS=5.009, DIFF=.330; BLACK:INT=4.038, BIAS=4.368, DIFF=.330. T/R CABLETENSION: L=155LBS, R=155LBS, TEMP=70F.OUT=3.470, IN=0.024.

25-Apr-2012 2

CAMP BONDSTEEL

RS784200

DYNCORP INTL, LLCCOMPLETED PMI #1 @ 4917.3 NEXT PMI #2DUE @ 5277.3 ACFT HRS

25-Apr-2012 3

CBS, KOSOVO

BH986618



8.7.DATE

6.REMARKS

4. 5.



CO B 777 ASBH-60-11-AMAM-20: MAINTENANCEMANDATORY, ALL CH-47D AND EH/UH -60A/LSERIES AIRCRAFT, AN/ASN-128D DOPPLERAND AVIATION MISSION PLANNING SYSTEM(AMPS) SOFTWARE UPGRADE COMPLIEDWITH.

30-May-2012 1

CAMP BONDSTEEL

AL727224

CO B 777 ASBH-60-12-AMAM-09, ALL H-60 SERIES ACFT,HYDRAULIC LINE CHAFE DUE TO MISSINGCLAMPS. COMPLIED WITH.

08-Jun-2012 1

CAMP BONDSTEEL

AL727224

CO B 777 ASBAirworthiness Release (AWR) for Use ofForestPenetrator (NSN 4240~00-199-7353, PIN K26-1000-9), Forest Penetrator (NSN 4240-01-500-8115, PIN K26-1000-105), Survivor's Sling,SKED Rescue System, Rescue Net, RescueStrop, and Rescue Seat with UHlHH-60AlLIMHelicopters Equipped with a Rescue Hoist(AWR 980) DATED 16 DEC 11

02-Jul-2012 1

CBS

AL727224

CO B 777 ASBAirworthiness Release (AWR) for UH-60AlL andHH-60AlL Helicopters Equipped with SEIIndustries Bambi Water Buckets (AWR 1054)DATED 9 MAR 11

02-Jul-2012 2

CBS

AL727224

CO B 777 ASBAirWorthiness Release (A WR) to Conduct Heli-Basket Operations with Electric Long Line(ELL) on UH-60AlL Helicopters (A WR 1127)DATED 16 DEC 11

02-Jul-2012 3

CBS

AL727224

CO B 777 ASBAirworthiness Release (AWR) for Operation ofthe Goodrich 42305-3/-5 Internal Rescue Hoist(IRH) on UH-60AlL Helicopters (A WR 1308)DATED 23 DEC 11.

02-Jul-2012 4

CBS

AL727224

CO B 777 ASBAIRWORTHINESS RELEASE (AWR) FOR EH-60A AND UH/HH-60 A/L/M HELICOPTERSEQUIPPED WITH OREGON AERO SEATCUSHIONS (AWR 1309) DATED 10 Feb 12.

02-Jul-2012 5

CBS

AL727224

CO B 777 ASBAIRWORTHINESS RELEASE (AWR) FOR ALLUH-60A/L AND EH-60A HELICOPTERSEQUIPPED WITH RT-1518C/ARC-164 HAVEQUICK II (HQII) UHF/AM RADIOS (AWR 1310)DATED 4 NOV 05.

02-Jul-2012 6

CBS

AL727224

CO B 777 ASBAirworthiness Release (AWR) forthe Operationof Common Missile Warning System (CMWS)and Improved Countermeasures Dispenser(ICMD) on UH-60AIL Helicopters (AWR1324)DATED 1 JUN 12.

02-Jul-2012 7

CBS

AL727224

CO B 777 ASBAirworthiness Release (A WR) for UHIHH-60AlLIM Helicopters Equipped withPatientMovement Items (PMI) (A WR 1330) DATED 3AUG 12.

02-Jul-2012 8

CBS

AL727224

CO B 777 ASBAirworthiness Release (AWR) for US Army UH-60A/L Helicopters Equipped with theTelephonics Aircraft Wireless Intercom System(AWIS) with Aircraft Interface Unit (AIU) (AWR1378) DATED 21 JAN 11.

02-Jul-2012 9

CBS

AL727224



8.7.DATE

6.REMARKS

4. 5.



CO B 777 ASBAirworthiness Release (AWR) for the Operationof Common Missile WarningSystem (CMWS),Improved Countermeasures Dispenser (ICMD),and Pre-Planned ProductImprovement (P31), onUH-60AiL Helicopters (A WR1425) DATED 29JUN 12.

02-Jul-2012 10

CBS

AL727224

CO B 777 ASBAIRWORTHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS TO OPERATE WITHENVIRO SYSTEMS, INC. HEATER (AWR 1447)DATED 27 JUL 12.

02-Jul-2012 11

CBS

AL727224

CO B 777 ASBAirworthiness Release for all UHfHH -60A/LHelicopters Equipped with the LC-6 DigitalChronometer (A WR1452) DATED 29 DEC 09.

02-Jul-2012 12

CBS

AL727224

CO B 777 ASBAirworthiness Release for all UHlEH-60A/LHelicopters Equipped with the Battelle CautionAdvisory Panel (CAP) (AWR1455) DATED 10NOV 11.

02-Jul-2012 13

CBS

AL727224

CO B 777 ASBAirworthiness Release (A WR) for the GanninGPSMAP 696, 695, 496, 495, 396,296 or 295 onUS Anny UHlHH-60A!LIM Helicopters (A WR1466) DATED 31 AUG 11.

02-Jul-2012 14

CBS

AL727224

CO B 777 ASBAirworthiness Release (AWR) for UH-60A andEH-60A Helicopters with Main ModuleAssemblies (Part Numbers 70351-08100-075and 70351-08100-076) Equipped with theImproved Planetary Carrier Assembly, PartNumber 70351-08175-046 (A WR 1479) DATED13 JAN 12.

02-Jul-2012 15

CBS

AL727224

CO B 777 ASBAirworthiness Release (A WR) for UH-60AILHelieopters Equipped with theCommon MissileWarning System (CMWS) 5TH Sensor A and BKit (AWR 1494) DATED 29 JUN 12.

02-Jul-2012 16

CBS

AL727224

CO B 777 ASBAirworthiness Release (A WR) for US Army HH-60AlL Helicopters Equipped with theTelephonics Aircraft Wireless Intercom System(AWLS) with Aircraft Interface Unit (AIU) (AWR1564) DATED 12 NOV 10.

02-Jul-2012 18

CBS

AL727224

CO B 777 ASBAirworthiness Release (A WR) for all UHIHH-60AlLIM Helicopters Equipped with theTitanium (1000997-001 (S7020-12008-043)) orStainless Steel Rescue Hoist Cable (Guard)Deflector (A WR 1566) DATED 18 MAR 11.

02-Jul-2012 19

CBS

AL727224

CO B 777 ASBAirworthiness Release (AWR) for the Operationof the Light Emitting Diode (LED) CentralDisplay Unit (CDU) and Pilot Display Unit (PDU)on UH/HH-60AlL Helicopters (AWR 1607)DATED 27 MAR 12.

02-Jul-2012 20

CBS

AL727224

CO B 777 ASBAirworthiness Release (A WR) for UWHH-60AILHelicopters Equipped with the Dual I StabilatorController (DSC) (AWR 1694) DATED 5 JAN 12.

02-Jul-2012 21

CBS

AL727224

CO B 777 ASBAirworthiness Release (AWR) for UH-60A/LHelicopters Equipped with ANIAPX-118Common Transponder (CXP) (A WR 1738)DATED 1 FEB 11.

02-Jul-2012 22

CBS

AL727224



8.7.DATE

6.REMARKS

4. 5.



CO B 777 ASBAirworthiness Release (AWR) for Operationofthe Aviator's Night Vision Imaging System(ANVIS) AN/AVS-6 Series Night Vision Goggles(NVG) in UH/HH-60AILIM Aircraft (AWR 1750)DATED 27 MAR 12.

02-Jul-2012 23

CBS

AL727224

CO B 777 ASBAIRWORTHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS EQUIPPED WITH THEDOPPLER GLOBAL POSITIONING SYSTEMNAVIGATION SYSTEM (DGNS), AN/ASN-128B/D(AWR 1753 DATED 31 AUG 11.

02-Jul-2012 24

CBS

AL727224

CO B 777 ASBAIRWORTHINESS RELEASE (AWR) FOR THEELECTRONIC DATA MANAGER (EDM) AND/ORBLUE FORCE TRACKING SYSTEM (BFT) ONUH/EH/HH-60A/L HELICOPTERS (AWR 1800)DATED 20 JUL 12.

02-Jul-2012 25

CBS

AL727224

CO B 777 ASBInterim Statemenot f AirworthinessQualification( ISAQ) for all UH-60NLHelicoptersEquipped with Advanced Flight ControlComputer (AFCC) (ISAQI05) DATED 4 OCT 02.

02-Jul-2012 26

CBS

AL727224

CO B 777 ASBAirworthiness Release (A WR) for UH/HH-60AllJM with a NCS Magnus modelRNM101Laptop Onboard and Operating (AWR 1648)DATED 9 MAR 12.

02-Jul-2012 27

CAMP BONDSTEEL

AL727224

CO B, 777TH ASBCOMPLIED WITH THE REQUIREMENTS OF H-60-12-AMAM-12, RESCINDED COMMONCOMPONENT REMOVAL DATES AT 4960.7ACFT HOURS

11-Jul-2012 1

CAMP BONDSTEEL

DM649028

CO B, 777TH ASBH-60-12-AMAM-13, INFORMATIONAL,CHANGES TO HEALTH INDICATOR TEST (HIT)CHECK PROCEDURES

12-Jul-2012 1

CAMP BONDSTEEL

DM649028

777TH ASBH-60-12-ASAM-08 CARGO HOOK MANUALRELEASE SPRING ASSEMBLY INSTALLATION,COMPLIED WITH, NO DEFECTS

19-Jul-2012 1

CAMP BONDSTEEL

KC941410

DYNCORP INTL LLCCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-07, H-60 SERIES AIRCRAFT,ELECTRICAL WIRING CHAFFING. REPAIRED:FLOOR BUNDLE AFT OF CENTER CONSOLE,P333 DE-ICE CONNECTOR CHAFFING, L/HOVERHEAD CIRCUIT PANEL WIRINGCHAFFING, & R/H CIRCUIT BREAKER PANELCHAFFING AGAINST HUD CABLE.

23-Jul-2012 1

CAMP BONDSTEEL

RS784200

CO B 777TH ASBH-60-12-AMAM-14: AN/ARN-149 LF ADF (UH-60L MODELS ONLY)

24-Jul-2012 1

CAMP BONDSTEEL

DM649028

B CO 777 ASB KFOR 16Airworthiness Release (A WR) for the GanninGPSMAP 696, 695, 496, 495, 396,296 or 295 onUS Anny UHlHH-60A!LIM Helicopters (A WR1466) DATED 22 AUG 12.

22-Aug-2012 1

CAMP BONDSTEEL

WA754583

CO B 777 TH ASBCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-09 (RESCUE HOIST CARTRIDGEACTUATED DEVICE (CAD) ELECTRICALCONNECTOR) EXTERNAL RESCUE HOIST NOTINSTALLED

23-Aug-2012 1

CAMP BONDSTEEL

ES645237



8.7.DATE

6.REMARKS

4. 5.



B CO 777TH ASB/TFAVN

COMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-15 AT 5022.5 ACFT HOURS. ( TRIMACTUATORS)

04-Sep-2012 1

CAMP BONDSTEEL

WA754583

B CO 777 ASB KFOR 16Airworthiness Release for all UHlEH-60A/LHelicopters Equipped with the Battelle CautionAdvisory Panel (CAP) (AWR1455) DATED 18SEP 12.

18-Sep-2012 1

CAMP BONDSTEEL

WA754583

B CO 777 ASB KFOR 16Airworthiness Release (AWR) for the Operationof Common Missile WarningSystem (CMWS),Improved Countermeasures Dispenser (ICMD),and Pre-Planned ProductImprovement (P31), onUH-60AiL Helicopters (A WR1425) DATED 18SEP 12.

18-Sep-2012 2

CAMP BONDSTEEL

WA754583

B CO 777 AS KFOR 16Airworthiness Release (AWR) forthe Operationof Common Missile Warning System (CMWS)and Improved Countermeasures Dispenser(ICMD) on UH-60AIL Helicopters (AWR1324)DATED 18 SEP 12.

18-Sep-2012 3

CAMP BONDSTEEL

WA754583

B CO 777 ASB KFOR 16OPERATE IAW Airworthiness Release (AWR)for UH-60AlL and HH-60AlL HelicoptersEquipped with SEI Industries Bambi WaterBuckets (AWR 1054) DATED 16 NOV 12

16-Nov-2012 1

CAMP BONDSTEEL

WA754583

CO B 777TH ASB GSCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-02 (AHRS), PASS

21-Nov-2012 1

CAMP BONDSTEEL

ES645237

B CO 777 ASB KFOR 16OPERATE IAW AIRWOTHINESS RELEASE(AWR R5) INTEGRATED PERFOMANCE A/CCONFIG (IPAC) DATED 27 NOV 12.

27-Nov-2012 1

CAMP BONDSTEEL

WA754583

DYNCORPINTERNATIONAL LLC

COMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-01 @ 5096.1 ACFT HOURS. GRIMESPOWER SUPPLY INSTALLED ON THIS ACFT.

28-Nov-2012 1

CAMP BONDSTEEL

RS784200

CO B 777 TH ASBCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-03 (DECU/EDECU, TGT BIAS), ACFTNOT AFFECTED T700-GE-700 ENGINESINSTALLED

29-Nov-2012 1

CAMP BONDSTEEL

ES645237

B CO 777 ASB KFOR 16Airworthiness Release (A WR) for UHIHH-60AlLIM Helicopters Equipped withPatientMovement Items (PMI) (A WR 1330) DATED 30NOV 12.

30-Nov-2012 1

CAMP BONDSTEEL

WA754583

CO B 777TH ASB, KFOR16

COMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-05 (M/L/G WHEEL BRAKE ASSY.) @5159.4 ACFT HOURS, COMP #1 PASS, COMP #2PASS

23-Jan-2013 1

CAMP BONDSTEEL

ES645237

B CO 777 ASB KFOR16OPERATE IAW AirWorthiness Release (A WRR5) to Conduct Heli-Basket Operations withElectric Long Line (ELL) on UH-60AlLHelicopters (A WR 1127) DATED 25 JAN 13.

25-Jan-2013 1

CAMP BONDSTEEL

WA754583

B CO 777 ASB KFOR 16Airworthiness Release (AWR) for UH-60A/LHelicopters Equipped with ANIAPX-118Common Transponder (CXP) (A WR 1738)DATED 1 FEB 13.

01-Feb-2013 1

CAMP BONDSTEEL

WA754583

CO B 777TH ASB/KFOR16

COMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-04, PARSED AMCOM LCF CHANGE 63FILES

09-Feb-2013 1

CAMP BONDSTEEL

ES645237



8.7.DATE

6.REMARKS

4. 5.




COMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-06 (CEFS) N/A THIS AIRCRAFT,AIRCRAFT DOES NOT HAVE ESSS HARDPOINTS, NO CEFS TANKS ARE PRESENT ATCAMP BONDSTEEL

13-Feb-2013 1

CAMP BONDSTEEL

ES645237

B CO. 777 ASBOPERATE IAW (AWR 1872 R0) AWIS, DATED 24JAN 13.

17-Feb-2013 1

CAMP BONDSTEEL

SH152661

B CO. 777 ASBOPERATE IAW (AWR 1127 R5) HELI-BASKETOPERATIONS WITH ELECTRIC LONG LINE,DATED 25 JAN 13.

17-Feb-2013 2

CAMP BONDSTEEL

SH152661

B CO. 777 ASBOPERATE IAW (AWR 1452 R3) LC-6 DIGITALCHRONOMETER, DATED 18 JAN 13.

17-Feb-2013 3

CAMP BONDSTEEL

SH152661

B CO. 777 ASBOPERATE IAW (AWR 1738 R1) AN/APX-118COMMON TRANSPONDER, DATED 01 FEB 13.

17-Feb-2013 4

CAMP BONDSTEEL

SH152661

B CO 777 ASB, KFOR 16AIRWORTHINESS RELEASE (AWR) FOR THEELECTRONIC DATA MANAGER (EDM) AND/ORBLUE FORCE TRACKING SYSTEM (BFT) ONUH/EH/HH-60A/L HELICOPTERS (AWR 1800)DATED 8 MAR 13.

08-Mar-2013 1

CAMP BONDSTEEL

WA754583

B CO 777 ASB, KFOR 16Airworthiness Release (AWR) for Use ofForestPenetrator (NSN 4240~00-199-7353, PIN K26-1000-9), Forest Penetrator (NSN 4240-01-500-8115, PIN K26-1000-105), Survivor's Sling,SKED Rescue System, Rescue Net, RescueStrop, and Rescue Seat with UHlHH-60AlLIMHelicopters Equipped with a Rescue Hoist(AWR 980) DATED 15 MAR 13.

15-Mar-2013 1

CAMP BONDSTEEL

WA754583

B CO 777TH ASB, KFOR16

OPERATE IAW (AWR 1566 R3) HELICOPTERSEQUIPPED WITH THE TITANIUM (1000997-001(S7020-12008-043)) OR STAINLESS STEELRESCUE HOIST CABLE (GUARD) DEFLECTORDATED 18 MAR 2013.

18-Mar-2013 1

CAMP BONDSTEEL

WA754583

B CO 777TH ASB, KFOR16

COMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-04 (PLASTIC MEDIA BLAST AND OXIDEFLAKE RESIDUE) @5240.9 ACFT HRS. ALLCOMPONENTS WERE NOT LISTED FROM THEAFFECTED S/N. IGB HAS NOT BEENOVERHAULED SINCE INSTALLATION.

21-Mar-2013 1

CAMP BONDSTEEL

WA754583

B CO 777 ASB, KFOR 16OPERATE IAW AIRWOTHINESS RELEASE(AWR1513 R6) INTEGRATED PERFOMANCEA/C CONFIG (IPAC) DATED 22 MAR 2013 .

22-Mar-2013 1

CAMP BONDSTEEL

WA754583

B CO 777 ASB, KFOR 16Airworthiness Release (AWR) for the Operationof the Light Emitting Diode (LED) CentralDisplay Unit (CDU) and Pilot Display Unit (PDU)on UH/HH-60AlL Helicopters (AWR 1607)DATED 29 MAR 13.

29-Mar-2013 1

CAMP BONDSTEEL

WA754583

B CO 777 ASB, KFOR 16Airworthiness Release (AWR) for Operationofthe Aviator's Night Vision Imaging System(ANVIS) AN/AVS-6 Series Night Vision Goggles(NVG) in UH/HH-60AILIM Aircraft (AWR 1750)DATED 1 APR 15.

29-Mar-2013 2

CAMP BONDSTEEL

WA754583



8.7.DATE

6.REMARKS

4. 5.




AVIATION ENGINEERING DIRECTORATE HASGRANTED A EXTENSION (MEC: F163386) OFTHE OIL COOLER ASSY. (FAN AXIAL, PN:70361-03005-107, SN: 06811718SB) &BEARINGS (BALL BRNG ANN (OIL COOLERFWD) PN: Z33C32, SN: UNK18SB #1) (BALLBRNG ANN (OIL COOLER FWD) PN: Z33C32,SN: UNK18SB #2) TBO BY 24.3 HOURS TOALIGN THE REPLACEMENT WITH THE PMI DUEAT 5277.3; BEARINGS ORIGINAL TBO TIME IS5253.0 HRS; NEW TBO FOR THE THREEAVOVE MENTIONED COMPONENTS IS NOT TOEXCEED 5277.3 ACFT HOURS.

02-Apr-2013 1

CAMP BONDSTEEL

ES645237

B CO 777 ASB, KFOR 16Airworthiness Release (A WR) for UHIHH-60AlLIM Helicopters Equipped withPatientMovement Items (PMI) (A WR 1330) DATED 4APR 13.

04-Apr-2013 1

CAMP BONDSTEEL

WA754583

B CO. 777 ASB KFOR 16COMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-05 EXTERNAL BREEZE EASTERN HOIST

09-Apr-2013 1

CAMP BONDSTEEL

SH152661


COMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-07 @ 5257.4 ACFT HOURS. NODEFECTS FOUND

11-Apr-2013 1

CAMP BONDSTEEL

RS784200

B CO 777 ASB, KFOR 16OPERATE IAW (AWR 1452 R4) LC-6 DIGITALCHRONOMETER, DATED 12 APR 13.

12-Apr-2013 1

CAMP BONDSTEEL

WA754583

DYNCORPINTERNATIONAL DIFZ

COMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-16 (COMPONENT UPDATE). UPDATEDMCDS AND ULLSA-E SYSTEMS WITHCURRENT SPINDLE BEARING INFORMATION.

18-Apr-2013 1

CAMP BONDSTEEL

RS784200


COMPLIED WITH TAIL ROTOR GEARBOXBEVEL GEAR NDI REQUIREMENTS OF H-60-12-ASAM-01. NO DEFECTS FOUND DURINGINSPECTION. COMPLETED @ 5257.4 ACFTHOURS DURING PMI-2 INSPECTIONS

24-Apr-2013 1

CAMP BONDSTEEL

RS784200


COMPLIED WITH REQUIREMENTS OF GEN-13-AMAM-02 CMWS COMPONENT UPDATE.UPDATED ULLSA-E & MCDS DATABASESCURRENT INFORMATION.

30-Apr-2013 1

CAMP BONDSTEEL

RS784200


PERFORMED COMPLETE TAIL ROTORRIGGING PROCEDURES IAW H-60-13-AMAM-01.BLADE ANGLE MEASUREMENTS:RED:BLADE SET-0.0; 1ST-3.0; 2ND-3.0; FINAL-3.1BLACK: BLADE SET-0.0; 1ST-3.0; 2ND-3.0;FINAL-3.1YELLOW: BLADE SET- 0.0; 1ST-3.0;2ND-3.0; FINAL-3.0BLUE: BLADE SET- 0.0; 1ST-3.0; 2ND-3.0; FINAL-3.0DIMENSIONALCHECK:RED: DIM A= 4.833; DIM B= 5.144;DIFF= 0.311BLACK: DIM A= 4.123; DIM B=4.420; DIFF= 0.297YELLOW: DIM A= 4.806; DIMB= 5.100; DIFF= 0.294BLUE: DIM A= 4.033; DIMB= 4.362; DIFF= 0.329SERVO OUT= 3.51; IN=.018CABLE TENSION: L/H= 155LBS; R/H=155LBS; TEMP 22'C

02-May-2013 1

CAMP BONDSTEEL

RS784200



8.7.DATE

6.REMARKS

4. 5.




COMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-01 ( NEW FLIGHT CONTROL RIGGINGPROCEDURES) @ 5257.4 ACFT HOURS AFTERCOMPLETION OF PMI-2 INSPECTIONS.

02-May-2013 2

CAMP BONDSTEEL

RS784200


COMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-06 (INBOARD RETENTION PLATETORQUE CHECK) @ 5257.4 ACFT HOURSDURING PMI-2 INSPECTIONS ON 19-APRIL-2013.

08-May-2013 1

CAMP BONDSTEEL

RS784200


COMPLETED PMI-2 INSPECTIONS @ 5257.4ACFT HOURS. NEXT PMI DUE @ 5617.4 ACFTHOURS.

16-May-2013 1

CAMP BONDSTEEL

RS784200

KFOR-17H-60-13-SOF-01 ATTITUED HEADINGREFERENCE SET INSPECTION COMPLIEDWITH

01-Jun-2013 1

CAMP BONDSTEEL

JH780400

DET 2 B CO 638TH ASB H-60-13-AMAM-11 MAIN TRANSMISSIONFILTER BOWL HARDWARE COMPLIED WITH

03-Jul-2013 1

CAMP BONDSTEEL

DJ071045

DET 2 CO B 638TH ASBCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-10 (LCF CHANGE 64 REQUIREMENTS)

03-Aug-2013 1

CAMP BONDSTEEL

JK567294

DET 2 CO B 638TH ASBCOMPLIED WITH REQUIREMENTS OF GEN-13-AMAM-04 (APN-209 RADAR ALTIMETERCOMPONENT TRACKING)

08-Aug-2013 1

CAMP BONDSTEEL

JK567294

DET 2 CO B 638TH ASBCOMPLETED MAIN ROTOR RIG @ 5315.6 ACFTHOURS. LCA= 90RT: 8.4, 180FWD: -3.0, 270LFT:-9.5AFT: 2.1, TOTAL: 2.0, AVG: -0.5. HCA=90RT: 19.4, 180FWD: 10.4, 270LFT: 10.8, 0AFT:19.8, TOTAL: 60.4, AVG: 15.1. FCA= 90RT: -2.4,270LFT: 31.1, TOTAL: 33.5. ACA= 90RT: 25.3,270LFT: 4.3, TOTAL: 21.0. LCA= 180FWD:8.4,0AFT: 7.4 . RCA= 180FWD: 7, 0AFT: 7.5, TOTAL:14.5. LENGTHENED LAT PRIMARY CONT ROD1/2 TURN.

23-Aug-2013 1

CAMP BONDSTEEL

JK567294

DET 2 CO B 638TH ASBPERFORMED REPAIR AT BOTH AFT LOWERCORNERS OF CREW WINDOW AREA; APPROXFS295L WL 235, AND FS295R WL235 USING.063" 7075T6 ALUMINUM. RMVD ORIGINALMETAL AND REPLACED WITH A 4" X 4 "SHEET AT THE LOWER WINDOW FRAME ANDDOUBLED WITH A 6" X 9" T-SHAPED PIECEFROM THE WINDOW FRAME TO THE FS295BEAM. REPAIRS PERFORMED IAW TM 1-1500-204-23-10 AND TM 1-1520-237-23 @ 5315.6ACFT HRS.

23-Aug-2013 2

CAMP BONDSTEEL

JK567294

DET 2 CO B 638TH ASBCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-15 (CEFS RIGHT HAND FUEL CELLCOVER PLATE) ACFT NOT EQUIPPED WITHCEFS.

27-Sep-2013 1

CAMP BONDSTEEL

JK567294

DET 2 CO B 638TH ASBCOMPLIED WITH REQUIREMENTS OF H-60-14-SOF-01. (BREEZE EXTERNAL HOIST)AIRCRAFT NOT EQUIPPED WITH EXTERNALHOIST.

03-Nov-2013 1

CAMP BONDSTEEL

JK567294

B CO 638TH ASBCOMPLIED WITH REQUIREMENTS OF H-60-ASAM-02 (IVHUMS) N/A, IVHUMS NOTINSTALLED

22-Nov-2013 1

CAMP BONDSTEEL

KB629574



8.7.DATE

6.REMARKS

4. 5.



DET 2 CO B 638TH ASBCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-03. (DISCREPANT CONNECTING LINKS)

24-Dec-2013 1

CAMP BONDSTEEL

JK567294

DET 2 CO B 638TH ASBCOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-03. (EIBF MOUNT BRACKETS)

31-Dec-2013 1

CAMP BONDSTEEL

JK567294

DET 2 CO B 638TH ASBCOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-04. ( M/R HUB ASSY)

31-Dec-2013 2

CAMP BONDSTEEL

JK567294

W3VA7JCOMPLIED WITH REQUIREMENTS OF H-60-14-SOF-02, T/R PITCH CHANGE SHAFT ASSYCOTTER PIN. PASSED

27-Jan-2014 1

CAMP BONDSTEEL

JA179325

2-211 GSABAIRWORTHINESS RELEASE FOR H-60HELICOPTERS EQUIPPED WITH PATIENTMOVEMENT ITEMS AWR 1330 R29 24 JAN 14

30-Jan-2014 1

CAMP BONDSTEEL

SM746962

2-211 GSABCOMPLI ED WITH REQUIREMENTS OF AGSE-14-ASAM-01, DAWS SCALES PN ULP400-000001-1 NOT USED ON ACFT

27-Feb-2014 1

CAMP BONDSTEEL

SM746962

2-211 GSABCOMPLIED WITH H-60-14-AMAM-08, N/A TOTHIS ACFT (CIRUICT BREAKER PROTECTION)

10-Mar-2014 1

CAMP BONDSTEEL

SM746962

2-211 GSABAWR 1648 R3 DATED 28 MAR 14 (NCSMAGNUS MODEL RNM101 LAPTOP ONBOARDAND OPERATING)

21-Mar-2014 1

CAMP BONDSTEEL

SM746962

B CO 2/211 GASBCOMPLIED WITH H-60-14-AMAM-10, HONTEKCOATED MAIN ROTOR BLADES N/A TO THISAIRCRAFT

08-Apr-2014 1

CAMP BONDSTEEL

SM746962


COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-10 ( HONTEK COATED BLADES ). NOPN 70150-09100-047 BLADES INSTALLED ONTHIS ACFT.

08-Apr-2014 2

CAMP BONDSTEEL

RS784200

B CO 2/211 GASBCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-05 (LCF 65 CHANGE REQUIREMENT)

10-Apr-2014 1

CAMP BONDSTEEL

SM746962


COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-09 (MAIN TRANSMISSIONATTACHMENT HARDWARE) @ 5534.9 ACFTHOURS. REPLACED ALL RELATEDHARDWARE.

15-Apr-2014 1

CAMP BONDSTEEL

RS784200


COMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-06 (FLIGHT CONTROL MIXER) @ 5534.9ACFT HOURS. FABRICATED AND INSTALLEDDATA PLATE ON MIXER ASSEMBLY WITHENGRAVED SN & PN INFORMATION. LUBEDMIXER IAW SUPPLEMENT TO H-60-14-ASAM-06WP1715 OF TM 1-1520-237-23-12..

19-Apr-2014 1

CAMP BONDSTEEL

RS784200



8.7.DATE

6.REMARKS

4. 5.




AFTER REPLACEMENT OF MAINTRANSMISSION COMPLETED MAIN ROTORRIG CHECK IAW ADDENDUM 1 OF H-60-13-AMAM-01 @ 5534.9 ACFT HOURS. LCA: 90*RT=08.2; 180*FWD= -1.0; 270*LFT= -9.0; 0*AFT= 0.2;TOTAL= -1.7; AVG= -0.425.HCA: 90*RT= 20.4;180*FWD= 12.0; 270*LFT= -42.4; 0*AFT= 18.4;TOTAL= 60.8; AVG= 15.2. FCA: 90*RT= -02.2;270*LFT= 31.6; TOTAL= 33.8. ACA: 90*RT= -25.1; 270*LFT= 05.3; TOTAL= 19.8. LCA:180*FWD= 07.8; 0*AFT= 08.2; TOTAL= 16.0.RCA: 180*FWD= 07.3; 0*AFT= 07.7; TOTAL=15.0.

21-Apr-2014 1

CAMP BONDSTEEL

RS784200

W3VA7GCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-12 (M/R SPINDLE NUT RETIREMENTLIFE EXTENSION)

24-Apr-2014 1

CAMP BONDSTEEL

JA179325

W3VA7GCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-14 (IVHMS CABLING)

28-May-2014 1

CAMP BONDSTEEL

DP508312

B CO 2/211 GSABAWR 1505 R6 EH-60 AND UH-60A/L/MHELICOPTERS FOR AVIATION CENTERLOGISTICS COMMAND, WARFIGHTINGCENTER AND US ARMY AVIATION FLIGHTTEST DIRECTORATE. DOES NOT APPLY TOTHIS AIRCRAFT. DATED 6 JUN 14

06-Jun-2014 1

CAMP BONDSTEEL

SM746962

B CO 2/211 GSABAWR REQUIREMENTS FOR UH-60A/L/MCAVING LADDER INSTALLATION (TN 134846)DATED 29 MAY 14 N/A TO THIS AIRCRAFT

06-Jun-2014 2

CAMP BONDSTEEL

SM746962

B CO 2/211 GASBAWR 1930 H-60 EQUIPPED WITH PATIENTMOVEMENT ITEMS (PMI) 20 MAY 14,REPLACED AWR 1330 R29

06-Jun-2014 3

CAMP BONDSTEEL

SM746962

W3VA7GAIRWORTHINESS RELEASE 1511R3 FORUH/HH-60A/L/M HELICOPTERS TO OPERATEWITH THE CHILD AVIATION RESTRAINTSYSTEM (CARES) INSTALLED IS N/A TO THISAIRCRAFT

07-Jun-2014 1

CAMP BONDSTEEL

JA179325

B CO 2/211 GASBAWR 1515 R3 DATED 2JUN14 UH/HH-60A/LEQUIPED WITH THE TECHNOLOGYRESEARCHCONSULTANTS, INC. CN-1552B/AAND CN-1564CF/A MICRO-ELECTROMECHANICAL SYSTEMS (MEMS) RATEGYROSCOPES, N/A TO THIS AIRCRAFT

11-Jun-2014 1

CAMP BONDSTEEL

SM746962

B CO 2/'211 GASBCOMPLIED WITH REQUIREMENTS OF GEN-MIM-14-004 (AN/APX-123 TRANSPONDER TAMPERREPORTING AND QUADRANT KEYENCRYPTION KEY) N/A TO THIS AIRCRAFT

16-Jun-2014 1

CAMP BONDSTEEL

SM746962

B CO. 2-211TH GSABCOMPLIED WITH REQUIREMENTS OF H-60-14-SOF-03 (DISCREPANT SELF-LOCKINGDOUBLE HEXAGON NUTS). NO DISCREPANTHARDWARE INSTALLED ON ACFT.

02-Jul-2014 1

CAMP BONDSTEEL

DP508312

B CO 2/211 GSABAWR 1372 R4 (FREQUENCY MODULATED (FM)HIGH BAND TFM-138B OR KFM-985 RADIOSINSTALLED) N/A TO THIS ACFT

06-Jul-2014 1

CAMP BONDSTEEL

SM746962



8.7.DATE

6.REMARKS

4. 5.



B CO 2/211TH GSABAWR 1343 R6 1JUL14 (OPERATE WITHMODIFIED APPLICATION OF BLADE EROSIONTAPE IN SUPPORT OF COMBAT OPERATIONS)N/A TO THIS AIRCRAFT

07-Jul-2014 1

CAMP BONDSTEEL

SM746962

B CO. 2/211TH GSABCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-16 (AHRU 2410 TRACKING) ENTEREDREQUIRED INFORMATION IN ULLSA-(E) ANDMCDS SYSTEMS.

16-Jul-2014 1

CAMP BONDSTEEL

DP508312

B CO 2/211 GSABAWR 1128 R4 15 JUL 14 (PERFORM HIGHALTITUDE-HIGH AMBIENT TEMPERATUREENGINE STARTS IN DESERT COMBATOPERATIONS)

17-Jul-2014 1

CAMP BONDSTEEL

SM746962

B CO 2/211 GSABAWR 1447 R11 18 JUL 14 (OPERATE WITHENVIRO SYSTEMS, IN C. HEATER)

17-Jul-2014 2

CAMP BONDSTEEL

SM746962

B CO 2/211TH GSABAWR 1119 R7 1 AUG 14 (DESERT COMBATOPERATIONS)

03-Aug-2014 1

CAMP BONDSTEEL

SM746962

B CO 2/211TH GSABAWR 1930 R1 31 JUL 14 (PATIENT MOVEMENTITEMS (PMI))

03-Aug-2014 2

CAMP BONDSTEEL

SM746962

B CO 2/211TH GSABAWR 1451 R5 28 JUL 14 (CRASHWORTHYEXTERNAL FUEL TANK SYSTEM (CEFS))

03-Aug-2014 3

CAMP BONDSTEEL

SM746962

B CO 2/211TH GSABAWR 1939 R3 4 AUG 14 (AEROSPACEFILTRATION SYSTEM (AFS) APU INLETBARRIER FILTERS)

05-Aug-2014 1

CAMP BONDSTEEL

SM746962

DYNCORP / DIFZ, LLCREPAIR TO AFT END OF 34.5 CHANNELCOMPLETED IAW MEC #F186801

11-Aug-2014 1

CBS, KOSOVO

BH986618

DYNCORP / DIFZ, LLCREPAIR TO FWD END OF 34.5 CHANNELCOMPLETED IAW MEC #F187303

11-Aug-2014 2

CBS, KOSOVO

BH986618

DYNCORP INTL / DIFZ,LLC

COMPLETED MAIN ROTOR RIG CHECK IAW TM1-1520-237-23&P. LOW COLLECTIVE ANGLEAVG: -.235. HIGH COLLECTIVE ANGLE:15.4.COLLECTIVE RANGE H&L: 15.635

27-Aug-2014 1

CBS, KOSOVO

BH986618

DYNCORP INTL / DIFZ,LLC

T/R, RIG COMPLETED. T/R BIAS RED: 3.1,YEL:3.0, BLK: 3.0, BLU: 3.0. PISTON OUT: 3.49,PITSTON IN: .035 T/R CABLE TENSION L/H=150LBS, R/H=150 LBS @ 26C DEGREES

27-Aug-2014 2

CBS, KOSOVO

BH986618

B CO 248TH ASBCOMPLIED WITH H-60-14-ASAM-10 (MAINTRANSMISSION PLANETARY CARRIERASSEMBLY)

02-Sep-2014 1

CAMP BONDSTEEL

DS651795

B CO 248TH ASBCOMPLIED WITH H-60-14-SOF-04 (OPERATORSAND CREMEMBERS CHECKLIST PAGE E-17 &E-18 OMISSION)

03-Sep-2014 1

CAMP BONDSTEEL

DP508312

B CO 2/211 GSABCOMPLIED WITH REQUIREMENT OF GEN-12-AMAM-07 (UPDATED FIRST AID KITMODERNIZATION)

03-Sep-2014 2

CAMP BONDSTEEL

SM746962

KFOR 19EFFECTIVE THIS DATE H-60-15-AMAM-02 WASCOMPLIED WITH @5893.4 (IVHMS WIRING)

21-Oct-2014 1

CAMP BONDSTEEL

MB694481

KFOR 19EFFECTIVE THIS DATE H-60-15-AMAM-02 WASCOMPLIED WITH @5666.0 (IVHMS WIRING)(ADMENDED A/C HOUR AT SIGNOFF 5893.4 INERROR)

21-Oct-2014 2

CAMP BONDSTEEL

MB694481



8.7.DATE

6.REMARKS

4. 5.



D CO 1-150 GSABEFFECTIVE THIS DATE H-60-15-SOF-01 WASCOMPLETED AT 5668.0 ACFT HOURS (OILCOOLER BNG TBO/IVHMS)

29-Oct-2014 1

CAMP BONDSTEELKOSOVO

MB694481

AASF#1 NJARNGCOMPLIED WITH THE REQUIREMENTS OF H-60-15-AMAM-05 (AHRS EMERGENCYPROCEDURE)

20-Feb-2015 1

LAKEHURST, NJ

SD626046

AASF#1 NJARNGCOMPLIED WITH THE REQUIREMENTS OF H-60-15-ASAM-01 (LED CAUTION ADVISORYPANEL)

20-Feb-2015 2

LAKEHURST, NJ

SD626046

AASF#1 NJARNGCOMPLIED WITH THE REQUIREMENTS OF H-60-14-AMAM-19 (ULLSA(E) CHANGE 66)

20-Feb-2015 3

LAKEHURST, NJ

WH764732

AASF#1COMPLIED WITH H-60-15-AMAM-06(IDENTIFICATION OF ASE)

04-Mar-2015 1

LAKEHURST, NJ

CA629236

AASF #1COMPLIED WITH H-60-15-ASAM-03(TROOP/GUNNER SEAT ENERGYATTENUATORS).

16-Apr-2015 1

LAKEHURST, NJ

CA629236

AASF#1 NJARNGCOMPLIED WITH THE REQUIREMENTS OF H-60-15-AMAM-10 (AV-DEC GASKET INSPECTION)

20-May-2015 1

LAKEHURST, NJ

MF827912

AASF#1COMPLIED WITYH REQUIREMENTS OF H-60-15-AMAM-11 MODE-S TRANSPONDER ADDRESSREVIEW(53405351)MODE 5 PIN;06563MODE S,N.O 0034

23-Jun-2015 1

LAKEHURST, NJ

CA629236

AASF#1 NJARNGCOMPLIED WITH THE REQUIREMENTS OF H-60-15-AMAM-14 (AMCOM CHANGE 67REQUIREMENTS)

24-Jul-2015 1

LAKEHURST, NJ 08733

DM649028

L-3ACE COMPLETED AT 5732.7 A/C HRS. BY ACETEAM MEMBERS B/G. AFMA, RASME, AMCOM.

05-Aug-2015 1

LAKEHURST, NJ

JG389608

AASF#1 NJARNGPMI I PHASE INSPECTION COMPLETED @4917.3 AIRRAFT HOURS, PMI II DUE @ 5277.3AIRCRAFT HOURS.

05-Aug-2015 2

LAKEHURST, NJ

SD626046

AASF#1 NJARNGCOMPLIED WITH THE REQUIREMENTS OF H-60-15-SOF-02 (FRIES RELEASE CABLE)

25-Sep-2015 1

LAKEHURST, NJ

SD626046

AASF #1 NJARNGRBL34.5 CHANNEL HAS MISLOCATEDDRILLED HOLES FOR THE UPPER HOISTBRACKET NUTPLATE. AS PER AMCOM LARJOE PECA, AREA WAS CLEANED UP ANDSCHEDULED FOR CONDITION II CHANNELREPAIR AT PMI DUE AT 5975.7 ACFT HOURS.DETAILS OF CLEANUP FILED IN ACFTHISTORICAL BINDER.

01-Oct-2015 1

LAKEHURST, NJ

SZ628863

AASF#1 NJARNGCOMPLIED WITH THE REQUIREMENTS OF H-60-16-AMAM-01 (EIBF FRAMES)

28-Oct-2015 1

LAKEHURST, NJ

SD626046

AASF#1 NJARNGCOMPLIED WITH THE REQUIREMENTS OF H-60-16-AMAM-18 (MEDEVAC CAROUSEL)

29-Oct-2015 1

LAKEHURST, NJ

SD626046

AASF #1 NJARNGCOMPLIED WITH THE REQUIREMENTS OF H-60-16-ASAM-01 (INBOARD RETENTION PLATETORQUE CHECKS)

17-Nov-2015 1

LAKEHURST, NJ

SZ628863

AASF #1 NJARNGCOMPLIED WITH THE REQUIREMENTS OF H-60-16-AMAM-03 (PLS REMOVAL)

24-Nov-2015 1

LAKEHURST, NJ

MS847316



8.7.DATE

6.REMARKS

4. 5.



AASF #1 NJARNGCOMPLIED WITH THE REQUIREMENTS OF H-60-16-AMAM-04, T-CLIP INSTALLATION. N/A THISAIRCRAFT.

06-Jan-2016 1

LAKEHURST, NJ

SZ628863

AASF#1 NJARNGCOMPLIED WITH THE REQUIREMENTS OF H-60-16-ASAM-02 (DEFECTIVE FUEL HOSES)

09-Jan-2016 1

LAKEHURST, NJ

MS847316

AASF #1COMPLIED WITH THE REQUIREMENTS OF H-60-15-ASAM-07 MAIN ROTOR BLADEDEBONDING AND TIP RIB CRACKING

23-May-2016 1

LAKEHURST, NJ

KM583898

AASF #1COMPLIED WITH THE REQUIREMENTS OF H-60-16-AMAM-09, ULLS-A (E) COMPONENTSDUPLICATION

14-Jun-2016 1

LAKEHURST, NJ

KM583898

L-3ACE COMPLETED AT 5792.7 A/C HRS. BY ACETEAM MEMBER G. AFMA, RASME, AMCOM.

22-Jun-2016 1

LAKEHURST, NJ

JG389608

AASF #1COMPLIED IAW H-60-16-SOF-01, UPPER CABINFRAME CRACKING

23-Jun-2016 1

LAKEHURST, NJ

KM583898

AASF #1COMPLIED WITH THE REQUIREMENTS OF H-60-16-AMAM-09, COMPONENT PN/SNDUPLICATIONS

11-Jul-2016 1

LAKEHURST, NJ

KM583898

AASF #1COMPLIED WITH THE REQUIREMENTS OF H-60-16-AMAM-10 PHASE LCF UPDATES

01-Aug-2016 1

LAKEHURST, NJ

KM583898

AASF #1AIRCRAFT TRANSFER TO BEST PROGRAMON, 22 AUGUST, 2016, FOR ARMY / BESTPROGRAM BY: A CO 1/150TH, LAKEHURST NJ,AT (5792.7) TOTAL AIRCRAFT HOURS, DATAPLATE REMAINED INSTALLED.

03-Aug-2016 1

LAKEHURST, NJ

KM583898

AASF#1 NJARNGCOMPLIED WITH THE REQUIREMENTS OF H-60-16-SOF-02 (RESCUE HOIST OPERATIONALRESTRICTIONS)

15-Aug-2016 1

LAKEHURST, NJ

KS684039

SCIENCE ANDENGINEERINGSERVICES

H-60-16-AMAM-07, TAIL ROTOR SERVOSAFETY CABLE NOT COMPLIED WITH

15-Sep-2016 1

HUNTSVILLE

CB902364

SCIENCE ANDENGINEERINGSERVICES

H-60-16-ASAM-06, IMPROVED TAIL ROTORQUADRANT SUPPORT NOT COMPLIED WITH

15-Sep-2016 2

HUNTSVILLE

CB902364


DATE AC HRS SHAFT VERTICAL REASON FOR VIB CHECKLONGITUDINALLATERAL

IPS READINGS4.

7923340HELICOPTER, UTILITYUH-60A3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Report Date: 16-Sep-2016 1/5

100 HR INSP21-Jun-2002 #1ENG 0.18002340

100 HR INSP21-Jun-2002 #2ENG 0.2002340

100 HR INSP21-Jun-2002 OIL COOLER 0.150.3202340

COMPLETION OF PHASE INSP17-Feb-2004 #1ENG 0.41002733.2

COMPLETION OF PHASE INSP17-Feb-2004 #2ENG 0.48002733.2

COMPLETION OF PHASE INSP17-Feb-2004 OIL COOLER 0.130.1502733.2

COMPLETION OF PHASE INSP17-Feb-2004 TAIL ROTOR 0.1002733.2

100 HR INSP12-Aug-2004 #1ENG 0.31002831.4

100 HR INSP12-Aug-2004 #2ENG 0.4002831.4

100 HR INSP12-Aug-2004 OIL COOLER 0.120.2502831.4

100 HR INSP12-Aug-2004 TAIL ROTOR 0.08002831.4

100 HR INSP10-Feb-2005 #1 ENGINE 0.29002924.2

100 HR INSP10-Feb-2005 #2 ENGINE 0.37002924.2

100 HR INSP10-Feb-2005 OIL COOLER 0.180.2802924.2

100 HR INSP10-Feb-2005 TAIL ROTOR 0.02002924.2

ENG INSTALL24-May-2005 #1ENG 0.32002934.9

ENGINE REINSTALLATION02-Jun-2005 #1ENG 0.14002936.4

120 HR INSP02-Sep-2005 #1 ENG 0.37003047.8

120 HR INSP02-Sep-2005 #2 ENG 0.36003047.8

120 HR INSP02-Sep-2005 TAIL ROTOR 0.02003047.8

120 HR INSP02-Sep-2005 OIL COOLER 0.160.3503047.8

R&R T/R BLADES FOR TQ CKS04-Jun-2006 TAIL ROTOR 0.039003094.6

UNFOLDINH T/R BLADES FOR SHIPMENT27-Aug-2006 T/R 00.1803116.2

UNFOLDING OF T/R BLADES FROM SHIPMENT27-Aug-2006 T/R 00.0304232.8

120 HOUR10-Oct-2006 #1 ENG 0.363003193

120 HOUR10-Oct-2006 #2 ENG 0.44003193

120 HOUR10-Oct-2006 OIL COOLER 0.1270.1603193

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

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


IPS READINGS4.



120 HOUR10-Oct-2006 TAIL 0.02003193

T/R DEICE BRACKET REPLACED30-Nov-2006 T/R 0.04003301.6

120 HOUR01-Dec-2006 #1 ENG 0.01003311.8

120 HOUR01-Dec-2006 #2 ENG 0.03003311.8

120 HOUR01-Dec-2006 OIL COOLER 0.130.3503311.8

120 HOUR01-Dec-2006 TAIL 0.04003311.8

POST PMI29-Jan-2007 #1 ENG 0.24003410.1

POST PMI29-Jan-2007 #2 ENG 0.33003410.1

POST PMI29-Jan-2007 T/R 0.07003410.1

POST PMI29-Jan-2007 OIL COOLER 00.1203410.1

T/R INBOARD RETENTION PLATE RETORQUE02-Feb-2007 T/R 0.1003419.2

120 HOUR02-Apr-2007 TAIL ROTOR 0.03003530.6

120 HOUR02-Apr-2007 OIL COOLER 00.1903530.6

120 HOUR02-Apr-2007 # 1 ENG 0.29003530.6

120 HOUR02-Apr-2007 # 2 ENG 0.42003530.6

?14-May-2007 TAIL ROTOR 0.04003647.3

REPLACEMENT OF RED T/R PADDLE BOOT15-Jun-2007 TAIL ROTOR 0.15003750.5

POST PMI 229-Jun-2007 OIL COOLER 0.060.3603766.8

POST PMI 229-Jun-2007 TAIL ROTOR 0.02003766.8

POST PMI 229-Jun-2007 #2 ENG 0.3003766.8

POST PMI 229-Jun-2007 #1 ENG 0.26003766.8

REMOVAL/REINST OF TAIL ROTOR PADDLES06-Jul-2007 TAIL ROTOR 0.02003776.8

POST RESET28-Jan-2008 #1 ENG 0.05003874.9

POST RESET28-Jan-2008 #2 ENG 0.1003874.9

POST RESET28-Jan-2008 TAIL ROTOR 0.12003874.9

POST RESET28-Jan-2008 OIL COOLER 00.0903874.9

REMOVAL/REINST OF TAIL ROTOR PADDLES12-Feb-2008 TAIL ROTOR 0.11003883.9




IPS READINGS4.



REMOVAL/REINST OF SECT I D/S12-Feb-2008 OIL COOLER 00.2503883.9

120 HOUR13-Aug-2008 #1 ENG 0.2003995.9

120 HOUR13-Aug-2008 #2 ENG 0.04003995.9

120 HOUR13-Aug-2008 OIL COOLER 00.2103995.9

120 HOUR13-Aug-2008 TAIL ROTOR 0.06003995.9

INST OF 5 PACK29-Dec-2008 OIL COOLER 00.404036.7

INST OF 5 PACK29-Dec-2008 TAIL ROTOR 0.09004036.7

INST OF 5 PACK29-Dec-2008 #1 ENG 0.3004036.7

INST OF 5 PACK29-Dec-2008 #2 ENG 0.4004036.7

120 HOURS27-Apr-2009 TAIL ROTOR 0.09004114.4

120 HOURS27-Apr-2009 #1 ENG 0.31004114.4

120 HOURS27-Apr-2009 #2 ENG 0.38004114.4

120 HOURS27-Apr-2009 OIL COOLER 00.2704114.4

ENGINE REPLACEMENT30-Jul-2009 #1 ENG 0.23004164.9

REPLACED DEICE SYS20-Oct-2009 TAIL ROTOR 0.03004207.1

POST PHASE15-Dec-2009 #1 HSS 0.14004216.1

POST PHASE15-Dec-2009 #2 HSS 0.04004216.1

POST PHASE15-Dec-2009 OIL COOLER 00.2504216.1

POST PHASE15-Dec-2009 TAIL ROTOR 0.06004216.1

REMOVAL/REINST OF ENGINE21-Jan-2010 #2 ENG 0.33004221.3

UNFOLDED T/R PADDLES POST A/C SHIPMENT03-Jun-2010 TAIL ROTOR 0.1004250.3

VISCOUS DAMPER REPLACEMENT19-Jul-2010 OIL COOLER 00.2704297.4

120 HR INSP28-Sep-2010 #1 ENG 0.07004336.6

120 HR INSP28-Sep-2010 #2 ENG 0.33004336.6

120 HR INSP28-Sep-2010 OIL COOLER 00.2804336.6


BLACK T/R CABLE REPLACEMENT04-Nov-2010 TAIL ROTOR 0.04004354




IPS READINGS4.



REPLACEMENT OF ENGINE15-Jan-2011 #1 ENG 0.3004402.4

120 HOUR INSPECTION31-Mar-2011 #1 ENG 0.39004455.1

120 HOUR INSPECTION31-Mar-2011 #2 ENG 0.35004455.1

120 HOUR INSPECTION31-Mar-2011 TAIL ROTOR 0.12004455.1

120 HOUR INSPECTION31-Mar-2011 OIL COOLER 0.16004455.1

POST PHASE28-May-2011 #1 ENG 0.23004563.5

POST PHASE28-May-2011 #2 ENG 0.09004563.5

POST PHASE28-May-2011 OIL COOLER 00.4104563.5

POST PHASE28-May-2011 TAIL ROTOR 0.1004563.5

120HR INSP.15-Sep-2011 #1 HSS 0.13004679.8

120HR INSP.15-Sep-2011 #2HSS 0.29004679.8

120HR INSP.15-Sep-2011 OIL COOLER 00.5704679.8

120 HR AND T/R BLADE CHANGED18-Sep-2011 TAIL ROTOR 0.08004681.3

120 HR INSP03-Dec-2011 #1 HSS 0.29004801.3

120 HR INSP03-Dec-2011 #2 HSS 0.16004801.3

120 HR INSP03-Dec-2011 OIL COOLER 00.4404801.3

120 HR INSP03-Dec-2011 TAIL ROTOR 0.08004801.3

48 MO CONTROL ROD INSP20-Jan-2012 TAIL ROTOR 0.07004820.7

PMI #124-Apr-2012 #1 HSS 0.14004917.3

PMI #124-Apr-2012 #2 HSS 0.47004917.3

PMI #124-Apr-2012 OIL COOLER 00.4604917.3

PMI #124-Apr-2012 T/R 0.09004917.3

120 HR INSP21-Sep-2012 #1 HHS 0.09005035.9

120 HR INSP21-Sep-2012 #2 HHS 0.19005035.9

120 HR INSP21-Sep-2012 OIL COOLER 00.2905035.9


REPLACEMENT OF BLUE BOOT02-Dec-2012 TAIL ROTOR 0.07005096.1




IPS READINGS4.



POST PMI ENG REINSTALL30-May-2013 #1 HSS 0.31005261.9

POST PMI / ENGINE REINSTALL30-May-2013 #2 HSS 0.36005261.9

POST PMI30-May-2013 OIL COOLER 00.0705261.9

POST PMI30-May-2013 TAIL ROTOR 0.04005261.9

REPLACEMENT OF MAIN TRANSMISSION.23-Apr-2014 #1 HSS 0.35005536.9

REPLACEMENT OF MAIN TRANSMISSION.23-Apr-2014 #2 HSS 0.34005536.9

REPLACEMENT OF MAIN TRANSMISSION.23-Apr-2014 OIL COOLER 00.3505536.9

POST PMI10-Sep-2014 TAIL ROTOR 0.05005615.7

POST PMI ENGINE REINSTALL10-Sep-2014 #1 HSS 0.22005615.7

POST PMI ENGINE REINSTALL10-Sep-2014 #2 HSS 0.29005615.7

POST PMI10-Sep-2014 OIL COOLER 0.33005615.7

6. Remarks




7923340HELICOPTER, 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 5802.710TM 1-1520-237-PMDPERFORM M/R SPINDLE LUGS,M/R CUFF, TIP CAPSINSPECTION

5792.7H

A022 14 Jun 201614TM 1-1520-237-23-914 DAY FLYABLE STORAGEENGINE RUN UP

31 May 2016D

A092 10 Jul 201630TM 11-6140-203-23&P30 DAY SLAB BATTERYINSPECTION (D8565/11-1)

10 Jun 2016D

A100 12 Sep 201630DA PAM 738-751#1 ENGINE HISTORY RECORDERREADING DUE

13 Aug 2016D

A101 12 Sep 201630DA PAM 738-751#2 ENGINE HISTORY RECORDERREADING DUE

13 Aug 2016D

A103 01 Jul 201630TM 1-1500-344-23AIRCRAFT WASH DUE 01 Jun 2016D

A110 5815.740TM 1-1520-237-PMSPMS 40 HOUR INSPECTION 5775.7H

A115 06 Jul 201630TM 1-1520-237-23-12LUBE REQUIRMENTS 06 Jun 2016D

A115 5832.740TM 1-1520-237-23-12LUBE REQUIRMENTS 5792.7H

A116 6147.6360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

5787.6H

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

23 Apr 2016M

A117 6147.6360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 5787.6H

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

A160 01 Sep 201690TM 1-1520-237-23-1290 DAY CORROSIONINSPECTION

03 Jun 2016D

A177 04 Aug 201690AR 95-190 DAY REVIEW/UPDATE OF 365-4 ENTRIES

06 May 2016D

A210 5855.7120TM 1-1520-237-23-12120 HOUR INSPECTIONREQUIREMENTS

5735.7H

A211 6147.6360H-60-10-AMAM-11APU OIL SAMPLE 5787.6H

A211 28 Apr 201712H-60-10-AMAM-11APU OIL SAMPLE 28 Apr 2016M

A213 5855.7120TM 1-2840-248-23ENGINE COMPRESSORCLEANING

5735.7H

A214 5855.7120TM 1-1520-237-23-12CLEAN TAIL WHEEL ADAPTER 5735.7H

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

18 Mar 2016D

A230 08 Sep 2016120MWO 1-1520-237-50-77INSPECT BATTERYCOMPARTMENT FORCORROSION (SLAB)

11 May 2016D

A288 148350055-2835-209-23/1-2835-209

FUEL NOZZLE ASSEMBLYINSPECTION(GARRETT/HONEYWELL)

983A

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

A289 733250TM 1-2835-209-23ORIFICE FITTING INSPECTION(GARRETT/HONEYWELL)

483A

A290 733250TM 1-2835-209-23IGNITER PLUG ASSYINSPECTION(GARRETT/HONEYWELL)

483A

A291 915.2250TM 1-2835-209-23MAGNETIC DRAIN PLUG ASSYINSPECTION(GARRETT/HONEYWELL)

665.2A

A291 29 Apr 201712TM 1-2835-209-23MAGNETIC DRAIN PLUG ASSYINSPECTION(GARRETT/HONEYWELL)

29 Apr 2016M

A292 915.2250TM 1-2835-209-23DRAIN REFILL LUBRICATING OIL(GARRETT/HONEYWELL)

665.2A

A292 30 Apr 201712TM 1-2835-209-23DRAIN REFILL LUBRICATING OIL(GARRETT/HONEYWELL)

30 Apr 2016M

A293 915.2250TM 1-2835-209-23REMOVE REPLACE OIL FILTERELEMENT(GARRETT/HONEYWELL)

665.2A

A293 29 Apr 201712TM 1-2835-209-23REMOVE REPLACE OIL FILTERELEMENT(GARRETT/HONEYWELL)

29 Apr 2016M

A295 5975.7360TM 1-1520-237-23-12STABILATOR ACTUATOR ASSYLUBE

5615.7H

A296 5975.7360TM 1-1520-237-23-12STABILATOR INSPECTION 5615.7H

A298 6101.8360TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 5741.8H

A298 03 Sep 201612TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 03 Sep 2015M

A299 6147.4360TM 1-1520-237-23-12SWASHPLATE LUBE 5787.4H

A299 19 Apr 201712TM 1-1520-237-23-12SWASHPLATE LUBE 19 Apr 2016M

A320 5981.2360TM 1-2840-248-23ENGINE INSPECTION &CLEANING

5621.2H

A340 6034.9500TM 1-1520-237-23-12REPLACE OIL COOLER VISCOUSDAMPER BRING (NON-VENTED)

5534.9H

A400 6335.7720TM 1-1520-237-PMIPMI-1 5615.7H

A401 5975.7720TM 1-1520-237-PMIPMI-2 5255.7H

A408 5975.7720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-2, AREA 5 AND 6)

5255.7H

A410 6335.7720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-1, AREA 1 THRU 4)

5615.7H

A415 5975.7720H-60-10-AMAM-11MAIN GEARBOX OIL SAMPLE-PART # 073, 074, 076

5255.7H

A440 5975.7720TM 1-1520-237-23-12CLEAN TAIL WHEEL LOCKPIN 5255.7H






7. FREQUENCY 4.




INSP

A466 9941000TM 1-2835-209-23HOT SECTION INSPECTION(GARRETT/HONEYWELL)

-6A

A467 9941000TM 1-2835-209-23FUEL FILLER ELEMENTINSPECTION(GARRETT/HONEYWELL)

-6A

A470 6757.41500TM 1-1520-237-23-12REPLACE NUMBER TWOCROSSFEED VALVE

5257.4H

A471 60452160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

3885H

A472 60452160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

3885H

A473 6457.42160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

4297.4H

A476 7733.45000TM 1-1520-237-23-12REPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

2733.4H

A477 9561.55000TM 1-1520-237-23-12REPLACEMENT OF STABILATORACTUATOR BOLTS

4561.5H

A480 7733.25000TM 1-1520-237-23-12REPLACE PIVOT BOLT 70400-08159-101,102,103,104

2733.2H

A485 7733.25000TM 1-1520-237-23-12REPLACE BELLCRANK BOLT70400-08159-105,106,107,108

2733.2H

A496 19 Oct 20166TM 1-1500-204-23-1CF3BR FIRE EXTINGUISHERWEIGHT TEST & INSPECTION

19 Apr 2016M

A501 19 Oct 20166TM 1-1520-237-23-12MAIN ROTOR BLADE PRESSURECHECK

19 Apr 2016M

A502 18 Oct 20166TM 1-1520-237-23-12INSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

18 Apr 2016M

A530 18 Feb 201712DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

18 Feb 2016M

A532 09 May 201712TM 1-1500-204-23-4COMPASS SWING / RMI 09 May 2016M

A533 29 Apr 201712TM 1-1520-237-23-12PITOT STATIC SYSTEMINSPECTION

29 Apr 2016M

A534 20 Aug 201724TM 1-1500-204-23-1FIRST AID KIT INSPECTION 20 Aug 2015M

A538 31 Jan 201712TM 1-1520-237-23-12FAT/OAT GAUGEINSPECTION/TEST

31 Jan 2016M

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

08 Feb 2016M

A553 01 Oct 201612AR 95-1AIRCRAFT WEIGHINGINVENTORY (365-1)

01 Oct 2015M

A580 20 Oct 201724TM 11-6140-203-23&PRETURN SLAB TO AVIM FORCAPACITY CHECK (VEREY 24MONTH)

20 Oct 2015M

A621 30 Oct 201724AR 95-1AIRCRAFT WEIGHING CLASS 2 30 Oct 2015M






7. FREQUENCY 4.




INSP

A625 11 Oct 201660TM 11-6140-203-23&PREPLACEMENT OF SLABBATTERY (SLAB)

11 Oct 2011M

A630 01 Apr 2021114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Oct 2011M

A633 01 Apr 2021114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Oct 2011M

A638 01 Apr 2021114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

01 Oct 2011M

A640 01 Apr 2021114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

01 Oct 2011M

A648 12 Dec 2022180TM 1-1520-237-23REPLACE T/R SPRING CAPSULEASSY

12 Dec 2007M

A660 01 Dec 201972TB 9-1300-385REPLACE THRUSTEREMERGENCY RELEASE CARGOHOOK, MJ20

01 Dec 2013M

A665 10 Apr 202048H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

10 Apr 2016M

A670 14 Jan 202048TM 1-1520-237-23-1CABIN TUB INSPECTION 14 Jan 2016M

A673 15 Feb 202048TM 1-1520-237-23-12FUEL CELL CORROSIONINSPECTION

15 Feb 2016M

A675 14 Jan 202048TM 1-1520-237-23-12FLIGHT CONTROL ROD INSP 14 Jan 2016M

A695 5975.7720H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

5255.7H

A695 16 Apr 201848H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

16 Apr 2014M

A755 90009000H-60-10-ASAM-11PC LINK TO SWASHPLATEBOLTS REPLACEMENT

0H

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

13 May 2016D

E108 13 Jul 201630TM 11-5810-262-23KY-58 PMCS/OPNL CHECK(STANDBY)

13 Jun 2016D

E135 09 Nov 20166TM 11-5821-333-12AN/ARC-201(V) SINCGARSRADIO HUB BATT REPL

09 May 2016M

E155 12 Nov 2016180TM 11-5810-262-23KY-58 BATTERY REPLACEMENT 16 May 2016D

E300 10 Jul 201630AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

10 Jun 2016D

E300 5912.7120AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

5792.7H

E320 23 Jan 2017360AWR 1516 FOR ELTEMERGENCY LOCATORTRANSMITTER G-SWITCH (EBC-406HM)

29 Jan 2016D






7. FREQUENCY 4.




INSP

E330 24 Feb 20226AWR1346R16UNDER WATER ACOUSTICBEACON BATTERYREPLACEMENT

24 Feb 2016Y

E351 16 Oct 20166TM 11-5895-1841-13PREPLACE APX-118TRANSPONDER BATTERY

16 Apr 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

79233401520010350266 00HELICOPTER, UTILITY

156001095713502C12D

002334070219-05001-042TAIL CONE FITTING CCCC COND COND

162001231183103A01

4503875IA-0133870250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001231183103A01

35063875M001-R-01001570250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001421089003B01

03074BMC115870250-13101-044SHOCK ABSORBER (TAIL) CCCC COND COND

165001285302405A01Z RED

31624373A106-0911070106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z BLUE

04562R106-0427270106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z YELLOW


165001285302405A01Z BLACK


531501537465205A02H BLACK LD

04336B9412539370103-08108-041SOLID BLADE PIN CCCC COND COND

531501537465205A02H BLUE LAG


531501537465205A02H YELLOW LD


531501537465205A02H RED LAG


531501537465205A02H YELLOW LG


531501537465205A02H RED LEAD


531501537465205A02H BLACK LAG


531501537465205A02H BLUE LEAD


161501199764605A03A

03875015152-200370104-08000-050SWASHPLATE ASSY CCCC COND COND

161501078571806A11 #2 POSITION

17322259A2580086370351-08080-043ACCESSORY MODULE CCCC COND COND

161501078571806A11 #1 POSITION

17322259A2580086470351-08080-043ACCESSORY 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

65845535A2650108770351-08100-076MAIN TRANSMISSIONMODULE

CCCC COND COND

161501074121906E 2

20523074A264-0046270351-08001-043INPUT MODULE CCCC COND COND

161501230621806E 1

4862259A2640356370351-08001-046INPUT MODULE CCCC COND COND

168001074515206F

8032259A0050077470357-06300-042INTERMEDIATE GEARBOX CCCC COND COND

161501376508906G01

03875A006-0362470358-06600-046TAIL ROTOR GEARBOXASSY

CCCC COND COND

161501524780506H04 1

03875C845-0373170361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501524780506H04 2

03875C845-0373970361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501081277506H06

22592259A2710017070361-03001-045SHAFT ASSY, T/R DRV SEC1

CCCC COND COND

161501158951706H08

02733WG9499-0010270361-03009-047SHAFT ASSY, T/R DRV SEC2

CCCC COND COND

161501082650006H09 #5 POSITION

22592259A2720050370361-05001-045SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501082650006H09 #4 POSITION


CCCC COND COND

161501082650006H09 #3 POSITION


CCCC COND COND

161501083295306H11

03408D54770361-05002-045SHAFT ASSY, T/R DRV SEC6

CCCC COND COND

161501158578806H12

03074WG10205-00029

70361-06002-047SHAFT ASSY, T/R DRV SEC7

CCCC COND COND

432001207722807A01 BACK UP

22743193251466A53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01 #2

12664777K5165ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01 #1

03296K5579ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

481001102247307B05A 1

05364141813213850-3-1VALVE, SOLENIOD CCCC COND COND

481001102247307B05A #2

04562167293213850-3-1VALVE, SOLENIOD CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






165001222431607B11

045625171A3197170-5ACCUMULATOR CCCC COND COND

168001342049608B20 PILOT

02722067100-601561-000PANEL INDICATOR (PDU) CCCC COND COND

168001342049608B20 COPILOT

02722836100-601561-000PANEL INDICATOR (PDU) CCCC COND COND

611501114969609A01

58847811128B302-8-DMGENERATOR CCCC COND COND

611501114969609A01 #2

0340876-A278370550-02031-111GENERATOR CCCC COND COND

161501260074911C21

05535TMD04643740770400-02300-046MIXER ASSEMBLY CCCC COND COND

168001261204411D25 UPPER

15385685224070400-06641-117STABILATOR ACTUATOR CCCC COND COND

168001261204411D25 LOWER

27665685AV0602DL2155M20STABILATOR ACTUATOR CCCC COND COND

599601547345211D26

0568537521011445-1STABILATOR AMPLIFIER(DUAL)

CCCC COND COND

611001328525815A04

782384978-B06182118806-2-2ENGINE SEQUENCINGUNIT

CCCC COND COND

589501245909019E05A

05310808ASM-C-967292RECEIVER-TRANSMITTERRADAR

CCCC COND COND

584101245909219E05C

053101163FFSM-C-967226INDICATOR HEIGHT CCCC COND COND

660501503528419E06A

0561611012765100-20ATTITUDE HEADINGREFERENCE UNIT

CCCC COND COND

661001490516852A

054283439749825050-1-001AUTOMAT FLT CONTCOMPUTER

CCCC COND COND

SIGNIFICANT HISTORICAL EVENTS7.



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE









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

156001081924402C15J20855

UNK340 2259311470209-06051-043TAIL PYLON FITTING RCRC20000

161501450483405A01A TOP9662

B303-00089 0456270103-08112-047HUB, M/R ROTOR ASSY RCRC5100

161501374720305A01I BLACK6367

32895-343 500376770102-08200-056MAIN ROTOR SPINDLEASSY

RCRC3100

161501442692605A01I RED11657

A00111472 0525770102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501442692605A01I YELLOW11657

A00111903 0525770102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501442692605A01I BLUE10167

B001-00225 0376770102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501074515105A01L17074

1515201944 0307470351-08186-043MAIN ROTOR SHAFTEXTENDER

RCRC14000

161501127738805A01T13000

327-00310 4308430870107-08400-046BIFILAR, M/R ROTORASSY

RCRC13000

161501106190305A0210416

A007-06849 4977579370150-09100-043MAIN ROTOR BLADEASSY

RCRC9600

161501106190305A0213109


RCRC9600

161501106190305A0214345


RCRC9600

161501106190305A0213311


RCRC9600

161501113818805B02 R/Y13171

A009-06636 1509468070101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501113818805B02 BL/BLK13872

A009-08725 335420770101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501083681206G01B13321

R25700229 938225970102-11101-042O/B RETENTION PLATE(T/R)

RCRC12000

414001329342806H237777

988 401525752E15-1FAN AXIAL 012520

156001129125607A24 ROLL17562

B112-03182 7100456270410-02500-049SAS ACTUATOR RCRC13000

156001129125607A24 PITCH17562

B112-09163 2770456270410-02500-049SAS ACTUATOR RCRC13000

156001129125607A24 YAW16885

C112-03463 360388570410-02500-049SAS 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

161501141753211C236035

D233-00159 1994387570400-06100-042TAIL ROTOR PITCHCHANGE SHAFT

012160

165001305695411C2514767

B300--00211 5955376770410-06520-046SERVO ASSY, TAILROTOR

RCRC11000

165001143122611D0128962

B303-03284B 3835456270410-02820-054MAIN ROTOR PRIMARYSERVO

RCRC24400

165001143122611D0128962

B303-11821 1465456270410-02820-054MAIN ROTOR PRIMARYSERVO

RCRC24400

165001143122611D0130016

B30301922 4070561670410-02820-054MAIN ROTOR PRIMARYSERVO

RCRC24400

156001158968511D04 AFT17308

32636-350 4308430870400-08102-045AFT BELLCRANK RCRC13000

156001082921311D0517005

B39100010 5570400-08112-044AFT TIE ROD SUPTFITTING

RCRC17000

168001164416011D066655

MM00155 0445570400-08111-042AFT TIE ROD ASSY RCRC2200

156001286887011D079716

390-02762 0531670400-08117-049AFT BELLCRANK SPTASSY

RCRC4400

304001287243811D0816535

1515204260 0553570400-08151-061LATERAL SWASHPLATELINK

RCRC11000

161501158965811D098233

A28900459 630273370400-08150-045LATERAL SERVOBELLCRANK

RCRC5500

168001158965311D1111005

C346-00715 5570400-08104-048AFT WALKING BEAM RCRC11000

156001289269711D1318917

34402342 0491770400-08115-046LEFT TIE ROD RCRC14000

156001296948611D149035

288-00634 0553570400-08114-051RIGHT TIE ROD ASSY RCRC3500

168001090204811D1517733

D355-00122 2707273370400-08101-044FORWARD BELLCRANK RCRC15000

156001221261911D16 UH60A-3409010

B367-04212 0341070400-08162-042FWD BELLCRANK SPTASSY

RCRC5600

156001095713211D1720000

10695 0070219-02134-046SERVO BEAM FITTING RCRC20000













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 7923340 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 8 of 12

16-Sep-2016

COND COND

156001095713502C12D

00TAIL CONE FITTING 2334070219-05001-042 CCCC

20000 20855

156001081924402C15J

22593114TAIL PYLON FITTING UNK34070209-06051-043 RCRC

COND COND

162001231183103A01

4503875FWD FIXED GEARSHOCK

IA-0133870250-12051-045 CCCC

COND COND

162001231183103A01


M001-R-01001570250-12051-045 CCCC

COND COND

162001421089003B01

03074SHOCK ABSORBER(TAIL)

BMC115870250-13101-044 CCCC

5100 9662

1615014504834 TOP05A01A

04562HUB, M/R ROTOR ASSY B303-0008970103-08112-047 RCRC

3100 6367

1615013747203 BLACK05A01I

5003767MAIN ROTOR SPINDLEASSY

32895-34370102-08200-056 RCRC

6400 11657

1615014426926 RED05A01I


A0011147270102-08200-069 RCRC

6400 11657

1615014426926 YELLOW05A01I


A0011190370102-08200-069 RCRC

6400 10167

1615014426926 BLUE05A01I


B001-0022570102-08200-069 RCRC

14000 17074

161501074515105A01L

03074MAIN ROTOR SHAFTEXTENDER

151520194470351-08186-043 RCRC

13000 13000

161501127738805A01T

43084308BIFILAR, M/R ROTORASSY

327-0031070107-08400-046 RCRC

COND COND

1650012853024 RED05A01Z

31624373DAMPER ASSY, M/R A106-0911070106-08100-046 CCCC

COND COND

1650012853024 BLUE05A01Z

04562DAMPER ASSY, M/R R106-0427270106-08100-046 CCCC

COND COND

1650012853024 YELLOW05A01Z


COND COND

1650012853024 BLACK05A01Z


9600 10416

161501106190305A02

49775793MAIN ROTOR BLADEASSY

A007-0684970150-09100-043 RCRC

9600 13109

161501106190305A02


A007-1224570150-09100-043 RCRC

9600 14345

161501106190305A02


A007-1242370150-09100-043 RCRC

9600 13311

161501106190305A02


A007-1484470150-09100-043 RCRC

COND COND

5315015374652 BLACK LD05A02H

04336SOLID BLADE PIN B9412539370103-08108-041 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

5315015374652 BLUE LAG05A02H


COND COND

5315015374652 YELLOW LD05A02H


COND COND

5315015374652 RED LAG05A02H


COND COND

5315015374652 YELLOW LG05A02H


COND COND

5315015374652 RED LEAD05A02H


COND COND

5315015374652 BLACK LAG05A02H


COND COND

5315015374652 BLUE LEAD05A02H


COND COND

161501199764605A03A

03875SWASHPLATE ASSY 015152-200370104-08000-050 CCCC

10000 13171

1615011138188 R/Y05B02

15094680TAIL ROTOR BLADEASSY

A009-0663670101-31000-043 RCRC

10000 13872

1615011138188 BL/BLK05B02

3354207TAIL ROTOR BLADEASSY

A009-0872570101-31000-043 RCRC

COND COND

1615010785718 #2 POSITION06A11

17322259ACCESSORY MODULE A2580086370351-08080-043 CCCC

COND COND

1615010785718 #1 POSITION06A11

17322259ACCESSORY MODULE A2580086470351-08080-043 CCCC

COND COND

161501503311506A

65845535MAIN TRANSMISSIONMODULE

A2650108770351-08100-076 CCCC

COND COND

1615010741219 206E

20523074INPUT MODULE A264-0046270351-08001-043 CCCC

COND COND

1615012306218 106E

4862259INPUT MODULE A2640356370351-08001-046 CCCC

COND COND

168001074515206F

8032259INTERMEDIATEGEARBOX

A0050077470357-06300-042 CCCC

COND COND

161501376508906G01

03875TAIL ROTOR GEARBOXASSY

A006-0362470358-06600-046 CCCC

12000 13321

161501083681206G01B

9382259O/B RETENTION PLATE(T/R)

R2570022970102-11101-042 RCRC

COND COND

1615015247805 106H04

03875DRIVESHAFT ASSYENGINE

C845-0373170361-08014-041 CCCC

COND COND

1615015247805 206H04

03875DRIVESHAFT ASSYENGINE

C845-0373970361-08014-041 CCCC

COND COND

161501081277506H06

22592259SHAFT ASSY, T/R DRVSEC 1

A2710017070361-03001-045 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 10 of 12

16-Sep-2016

COND COND

161501158951706H08


WG9499-0010270361-03009-047 CCCC

COND COND

1615010826500 #5 POSITION06H09

22592259SHAFT ASSY, T/R SEC3,4,5

A2720050370361-05001-045 CCCC

COND COND

1615010826500 #4 POSITION06H09


A2720050470361-05001-045 CCCC

COND COND

1615010826500 #3 POSITION06H09


A2720050570361-05001-045 CCCC

COND COND

161501083295306H11


D54770361-05002-045 CCCC

COND COND

161501158578806H12


WG10205-0002970361-06002-047 CCCC

2520 7777

414001329342806H23

4015257FAN AXIAL 98852E15-1 01

COND COND

4320012077228 BACK UP07A01

22743193PUMP MODULE ASSY,HYDRAUL

251466A53023-06 CCCC

COND COND

4320012077228 #207A01


K5165ABR53023-06 CCCC

COND COND

4320012077228 #107A01


K5579ABR53023-06 CCCC

13000 104621560011291256 ROLL07A24

71004562SAS ACTUATOR B112-0318270410-02500-049 RCRC

13000 147921560011291256 PITCH07A24

27704562SAS ACTUATOR B112-0916370410-02500-049 RCRC

13000 165251560011291256 YAW07A24

3603885SAS ACTUATOR C112-0346370410-02500-049 RCRC

COND COND

4810011022473 107B05A

05364VALVE, SOLENIOD 141813213850-3-1 CCCC

COND COND

4810011022473 #207B05A

04562VALVE, SOLENIOD 167293213850-3-1 CCCC

COND COND

165001222431607B11

04562ACCUMULATOR 5171A3197170-5 CCCC

COND COND

1680013420496 PILOT08B20

02722PANEL INDICATOR (PDU) 067100-601561-000 CCCC

COND COND

1680013420496 COPILOT08B20

02722PANEL INDICATOR (PDU) 836100-601561-000 CCCC

COND COND

611501114969609A01

5884781GENERATOR 1128B302-8-DM CCCC

COND COND

6115011149696 #209A01

03408GENERATOR 76-A278370550-02031-111 CCCC

COND COND

161501260074911C21

05535MIXER ASSEMBLY TMD04643740770400-02300-046 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 11 of 12

16-Sep-2016

2160 6035

161501141753211C23

19943875TAIL ROTOR PITCHCHANGE SHAFT

D233-0015970400-06100-042 01

11000 8812165001305695411C25

59553767SERVO ASSY, TAILROTOR

B300--0021170410-06520-046 RCRC

24400 25127165001143122611D01

38354562MAIN ROTOR PRIMARYSERVO

B303-03284B70410-02820-054 RCRC

24400 27497165001143122611D01


B303-1182170410-02820-054 RCRC

24400 25946165001143122611D01


B3030192270410-02820-054 RCRC

13000 130001560011589685 AFT11D04

43084308AFT BELLCRANK 32636-35070400-08102-045 RCRC

17000 17000156001082921311D05

55AFT TIE ROD SUPTFITTING

B3910001070400-08112-044 RCRC

2200 6655

168001164416011D06

04455AFT TIE ROD ASSY MM0015570400-08111-042 RCRC

4400 9716

156001286887011D07

05316AFT BELLCRANK SPTASSY

390-0276270400-08117-049 RCRC

11000 16535

304001287243811D08

05535LATERAL SWASHPLATELINK

151520426070400-08151-061 RCRC

5500 7603161501158965811D09

6302733LATERAL SERVOBELLCRANK

A2890045970400-08150-045 RCRC

11000 11000168001158965311D11

55AFT WALKING BEAM C346-0071570400-08104-048 RCRC

14000 18917

156001289269711D13

04917LEFT TIE ROD 3440234270400-08115-046 RCRC

3500 9035

156001296948611D14

05535RIGHT TIE ROD ASSY 288-0063470400-08114-051 RCRC

15000 15026168001090204811D15

27072733FORWARD BELLCRANK D355-0012270400-08101-044 RCRC

5600 9010

1560012212619 UH60A-34011D16

03410FWD BELLCRANK SPTASSY

B367-0421270400-08162-042 RCRC

20000 20000

156001095713211D17

00SERVO BEAM FITTING 1069570219-02134-046 RCRC

COND COND

1680012612044 UPPER11D25

15385685STABILATOR ACTUATOR 224070400-06641-117 CCCC

COND COND

1680012612044 LOWER11D25

27665685STABILATOR ACTUATOR AV0602DL2155M20 CCCC

COND COND

599601547345211D26

05685STABILATOR AMPLIFIER(DUAL)

37521011445-1 CCCC

COND COND

611001328525815A04

7823849ENGINE SEQUENCINGUNIT

78-B06182118806-2-2 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 12 of 12

16-Sep-2016

COND COND

589501245909019E05A

05310RECEIVER-TRANSMITTER RADAR

808ASM-C-967292 CCCC

COND COND

584101245909219E05C

05310INDICATOR HEIGHT 1163FFSM-C-967226 CCCC

COND COND

660501503528419E06A

05616ATTITUDE HEADINGREFERENCE UNIT

11012765100-20 CCCC

COND COND

661001490516852A

05428AUTOMAT FLT CONTCOMPUTER

3439749825050-1-001 CCCC

7. SIGNIFICANT HISTORICAL DATA




HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 IA-01338 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

16-Sep-2016

9000 12425

165001125090703A01A

00PISTON, MAIN L/GEARSTR

IA0719970250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 IA-01338 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

16-Sep-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 M001-R-010015 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

16-Sep-2016

9000 9369

165001125090703A01A

28342834PISTON, MAIN L/GEARSTR

023870250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 M001-R-010015 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

16-Sep-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615013747203MAIN ROTORSPINDLE ASSY

70102-08200-056 32895-343 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

16-Sep-2016

COND COND

3110011589607 BLACK05A01I02C

6951990THRUST BEARING B326-28630SB7002-048 CCCC

COND COND

1615011614373 BLACK05A01I02

6951990ELASTOMERIC BEARING B324-20290SB7001-048 CCCC

13000 15760

5310011269444 BLACK05A01I04

1007500M/R SPINDLE NUT D479-0169370102-08105-102 RCRC

3100 6867

1560012207228 BLACK05A01I06

0500TIE ROD (M/R SPINDLE) C504-1021570102-08102-102 RCRC

20000 21210

1615012149140 BLACK05A01I07

2557500HORN ASSEMBLY A241-0245370102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-056 32895-343 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

16-Sep-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 A00111472 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

16-Sep-2016

COND COND

3110011589607 RED05A01I02C


COND COND

1615011614373 RED05A01I02


13000 18257

5310011269444 RED05A01I04

00M/R SPINDLE NUT F479-0878570102-08105-102 RCRC

6400 11657

5306014606020 RED05A01I06


20000 25257

1615012149140 RED05A01I07

00HORN ASSEMBLY H241-0143070102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

16-Sep-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

16-Sep-2016

COND COND

3110011589607 YELLOW05A01I02C


COND COND

1615011614373 YELLOW05A01I02


13000 18257

5310011269444 YELLOW05A01I04

00M/R SPINDLE NUT F479-0968870102-08105-102 RCRC

6400 11657

5306014606020 YELLOW05A01I06


20000 25257

1615012149140 YELLOW05A01I07

00HORN ASSEMBLY G241-0390470102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

16-Sep-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 B001-00225 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

16-Sep-2016

COND COND

3110011589607 BLUE05A01I02C


COND COND

1615011614373 BLUE05A01I02


13000 16767

5310011269444 BLUE05A01I04

00M/R SPINDLE NUT C479-1280170102-08105-102 RCRC

6400 10167

5306014606020 BLUE05A01I06


20000 23767

1615012149140 BLUE05A01I07

00HORN ASSEMBLY A241-1649270102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 B001-00225 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

16-Sep-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70150-09100-043 A007-06849 05A024. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

16-Sep-2016

COND COND

156001447977405A02E

49774977M/R BLADE TIP CAP A849-1514770150-09207-041 CCCC

5000 5816

161501099234105A02I

49774977M/R BLADE CUFF G237-0458470150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

16-Sep-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

16-Sep-2016

COND COND

156001447977405A02E


5000 8509

161501099234105A02I

22842284M/R BLADE CUFF G237-0306770150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

16-Sep-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

16-Sep-2016

COND COND

156001447977405A02E


5000 9745

161501099234105A02I

10481048M/R BLADE CUFF A237-0454470150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

16-Sep-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

16-Sep-2016

COND COND

156001447977405A02E


5000 8711

161501099234105A02I

20822082M/R BLADE CUFF A237-1542570150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

16-Sep-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615011997646SWASHPLATE ASSY 70104-08000-050 015152-2003 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

16-Sep-2016

COND COND

161501087160205A03A01

902902STATIONARYSWASHPLATE

015152-165170104-08010-044 CCCC

11000 14875

161501357508905A03A02

00ROTATINGSWASHPLATE ASSEMBL

015152-200370104-08001-045 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615011997646SWASHPLATE ASSY 70104-08000-050 015152-2003 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

16-Sep-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70351-08100-076 A26501087 06A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

16-Sep-2016

17000 21203

161501078571106A08

13326584SWASHPLATE GUIDE AER0225170351-08227-041 RCRC

3000 8535

161501110149106A13

06584HOUSING ASSY MGB F2110019870351-08110-045 RCRC

7600 12203

304001415838806A18

9326584MAIN ROTOR SHAFT E2530371970351-08131-048 RCRC

12000 16201

161501497725706A19

13346584PLANETARY CARRIERASSY

A2400113570351-08175-046 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70351-08100-076 A26501087 06A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

16-Sep-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615013765089TAIL ROTORGEARBOX ASSY

70358-06600-046 A006-03624 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

16-Sep-2016

12000 15875

161501074515306G01C

00I/B RETENTION PLATET/R

K259-0101370358-06612-042 RCRC

5000 8875

304001292161706G01D

00GEARSHAFT, BEVEL F320-0106670358-06620-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615013765089TAIL ROTORGEARBOX ASSY

70358-06600-046 A006-03624 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

16-Sep-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



4140013293428FAN AXIAL 52E15-1 988 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

16-Sep-2016

2520 7777

311001127300506H23A

0401BALL BRNG ANN (OILCOOLER FWD)

6171210SFFC3 RCRC

2520 7777

311001127300506H23A

0401BALL BRNG ANN (OILCOOLER FWD)

6213210SFFC3 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



4140013293428FAN AXIAL 52E15-1 988 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

16-Sep-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70400-06100-042 D233-00159 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

16-Sep-2016

2160 6035

311001113828811C23A

01994BRNG T/R PITCH CHGSHAFT

B840-05484SB1162-102 RCRC

COND COND

534001094578911C23C

24272427CLEVIS, ROD END D233-001590015906072010

70400-06702-041 CCCC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70400-06100-042 D233-00159 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

16-Sep-2016




T/T I HIST RCDR SNSERIAL NO. OP HRSLCF-2LCF-1POSHOURSAIRCRAFT AIRCRAFT ENGINE SERIAL NO. 13.12.11. 14.10.9.8.7.6.

(256)123-3456HUNTSVILLEK08DD23. UIC 5. TELEPHONE NUMBER4. LOCATION

16228 SESI

2. Organization

CSGLD-1052

REQUIREMENT CONTROL SYMBOL(Julian)1. PERIOD ENDING DATE


1GE-E-306785 ECD017355688162977907226286488424023

1GE-E-306785 ECD017355691162977909226386518424023

1GE-E-306785 ECD017355702162977953226886628424023

2GE-E-207565 CAO0089569202531914979340986488424023

2GE-E-207565 CAO0089569222531914985341086518424023

2GE-E-207565 CAO0089569332531915071341586628424023

1GE-E-307057 CAO0054150081410730539577187978624568

2GE-E-307026 ECDH06219258753525464396287978624568

1GE-E-207370 CAO004694186200368597218476208724673

2GE-E-207533 ECDH0817328389667540164776208724673

1GE-E-306730 CAO014454623177849720262856127923291

2GEE207940 CAO006166519538114423230456127923291

1GEE306565 ECD0287144852960010127236455207923305

2GEE306891 ECD0102832571057224859155207923305

1GE-E-306740 CAO0217055401486812484299357937923340

2GE-E-307131 CAO01743249627095093141757937923340

1GEE763238C LMDH393410732844166450246768023463

2GEE761402C ECDH827210573468183153346768023463

1GE-E-374746C LMDH404615775634446298047808023468

2GE-E-374729C LMDH518510713140200955247808023468

1GE-E-307098 ECD006384656189459754287260698123564

2GE-E-307078 ECD025105063169468500238160698123564

1GEE207783 ECDH0338456914716375777055468123582

2GEE306017 CAO0120853389042352771755468123582


ENGINE COMPONENT OPERATING HOURS RECORDDA FORM 2408-19-3 E, DEC 1991

James.Harper

Highlight

360

360

5715.1

7923340 4336.7 2259

e. ACFT HRS INSTALLEDc. TIME SINCE NEW OR OVERHAULc. SERIAL NUMBER

UH-60A A00500774 Days

b. MAKE OR TYPE d. ACFT HRS LAST OIL CHANGEb. SERIAL NUMBER

HELICOPTER, UTILITY INTERMEDIATE GEARBOX Hrs

a. NOMENCLATURE AND TYPEa. NOMENCLATUREFREQUENCY

COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b

SAMPLE DATE PIDSAMPLELAST OILEND ITEM

RESULTSDATE RESULTS RECEIVED7. 8.6. REASON FORHOURS5.4.

COMPONENTCHANGE

WT52434228-Jun-2006NORMALROUTINE855.01658311421-Jun-2006

SM13183305-Oct-2006NORMALROUTINE898.01701315702-Oct-2006

SM13183305-Oct-2006NORMALROUTINE910.01713316904-Oct-2006

RG41408912-Oct-2006NORMALROUTINE934.01737319310-Oct-2006

RG41408930-Oct-2006NORMALROUTINE968.01771322728-Oct-2006

RG41408921-Nov-2006NORMALROUTINE1011.01814327019-Nov-2006

SM13183302-Dec-2006NORMALROUTINE1053.01856331201-Dec-2006

SM13183314-Dec-2006NORMALROUTINE1096.01899335511-Dec-2006

SM13183301-Jan-2007NORMALROUTINE1136.01939339528-Dec-2006

SM13183305-Jan-2007NORMALROUTINE1151.01954341003-Jan-2007

RG41408922-Feb-2007NORMALROUTINE1191.01994345021-Feb-2007

RG41408924-Mar-2007NORMALROUTINE1232.02035349123-Mar-2007

KB29612603-Apr-2007NORMALROUTINE1272.02075353102-Apr-2007

KB29612622-Apr-2007NORMALROUTINE1313.02116357221-Apr-2007

KB29612605-May-2007NORMALROUTINE1346.02149360502-May-2007

GE76574915-May-2007NORMALROUTINE1384.02187364314-May-2007

KB29612628-May-2007NORMALROUTINE1427.02230368626-May-2007

KB29612612-Jun-2007NORMALROUTINE1466.02269372510-Jun-2007

RH17052703-Jul-2007NORMALBASELINE1508.02311376702-Jul-2007

RH17052714-Jul-2007NORMALROUTINE1546.02349380514-Jul-2007

PT72154628-Jul-2007ABNORMALROUTINE1583.02386384226-Jul-2007

RH17052730-Jul-2007NORMALSPECIAL1595.02398385430-Jul-2007

TK00599526-Nov-2007NORMALPRE-RESET1616.02419387521-Nov-2007

TK00599530-Jan-2008NORMALPOST RESET1616.02419387529-Jan-2008

CG45046422-May-2008NORMALROUTINE39.02458391416-May-2008

CG45046423-Jun-2008NORMALROUTINE79.02498395413-Jun-2008

KL41517022-Aug-2008NORMALROUTINE121.02540399613-Aug-2008

CS45250420-Oct-2008NORMALROUTINE162.02581403714-Oct-2008

CS45250424-Feb-2009NORMALROUTINE202.02621407718-Feb-2009

KL41517024-Apr-2009NORMALROUTINE239.02658411421-Apr-2009

CB63682801-Sep-2009NORMALROUTINE332.02751420718-Aug-2009

BS08480402-Feb-2011NORMALROUTINE529.02948440426-Jan-2011

JH43086828-Nov-2011NORMALROUTINE889.03308476404-Nov-2011

KC94141009-May-2012NORMALPOST PHASE1043.03462491826-Apr-2012

WA75458318-Apr-2013NORMALROUTINE1382.03801525709-Apr-2013

JA17932505-May-2014NORMALROUTINE1661.94080.95536.924-Apr-2014

DP50831218-Sep-2014NORMALROUTINE1740.74159.75615.706-Jul-2014

RF84423930-Apr-2015NORMALROUTINE99.44259.15715.123-Apr-2015

KM58389802-May-2016NORMALROUTINE72.54331.65787.626-Apr-2016

For use of this form, see DA PAMs 738-751; the proponent agency is DCSLOGDA FORM 2408-20, DEC 91, MAY BE USED

OIL ANALYSIS LOGDA FORM 2408-20, OCT 1997

360

360

5715.1

7923340 4336.7 2259


UH-60A A00500774 Days


HELICOPTER, UTILITY INTERMEDIATE GEARBOX Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


9. REMARKS:



0

720

0

7923340 6841.7 5535


UH-60A A26501087 Days


HELICOPTER, UTILITY MAIN TRANSMISSION MODULE Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

JA17932505-May-2014NORMALBASELINE5536.96585.95536.924-Apr-2014

9. REMARKS:



360

360

5715.1

7923340 1917.7 3875


UH-60A A006-03624 Days


HELICOPTER, UTILITY TAIL ROTOR GEARBOX ASSY Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

TK00599530-Jan-2008ABNORMALPOST RESET3875.0387529-Jan-2008

TK00599531-Jan-2008ABNORMALLAB REQUES3877.02387731-Jan-2008

TK00599505-Feb-2008ABNORMALLAB REQUES3879.04387905-Feb-2008

TK00599507-Feb-2008NORMALLAB REQUES3882.07388206-Feb-2008

TK00599511-Feb-2008ABNORMALBASELINE3883.08388311-Feb-2008

TK00599512-Feb-2008SERVICESPECIAL3884.09388412-Feb-2008

TK00599514-Feb-2008NORMALLAB REQUES3885.010388514-Feb-2008

TK00599519-Feb-2008NORMALSPECIAL3885.011388515-Feb-2008

CG45046422-May-2008NORMALROUTINE44.044391916-May-2008

CG45046423-Jun-2008NORMALROUTINE79.079395413-Jun-2008


CS45250420-Oct-2008NORMALROUTINE162.0162403714-Oct-2008

CS45250424-Feb-2009NORMALROUTINE202.0202407718-Feb-2009


CB63682801-Sep-2009NORMALROUTINE332.0332420718-Aug-2009


KC94141028-Nov-2011NORMALROUTINE889.0889476404-Nov-2011


WA75458311-Dec-2012NORMALBASELINE1221.01221509602-Dec-2012


JA17932505-May-2014NORMALROUTINE1661.91661.95536.924-Apr-2014

DP50831218-Sep-2014NORMALROUTINE1740.71740.75615.706-Sep-2014

RF84423930-Apr-2015NORMALROUTINE99.41840.15715.123-Apr-2015

KM58389802-May-2016NORMALROUTINE72.51912.65787.626-Apr-2016

REPLACED INPUTSEAL

9. REMARKS:



0

120

5786.6

7923340 4446 0


UH-60A P1340 Days


HELICOPTER, UTILITY AUXILIARY POWER UNIT Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

RH17052730-Jul-2007NORMALBASELINE3849.03849384928-Jul-2007

TK00599526-Nov-2007NORMALROUTINE3875.010387521-Nov-2007

TK00599530-Jan-2008NORMALROUTINE3875.010387529-Jan-2008




KC94141028-Nov-2011NORMALROUTINE4764.010476404-Nov-2011



DP50831229-Apr-2014NORMALROUTINE5543.95725543.929-Apr-2014

DP50831203-May-2014NORMALBASELINE5543.95725543.903-May-2014

DP50831218-Sep-2014NORMALROUTINE5615.75785615.706-Jul-2014

RF84423930-Apr-2015NORMALROUTINE99.442985715.123-Apr-2015

KM58389802-May-2016NORMALROUTINE1.05787.626-Apr-2016

9. REMARKS:



PIDMWODATE HRS



ACCESSORY MODULE 7923340A258008631. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 CM

WA75458321-Mar-2013

0.1B CO 777THASB, KFOR 16

H-60 SERIES AIRCRAFT, PLASTICMEDIA BLAST (PMB) AND OXIDEFLAKE RESIDUE H-60-13-ASAM-04

H-60-13-ASAM-04MWO:

Priority Mnt Level


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

PIDMWODATE HRS



ACCESSORY MODULE 7923340A258008641. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 CM

WA75458321-Mar-2013



H-60-13-ASAM-04MWO:

Priority Mnt Level




79233403800480-2AUXILIARY POWER UNITP1340

10

10

60

60

0

0

0

0

5=

TOTAL COMPONENT COUNTS

COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-

READING AT INSTALLATION OF

MODULE/RECORDER3

READING AT REMOVAL OF

7. HISTORY RECORDER S/N

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE

OPERATING HOURSTEMP/TEMP INDEXLCF - 2LCF - 1

HISTORICAL COUNTS ON COMPONENT/MODULE

7. HISTORY RECORDER S/N6.

5. NHA - Serial Number4. P/N3. NOMENCLATURE2. Serial Number1. MODEL

**Note - APU Information LCF1 = NUMBER OF OVERHAULS LCF2 = STARTS SINCEOVERHAUL TTI = STARTS SINCE NEW OPH = ONLY FOR APU's WITH HOUR METERINSTALLED - ENTER TIME ON METER

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

HISTORY RECORDER, COMPONENT, MODULE RECORDDA FORM 2408-16-1-E, OCT91

OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-

12.HISTORY COUNTS AT LAST DEPOTREPL

11.

O/H OR

10.

SERIAL NUMBER9.PART NUMBERNOMENCLATURE

8.

ReportDate:

Major Nomenclature Major Part NumberMajor Wuc Major Serial Number

16-Sep-2016 2/2

15B 3800480-2 AUXILIARY POWER UNIT P1340

0000

0000503501046133822101-2WHEEL,COMPRESSOR

COND

COND

0000

0000501345100243842133-1WHEEL, TURBINE

COND

COND


1/2/200812:00:00 AM

1 27 DEC 07: RECEVIED FOR RESET INSPECTION. RELACED ALLFILTERS/FLUIDS. MOC COMPLETED. ENTERED BY KF7892, ESRA, FTCKY42223. DSN 635-6201

TK005995 ESRA, RESET FTCKY, 42223

REVERSE OF DA FORM 2408-16-1 E, OCT 91


CAO02170

79233406035T00G01ENGINE ASSY, TURBINEGE-E-306740

3371

5354

9487

14805

11952

12134

2403

2901

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE





T700-GE-700




OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


16-Sep-2016 2/12

04A 6035T00G01 ENGINE ASSY, TURBINE GE-E-306740

33719487119522403

41492488888502650GEC0079836035T02G01COLD SECTIONMODULE

COND

COND

2552000

1580000GGM8T8AC6064T55G01COMBUSTION LINER

COND

COND

3367000

14661097247631309MRSG44796055T20G03MTCHDROTOR/STATOR ASSY

COND

COND

2552000

3296000AMDA28325043T24G14STAGE 1 NOZZLEASSY

COND

COND

2552884896701857

30002637464071452GEL0378706064T98G01POWER TURBINEMODULE

COND

COND

2552000

4568000GED0070916035T01G01ACCESSORY MODULE

COND

COND

2552000

3564000FIAG77096034T62P13PARTICLESEPARATOR BLOWER

COND

COND

3371000

5316000UDAJ35545074T79G07FUEL CONTROL

COND

COND

2552000

1207000APM584RS4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

3371000

4121000ECD002294046T29G11ELECTRICALCONTROL UNIT

COND

COND

2552884896701857

45351416698522355CAO021704046T26G03HISTORY RECORDER

COND

COND


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


16-Sep-2016 3/12


2552000

4749000UDC018194046T25G01COOLER, OIL

COND

COND

3371000

0000COMH133064046T28G14ANTI-ICE VALVE

COND

COND




CAO02170

GE-E-3067406035T02G01COLD SECTION MODULEGEC007983

4535

4149

14166

24888

9852

8850

2355

2650

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


16-Sep-2016 5/12

04A01 6035T02G01 COLD SECTION MODULE GEC007983

41472476488432648

31253719578661595ACH315335056T66G02POWER TAKEOFFDRIVE

COND

COND

41472476488432648

41472476488432648GLB007396035T77G10COMPRESSORROTOR ASSEMBLY

COND

COND

41472476488432648

49322172150941541GAT596576035T88P03GAS GENERATORTURBINE SHAFT

10601

11000

41472476488432648

0000WEST47765036T95P01INNER BALANCEPISTON SE

COND

COND

41472476488432648

0000MLEWF1546035T79P04COMPRESSORDISCHARGE SEAL

COND

COND

41472476488432648

0000FIAAYEWA6035T83P01COMPRESSOR REARSHAFT

9533

5000

41472476488432648

0000VAEFL2425044T07P01NO 3 LABYRINTHSEAL

COND

COND

41472476488432648

32501499463503227BIWCC7695035T57P02VORTEX SPOILER

COND

COND

41472476488432648

116239161946745GATHL8RA5043T04P02TIE ROD,COMPRESSOR

13371

10000

41472476488432648

6107651610426PAMGY7715066T79P01RING, SPACERCOMPRESSOR

13923

10000

41472476488432648

0000GLHTRONK6055T59P01COMPRESSORIMPELLER

9533

5000


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


16-Sep-2016 6/12


41472476488432648

0000GGTA79703065T21G01OUTPUT SHAFT ASSY

COND

COND

41472476488432648

0000GLHTPND66032T26G09STAGE 1 BLISK

9533

5000

41472476488432648

0000GLHTR3M66032T27P08STAGE 2 BLISK

11533

7000

41472476488432648

0000GLHTR3MK6038T08P04STAGE 3 & 4 BLISK

11533

7000

41472476488432648

0000GLHTR41T6038T09P04STAGE 5 BLISK

11533

7000

41472476488432648

6107651610426TMKAE0UY6064T35P01NO 3 BALL BEARING

COND

COND

41472476488432648

110030823733446FCAT15236064T15P03NO 4 ROLLERBEARING

COND

COND




CAO02170

GEC0079833065T21G01OUTPUT SHAFT ASSYGGTA7970

4535

2

14166

124

9852

7

2355

2

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


16-Sep-2016 8/12

04A01G 3065T21G01 OUTPUT SHAFT ASSY GGTA7970

0000

0000FCAAU6006064T34P02NO 1 BALL BEARING

COND

COND

0000

0000FCABB8165121T46P02NO 2 ROLLERBEARING

COND

COND




CAO02170

GE-E-3067406055T20G03MTCHD ROTOR/STATORASSY

MRSG4479

5350

1466

14166

19820

9852

14433

2355

3166

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


16-Sep-2016 10/12

04A02B 6055T20G03 MTCHD ROTOR/STATOR ASSY MRSG4479

14661097247631309

8019011754356GATHAGCP6064T85P01STAGE 1 TURBINEDISK

9549

5000

14661097247631309

14661097247631309GGAC34766039T57G22G/G STATOR ASSY

COND

COND

14661097247631309

33449341572108GATHA7MC6064T86P01STAGE 2 TURBINEDISK

10016

5000

14661097247631309

0000GFF5D3PG6064T81P01STAGE 1 FWDCOOLING PLATE

10350

5000

14661097247631309

0000GFF5D1HE6064T82P01STAGE 1 REARCOOLING PLATE

10350

5000

14661097247631309

0000PAMEU7386064T83P01STG 2 FWD COOLINGPLATE

10350

5000

14661097247631309

0000GFF5D29R6064T84P02STAGE 2 REARCOOLING PLATE

10350

5000

14661097247631309

14661097247631309GGAG44796039T54G13G/G ROTORASSEMBLY

COND

COND

14661097247631309


COND

COND




CAO02170

GE-E-3067406064T98G01POWER TURBINE MODULEGEL037870

4535

3000

14166

26374

9852

6407

2355

1452

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


16-Sep-2016 12/12

04A03 6064T98G01 POWER TURBINE MODULE GEL037870

29992635764051450

29992635764051450GGAP08595043T75G07POWER TURBINEROTOR

COND

COND

29992635764051450

0000GATHNWLM6038T32P02STAGE 3 TURBINEDISK

9534

5000

29992635764051450

38413921182247GATA135K6038T34P05STAGE 4 TURBINEDISK

9150

5000

30002637464071452

63412981430371GATHHDMR5125T92G01POWER TURBINESHAFT

8901

5000

29992635764051450

34101707888892465MAB452715034T27P01NO 5 ROLLERBEARING

COND

COND

29992635764051450

0000TMKAFFVN6064T36P01NO 6 BALL BEARING

COND

COND




CAO01743

79233406035T00G01ENGINE ASSY, TURBINEGE-E-307131

2313

6412

2591

6261

4923

15191

1350

3581

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE





T700-GE-700




OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


16-Sep-2016 2/12


3906327498122123

2496755356711473GEC0076776035T02G01COLD SECTIONMODULE

COND

COND

47504704113862548

2842000GGMC17436039T58G02COMBUSTION LINER

COND

COND

64126261151913581

252828615150141687MRSG62136055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

3906000

1834000AMDA06175043T24G04STAGE 1 NOZZLEASSY

COND

COND

64126261151913581

481520773113432555GEL0074776064T98G01POWER TURBINEMODULE

COND

COND

00022590

0000GE-D-0371316035T01G01ACCESSORY MODULE

COND

COND

3604000

0000SUPJ96506034T62P18PARTICLESEPARATOR BLOWER

COND

COND

6522000

5665000UDA967765074T79G07FUEL CONTROL

COND

COND

5663000

4763000APM412RU4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

6412000

6254000ECD010404046T29G13ELECTRICALCONTROL UNIT

COND

COND

41013671102682231

0000CAO017434046T26G03HISTORY RECORDER

COND

COND


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


16-Sep-2016 3/12


0000

0000SUSJ0740C4046T25G03COOLER, OIL

COND

COND

5961000

0000COMH132064046T28G14ANTI-ICE VALVE

COND

COND


10/17/200112:00:00 AM

1 WUC: 04A PN: 6035T00G01 PSN: GE-E-307131T700-GE-700 ENGINE ASSY, TURBINE 17 0CT 01 - INSTALLED ENG ASSY ON ACFT8724652 AT 8349.1 ACFT HRS W/TTSN:3476 (EDC00763) READINGS MATCHENG CUMULATIVE COUNTS AT LCF1:1917 LCF2:8933 TTI:2454HRS:3476/MA4187 R/CLK USAAVNC, FT. RUCKER, AL

QC000002 ASAAVNC FT RUCKER, AL

8/27/200412:00:00 AM

1 WUC: 04A PN: 6035T00G01 PSN: GE-E-307131T700-GE-700 ENGINEASSY, TURBINE 27 AUG 04 - REPLACED HISTORY COUNTER DUE TOFAILURE OF HR METER AT LCF1:2231 LCF2:10268 TTI:3671 HR:3949. HRSCOMPARED TO OTHER ENGINE TO ADJUST OPERATING HRS. COUNTSADJUSTED TO - LCF1:2231 LCF2:10268 TTI:3671 HRS:4101. NEW COUNTERS/N: CAO01743 INSTALLED WITH LCF1:0 LCF2:0 TTI:1 HR:2 GS5800 AASFBOONE, IA

QC000002 AASF BOONE, IA

9/27/200412:00:00 AM

1 WUC: 04A PN: 6035T00G01 PSN: GE-E-307131T700-GE-700 ENGINE ASSY,TURBINE 27 SEP 04 - ENGINE CONTROLLED EXCHANGE TO ACFT 88-26079AT 3923.4 ACFT HRS. CUMULATIVE COUNTS: LCF1:2231 LCF2:10268TTI:3671 HRS:4101. HISTORY COUNTER S/N CAO01743 READINGS:LCF1:000000 LCF2:000000 TTI:000001 HRS:000002 GS5800 AASF BOONE,IA

QC000002 AASF BOONE, IA



CAO01743

GE-E-3071316035T02G01COLD SECTION MODULEGEC007677

0

2691

0

7950

0

6127

0

1581

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


16-Sep-2016 5/12


2496755356711473

1802380629821008AGRA-30115044T27G02POWER TAKEOFFDRIVE

COND

COND

2496755356711473

2496755356711473GLB-003226035T77G10COMPRESSORROTOR ASSEMBLY

COND

COND

2496755356711473

2496755356711473GAT-598236035T88P03GAS GENERATORTURBINE SHAFT

8309

11000

2496755356711473

0000BJWE-48365036T95P01INNER BALANCEPISTON SE

COND

COND

2496755356711473

0000MMTF-01296035T79P04COMPRESSORDISCHARGE SEAL

COND

COND

2496755356711473

1899258232405749GATW-30606035T83P01COMPRESSOR REARSHAFT

2906

5000

2496755356711473

2496755356711473GATB-64235044T07P01NO 3 LABYRINTHSEAL

COND

COND

2496755356711473

2496755356711473ASV-002885035T57P02VORTEX SPOILER

COND

COND

2496755356711473

2496755356711473GATA-05815043T04P02TIE ROD,COMPRESSOR

7309

10000

2496755356711473

180693035965556GAT-8575L4045T08P01RING, SPACERCOMPRESSOR

7999

10000

2496755356711473

0000GLTHG-8D56055T59P01COMPRESSORIMPELLER

4805

5000


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


16-Sep-2016 6/12


2496755356711473

2172767444141193GGAC-77236039T56G05OUTPUT SHAFT ASSY

COND

COND

2496755356711473

0000GLHTG-7K86032T26G09STAGE 1 BLISK

4805

5000

2496755356711473

0000GLHTG-5K96032T27P08STAGE 2 BLISK

6805

7000

2496755356711473

0000GLHTG-C926038T08P04STAGE 3 & 4 BLISK

6805

7000

2496755356711473

0000GLHTG-E476038T09P04STAGE 5 BLISK

6805

7000

2496755356711473

3546659945501157MDAM-33596038T48P02NO 3 BALL BEARING

COND

COND

2496755356711473

3751084MDA-958UN6064T14P01NO 4 ROLLERBEARING

COND

COND




CAO01743

GEC0076776039T56G05OUTPUT SHAFT ASSYGGAC-7723

5288

6129

5657

6439

13038

13979

2951

3326

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


16-Sep-2016 8/12

04A01G 6039T56G05 OUTPUT SHAFT ASSY GGAC-7723

2172767444141193

22582297059951933MDA0V9545043T18P01NO 1 BALL BEARING

COND

COND

2172767444141193

1509855945031225MAB488035035T69P01NO 2 ROLLERBEARING

COND

COND




CAO01743

GE-E-3071316055T20G05MTCHD ROTOR/STATORASSY

MRSG6213

2311

2528

2590

28615

4923

15014

1350

1687

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


16-Sep-2016 10/12

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRSG6213

252828615150141687

17617130071GATHG8E86064T85P01STAGE 1 TURBINEDISK

7135

5000

252828615150141687

252828615150141687GGAC48286039T57G24G/G STATOR ASSY

COND

COND

252828615150141687

0000GATHGLCM6064T86P02STAGE 2 TURBINEDISK

7311

5000

252828615150141687

0000GFF5DMH26064T81P01STAGE 1 FWDCOOLING PLATE

7311

5000

252828615150141687

104484052705672GFFR8KRK6064T82P01STAGE 1 REARCOOLING PLATE

6267

5000

252828615150141687

84948861650531GFFN89796064T83P01STG 2 FWD COOLINGPLATE

6462

5000

252828615150141687

95026041403400GFFN82286064T84P02STAGE 2 REARCOOLING PLATE

6361

5000

252828615150141687


COND

COND




CAO01743

GE-E-3071316064T98G01POWER TURBINE MODULEGEL007477

2311

4815

2590

20773

4923

11343

1350

2555

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


16-Sep-2016 12/12

04A03 6064T98G01 POWER TURBINE MODULE GEL007477

481420714113382553

481420714113382553GGA072125043T75G07POWER TURBINEROTOR

COND

COND

481420714113382553

96726601885507GATH6ROD6038T32P01STAGE 3 TURBINEDISK

6343

5000

481420714113382553

96726601885507GATH6NL76038T34P05STAGE 4 TURBINEDISK

6343

5000

481420714113382553

50620041066247GATHJ5T85125T92G01POWER TURBINESHAFT

6804

5000

481420714113382553

0000FCAV76595034T27P02NO 5 ROLLERBEARING

COND

COND

481420714113382553

57630641346275392331276064T36P02NO 6 BALL BEARING

COND

COND



PIDMWODATE HRS



ENGINE ASSY, TURBINE 7923340GE-E-3071311. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


15-Feb-1987 OM

QC00000218-May-1996

0.5CCAD (LF0000)ONE TIME INSPECTION OF TORQUEFUEL DIFFER PRESSUREINDICATOR

55-2840-248-50-44MWO:

Priority Mnt Level

31-Jul-1989 OM

QC00000218-May-1996

3.3CCAD (LF0000)MODIFICATION OF GG ROTORASSEMBLY T700/701 REWORK T700ENGINES

55-2840-248-50-32MWO:

Priority Mnt Level

15-Aug-1990 OM

QC00000218-May-1996

1CCAD (LF0000)INSTALLATION OF SELF SEALADAPTER ASSEMBLY

55-2840-248-50-28MWO:

Priority Mnt Level

25-Jan-1991 DN

QC00000218-May-1996

20CCAD (LF0000)MODIFICATION OF POWER TAKEOFFDRIVE ASSEMBLY P/N 5044T27G01

55-2840-248-50-27MWO:

Priority Mnt Level

31-Mar-1993 DR

QC00000215-May-1996

1.5CCAD (LF0000)INSTALLATION OF PTO DRIVEASSEMBLY P/NS 5044T27G02 OR5056T66G02 (T700-GE-700 AND 701ENGINES)

1-2840-248-50-29MWO:

Priority Mnt Level

31-May-1994 OM

QC00000218-May-1996

3.6CCAD (LF0000)LIFE LIMITS FOR T-700-GE-701 ANDT701 ENGINE COMPONENTS

1-2840-248-20-18MWO:

Priority Mnt Level

30-Jun-1994 OR

QC00000223-May-1996

4CCAD (LF0000)ONE TIME INSPECTION ANDCONVERSION OF FORMS ANDRECORDS FOR T700-GE-700, -701AND -701C SERIES GAS TURBINEENGINES

1-2840-248-20-2MWO:

Priority Mnt Level

02-Aug-1999 FM

QC00000203-Aug-1999

3USAAVNC, FT.RUCKER, AL.(PH4947)

ALL AH-64 AND UH-60 SERIESAIRCRAFT - ONE TIME INSPECTIONOF T700-GE-700/701/701C ENGINES


Priority Mnt Level

16-Aug-1999 OM

QC00000219-Aug-1999

0.5USAAVNC, FT.RUCKER, AL.(PH4947)

ALL UH-60A, EH-60A AND UH-60QAIRCRAFT, SUBJECT: INSPECTIONINTERVAL CHANGE FOR HAMILTONSTANDARD HYDRO MECHANICALUNITS (HMU) P/NS 4046T52G01,4046T52G04, 4046T52G06,4046T52G09 AND 4046T52G11 USEDON THE T700-GE-700 ENGINE


Priority Mnt Level

QC00000217-Jul-2007

0.5AASF #1BOONE, IA(PT1630)

ALL H-60 SERIES AIRCRAFT,HAMILTON-SUNDSTRAND HYDRO-MECHANICAL UNITS PN 4046T52G01AND 4046T52G04 REMOVE FROMSERVICE




PIDMWODATE HRS



ENGINE ASSY, TURBINE 7923340GE-E-3071311. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


16-Jul-2007 OM

AASF #1BOONE, IA(PT1630)

ALL H-60 SERIES AIRCRAFT,HAMILTON-SUNDSTRAND HYDRO-MECHANICAL UNITS PN 4046T52G01AND 4046T52G04 REMOVE FROMSERVICE

Priority Mnt Level

13-Aug-2007 OM

QC00000214-Aug-2007

0.5AASF #1BOONE, IA(PT1630)

ALL H-60 SERIES AIRCRAFT, MAINFUEL MANIFOLD CHAFING


Priority Mnt Level

20-Dec-2007 OM

JP80042002-Jan-2008

0.1AASF #1BOONE, IA 50036

ALL H-60 AND ALL AH-64 SERIESAIRCRAFT, MIL-PRF-23699 HIGHTEMPERATURE STABILITY (HTS) OIL

H-60-08-ASAM-03MWO:

Priority Mnt Level

22-Sep-2008 OM

JZ92432230-Sep-2008

0.2AASF #1 BOONEIA

SUSPECT ENGINE HARNESSESH-60-08-ASAM-14MWO:

Priority Mnt Level

12-Jan-2009 FM

SK40374812-Jan-2009

0.1LSI MO-AVCRADALL H-60A/K/L AND AH-64 SERIESAIRCRAFT, T701C GAS GENERATORROTOR ASSEMBLIES, FOR SN'SINSTALLED.


Priority Mnt Level

29-Jul-2010 OM

RM23510727-Aug-2010

1DET 1 B CO 777ASB

ALL H-60 AND AH-64 SERIESAIRCRAFT, T700 SERIES ENGINESCOMMON OMPONENT RETIREMENTCHANGE TIMES

H-60-10-ASAM-12MWO:

Priority Mnt Level



PIDMWODATE HRS



FAN AXIAL 79233409881. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


22-Jul-2008 DR

JL906423-Nov-2010

22CCAD/WOMUAARECAPPEDDMWR 1-4140-228 31DEMWO:

Priority Mnt Level



PIDMWODATE HRS



FUEL CONTROL 7923340UDAJ35541. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


01-Oct-2009 ON

QC00000001-Oct-2009

1DET 1 B CO777TH ASB

HMU SUSPECTED PART NUMBERH-60-10-ASAM-01MWO:

Priority Mnt Level

23-Nov-2010 OM

BS08480406-Dec-2010

0.5WUAUC0ALL H-60 SERIES AIRCRAFT,HAMILTON STANDARD HYDRO-MECHANICAL UNITS PN 5074T79GO2, 5074T79GO3, AND 5074T79GO5REMOVE FROM SERVICE. REMOVEPN 5074T79GO7 IF LAST DEPOTREPAIR PRIOR TO 01 JAN 2003.

H-60-11-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



HUB, M/R ROTOR ASSY 7923340B303-000891. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


30-Dec-2013 FM

JK56729431-Dec-2013

0.1DET 2 CO B638TH ASB

MAIN ROTOR HUB ASSEMBLYH-60-14-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



INPUT MODULE 7923340A264-004621. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 CM

WA75458321-Mar-2013



H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



INPUT MODULE 7923340A264035631. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 CM

WA75458321-Mar-2013



H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



INTERMEDIATE GEARBOX 7923340A005007741. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 FM

WA75458321-Mar-2013


ONE-TIME INSPECTION OF SUSPECTSERIAL NUMBERED COMPONENTSFOR PLASTIC MEDIA BLAST (PMB)AND OXIDE FLAKE RESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



LATERAL SERVO BELLCRANK 7923340A289004591. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


07-Jan-1997 OM

QC00000014-Jul-1998

1.5CCAD, CORPC,TX 78419(ER5987)

ALL H-60 AIRCRAFT WITH THELATERAL BELLCRANK ASSEMBLY,P/N 70400-08150-045,MANUFACTURED BY PURDYMACHINE COMPANY (CAGE CODE15152)


Priority Mnt Level

05-Jan-2001 OT

QC00000018-Jan-2001

0.5AR AASF N.L.R.AR 72199(BM3659)

H-60 SERIES AIRCRAFT, REMOVALOF LATERAL SERVO BELLCRANKASSEMBLY MANUFACTURED BY THEPURDY MACHINE COMPANY, CAGECODE 15152

UH-60-01-03MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR PRIMARY SERVO 7923340B303-03284B1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


18-Feb-2006 DM

LU00605209-Feb-2011

25CCAD/WOMUAARETORQUEING OF PRIMARY SERVOINPUT LINKAGE ASSYEMBLE NUTI/A/W DMWR 1-1650-281

DMWR 1-1650-381MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 792334032895-3431. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 FM

SH15266126-Sep-2012

1B CO 777 KFOR-16

ALL H-60 SERIES AIRCRAFT, MAINROTOR SPINDLE SUB-COMPONENTTRACKING REQUIREMENTS

H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

WA75458326-Feb-2013

0.8B CO 777TH ASBKFOR 16

PERFORM ONE-TIME INSPECTIONFOR SUSPECT MAIN ROTORSPINDLE ANTI-FLAP BRACKETASSEMBLIES

H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 7923340A001114721. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 FM

RS78420018-Apr-2013

3DYNCORPINTERNATIONALDIFZ


H-60-12-AMAM-16MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 7923340A001119031. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 FM

RS78420018-Apr-2013

3DYNCORPINTERNATIONALDIFZ


H-60-12-AMAM-16MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 7923340B001-002251. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 FM

SH15266126-Sep-2012

1B CO 777 KFOR-16


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

WA75458326-Feb-2013


PERFORM ONE-TIME INSPECTIONFOR SUSPECT MAIN ROTORSPINDLE ANTI-FLAP BRACKETASSEMBLIES

H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN TRANSMISSION MODULE 7923340A265010871. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


23-Jul-2008 DT

AB242227-May-2010

1CCADRECAPITALIZATION REQUIREMENTSFOR UH60 MAIN TRANSMISSIONMODULE COMPLIED WITH. CCAD.

DMWR 1-1615-371MWO:

Priority Mnt Level

10-Nov-2009 OT

AB242227-May-2010

1CCADALL H-60 SERIES AIRCRAFTREDESIGNED PLANETARY GEARCARRIER RETIREMENT LIFE

H-60-10-AMAM-02MWO:

Priority Mnt Level

26-Mar-2014 FM

JA17932526-Mar-2014

0.5W3VA7GMAIN TRANSMISSION FILTER BOWLAND CHIP DETECTOR ATTACHMENTHARDWARE REPLACEMENT.

H-60-14-AMAM-09MWO:

Priority Mnt Level



SECTION I COCKPITSES BEST

4. EQUIPMENT CHECKLIST

7923340 UH-60A

3. AREA NAME 2. MODEL 1. SERIAL NUMBER


1RECEIVER RADIO - R-1496A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER

QTY REQ:NOMENCLATURITEM NO

1DISPLACEMENT GYRO - CN-1314/A (9000C)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GYRO, DIRECTIONAL - CN-998/ASN-43

Unt

UUUUUUnt

Unt

Un

Unt

Un0

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SIGNAL DATA CONVERTER - CV-3338A/ASN-128B

Unt

UUUUUUnt

Unt

Un

Unt

Un0

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U

Unt

UUUUUUnt

Unt

Un

Unt

Un1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER - R-2139/ARN-123(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING - MT-4834/ARN-123(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMMAND INSTR SYS PROCESSOR - 70600-01038-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING RACK - 70600-01038-102

Unt

UUUUUUnt

Unt

Un

Unt

Un1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT FOR TSEC/KY-58 - 5290279-502

Unt

UUUUUUnt

Unt

Un

Unt

Un1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM ANTENNA - AS-4171/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SAS AMPLIFIER - 70901-02908-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY - 70600-01047-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2RATE GYRO - TRU-2A/A

Unt

UUUUUUnt

Unt

Un

Unt

Un1

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1AMPILIFIER IMPEDANCE - AM-4859A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

AIRCRAFT INVENTORY RECORDDA FORM 2408-17 E, NOV 91



7923340 UH-60A



1VHF/AM ANTENNA FILTER - 70600-01012-102

Unt

UUUUUUnt

Unt

Un

Unt

Un1

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2VHF/FM ANTENNA FILTER - 70600-01011-103

Unt

UUUUUUnt

Unt

Un

Unt

Un2

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER RADAR - RT-1193/ASN-128

Unt

UUUUUUnt

Unt

Un

Unt

Un0

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2ANTENNA - AS-3831/APN-209(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un2

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GLIDE SLOPE ANTENNA - 70600-01043-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM, VHF-AM SENSE ANTENNA - 70600-01019-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2FIRST AID KIT - 6545-00-919-6650

Unt

UUUUUUnt

Unt

Un

Unt

Un0

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRE EXTINGUISHER - FR23-4-11848

Unt

UUUUUUnt

Unt

Un

Unt

Un0

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BAROMETERIC ALTIMETER - AAU-31/A-1

Unt

UUUUUUnt

Unt

Un

Unt

Un1

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BAROMETERIC ALTIMETER - AAU-32/A

Unt

UUUUUUnt

Unt

Un

Unt

Un1

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CREW SEAT - D3801-2

Unt

UUUUUUnt

Unt

Un

Unt

Un2

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF-AM RADIO SET - RT-1518/ARC-164(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

31

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2INTERPHONE CONTROL - C6533/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un2

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER - RT-1115D/APN-209

Unt

UUUUUUnt

Unt

Un

Unt

Un1

33

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1INDICATOR ALTIMETER - ID-1917C/APN-209

Unt

UUUUUUnt

Unt

Un

Unt

Un1

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






7923340 UH-60A



1CONTROL RADIO SET - C-7392/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

35

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CONTROL - C-10604(V)6/ARN-184

Unt

UUUUUUnt

Unt

Un

Unt

Un1

36

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPARATOR SIGNAL DATA - CM482/ARC-186(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

38

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2MOUNTREVERSIBLE ARC-186/ARC-201 - 4290268-501

Unt

UUUUUUnt

Unt

Un

Unt

Un2

40

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPUTER DISPLAY UNIT - CP-1252C/ASN-128B

Unt

UUUUUUnt

Unt

Un

Unt

Un0

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CIVIL NAVIGATION CONTROL - C-10048/ARN-123(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

43

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS SET CONTROLLER - C-8021E/ASN-75

Unt

UUUUUUnt

Unt

Un

Unt

Un0

44

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADIO RETRANSMISSION PANEL -70550-01008-042

Unt

UUUUUUnt

Unt

Un

Unt

Un1

45

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MAGNETIC COMPASS - MS17983-4

Unt

UUUUUUnt

Unt

Un

Unt

Un1

46

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2OUTSIDE AIR TEMP INDICATOR - MS28028-1

Unt

UUUUUUnt

Unt

Un

Unt

Un2

47

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOR WING PANEL - 70500-01152-093

Unt

UUUUUUnt

Unt

Un

Unt

Un1

48

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOR WING PANEL - 70500-01152-094

Unt

UUUUUUnt

Unt

Un

Unt

Un1

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MISC. SWITCH PANEL - 70450-01090-044

Unt

UUUUUUnt

Unt

Un

Unt

Un1

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1STABILATOR/FLT CONT PANEL - 70902-01070-048

Unt

UUUUUUnt

Unt

Un

Unt

Un1

51

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2AHRU MOUNTING PLATE FOGS

Unt

UUUUUUnt

Unt

Un

Unt

Un1

60

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






7923340 UH-60A



1MOUNTING BASE APX-118

Unt

UUUUUUnt

Unt

Un

Unt

Un1

61

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1765200-20 FOGS CONTROL UNIT (AHRU)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

62

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2ATTITUDE & HEADING REFERENCE UNIT, CN-1716/A (FOGS)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

63

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY 70600-01213-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

64

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER




5/6Report Date: 16-Sep-2016AREA NAMEMODELSERIAL NUMBER

SECTION I COCKPITSES BEST7923340 UH-60A

NAME OR PIDNUMBER DATE

db c

DATE NUMBER RANKRANK NAME OR PID

CHECK CHECK

ba ad

5. VERIFICATION

c

CB9023641 CIV 15-Sep-2016

b. LOCATION/REMARKSCHECK NO.

6. LOCATION OR REMARKS

a. ITEM NUMBER

Nomenclature

GYRO, DIRECTIONAL - CN-998/ASN-43

1 NOT INSTALLED ON ACFT3

SIGNAL DATA CONVERTER -CV-3338A/ASN-128B


RATE GYRO - TRU-2A/A1 NOT INSTALLED ON ACFT14

RECEIVER RADAR - RT-1193/ASN-128


FIRST AID KIT - 6545-00-919-6650

1 NOT INSTALLED ON ACFT IN COCKPIT SECTION.24

FIRE EXTINGUISHER - FR23-4-11848

1 NOT INSTALLED ON ACFT IN COCKPIT SECTION.25

CONTROL - C-10604(V)6/ARN-184


COMPUTER DISPLAY UNIT -CP-1252C/ASN-128B


COMPASS SET CONTROLLER- C-8021E/ASN-75


AHRU MOUNTING PLATEFOGS


REVERSE OF DA FORM 2408-17 E, NOV 91


SECTION I COCKPITSES BEST7923340 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

CB9023641 CIV 15-Sep-2016

765200-20 FOGS CONTROLUNIT (AHRU)


ATTITUDE & HEADINGREFERENCE UNIT, CN-1716/A(FOGS)


RATE GYRO ASSEMBLY 70600-01213-041



SECTION II CABINSES BEST


7923340 UH-60A



1CARGO HOOK, FE-7590-145 70800-02503-111

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MARKER BEACON ANTENNA - 70600-02011-103

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-105

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRST AID KIT - 6545-00919-6650

Unt

UUUUUUnt

Unt

Un

Unt

Un3

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2FIRE EXTINGUISHER - FR23-4-11848

Unt

UUUUUUnt

Unt

Un

Unt

Un2

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRASH AXE - 56D6221

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HAND SET - H-250/U

Unt

UUUUUUnt

Unt

Un

Unt

Un1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SLAB BATTERY -D8565/11-1

Unt

UUUUUUnt

Unt

Un

Unt

Un1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3INTERPHONE CONTROL - C6533/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un3

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ADAPTER FUEL DRAIN - 70307-03018-102

Unt

UUUUUUnt

Unt

Un

Unt

Un1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4LOCK ASSY BLADE TIEDOWN - 70700-20369-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2PLUG ASSY INTAKE - HIRSS SUPP - 70700-20515-041/042

Unt

UUUUUUnt

Unt

Un

Unt

Un2

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2PLUG ASSY EXHAUST - HIRSS - 70700-20515-043

Unt

UUUUUUnt

Unt

Un

Unt

Un0

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PLUG ASSY APU EXHAUST - 70700-20509-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






7923340 UH-60A



1COVER ASSY OIL COOLER - 70700-20511-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BLADE FOLD SET - 70700-20412-011

Unt

UUUUUUnt

Unt

Un

Unt

Un1

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER PITOT TUBE - 70700-20460-041

Unt

UUUUUUnt

Unt

Un

Unt

Un2

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


7TROOP SEATS - 70500-02151-045

Unt

UUUUUUnt

Unt

Un

Unt

Un7

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3TROOP SEATS - 70500-02151-047

Unt

UUUUUUnt

Unt

Un

Unt

Un3

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


10RESTRAINT SYSTEM - 70500-02153-103

Unt

UUUUUUnt

Unt

Un

Unt

Un10

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GUNNER SEAT - 70500-02152-047

Unt

UUUUUUnt

Unt

Un

Unt

Un1

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GUNNER SEAT - 70500-02152-048

Unt

UUUUUUnt

Unt

Un

Unt

Un1

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2RESTRAINT SYSTEM - 70500-02156-102

Unt

UUUUUUnt

Unt

Un

Unt

Un2

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ICS WALK-AROUND CORD - 70602-02016-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PORTABLE INSP. FLOOD LIGHT - 15-0366-1

Unt

UUUUUUnt

Unt

Un

Unt

Un0

29

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HYD. PUMP HANDLE - 15400-50126

Unt

UUUUUUnt

Unt

Un

Unt

Un1

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRING KEY - 70550-03101-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

31

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2EQUIPMENT LOGBOOK - MIL-D-43064

Unt

UUUUUUnt

Unt

Un

Unt

Un0

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1WEIGHT AND BALANCE HANDBOOK - TM 55-1500-342-23

Unt

UUUUUUnt

Unt

Un

Unt

Un1

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






7923340 UH-60A



1ELECTRONIC SEQUENCE UNIT - 163290-100-E

Unt

UUUUUUnt

Unt

Un

Unt

Un1

52

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION II CABINSES BEST7923340 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

CB9023641 CIV 15-Sep-2016



a. ITEM NUMBER

Nomenclature

FIRST AID KIT - 6545-00919-6650

1 INSTALLED ON ACFT5

LOCK ASSY BLADE TIEDOWN- 70700-20369-041


PLUG ASSY EXHAUST - HIRSS- 70700-20515-043


COVER ASSY OIL COOLER -70700-20511-041


PORTABLE INSP. FLOODLIGHT - 15-0366-1


EQUIPMENT LOGBOOK - MIL-D-43064



SECTION III TRANSITION SECTIONSES BEST


7923340 UH-60A



1ANTENNA LOOP - AS-2108A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2IFF ANTENNA - 70600-02010-103

Unt

UUUUUUnt

Unt

Un

Unt

Un2

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF/AM ANTENNA - 70600-03002-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PUMP FUEL SAMPLER - 82829/4P156-3

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPENSATOR MAGNETIC FLUX - CN-405/ASN

Unt

UUUUUUnt

Unt

Un

Unt

Un1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS TRANSMITTER - T-611/ASN-43

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS ANTENNA - 22433-40

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF AMPLIFIER - AM-7531/URC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA. GPS (BFT) S67-1575-863

Unt

UUUUUUnt

Unt

Un

Unt

Un1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA, L-BAND (BFT) S65-8282-301

Unt

UUUUUUnt

Unt

Un

Unt

Un1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT, IFM AMPLIFIER-MT-6592/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un1

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3933/ARN-149(V)1, ANTENNA, LOOP

Unt

UUUUUUnt

Unt

Un

Unt

Un0

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP COMMANDER ANTENNA (CMWS ONLY)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IVHMU (CBM MONITOR SYSTEM)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

55

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION III TRANSITION SECTIONSES BEST7923340 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

CB9023641 CIV 15-Sep-2016



a. ITEM NUMBER

Nomenclature

HF AMPLIFIER - AM-7531/URC1 ACFT ENTERED IN TO BEST PROGRAM8

AS-3933/ARN-149(V)1,ANTENNA, LOOP

1 ACFT ENTERED IN TO BEST PROGRAM49

IVHMU (CBM MONITORSYSTEM)



SECTION III TRANSITION SECTIONSES BEST


7923340 UH-60A



1ANTENNA LOOP - AS-2108A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2IFF ANTENNA - 70600-02010-103

Unt

UUUUUUnt

Unt

Un

Unt

Un2

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF/AM ANTENNA - 70600-03002-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PUMP FUEL SAMPLER - 82829/4P156-3

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPENSATOR MAGNETIC FLUX - CN-405/ASN

Unt

UUUUUUnt

Unt

Un

Unt

Un1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS TRANSMITTER - T-611/ASN-43

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS ANTENNA - 22433-40

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF AMPLIFIER - AM-7531/URC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA. GPS (BFT) S67-1575-863

Unt

UUUUUUnt

Unt

Un

Unt

Un1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA, L-BAND (BFT) S65-8282-301

Unt

UUUUUUnt

Unt

Un

Unt

Un1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT, IFM AMPLIFIER-MT-6592/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un1

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3933/ARN-149(V)1, ANTENNA, LOOP

Unt

UUUUUUnt

Unt

Un

Unt

Un0

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP COMMANDER ANTENNA (CMWS ONLY)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IVHMU (CBM MONITOR SYSTEM)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

55

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION III TRANSITION SECTIONSES BEST7923340 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

CB9023641 CIV 15-Sep-2016



a. ITEM NUMBER

Nomenclature

HF AMPLIFIER - AM-7531/URC1 ACFT ENTERED IN TO BEST PROGRAM8

AS-3933/ARN-149(V)1,ANTENNA, LOOP


IVHMU (CBM MONITORSYSTEM)



SECTION IV TAIL CONESES BEST


7923340 UH-60A



2VOR/LOC ANTENNA - 70600-05002-101

Unt

UUUUUUnt

Unt

Un

Unt

Un2

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IFM AMPLIFIER - AM-7189A/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF ANTENNA - 4700516-30

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION IV TAIL CONESES BEST7923340 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

CB9023641 CIV 15-Sep-2016



a. ITEM NUMBER

Nomenclature

IFM AMPLIFIER - AM-7189A/ARC



SECTION V TAIL ROTOR PYLONSES BEST


7923340 UH-60A



1CU-2457/ARC(405-11-1), VHF-FM #1 COUPLER ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un0

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM10-267, VHF-FM #2 (LEADING EDGE) ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM10-3230, VHF-FM TROOP COMMANDER ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un0

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION V TAIL ROTOR PYLONSES BEST7923340 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

CB9023641 CIV 15-Sep-2016



a. ITEM NUMBER

Nomenclature

CU-2457/ARC(405-11-1), VHF-FM #1 COUPLER ANTENNA


FM10-3230, VHF-FM TROOPCOMMANDER ANTENNA



SECTION V TAIL ROTOR PYLONSES BEST


7923340 UH-60A



1CU-2457/ARC(405-11-1), VHF-FM #1 COUPLER ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un0

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM10-267, VHF-FM #2 (LEADING EDGE) ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM10-3230, VHF-FM TROOP COMMANDER ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un0

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION V TAIL ROTOR PYLONSES BEST7923340 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

CB9023641 CIV 15-Sep-2016



a. ITEM NUMBER

Nomenclature

CU-2457/ARC(405-11-1), VHF-FM #1 COUPLER ANTENNA


FM10-3230, VHF-FM TROOPCOMMANDER ANTENNA



PIDMWODATE HRS



SERVO ASSY, TAIL ROTOR 7923340B300--002111. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


13-Oct-2010 OT

BS08480414-Oct-2010

0.5DET 1 B CO777TH AVN

COMPLIED WITH REQUIREMENTSOF H-60-11-ASAM-12.

H-60-11-ASAM-02MWO:

Priority Mnt Level



PIDMWODATE HRS



SWASHPLATE ASSY 7923340015152-20031. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


12-Jun-2006 OM

QC00000012-Jun-2006

1DET 1 B CO777TH ASB

ALL H-60 SERIES AIRCRAFT,SWASHPLATE DUPLEX BEARING


Priority Mnt Level



16-Sep-2016

T700-GE-700ENGINE ASSY, TURBINE

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

GE-E-306740

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

10-Sep-2014 7923340 POST PMI1740 103 103 198.4195355 851


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

16-Sep-2016

T700-GE-700ENGINE ASSY, TURBINE

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

GE-E-307131

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

10-Sep-2014 7923340 POST PMI1740 100 103 0.9797192313 845


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

PIDMWODATE HRS



TAIL ROTOR GEARBOX ASSY 7923340A006-036241. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 FM

WA75458321-Mar-2013


ONE-TIME INSPECTION OF SUSPECTSERIAL NUMBERED COMPONENTSFOR PLASTIC MEDIA BLAST (PMB)AND OXIDE FLAKE RESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR PITCH CHANGE SHAFT 7923340D233-001591. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


24-Jan-2014 FT

JA17932524-Jan-2014

1W3VA7GALL UH-60 SERIES AIRCRAFT,PERFORM ONE TIME INSPECTIONOF THE TAIL ROTOR PITCH CHANGESHAFT ASSEMBLY (SERVOCOUPLING ASSEMBLY)

H-60-14-SOF-02MWO:

Priority Mnt Level



UNIT UNIQUE INVENTORY ITEMSSES BEST


7923340 UH-60A



1BFT PALLET ASSEMBLY (040537-001)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

66

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





UNIT UNIQUE INVENTORY ITEMSSES BEST7923340 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

CB9023641 CIV 15-Sep-2016



a. ITEM NUMBER

Nomenclature

BFT PALLET ASSEMBLY(040537-001)



DA Form 2408-5 - Equipment Modification Record

Documents