da form 2408-5 - equipment modification record€¦ · mwo:1-1520-237-50-bft2 prioritymnt level...

PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN

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

8223745UH-60AHELICOPTER, UTILITY

3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE

Report Date: of 826-Jan-2017

DN26-Mar-1984

DYNALECTRON(GR2306)

501-Feb-1989

INCORPORATION OF BLADE DEICEFAULT MONITOR FIXED PROVISIONS

55-1520-237-50-2MWO:

Mnt LevelPriority

DN15-Nov-1990

DYNALECTRON(GR2306)

201-Jul-1991

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

1-1520-237-50-61MWO:

Mnt LevelPriority

DR02-Aug-2001

DYNCORP-OLR(AB6076)

401-Nov-2001

INSTALLATION OF THE AN/ARN-123VOR/ILS RECEIVER IN UH-60 SERIESHELICOPTER RECEIVER (NSN: 5821-01-478-6865) (EIC: N/A)

1-1520-237-50-83MWO:

Mnt LevelPriority

DR30-Apr-1991

DYNALECTRON(GR2306)

10502-Apr-1993

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

1-1520-237-50-63MWO:

Mnt LevelPriority

OE30-Apr-1986

HQ 421STMED(GR2306)

1202-May-1986

RELOCATION OF THE AUTOMATICFLIGHT CONTROL SYSTEM (AFCS)PANEL

55-1520-237-20-1MWO:

Mnt LevelPriority

DN15-Jan-1991

DYNALECTRON(GR2306)

803-Jul-1991

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

55-1520-237-50-58MWO:

Mnt LevelPriority

OM24-Sep-2002

236TH MEDCO(RB6944)

0.504-Oct-2002

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

UH-60-02-ASAM-11MWO:

Mnt LevelPriority

DN05-Oct-1994

DYNCORP-E(AJ1671)

15006-Aug-1997

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

1-1520-237-50-62MWO:

Mnt LevelPriority

FR25-Jun-2004

D CO 3-82 AVNREGT

1606-Oct-2007

INSTALLATION INSTRUCTIONS FORTHE MAVEN OPTION II CABIN HEATERSYSTEM

1-1520-237-50-36MWO:

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






DN23-Jan-1989

DYNALECTRON(GR2306)

4207-Apr-1989

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

55-1520-237-50-44MWO:

Mnt LevelPriority

DN24-Mar-1988

DYNALECTRON(GR2306)

65.508-Aug-1988

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

55-1520-237-50-47MWO:

Mnt LevelPriority

DN23-Apr-2004

DYNCORP-OLR(JB9689)

412-Dec-2005

INSTALLATION OF BALLISTICPROTECTION SYSTEM

1-1520-237-50-BPSMWO:

Mnt LevelPriority

DN01-Sep-1986

DYNALECTRON(GR2306)

108412-Mar-1987

INCORPORATION OF ANVISCOMPATIBLE LIGHTING SYSTEM

55-1520-237-50-20MWO:

Mnt LevelPriority

DN01-Aug-1991

DYNALECTRON(GR2306)

313-Feb-1991

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

DR15-Jul-1985

DYNALECTRON(GR2306)

4014-Apr-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

DU13-Jun-1985

DYNALECTRON(GR2306)

814-Nov-1985

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

55-1520-237-50-31MWO:

Mnt LevelPriority

DN15-Dec-1984

DYNALECTRON(GR2306)

215-Apr-1985

MODIFICATION OF MAIN ROTORSLIDING COVER (UH-60AHELICOPTERS)

55-1520-237-50-32MWO:

Mnt LevelPriority

DR25-Apr-2006

FORT BRAGGOLR/DS2

5815-Aug-2008

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE AIRWARRIOR MICROCLIMATE COOLINGSYSTEM AND THE MASK BLOWERWIRING ASSEMBLY ON THE UH-60A/LAIRCRAFT

01-1520-237-50-85MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN07-Mar-1995

DYNCORP-E(AJ1671)

6115-Jul-1997

INCORPORATION OF IMPROVEDAIRSPEED SYSTEM (UH-60AHELICOPTERS)

1-1520-237-50-22MWO:

Mnt LevelPriority

DN28-Oct-1996

DYNCORP-E(AJ1671)

615-Jul-1997

MODIFICATION OF CHIP DETECTORWIRING FOR UH-60A HELICOPTERS

1-1520-237-50-26MWO:

Mnt LevelPriority

DN31-Oct-1996

DYNCORP-E(AJ1671)

3515-Jul-1997

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

1-1520-237-50-74MWO:

Mnt LevelPriority

DN01-May-1994

DYNCORP-E(AJ1671)

12815-Jul-1997

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

1-1520-237-50-66MWO:

Mnt LevelPriority

DN01-Feb-1993

DYNCORP-E(AJ1671)

40015-Jul-1997

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

DN29-Jul-1994

DYNCORP-E(AJ1671)

18615-Jul-1997

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

1-1520-237-50-70MWO:

Mnt LevelPriority

DR25-Apr-2006

RASM-E AFMA L-3COMMUNICATIONS

4016-Dec-2011

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)

MWO 1-1520-237-50-84MWO:

Mnt LevelPriority

KO07-Nov-2008

RASM-E AFMAL3COMMUNICATIONS

10016-Dec-2011

INSTALLATION OF THE COUNTERMISSLE WARNING SYSTEM (CMWS)P3I

MWO-1-1520-237-50-97MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN30-Jun-2004

ALMB/DS2 7416-Jun-2008

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

1-1520-237-50-92MWO:

Mnt LevelPriority

DR27-Apr-2007

DS2/OLR 117-Dec-2008

AIRWORTHINESS RELEASE (AWR)FOR UH-60A/L HELICOTPERS WITHINTEGRATED VEHICLE HEALTHMANAGEMENT SYSTEM (IVHMS)HEALTH USAGE MANAGEMENTSYSTEM (HUMS) INSTALLED

AWR 1346 R8MWO:

Mnt LevelPriority

DT19-Dec-2007

DS2/OLR 100017-Dec-2008

INTEGRATED VEHICAL HEALTHMAINTENANCE (IVHMS)

SOW 1-1520-237-50-IVHMSMWO:

Mnt LevelPriority

DM22-Feb-1991

DYNCORP-E(AJ1671)

583.617-Feb-1994

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

1-1520-237-50-59MWO:

Mnt LevelPriority

DN09-Jun-1988

DYNALECTRON(GR2306)

9518-Mar-1991

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

55-1520-237-50-42MWO:

Mnt LevelPriority

DM18-Apr-1988

DYNALECTRON(GR2306)

2.519-Jul-1988

INSTALLATION OF IMPROVEDCARTRIDGE ACTUATED DEVICE

55-4030-237-50-1MWO:

Mnt LevelPriority

DN26-Mar-2009

SES-I, HSV, AL 31520-Feb-2009

CIV OLIVER,DANNY

TB 1-1520-237-XX-XXX (DRAFT)INSTALLATION OF FORWARDLOOKING INFRARED (FLIR) SPONSONMOUNT

TB 1-1520-237-XX-XXXMWO:

Mnt LevelPriority

FU05-Sep-2003

DYNCORP-OLR(DH6392)

5021-Mar-2006

INSTALLATION OF DUAL AN/PRC-117FSATCOM RADIOS

1-1520-237-50-SATCOMMWO:

Mnt LevelPriority

DU31-May-1995

DYNCORP-E(AJ1671)

2422-Jun-1996

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

1-1520-237-50-73MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN08-Mar-1984

SIKORSKY(GR2306)

222-Mar-1984

MAIN ROTOR DAMPER CABLE CYCLICHEADREST KIT

ECP 223MWO:

Mnt LevelPriority

DN08-Mar-1984

SIKORSKY(GR2306)

122-Mar-1984

MIXER BEARING RETENTION ANDSHAFT KIT

ECP 239MWO:

Mnt LevelPriority

OM16-May-2000

236TH MEDCO(GR2306)

223-May-2000

ALL H-60 SERIES AIRCRAFT, TAILNUMBERS 77-22715 THROUGH 90-26367, INSPECTION OF FIREEXTINGUISHER WIRING


Mnt LevelPriority

DR06-Aug-2004

DYNCORP-OLR(JB9689)

5023-Nov-2005

INSTALLATION OF AUXILIARY POWERUNIT (APU) INLET BARRIER (IBF)

AWR 1097 R3MWO:

Mnt LevelPriority

DR22-Sep-2005

DYNCORP-OLR(JB9689)

3923-Nov-2005

INSTALLATION OF ELECTRONIC DATAMANAGEMENT (EDM) SYSTEM FORBLUE FORCE TRACKING

RSN LSF01106MWO:

Mnt LevelPriority

DR21-Apr-2006

DYNCORP-OLR(JB9689)

90023-Nov-2005

INSTALLATION OF COMMON MISSILEWARNING SYSTEM (CMWS) ANDIMPROVED COUNTERMEASURESDISPENSER SYSTEM (ICDS)

1-1520-237-50-CMWSMWO:

Mnt LevelPriority

DM08-Feb-2005

DYNCORP-OLR(JB9689)

36123-Nov-2005

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

DM08-Feb-2005

DYNCORP-OLR(JB9689)

26023-Nov-2005

INSTALLATION OF BLUE FORCETRACKER REVISION 2

1-1520-237-50-BFT2MWO:

Mnt LevelPriority

DM01-Sep-1991

DYNALECTRON(GR2306)

224-Mar-1993

IMPROVED ENGINE COWLINGRELEASE HANDLE ASSEMBLY

1-1520-237-50-64MWO:

Mnt LevelPriority

DU10-Aug-1987

DYNALECTRON(GR2306)

624-Sep-1987

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

55-1520-237-50-46MWO:

Mnt LevelPriority



PIDMWODATE HRS






FR20-Mar-2006

ALMB/DS2 FTBRAGG NC28310

2.525-Apr-2008

INSTALLATION OF UH-60, EH-60, ANDHH-60 SERIES HELICOPTERS FORBODY PLUG CORROSIONINSPECTION.

1-1520-237-23-10MWO:

Mnt LevelPriority

FR20-May-2006

ALMB/DS2 FTBRAGG NC28310

525-Apr-2008

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

1-1520-237-23-9MWO:

Mnt LevelPriority

DR13-Apr-2001

DYNCORP-OLR(RR2743)

8025-Jul-2003

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

DR11-Aug-2000

DYNCORP-E(JH4279)

325-May-1999

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

1-1520-237-50-79MWO:

Mnt LevelPriority

FR18-Nov-2009

YULISTAAVIATION, INC.

426-Jun-2012

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF M4 GUNMOUNT ON THE UH-60A/L/M MODELBROOM CLOSET

1-1520-237-20-95MWO:

Mnt LevelPriority

DR29-Nov-2010

YULISTAAVIATION, INC.

1426-Jun-2012

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE M4 GUNMOUNT OF THE UH-60A/L MODELVERITCAL MOUNTS

1-1520-237-50-106MWO:

Mnt LevelPriority

DN30-Apr-1997

DYNCORP-OLR(SH6234)

5227-Feb-2001

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

1-1520-237-50-56MWO:

Mnt LevelPriority

DR08-Nov-1996

DYNCORP-OLR(SH6234)

17827-Feb-2001

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

1-1520-237-50-75MWO:

Mnt LevelPriority



PIDMWODATE HRS






DR04-Jun-2001

DYNCORP-OLR(SH6234)

30027-Feb-2001

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

1-1520-237-50-76MWO:

Mnt LevelPriority

DN15-Jan-1989

DYNALECTRON(GR2306)

1227-Oct-1989

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

1-5945-237-50-1MWO:

Mnt LevelPriority

DN17-Jan-1989

DYNALECTRON(GR2306)

227-Oct-1989

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

55-1520-237-50-52MWO:

Mnt LevelPriority

DR18-Jan-2011

AFMA RASM-P /PAE TECHNICALSERVICES

11028-OCT-2015

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THEENCRYPTED AIRCRAFT WIRELESSINTERCOM SYSTEM (EAWIS) ON THEUH-60 A/L AIRCRAFT.

MWO 1-1520-237-50-102MWO:

Mnt LevelPriority

DR15-Nov-2000

DYNCORP-OLR(GR7656)

429-Dec-2000

OF THE AN/ARN-147 VOR/ILSRECEIVER/ELECTRONIC MOUNTINGBASE IN UH-60 SERIES HELICOPTERRECEIVER (NSN: 5826-01-444-0314)(EIC: N/A) MOUNTING BASE (NSN:5975-01-465-1268) (EIC: N/A)

1-1520-237-50-81MWO:

Mnt LevelPriority

DR25-Jan-2007

D CO 3-82ND 629-Jan-2009

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

FR23-Aug-2013

PAE TECHNICALSERVICES(JBLM WA 98433)

70029-JAN-2016

MODIFICATION INSTRUCTIONS FORINSTALLATION OF DUAL CIVIL BANDRADIO IN THE UTILITY HELICOPTERUH-60A/L

MWO 1-1520-237-50-111MWO:

Mnt LevelPriority



PIDMWODATE HRS






DM31-May-1985

H 421STMED(GR2306)

429-Jun-1985

PRIMARY ROTOR SPINDLE ASSEMBLYMODIFICATION

55-1615-237-50-1MWO:

Mnt LevelPriority

DM15-Nov-1989

DYNALECTRON(GR2306)

1930-Apr-1990

MODIFICATION OF DOWEL PINRETENTION MAIN GEARBOX

55-1520-237-50-43MWO:

Mnt LevelPriority

DN01-Oct-1990

DYNALECTRON(GR2306)

1930-Apr-1990

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

55-1520-237-50-39MWO:

Mnt LevelPriority

DU30-Mar-1987

DYNALECTRON(GR2306)

430-Mar-1987

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

55-1520-237-50-36MWO:

Mnt LevelPriority

DM10-Oct-2002

159TH MEDCO(DW1719)

3031-Jul-2006

INTERIM STATEMENT OFAIRWORTHINESS QUALIFICATIONS(ISAQ) FOR BREEZE-EASTERNRESCUE HOIST MODEL NUMBERHS29900-30-1, INSTALLATION OF UH-60L SEARCH AND RESCUE (SAR), UH-60Q/HH-60L MEDEVAC, AND UH-60A/LAIRCRAFT

ISAQ 103MWO:

Mnt LevelPriority



NUMBERLOCATIONPIDENTRYORGANIZATION

8.7.DATE

6.REMARKS

4. 5.

UH-60A 8223745HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL

Report Date: Page 1 of 5722-Feb-2017

SIKORSKY AIRCRAFTAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG 70400-00003REV C SYSTEMS CONTROL HAVE BEENBIASED IN ACCORD A. AFT CONTROL SERVOINPUT ROD P/N 70400-02258-045 HAS BEENSHORTEN 1/4 TURN.B. LATERAL CONTROLSERVO INPUT ROD P/N 70400-02258-046 HASBEEN LENGTHEN 1/2 TURN.C. FORWARDCONTROL SERVO INPUT ROD P/N 70400-02258-047 HAS BEEN SHORTEN 1/2 TURN. NOTEWHEN AIRCRAFT RIGGING IS BIASEDRIGGING PIN HOLES ARE TEMPORARILYLOST AT THE ABOVE 3 POINTS (NO PID)

30-Jun-1983 1

STRATFORD, CT

QC000000

SIKORSKY AIRCRAFTUH-60-A-82-04 (TB 55-1520-237-30-1) ONE TIMEINSPECTION FOR UH-60A INLET DUCT ASSYP/N 70302-10100 ALIGNMENT PIN BRACKETP/N 70203-04301-044/-045 COMPLIED WITH (NOPID)

20-Jul-1983 1

STRATFORD, CT

QC000000

SIKORSKY AIRCRAFTUH-60-A-82-16 ONE TIME INSPECTION OFFLIGHT CONTROL MIXER LIMITER COMPLIEDWITH (NO PID)

22-Jul-1983 1

STRATFORD, CT

QC000000

B CO 394TH TRANS BNSOF UH-60-83-09 ONE TIME INSP OF STABAMSP COMPLETED (NO PID)

11-Oct-1983 1

APO NY 09061

QC000000

B CO 394TH TRANS BNSOF UH-60-83-10 ONE TIME INSP OFCOLLECTIVE BIAS TUBE ASSY ROD ENDBOLT WASHER, IAW TB 55-1520-237-20-44COMPLIED WITH 22.0 ACFT HRS (NO PID)

07-Nov-1983 1

APO NY 09061

QC000000

B CO 394TH TRANS BNSOF UH-60-83-12 ONE TIME INSP OF TAILROTOR SERVO INPUT LINKAGE IAW TB 55-1520-237-20-47 COMPLIED WITH AT 22.0AIRCRAFT HOURS (NO PID)

21-Nov-1983 1

APO NY 09061

QC000000

B CO 394TH TRANS BNSOF UH-60-83-11 INSP OF ACCESSORYMODULE OIL RETURN SCREEN IAW TB 55-1520-237-20-47 COMPLIED WITH AT 22.0 ACFTHRS (NO PID)

29-Nov-1983 1

APO NY 09061

QC000000

B CO 394TH TRANS BNSOF UH-60-84-01 ONE TIME INSP OF XMSNMAST FOR FLAWS COMPLETED THIS DATE(NO PID)

30-Jan-1984 1

APO NY 09061

QC000000

TSARCOM OCM/ACEOCM/ACE PERFORMED AT 226 A/C HRS ATNELLIGEN GER, BY ACE TEAM MEMBER (NOPID)

16-Feb-1984 1

ST LOUIS, MO

QC000000

B CO 394TH TRANS BNMAIN ROTOR DAMPER CABLE (ECP 223)INSTALLED ON ACFT BY SIKORSKY TEAM AT31.2 ACFT HRS (NO PID)

22-Mar-1984 1

APO NYY 09061

QC000000

B CO 394TH TRANS BNMIXER BEARING RETENTION (ECP 239)INSTALLED ON ACFT BY SIKORSKY TEAM AT31.2 ACFT HRS (NO PID)

22-Mar-1984 2

APO NYY 09061

QC000000

B CO 394TH TRANS BNSOF MESSAGE UH-60A-84-02 ONE TIME INSPWIRE ROUTING BETWEEN THE #1 AND #2JUNCTION BOXES COMPLETED WITH THISDATE (NO PID)

27-Mar-1984 1

APO NYY 09061

QC000000

B CO 394TH TRANS BNSOF MESSAGE UH-60-84-06 ONE TIME INSP OFGEAR BOX OIL LEVELS COMPLETED THISDATE (NO PID)

10-May-1984 1

APO NYY 09061

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 394TH TRANS BNONE TIME INSP OF ENGINE OUTPUT SHAFTSFOR -06 BOLTS COMPLETED THIS DATE, THISACFT HAS -08 BOLTS INSTALLED AT 41.1ACFT HRS (NO PID)

19-May-1984 1

APO NYY 09061

QC000000

B CO 394TH TRANS BNSOF UH-60-84-09 REVISION OF UH-60-84-07LISTED ABOVE COMPLETED THIS DATE (NOPID)

21-May-1984 1

APO NYY 09061

QC000000

421ST MED COONE TIME INSP OF CARGO HOOK SQUIB ASSYCOMPLETED IAW SOF UH-60A-84-08 DTD MAY84 (NO PID)

25-Jun-1984 1

APO NY 09061

QC000000

421ST MED COONE TIME INSP OF LONGITUDINAL &LATERAL LINK ASSY COMPLETED IAW SOFUH-60A-84-11 DTD JUL 84 (NO PID)

10-Jul-1984 1

APO NY 09061

QC000000

421ST MED COONE TIME INSP OF M/R SPINDLE ASSY PITCHCONTROL ARM ATTACHING BOLTS, IAW SOFMSG UH-60A-84-21 TWX#301535Z JUL 84 (NOPID)

31-Jul-1984 1

APO NY 09061

QC000000

421ST MED COONE TIME INSP AND PERMANENT INSP OFTAIL CONE CANTED HINGE BULKHEADRADIUS BLOCKS P/N 70215-85001-108/-105/-110/-111, IAW SOF UH-60A-84-10 TWX# 231820ZAUG 84 (NO PID)

07-Sep-1984 1

APO NY 09061

QC000000

421ST MED COONE TIME INSP OF TAIL ROTOR CONTROLCABLES AND PULLEY GUARDS COMPLETEDIAW SOF MSG UH-60A-84-14 TWX#310600ZOCT 84, CABLE TENSION 145 AT 19C (NO PID)

06-Nov-1984 1

APO NY 09061

QC000000

AVSCOM OCM SECOCM/ACE PERFORMED AT 102 A/C HRS, ATNELLIGEN, GER (NO PID)

26-Nov-1984 1

ST LOUIS MO

QC000000

421ST MED COREPLACED TURNBUCKLES MS21251 WITHTURNBUCKLES MS2125B5L1981 IAW SOF UH-60A-84-13 DTD 310730Z OCT 84 TEMP +14CTENSION 125 LBS (NO PID)

03-Dec-1984 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-84-17 281230Z DEC 84 ONETIME INSP OF MAIN GEAR BOX DOWEL PINS(5 EA) COMPLIED WITH 108.9 ACFT HRS (NOPID)

08-Jan-1985 1

APO NY 09061

QC000000

AVSCOM OCM SECPCM/ACE PERFORMED AT 221 A/C HRS (?) ATNELLIGEN, GER (NO PID)

15-Jan-1985 1

ST LOUIS MO

QC000000

421ST MED COSOF MSG UH-60A-85-02 270930Z FEB 85 ONETIME INSP AND REMOVAL OF ALLREDTRANSPARTENT ON ALL MAIN ROTORTACHOMETER INDICATORS AT 1131.0 ACFTHRS (NO PID)

05-Mar-1985 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-85-03 281000Z FEB 85 ONETIME INSP OF STABILATOR AMP SN'S AT 131.0ACFT HRS (NO PID)

06-Mar-1985 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-85-06 221400Z MAR 85 ONETIME INSP OF PRIMARY SRVO RETENTIONPLATE MODIFICATION COMPLETED AT 145.1ACFT HRS (NO PID)

03-Apr-1985 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-85-07 060535Z APR 85 ONETIME INSP OF FLIGHT CONTROLSCOMPLETED AT 145.1 ACFT HRS (NO PID)

09-Apr-1985 1

APO NY 09061

QC000000



8.7.DATE

6.REMARKS

4. 5.



421ST MED COSOF MSG UH-60A-85-10 ONE TIME INSP OFCOMPLETED ACFT COMPLETED AT 153.1ACFT HRS (NO PID)

03-May-1985 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-85-14 ONE TIME INSP OFMAIN ROTOR SHAFT HISTORICAL DATACOMPLETED AT 153.1 ACFT HRS (TB 55-1520-237-20-68) (NO PID)

03-Jun-1985 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-85-15 ONE TIME INSP OFMAIN ROTOR HUB HISTORICAL DATACOMPLETED AT 153.1 ACFT HRS (TB 55-1520-237-20-69) (NO PID)

03-Jun-1985 2

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-85-23 ONE TIME INSP OF T/RDRIVE SHAFT VISCOUS DAMPER BEARINGSCOMPLETED AT 153.1 ACFT HRS (NO PID)

29-Jul-1985 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-85-24 SUSPECT VISCOUSDAMPER BEARING RELEASED FOR FLIGHTIAW THIS SOF MSG 2406-16 NOT INITIATEDALL BEARINGS ONLY HAVE LOT NUMBERSCOMPLETED AT 153.1 ACFT HRS (NO PID)

02-Aug-1985 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-85-18 REQUIREMENTS FORUNGROUNDING (TB 55-1520-237-20-70) (MWO55-1615-237-50-1) COMPLETED AT 153.1 ACFTHRS (NO PID)

24-Oct-1985 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-85-25 (TB 55-1520-237-20-73)FOR TORQUE STABILIZATION OF MAINROTOR PITCH HORN ATTACHMENT BOLTSCOMPLETED AT 187.6 ACFT HRS (NO PID)

08-Nov-1985 1

APO NY 09061

QC000000

421ST MED COSOF MSG GEN 85-01 ONE TIME INSP OFMS25224 SERIES SWITCH GUARD AND TWOPOSITION SWITCHES FOR PROPERDEACTIVATION OF SWITCHES COMPLETEDAT 161.5 ACFT HRS (NO PID)

08-Nov-1985 2

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-01 (TB 55-1520-237-231)DTG 222005Z FEB 86 REPLACEMENT OF TAILROTOR DRIVE SHAFT BEARINGS PN SB 1138-101 COMPLETED AT 268.2 ACFT HRS (NO PID)

10-Mar-1986 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-03 (TB 55-1520-237-20-74)DTG 24195Z FEB 86 REVISION ONE TIMEINSPECTION OF TAIL ROTOR DRIVE SHAFTNUTS COMPLETED AT 268.2 ACFT HRS (NOPID)

10-Mar-1986 2

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-04 (TB 55-1520-237-23-01)DTG 070605Z MAR 86 REVISION TOREPLACEMENT OF TAIL ROTOR DRIVE SHAFTBEARINGS SB1138-101 COMPLETED AT 268.2ACFT HRS (NO PID)

10-Mar-1986 3

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-05 DTG 1301332Z MAR 86IMMDIATE GROUNDING OF UH-60A SERIESCOMPLETED AT 268.2 ACFT HRS (NO PID)

14-Mar-1986 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-06 (MWO 55-1520-237-55-2) DTG 181105Z APR 86 STABILATORAUTOMATIC FIGHT CONTROL SYSTEMCONTROL PANEL RETROFIT COMPLETED AT268.2 ACFT HRS (NO PID)

20-Mar-1986 1

APO NY 09061

QC000000



8.7.DATE

6.REMARKS

4. 5.



421ST MED COSOF MSG UH-60A-86-02 DTG 222015Z FEB 86TB 55-1520-237-20-74 TORQUE CHECK OF T/RD/S SELF LOCKING NUTS PN SS5086-C06S,SS5086-04, SS5086-05 COMPLETED AT 268.2ACFT HRS (NO PID)

10-Apr-1986 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-07 (MWO 55-1520-237-20-1) TB 55-1520-237-20-15 DTG 30065Z APR 86UNGROUNDING REQUIREMENTS COMPLETEDAT 268.2 ACFT HRS (NO PID)

09-May-1986 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-06 DTG 090805Z MAY 86(TB 55-1520-237-20-77) REPLACEMENT OF UH-60A SERIES ACFT STABILATOR ACTUATORPN 70400-06641-110 COMPLETED AT 391 ACFTHRS (?) (NO PID)

30-May-1986 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-09 DTG 020905Z JUNE 86(TB 55-2840-50-43) ONE TIME INSP OF OILCOOLER ASSEMBLIES AT 269.1 ACFT HRS(NO PID)

03-Jun-1986 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-10 DTG 131935Z JUNE 86(TB 55-1520-237-20-76) ONE TIME STAKING OFBEARING ON YAW LEVER ASSY COMPLETEDAT 308.1 ACFT HRS (?) (NO PID)

07-Aug-1986 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-11 DTG 181040Z JUNE 86REVISION REQUIREMENTS FOR REPORTINGUNGROUNDING OG UH-60A AIRCRAFTCOMLETED AT 308.1 ACFT HS (GM0000)

07-Aug-1986 2

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-12 DTG 011135Z AUG 86TB55-1520-237-20-78 CHANGE OUT OF LISTEDSERIAL NUMBERED YAW AND BOOSTSERVOS COMPLETED AT 308.1 ACFT HRS(GM0000)

07-Aug-1986 3

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-14 DTG 011136Z AUG 86REVISION TO PREVISOUS MESSAGECONCERNING LEVER ASSY COMPLETED AT308.1 ACFT HRS (GM0000)

07-Aug-1986 4

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-13 DTG 011136Z AUG 86REMOVAL OF AN 310-8 NUTS COMPLETED AT308.1 ACFT HRS (GM0000)

13-Aug-1986 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-15 DTG 191705Z AUG 86REVISION TO REMOVAL OF AN 310-8 NUTSCOMPLETED AT 308.1 ACFT HRS (GM0000)

21-Aug-1986 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-16 DTG 150920Z OCT 86REVISION TO ONE TIME STAKING OFBEARINGS ON YAW LEVER ASSEMBLYCOMPLETED AT 308.1 ACFT HRS (GM0000)

22-Oct-1986 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-18 DTG 240636Z OCT 86RESTRICTION FROM REPELLINGOPERATIONS ENTERED ON 2408-13 (GM0000)

28-Oct-1986 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-18 DTG 240636Z OCT 86OPERATIONAL RAPELLING PROHIBITED (NOTAPPLICABLE TO ACFT WITH AEROMEDICALEVACUATION KIT INSTALLED (KD0000)

07-Nov-1986 1

APO NY 09061

QC000000



8.7.DATE

6.REMARKS

4. 5.



421ST MED COSOF MSG UH-60A-86-20 DTG 070710Z NOV 86INSPECTION OF THE FIRST THREE T/RDRIVESHAFT SPLINE COUPLINGS AND XMSNOIL COOLER FAN SPLINES C/W AT 388.0 ACFTHRS (KD0000)

14-Nov-1986 1

APO NY 09061

QC000000

15TH MED DETSOF MSG UH-60A-86-20 DTG 070710Z NOV 86REMOVAL OF MATERIAL FROM UNDER CREWSEATS COMPLIED WITH AT 338.0 ACFT HRS(KD0000)

14-Nov-1986 2

APO NY 09061

QC000000

AVSCOM OCM SECOCM/ACE PERFORMED AT 407.0 A/C HRS ATGRAFENWOEHR,GER BY ACE TEAM MEMBER" E". (FE0000)

09-Dec-1986 1

ST LOUIS, MO

QC000000

15TH MED DETSOF MSG UH-60A-86-21 DATED 011200Z DEC86 ONE TIME INSP OF CREW SEATS FORLONGITUDINAL MOVEMENT OF LOCKPINADJUSTMENT COMPLIED WITH AT 411.1 ACFTHRS (JG0000)

16-Dec-1986 1

APO NY 09114

QC000000

421ST MED COSOF MSG UH-60A-86-22 DATED 180302Z DEC86 REVISION TO SOF MSG UH-6OA-86-17CONTRACTORS INSPECTION OFTRANSMISSION OIL COOLER FAN AND TAILROTOR SHAFT NOT APPLICABLE THIS YEARGROUP ACFT (RH0000)

18-Dec-1986 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-87-01 DATED 130705Z FEB87 (TB 55-1520-237-50-43) ONE TIME TORQUECHECK OF T700 ENGINES FUELDIFFERENTIAL PRESSURE INDICATORCOMPLETED AT 431.5 ACFT HRS (RH0000)

18-Feb-1987 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-87-02 DATED 190705Z FEB87 (TB 55-1520-237-50-44) REVISION TO SOFMSG UH-60A-87-01 CHANGES TB NUMBERNOTED (RH0000)

20-Feb-1987 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-87-03 DATED 140300Z MAR87 (TB 55-1520-237-20-89) ONE TIME ANDRECURRING INSPECTION ON THE FIRSTTHREE TAIL ROTOR DRIVESHAFT SPLINECOUPLINGS, COMPLETED AT 436.6 ACFT HRS(RH0000)

17-Mar-1987 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-87-04 DATED 240705Z MAR87 REVISION TO INSP OF EYEBOLTS AT STA308 COMPLETED AT 439.1 ACFT HRS (RH0000)

28-Mar-1987 1

APO NY 09061

QC000000

421ST MED COSOF MSG GEN 87-01 DTG 281505Z MAR 87MODIFICATION OF NVGS AND SPH4 HELMETSASSIGNED TO UNIT ENTERED ON DA FORM2408-13 AT 439.4 ACFT HRS (RH0000)

31-Mar-1987 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-87-05 DTG 120005Z APR 87STABILATOR OPERATIONAL PROCEDURES:RESTRICTED ACFT TO 3000 FEET AGL AT449.7 ACFT HRS (RH0000)

13-Apr-1987 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-87-06 DTG 040635Z MAY 87(TB 55-1520-237-50-2) ONE TIME ANDRECURRING INSP OF OIL COOLER SPLINESBY DESIGNED INSP TEAMS VERIFIED AT 460.4ACFT HRS (RH0000)

15-May-1987 1

APO NY 09061

QC000000



8.7.DATE

6.REMARKS

4. 5.



421ST MED COSOF MSG UH-60A-87-07 DTG 150205Z MAY 87ONE TIME AND RECURRING IINSP OFLONGITUDINAL AND LATERAL LINKASSEMBLIES EVERY 10 HRS 14 DAYSINTERVALS COMPLETED AT 460.4 ACFT HRS(RH0000)

16-May-1987 1

APO NY 09061

QC000000

AVSCOM/OCM SECOCM/ACE PERFORMED AT 475 ACFT HRS ATNELLIGAN, GER BY ACE TEAM MEMBER "B"(BC0000)

26-Jun-1987 1

ST LOUIS, MO

QC000000

421ST MED COSOF UH-60A-87-08 DTG 010535Z JUL 87 TB 55-1520-237-20-91 INSP AND MARKING OFMIDSECTION BELLCRANK COMPLIED WITH AT477.5 ACFT HRS (RH0000)

06-Jul-1987 1

APO NY 09061

QC000000

421ST MED COSOF GEN 87-02 DTG 300515Z JUN 87 TB 55-1500-200-20-25 RECORDS INSP FORNONCONFORMING FLIGHT SAFETY CRITICALCOMPONENTS COMPLIED WITH THIS DATE477.2 ACFT HRS (RH0000)

07-Jul-1987 1

APO NY 09061

QC000000

421ST MED COSOF UH-60A-87-10 DTG 132120Z OCT 87 TB 55-1520-237-20-32 ONE TIME INSP OF INPUTFLANGE ASSYS COMPLETED AT 500.0 ACFTHRS (RH0000)

16-Oct-1987 1

APO NY 09061

QC000000

421ST MED COSOF MSG UH-60A-86-17 DTG 220806Z OCT 86ONE TIME INSP OF MAIN MODULE TAKE OFFFLANGE AND OIL COOLER FAN SPLINES ANDTAIL ROTOR ALIGNMENT CHECK, NOTREQUIRED THIS YEAR GROUP ACFT (RH0000)

20-Oct-1987 1

APO NY 09061

QC000000

421ST MED COSOF UH-60-87-KSOF-02 TB 55-1520-237-20-93DTG 300735Z OCT 87 ONE TIME INSP OFENGINE COWLING COMPLETED AT 500.0 ACFTHRS (RH0000)

03-Nov-1987 1

APO NY 09061

QC000000

421ST MED COSOF UH-60-87-11 TB 55-1520-237-20-94 DTG300735Z OCT 87 ONE TIME INSP OF CARGODOOR UPPER AND LOWER SUPPORT ASSYCOMPLETED AT 500.0 ACFT HRS (RH0000)

03-Nov-1987 2

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60-87-12 DTG 03018Z DEC 87ONE TIME INSP OF GE-E-T700/701 ENGINESPOWER TURBINE MODULES SERIALNUMBERS FOR SUSPECT DEFECTIVEMODULES COMPLETED AT 500.0 ACFT HRS(RH0000)

03-Dec-1987 1

APO NY 09061

QC000000

45TH MED COPHASE MAINTENANCE INSPECTIONCOMPLETED AT 500.0 ACFT HRS NEXTINSPECTION DUE AT 1000.0 ACFT HRS(RH0000)

07-Dec-1987 1

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60A-88-01 TB 55-1520-237-20-35DTG 160500Z FEB 88 INSP OF CERTAINSERIAL NUMBER TAIL ROTOR BLADEASSEMBLIES COMPLETED AT 522.2 ACFT HRS(RH0000)

16-Feb-1988 1

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60-88-03 TB 55-1520-237-20-97DTG 1210 00Z MAY 88 LIFE EXTENSION OF UH-60A AIRCRAFT MAIN MODULE SHAFTCOMPLETED AT 5662.6 ACFT HRS (RH0000)

16-Mar-1988 1

APO NY 09061

QC000000



8.7.DATE

6.REMARKS

4. 5.



45TH MED COSOF MSG UH-60A-88-02 TB 55-1520-237-20-96DTG 180500Z MAR 88 ONE TIME INSP OF THETAIL ROTOR GEARBOX OUTPUT SHAFTCOMPLETED AT 532.5 ACFT HRS (RH0000)

30-Mar-1988 1

APO NY 09061

QC000000

421ST MED COTB 55-1520-237-20-79 29 JAN 87 INSP ANDREPLACEMENT OF ENGINE DESWIRL DUCTPN 12572-1568 ON UH60A ACFT COMPLETEDAT 545.5 ACFT HRS (RH0000)

05-May-1988 1

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60-88-04 DTG 130010Z MAY 88 TB55-1520 -237-20-96 ONE TIME INSP OF TAILROTOR GEARBOX OUTPUT SHAFT (REVISIONTO UH-60-60-88-02) COMPLETED (RH0000)

16-May-1988 1

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60-88-05 DTG 161200Z JUN 88 TB55-1520 -237-20-98 INITIATION OF AUXILLARYPOWER UNIT MAXIMUM ALLOWABLEOPERATION TIME (MAOT) IN TERMS OF APUOPERATING HOURS AND APU STARTSCOMPLETED AT 579.8 ACFT HRS (RH0000)

17-Jun-1988 1

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60-88-06 DTG 120130Z JUL 88 TB55-1520 -237-20-99 ONE TIME RECORDSCHECK TO VERIFY XMSN OIL COOLEROPERATION TIME AND TO CHANGE XSMN OILCOOLER FROM CONDITION COMPONENT TOTIME CHANGE COMPLETED AT 597.2 ACFTHRS (RH0000)

15-Jul-1988 1

APO NY 09061

QC000000

AVSCOM OCM SECTOCM/ACE PERFORMED AT 597.0 ACFT HRS ATNELLIGAN, GER BY ACE TEAM MEMBER "B"(BC0000)

18-Jul-1988 1

ST LOUIS, MO

QC000000

45TH MED COSOF MSG UH-60A-88-07 DTG 140045Z JUL 88TB 55-1520-237-20-98 REVISION OF SOF UH-60A-99-05 APU OPERATION AND TIME STARTCALCULATIONS COMPLETED AT 630.0 ACFTHRS (KH0000)

09-Aug-1988 1

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60A-88-08 DTG 272300Z JUL 88REVISION TO OVERHAUL LIFE FOR XMSN OILCOOLER BLOWER ASSYS COMPLETED AT630.0 ACFT HRS (KH0000)

09-Aug-1988 2

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60A-88-08 DTG 030100Z AUG 88TB 55-1520-237-20-100 INSP OF ARA SEATSFOR LOOSE CLEVIS BOLTS COMPLETED AT604.4 ACFT HRS (KH0000)

17-Aug-1988 1

APO NY 09061

QC000000

45TH MED COSOF MSG GEN-88-02 DTG 212230Z SEP 88 TB55-1500-200-20-001 ONE TIME INSP FORINSTALLATION OF CORRECT INTERNALPORTABLE FIRE EXTINGUISHER COMPLETEDAT 655.5 ACFT HRS (KH0000)

23-Sep-1988 1

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60A-88-10 DTG 060730Z OCT 88TB 55-1520-237-20-101 ONE TIME INSP OFGUNNERS SEAT SUPPORT BRACKETS ANDHARDWARE FOR PROPER INSTALLATION BYPART NUMBER COMPLETED AT 681.5 ACFTHRS (KH0000)

09-Nov-1988 1

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60A-88-11 DTG 180030Z OCT 88REVISION TO SOF UH-60A-86-18 H-60RESTRICTION OF RAPPELING OPERATIONSCOMPLETED AT 681.5 ACFT HRS (KH0000)

09-Nov-1988 2

APO NY 09061

QC000000



8.7.DATE

6.REMARKS

4. 5.



45TH MED COSOF MSG UH-60A-88-12 DTG 011702Z NOV 88TB 55-1520-237-20-101 REVISION TO SOF MSGUH-60A-88-10 ONE TIME INSP OF TROOPSGUNNERS SEAT AND 3 MAN MEDEVAC SEATSUPPER SUPPORTS INSTALLATIONCOMPLETED AT 681.5 ACFT HRS (KH0000)

09-Nov-1988 3

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60A-88-13 DTG 180630Z NOV 88TB 55-1520-237-20-102 ONE TIME INSP OF M/RBLADE EXPANDABLE PINS FOR MISSINGSEGMENTS PRIOR TO NEXT 10 HR/14 DAYINSP COMPLETED AT 690.0 ACFT HRS(KH0000)

30-Nov-1988 1

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60A-88-14 DTG 072330Z DEC 88TB 55-1520-237-20-103 ONE TIME INSP OF ALLUH-60A HIGH PERFORMANCE HOISTSYSTEMS COMPLETED AT 703.6 ACFT HRS(KH0000)

03-Jan-1989 1

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60-89-01 DTG 192230Z DEC 88 TB55-1520 -237-20-103 ONE TIME INSP OF T700-GE-T700 ENGINE RECORDS COMPLETED AT703.6 ACFT HRS (KH0000)

10-Feb-1989 1

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60-89-03 DTG 302230Z MAR 89 TB55-1520 -237-20-104 INSP OF ALL UH-60 MAINROTOR SPINDLE ASSYS COMPLETED AT 738.2ACFT HRS (KH0000)

10-Apr-1989 1

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60-89-04 DTG 010045Z APR 89REVISION TO SOF-UH-60-89-03 COMPLIEDWITH THIS DATE. (KH0000)

21-Apr-1989 1

APO NY 09061

QC000000

45TH MED COSOF MSG UH-60-89-05 (TB 55-1520-237-20-106)DTG 130730Z JUN89 ONE TIME INSPECTIONOF WIRE STRIKE PROTECTION SYSTEMCOMPLETED AT 779.4 ACFT HRS (KH0000)

19-Jun-1989 1

APO NY 09061

QC000000

AVSCOM OCM SEC, STOCM/ACE PERFORMED AT 779.0 A/C HRS, ATNELLIGEN, GE BY ACE TEAM MEMBERWRIGHT. (KW0000)

27-Jun-1989 1

LOUIS, MO 3625

QC000000

45TH MEDICALCOMPANY (AA),

SOF MSG UH-60A-89-06(TB 55-1520-237-20-107)DTG 180730Z JULY 89, ONE TIME INSPECTIONOF RIGHT AND LEFT HAND RELAYASSEMBLIES FOR SUSPECT GROUNDINGMODULES COMPLETED AT 793.2 ACFT HRS.(KH0000)

27-Jul-1989 1

APO NY 09061

QC000000


SOF MSG UH-60A-89-09(TB 55-1520-237-20-104)DTG 152202Z ONE TIME REVISION OF ACFTOVERHAUL/RETIREMENT LIFE COMPONENTSCOMPLETED AT 793.2 ACFT HRS (KH0000)

22-Aug-1989 1

APO NY 09061

QC000000


SOF MSG UH-60A-89-08(TB 55-1520-237-20-108)DTG 111500Z ONE TIME OPERATIONALINSPECTION OF THE FUEL BOOST PUMPHOSE INSTALLATION COMPLETED AT 793.2ACFT HRS (KH0000)

20-Sep-1989 1

APO NY 09061

QC000000


SOF MSG UH-60-89-10 DTG 141815Z SEP 89ONE TIME OPERATIONAL INSPECTION OFT700-GE-T700 GG ROTOR AND STATORSHROUDS COMPLETED AT 795.2 ACFT HRS.(KH0000)

26-Sep-1989 1

APO NY 09061

QC000000



8.7.DATE

6.REMARKS

4. 5.



45TH MEDICALCOMPANY (AA)

SOF MSG UH-60-89-11 (DTG 081454Z NOV 89)TB 55- 1520-237-20-19 ONE TIME INSPECTIONOF OIL COOLER AXIAL FAN COMPLETED AT822.0 ACFT HRS. (KH0000)

22-Nov-1989 1

APO NY 09061

QC000000


SOF MSG UH-60-89-12 (TB 55-1520-237-20-110)DTG 231045Z ONE TIME INSPECTION OF OILCOOLER AXIAL FAN AT 827.1 ACFT HRS.(KH0000)

30-Nov-1989 1

APO NY 09061

QC000000


SOF MSG UH-60-89-13 DTG 061915Z DEC 89 TB55-1520-237-20-19 ONE TIME INSPECTION OFCABIN TIEDOWNS COMPLETED AT 828.1 ACFTHRS. (KH0000)

08-Dec-1989 1

APO NY 09061

QC000000


SOF MSG UH-60-90-01 (TB 55-1520-237-20-113)DTG 100652Z APR 90 ONE TIME ANDRECURRING INSPECTION OF MAIN ROTOREXPANDABLE PINS COMPLETED AT 885.6ACFT HRS (KH0000)

21-Jan-1990 1

APO NY 09061

QC000000


TB 55-1520-237-20-113 DTD 30 JAN 90 ONETIME INSPECTION OF ICE RATE INDICATORSCOMPLETED AT 888.9 ACFT HRS (KH0000)

19-Jul-1990 1

APO NY 09061

QC000000


TB 55-1520-237-20-117 DTD 15 MAY 90 ONETIME INSPECTION OF M/R PITCH CHANGEHORNS COMPLETED AT 906.3 ACFT HRS(KH0000)

13-Aug-1990 1

APO NY 09061

QC000000


SOF MSG UH-60-90-02 (TB 55-1520-237-20-118)DTG 101030Z AUG 90 ONE TIME ANDRECURRING INSP OF T/R PITCH BEAM NUTCOMPLETED AT 906.3 ACFT HRS (KH0000)

13-Aug-1990 2

APO NY 09061

QC000000

AVSCOM OCM SEC,OCM/ACE PERFORMED AT 906.0 A/C HRS ATNELLIGGEN, GE BY ACE TEAM MEMBER P.(KH0000)

13-Aug-1990 3

ST LOUIS, MO

QC000000


TB 55-1520-237-20-111 DATED 30 JANUARY1990 ONE TIME INSPECTION OF UPPERPRESSURE PLATE AND SPINDLE TO HUBATTACHING BOLTS COMPLETED AT 919.6ACFT HRS (SP0000)

06-Sep-1990 1

APO NY 09061

QC000000


TB 55-1520-237-20-113 INSP FOR DEFECTIVEROSEMONT ICE RATE INDICATORSCOMPLETED AT 994.7 ACFT HRS (DT0000)

22-Jan-1991 1

APO NY 09175

QC000000

4/11 ACRGEN-91-ASAM-02 AUTHORIZATION FORINSTALLATION AND USINGCRYPOTOGRAPHIC COMPUTER KIT-1C(RR9167)

09-Feb-1991 1

APO AE 09146

QC000000

159TH MED CO (AA)UH-60-91-ASAM-05 (TB 55-1520-237-20-122)INSP FOR 4 UNSERVICEABLE SPINDLE ASSYCOMPLETED AT 994.7 ACFT HRS (DT0000)

21-Feb-1991 1

APO NY 091175

QC000000

159TH MED CO (AA)UH-60-91-ASAM-06 (TB 55-1520-237-20-124)ONE TIME INSP OF CARGO HOOK INTERNALWIRING ROUTING COMPLETED AT 994.7 ACFTHRS (DT0000)

18-Mar-1991 1

APO NY 091175

QC000000

AVSCOM OCM SECOCM/ACE PERFORMED AT 999.0 AC HRS ATDARMSTADT, GEBY ACE TEAM MEMBER W.(WT0000)

10-Jul-1991 1

ST LOUIS, MO

QC000000



8.7.DATE

6.REMARKS

4. 5.



159TH MED CO (AA)UH-60-91-ASAM-10 ONE TIME INSP ANDREPLACEMENT OF MAIN LANDING GEARBRAKE ASSY PISTONS COMPLETED AT 999.0ACFT HRS (DT0000)

31-Jul-1991 1

APO, NY 09175

QC000000

45TH MED CO (AA)UH-60-92-ASAM-01 (TB 1-1520-237-20-129) ALLUH-60 SERIES AIRCRAFT INSPECTION FORTHREE(3) UNSERVICEABLE SPINDLEASSEMBLIES, COMPLETED 28 JAN 92.(KD0000)

29-Jan-1992 1

APO, NY 09061

QC000000

159TH MED CO (AA)UH-60-91-ASAM-01 ONE TIME REPLACEMENTAND 30 HOUR SPECIAL INSPECTION OF THETAIL ROTOR PITCH BEAM RETAININGWASHER, COMPLETED AT 999.0 ACFT HRS(KD0000)

30-Jan-1992 1

APO, NY 09175

QC000000

45TH MED CO (AA)UH-60-91-ASAM-02 RECURRING EROSIONINSPECTION OF MAIN ROTOR BLADE TIPCAPS (DESERT SHIELD AIRCRAFT)N/A THISACFT. (KD0000)

30-Jan-1992 2

APO, NY 09061

QC000000

45TH MED CO (AA)UH-60-91-ASAM-03 EXTENDED TIME BETWEENOVERHAUL (TBO) UNDER DESERT SHEILDOPERATIONS FOR UH-60 OIL COOLERBLOWER AND TAIL ROTOR PITCH CHANGESHAFT BEARINGS. N/A THIS ACFT (KD0000)

30-Jan-1992 3

APO, NY 09061

QC000000

45TH MED CO (AA)UH-60-91-ASAM-04 TO PROVIDE GUIDANCEFOR SITUATIONS REQUIRING EXCEEDING THERETIREMENT(FINITE) LIFE OF CERTAINCOMPONENTS (OPERATION IN SWA DESERTSTORM), NA THIS ACFT (KD0000)

30-Jan-1992 4

APO, NY 09061

QC000000

45TH MED CO (AA)UH-60-91-ASAM-07 ADVANCE NOTIFICATIONOF MANUAL CHANGES CONCERNING MAINTRANSMISSION MODULES, COMPLETED1077.8 ACFT HRS. (KD0000)

30-Jan-1992 5

APO, NY 09061

QC000000

45TH MED CO (AA)UH-60-91-ASAM-08 ONE TIME INSPECTION OFFIRE EXTENGUISHER SYSTEM, COMPLETEDAT 999.0 (KD0000)

30-Jan-1992 6

APO, NY 09061

QC000000

45TH MED CO (AA)UH-60-91-ASAM-09 CHANGE TO INSPECTIONPROCEDURES FOR MAIN ROTORELASTOMERIC BEARINGS COMPLETED AT1077.8 ACFT HRS (KD0000)

30-Jan-1992 7

APO, NY 09061

QC000000

45TH MED CO (AA)UH-60-91-ASAM-11 REQUIREMENT TOOPERATE WITH BOOST PUMPS ON WHILEBURNING JP-4 FUEL, N/A THIS ACFT (KD0000)

30-Jan-1992 8

APO, NY 09061

QC000000

236TH MED COLATE ENTRY UH-60-92-ASAM-02 ONE TIMEINSP OF ENG OUTPUT SHAFT BOLTS ANDVIBRATION LEVEL N/A THIS SERIAL NUMBERACFT (RR9167)

18-May-1992 1

APO AE 09180

QC000000

236TH MED COLATE ENTRY UH-60-92-ASAM-04 USE OFRECOVERY/RECYCLE EQUIP ON ALLIARCONDOR REFRIG SYSTEM N/A THIS ACFT(RR9167)

23-Jul-1992 1

APO AE 09180

QC000000

45TH MED COUH-60-92-ASAM-03 UH-60A/EH-6OA ACFT, T700-GE-T700 GAS GENERATOR ROTOR TURBINEBLADE FAILURE/ENGINE CLEANING, ENGINELIFE LIMITED COMPONENTS TRACKINGCOMPLETED AT______ ACFT HRS (KD0000)

09-Nov-1992 1

APO NY 09061

QC000000



8.7.DATE

6.REMARKS

4. 5.



236TH MED COLATE ENTRY UH-60-93-ASAM-02 GASGENERATOR ROTOR FAILURE/ENG CLEANINGAND SINGLE ENG FAILURES PROCEDURESIAW UH-60-92-ASAM-07 INFO ONLY (RR9167)

25-Nov-1992 1

APO AE 09180

QC000000

45TH MED COUH-60-93-ASAM-05 ONE TIME INSPECTIONFOR TAIL ROTOR DRIVE SHAFT VISCOUSDAMPER BEARING COMPLIED WITH AT 1215.8ACFT HRS. 1281.6 AVFT HRS (RO0000)

23-Dec-1992 1

APO NY 09250

QC000000

45TH MED COUH-60-93-ASAM-06 ONE TIME INSPECTION TOREMOVE SUSPECT TAIL ROTOR PITCHBEAMS COMPLIED WITH AT 1215.8 ACFT HRS,PITCH BEAM SERIAL NUMBER A255-00493(RO0000)

23-Dec-1992 2

APO NY 09250

QC000000

236TH MED COLATE ENTRY UH-60-93-ASAM-07 NOMAINTENANCE REQUIRE (RR9167)

06-Jan-1993 1

APO AE 09180

QC000000

B CO 70TH TRANSUH-60-92-ASAM-05 ALL UH-60 SERIES ACFTINSPECTION & REPLACEMENT OF MAINROTOR BLADE EXPANDABLE PINCOMPLETED 1218.6 ACFT HRS. (LR0000)

01-Mar-1993 1

APO NY 09028

QC000000

B CO 70TH TRANSUH-60-92-ASAM-06 ALL UH-60 ARMY ACFTONE TIME INSPECTION FOR PROPERHARDWARE ON THE PEDAL ADJUSTERASSEMBLY COMPLETED AT 1281.6 ACFT HRS.(LR0000)

01-Mar-1993 2

APO NY 09028

QC000000

B CO 70TH TRANSUH-60-93-ASAM-03 MAINT MAND, ALL UH-60SERIES ACFTREVISION TO UH-60-92-ASAM-05INSPECTION AND REPLACE OF MAIN ROTORBLADE EXPANDABLE PINS COMPLETEDAT1218.6 ACFT HRS. (LR0000)

01-Mar-1993 3

APO NY 09028

QC000000

B CO 70 TH TRANSUH-60-93-ASAM-04 MAINT MAND, ALL UH-60SERIES ACFT REVISION TO UH-60-92-ASAM-06ONE TIME INSPECTION OF PROPERHARDWARE ON THE PEDAL ADJUSTER ASSYCOMPLETED AT 1218.6 ACFT HRS (LR0000)

01-Mar-1993 4

APO, NY 09028

QC000000

B CO 70 TH TRANS(AUGUSTA AEROSPACE

AUX HEATER SYSTEM INSTALLED THIS DATE@ 1218.6 ACFT HRS (SH0000)

10-Mar-1993 1

APO, NY 09028

QC000000

B CO 70 TH TRANSUH-60-93-ASAM-01 (TB 1-1520-237-20-135)MAINT MAND ALL H-60 ACFT ONE TIMEOPERATIONAL CHECK OF THE TRTRANSMISSION AND GEARBOX CHIPDETECTOR SYSTEM COMPLETED AT 12318.6ACFT HRS (LR0000)

15-Mar-1993 1

APO, NY 09028

QC000000

B CO 70 TH TRANSUH-60-93-ASAM-10 (TB 1-1520-237-20-141)MAINT MAND ALL H-60 ACFT ONE TIME ANDRECURRING INSPECTION/ CLEANING OF THEESSS VALVES AND PUEMATIC LINES N/A THISACFT AT 1218.6 ACFT HRS (LR0000)

05-Apr-1993 1

APO, NY 09028

QC000000

B CO 70 TH TRANSUH-60-93-ASAM-11 (TB 1-1520-237-20-142)MAINT MAND ALL H-60 ACFT INSPECT ANDREPLACE OF ARA REW RESTRAINTBUCKLE/CROTCH ASSEMBLIES COMPLETEDAT 1218.6 ACFT HRS (LR0000)

13-Apr-1993 1

APO, NY 09028

QC000000



8.7.DATE

6.REMARKS

4. 5.



B CO 70 TH TRANSSOF UH-60-93-01 ONE TIME VISUALINSPECTION OF T700-GE-T701C ENGINE FUELHOSE ASSY, N/A THIS ACFT AT 1218.6 ACFTHRS (LR0000)

26-Apr-1993 1

APO, NY 09028

QC000000

B CO 70 TH TRANSSOF UH-60-93-02 ONE TIME VISUALINSPECTION OF T700-GE-T701C ENGINE FUELHOSE ASSY FOR ADDITIONAL S/N N/A THISACFT AT 1218.6 ACFT HRS (LR0000)

26-Apr-1993 2

APO, NY 09028

QC000000

B CO 70 TH TRANSUH-60-ASAM-93-08 (TB 1-1520-237-20-138)MAINT MAND ALL UH-60 ACFT BULIT PRIORTO S/N 91-26354, TO BIAS TAIL ROTORRIGGING THREE DEGREES COMPLETED AT1218.6 ACFT HRS (LR0000)

28-Apr-1993 1

APO, NY 09028

QC000000

B CO 70 TH TRANSUH-60-ASAM-93-09 (TB 1-1520-237-20-140)MAINT MAND ALL UH-60 ACFT ONE TIMEINSPECTION TO DETERMINE COMPLIANCEWITH SYSTEM MWO'S COMPLETED AT 1218.6ACFT HRS (LR0000)

28-Apr-1993 2

APO, NY 09028

QC000000

B CO 70 TH TRANSUH-60-ASAM-93-12 (TB 1-1520-237-20-143)MAINT MAND OPERATIONAL ALL UH-60AIRCRAFT, ABRUPT CHANGE TO MAIN ROTORTRACK/VIBRATIONS COMPLETED AT 1218.6ACFT HRS (LR0000)

28-Apr-1993 3

APO, NY 09028

QC000000

B CO 70 TH TRANSREPLACE M/R BLADE EXPANDABLE PINS P/N-101 WITH ADEQUATE NO OF -102 EXP PINS(8EA) AT 1218.6 ACFT HRS. (LR0000)

28-Apr-1993 4

APO, NY 09028

QC000000

159TH MED CO(AA)UH-60-93-ASAM-13 (TB 1-1520-237-20-148) ALLH-60 WITH EXTERNAL STORES SUPPORTSYSTEM(ESSS) AND EXTENDED RANGE FUELSYSTEM (ERFS) MISSION KITS INSTALLEDDOES NOT APPLY TO THIS YEAR MODEL.(WC0000)

21-Jun-1993 1

APO, NY 09096

QC000000


21-Jun-1993 2

APO, NY 09096

QC000000


21-Jun-1993 3

APO, NY 09096

QC000000

AVSCOM OCM SECOCM/ACE PERFORMED AT 1239.0 AC HRS ATWEISBADEN, FRG BY ACE TEAM MEMBER K.(RL0000)

30-Jun-1993 1

ST. LOUIS, MO

QC000000

DYN CORP-EMWO VERIFACTION COMPLETED 16 AUG 93 @1254.9 ACFT HRS. (MS0000)

16-Aug-1993 1

APO-AE 09096

QC000000

159TH MED CO (AA)UH-60-93-ASAM-16 ONE TIME INSP OF THEHYDRAULIC PUMP MODULE KNURLEDBLEED/RELIEF KNOB SECURING PIN (TB 1-1520-237-20-146) (MS0000)

07-Sep-1993 1

APO-NY 09096

QC000000



8.7.DATE

6.REMARKS

4. 5.



236TH MED CO (AA)LATE ENTRY UH-60-93-ASAM-17 M/UH-60L/KACFT WITH T700-GE-701C. N/A THIS ACFT(RR9167)

15-Sep-1993 1

APO-AE 09180

QC000000

45TH MED CO (AA)UH-60-94-ASAM-02 RETURN FOR EXCHANGEOF CERTAIN (ARA) MANUFACUREDBUCKLE/CROTCH STRAP ASSEMBLIES (PND4495-28 UB AKKG-60 SERIES ACFT C/W1308.3 ACFT HRS. (LL0000)

18-Feb-1994 1

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-94-ASAM-04 ALL H-60 ARMY AIRCRAFTREISSUE OR ONE TIME INSPECTION TOREMOVE SUSPECT T/R PITCH BEAMS C/W1308.3 ACFFT HRS (LL0000)

18-Feb-1994 2

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-94-ASAM-05 ALL H-60 BLACKHAWKHELICOPTERS ONE TIME REMOVAL OF TAILG/B OUTPUT SHAFT P/N 70358-06620 FORREWORK, N/A THIS ACFT C/W 1308.3 ACFTHRS. (LL0000)

18-Feb-1994 3

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-94-ASAM-06 COCKPITSTANDARDIZATION OF PILOT & CO-PILOTRESTRAINT RELEASE SYSTEMS IN ALL H-60AIRCRAFT C/W AT 1308. ACFT HRS. (LL0000)

18-Feb-1994 4

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-94-ASAM-07 CHANGE TO H-60OVERHAUL AND RETIREMENT TABLE (TB 1-1520-237-20-154) C/W AT 1315.3 ACFT HRS.(LL0000)

11-Mar-1994 1

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-94-ASAM-08 ALL H-60 ACFT THIS IS AREVISION UH-60-ASAM-07 (TB 1-1520-237-20-154) C/W AT 1315.3 ACFT HRS. (LL0000)

11-Mar-1994 2

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-94-ASAM-03 ALL H-60 ARMY AIRCRAFTONE TIME REFURBISHMENT OF MAIN ROTORSPINDLE AND REPLACEMENT OF CERTAINM/R THRUST BEARINGS C/W 1482.0 ACFTHRS. (LL0000)

20-Mar-1994 1

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-94-ASAM-09 ALL H-60 ARMY REMOVALOF CERTAIN PRIMARY SERVO ASSEMBLIES(TB 1-1520-237-20-150) C/W AT 1355.1 ACFTHRS. (LL0000)

09-Apr-1994 1

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-94-ASAM-10 ONE TIMEREFURBISHMENT OF MAIN ROTOR SPINDLEAND REPLACEMENT OF CERTAIN MAINROTOR THRUST BEARING (LL0000)

21-Apr-1994 1

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-94-ASAM-11 INFORMATIONAL MAINROTOR BLADE DE-ICE HEATER MATRESISTENCE MEASUREMENT TEST UH-60 &EH-60 SERIES ACFT (LL0000)

21-Apr-1994 2

APO-AE 09250

QC000000

AVSCOM OCM SEC,OCM/ACE PERFORMED AT 1406.0 A/C HRS BYACE TEAM MEMBER L. (ST0000)

13-Jun-1994 1

ST. LOUIS, MO

QC000000

45TH MED CO (AA)UH-60 94-ASAM-02 UL60 (AUTHORIZED TO BEUTILIZED FOR EXTERNAL LOAD OPERATIONSLIMITED TO MAXIMUM 9000 POUND STATICWEIGHT (TB 1-1520-237-20-156) N/A THISACFT. (JM0000)

11-Aug-1994 1

APO-AE 09250

QC000000



8.7.DATE

6.REMARKS

4. 5.



45TH MED CO (AA)UH-60-95-ASAM-01 UH60/EH60 HOISTING ANDAERIAL RECOVERY OF UH60/EH60 ESSSFIXED PROVISIONSED HELICOPTER, N/A THISACFT. (JM0000)

13-Oct-1994 1

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-95-ASAM-02 ALL H60 ACFT REQ TOOPERATE THE FUEL TANK SUBMERGEDBOOST PUMPS ON AT ALL TIMES W/ALLFUELS DURING GROUND AND FLTOPERATIONS (JM0000)

28-Oct-1994 1

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-95-ASAM-03 ALL H60 ACFT SHALL REQRESHIMMINGOF T/R PIVOT BEARING PERREVISED PROCEDURES AND CERTAIN BLADEASSY WILL BE INSP FOR SPECIFIED SERIALNUMBERS WHICH CONTE IN COMPOSITEPIVOT BEARING RETAINERS. (JM0000)

28-Oct-1994 2

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-95-ASAM-04 ALL H60 AIRCRAFTREDUCTION IN TORQUE OF SELF-RETAININGPIVOT BOLTS TB 1-1520-237-20-16 (TB 1-1520-250-20-2). (JM0000)

09-Dec-1994 1

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-95-ASAM-08 GAS GENERATORTURBINE ROTOR BLADE INFORMATION C/W9(NO PID) (QC0000)

08-Jan-1995 1

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-95-SOF-01 ALL H-60 ACFT EXCEPT MH-60K ONE TIME RECORDS INSP OF ALL T/RG/B'S ULTRASONIC INSP OF DESIGNATED T/RG/B OUTPUT SHAFTS P/N 70358-06620-101AND REMOVAL OF T/R G/B'S WITH SHAFTSREQ REWORK (JM0000)

12-Jan-1995 1

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-95-ASAM-05 ALL H-60 ACFT CHANGESIN RETIREMENT FOR SERVO BEAM RAILS P/N70209-22130-050/052/054/056. (JM0000)

25-Jan-1995 1

APO-AE 09250

QC000000

B CO 7-159TH AVNUH-60-SOF-95-02 RETIREMENT LIFE CHANGEFOR CERTAIN M/R BLADE CUFFS COMP1480.2 ACFT HRS (JH0000)

15-Feb-1995 1

APO-AE 09182

QC000000

B CO 7-159TH AVNPMS-2 INSP COMP AT 1481.7 HRS. (JH0000) 20-Mar-1995 1

APO-AE 09182

QC000000

45TH MED CO (AA)UH-60-95-ASAM-06 ALL H-60 BLACKHAWKHELICOPTER ONE TIME INSP FOR CRACKEDXMSN BEAMS, UPPER DECK SKIN CRACKS,FRAME CRACKS AND IMPLEMENATION OF A100 HR INSP. (BW0000)

21-Jun-1995 1

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-95-ASAM-07 ALL H-60 ACFT TOPROVIDE REVISED REPLACEMENT CRITERIAFOR TROOP/GUNNER SEAT ATTENUATIONWIRES, EXPLICIT SHIMMING PROCEDURESFOR ATTENUATION ROLLERS (TB 1-1520-20-164) C/W 1552.5 ACFT HRS (BW0000)

13-Jul-1995 1

APO-AE 09250

QC000000

236TH MED CO (AA)UH-60-96-ASAM-01 REPLACEMENT OFCERTAIN BOLTS AND NUTS (RR9167)

06-Nov-1995 1

APO-AE 09180

QC000000



8.7.DATE

6.REMARKS

4. 5.



45TH MED CO (AA)UH-60-96-SOF-01 ALL UH/EH/MH-60 AIRCRAFTCHANGE IN RETIREMENT OF FWD BC SPT PN7040008116048, MANUFACTURED BYHICKSVILLE MACHINE WRKS AND REMOVALOF SPECIFIED SN FWD BC SPT ASSY'S (UH-60-96-SOF-01) (TB1-1520-237-20-172)C/W 1621.6ACFT HRS (BW0000)

08-Nov-1995 1

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-96-SOF-02 ALL H-60 BLACKHAWKHELICOPTERS ONE TIME INSP FOR SUSPECTT/R I/B RETENTION PLATES (UH-60-96-SOF-02)(TB 1-1520-237-20-173) C/W 1629.6 ACFTHRS (BW0000)

27-Nov-1995 1

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-96-ASAM-02 ALL H-60 BLACKHAWKHELICOPTERS, ONE TIME INSPECTION FORSUSPECT MAIN ROTOR SHAFT NUT BOLTS(UH-60-ASAM-96-02)(TB 1-1520-237-20-171) C/W1629.6 ACFT HRS (BW0000)

29-Nov-1995 1

APO-AE 09250

QC000000

45TH MED CO (AA)UH-60-96-SOF-03 ALL UH/EH/MH-60A/L/KAIRCRAFT CHANGE IN RETIREMENT LIFE OFMAIN ROTOR BLADE CUFF PN 70150-09109-041, MANUFACTURED BY FENNMANUFACTURING (TB 1-1520-237-20-174) C/W1633.0 ACFT HRS (BW0000)

05-Dec-1995 1

APO-AE 09250

QC000000

236TH MED CO (AA)UH-60-96-SOF-04 ONE TIME INSP FOR AFTBRIDGE ASSY WITH SPECIFIED SERIALNUMBERS COMPLIED WITH AT 1636.5 ACFTHRS (GH0000)

14-Dec-1995 1

APO-AE 09180

QC000000

236TH MED CO (AA)UH-60-96-ASAM-03 REVISION TO UH-60-96-ASAM-02 COMPLIED WITH AT 1667.6 ACFTHRS (GH0000)

11-Feb-1996 1

APO-AE 09180

QC000000

236TH MED CO (AA)UH-60-94-ASAM-01 ALL UH-60/EH-MH-60SERIES AIRCRAFT NIGHT VISION GOOGLE(NVG) COMPATIBILITY REWORK OF MASTERWARNING PANEL ASSEMBLIES TB 1-1520-237-20-139 .PCW (BS0000)

24-Feb-1996 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-94-ASAM-05 TB 1-1520-237-20-172 ONETIME INSP OF FWD SUPPORT ASSYCOMPLIED WITH AT 1816.1 ACFT HRS.(GH0000)

17-Jul-1996 1

APO AE 09180

QC000000

DYNCORP-EAWR DATED 1 JUNE 95 AUTHORIZATION TOOPERATE ALL UH-60A/L & EH-60 AIRCRAFTWITH RT-1518C ARC-164 HQII INSTALLED(JB0000)

23-Aug-1996 1

APO AE 09789

QC000000

236TH MED CO (AA)LATE ENTRY UH-60-96-ASAM-06INFORMATIONAL, UH-60 MAIN ROTORSPINDLE (RR0167)

26-Aug-1996 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-96-ASAM-10 ESTABLISHMENT OFREPLACEMENT OF TEFLON SLEEVE BEARINGIN THE SPHERICAL ELASTOMERIC BEARINGASSY AT PMS-2, COMPLIED WITH AT 1852.6ACFT HRS (RR0167)

16-Sep-1996 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-96-ASAM-08 ONE TIME VER OF AEREXINBOARD RETENTION PLATE (TB 1-1520-237-20-173) @ ACFT HRS 1851.4 (RR0167)

16-Sep-1996 2

APO AE 09180

QC000000



8.7.DATE

6.REMARKS

4. 5.



236TH MED CO (AA)UH-60-96-ASAM-09 ONE TIME INSP OF THESTABILATOR CLEVIS FOR EPOXY PRIMER (TB1-1520-250-20-179) @ ACFT HRS 1851.4(CW0000)

16-Sep-1996 3

APO AE 09180

QC000000

45TH MED CO (AA)LATE ENTRY UH 60-97-ASAM-01 ALL H-60BLACKHAWK HELICOPTERS INSPECTION OFALL MAIN ROTOR HUB ASSEMBLIES (TB 1-1520-237-181)(TB 1-1520-250-20-6) COMPLIEDWITH AT 1869.3 ACFT HRS. (BC0000)

08-Oct-1996 1

APO AE 09789

QC000000

45TH MED CO (AA)LATE ENTRY UH 60-97-ASAM-02 ALL H-60A/EH-60A/UH-60L/MH-60K HELICOPTERS ONE TIMEINSPECTION OF TAIL DRIVE FLEXIBLECOUPLING CONNECTIONS (TB 1-1520-237-20-184)(TB 1-1520-250-20-09) COMPLIED WITH AT1886.9 ACFT HRS. (BC0000)

25-Oct-1996 1

APO AE 09789

QC000000

45TH MED CO (AA)UH 60-97-ASAM-03 ALL UH-60A, EH-60AAIRCRAFT WITH T700-GE-T700 ENGINESSUBJECT REPLACEMENT OF UNDAMPED GASGENERATOR ROTOR/STATOR ASSEMBLIES(UH-60-97-ASAM-03)(TB 1-2840-248-20-19)COMPLIED WITH AT 1898.0 ACFT HRS.(BC0000)

01-Nov-1996 1

APO AE 09789

QC000000

45TH MED CO (AA)UH 60-97-SOF-01 REMOVAL OF CERTAINREWORKED MAIN ROTOR SWASHPLATESASSEMBLIES, ALL UH-60A, UH-60L, EH-60AAND MH-60K HELICOPTERS, (UH-60-97-01) (TB1-1520-237-20-185)(TB 1-1520-250-20-10)COMPLIED WITH AT 1918.2 ACFT HRS.(SK9320)

03-Dec-1996 1

APO AE 09789

QC000000

SIKORSKY ACFTUH 60-97-ASAM-01 ALL UH-60 BLACKHAWKHELICOPTERS INSPECTION OF ALL MAINROTOR HUBS ASSEMBLIES (TB1-1520-237-20-181)(TB1-1520-250-20-6) COMPLIED WITH AT1917.3 ACFT HRS (SK9320)

18-Dec-1996 1

APO AE 09789

QC000000

45TH MED CO (AA)UH 60-97-ASAM-04 ALL UH/EH-60A/L AND MH-60K CHANGE IN RETIREMENT LIFE OF MAINROTOR BLADE CUFF PN 70150-09109-043MANUFACTORED BY FENN MANUFAC (TB1-1520-237-20-186) (TB1-1520-250-20-11)COMPLIED WITH AT 1920.7 ACFT HRS(BC0000)

20-Dec-1996 1

APO AE 09789

QC000000

45TH MED CO (AA)LATE ENTRY,UH-60-97-ASAM-05 ALL UH-60A/EH-60A/UH-60L/MH-60K AIRCRAFT, ONETIME INSPECTION FOR REMOVAL ANDREWORK OF CERTAIN VISCOUS DAMPERBEARING SUPPORT ASSEMBLIES, (TB1-1520-237-23-3) (TB1-1520-250-23-1) COMPLIED WITHAT 1920.7 ACFT HRS (BC0000)

02-Jan-1997 1

APO AE 09789

QC000000

45TH MED CO (AA)UH-60-97-ASAM-06 INSP OF ALL H-60AIRCRAFT WITH LATERAL BELLCRANKASSEMBLY, PN 70400-08150-045,MANUFACTURED BY PURDY MACHINECOMPANY(CAGE CODE 15152)(UH-60-97-ASAM-06)(TB 1-1520-237-20-189)(TB 1-1520-250-23-1)COMPLIED WITH AT 1920.7 ACFT HRS(BC0000)

08-Jan-1997 1

APO AE 09789

QC000000



8.7.DATE

6.REMARKS

4. 5.



45TH MED CO (AA)UH-60-97-ASAM-07 ALL H-60 AIRCRAFTREPLACEMENT OF SPECIFIC SERIALNUMBERED T/R SERVO CYLINDER ASSY'S PN2227000-9,13,17 (TB1-1520-250-20-13)COPMPLIED WITH AT 1925.6 ACFT HRS.(LG0000)

14-Jan-1997 1

APO AE 09789

QC000000

45TH MED CO (AA)UH-60-97-ASAM-08 INSP OF ALL H-60 ACFTWITH THE CONNNECTING LINK ASSEMBLY PN70400-08155-056 MFD PURDY MACHINE CO(TB1-1520-2337-20-187) (TB1-1520-250-20-12)COMPLIED WITH AT 1925.6 ACFT HRS.(LG0000)

14-Jan-1997 2

APO AE 09789

QC000000

45TH MED CO (AA)UH-60-97-ASAM-09 ALL H-60 ACFT WITH THEM/R SHAFT EXT ASSY PN 70351-08186-043,MANUF BY FENN OR PURDY CORP (UH-60-97-ASAM-09) (TB1-1520-237-20-15) COMPLIEDWITH AT 2187.9 ACFT HRS. (LG0000)

23-Jan-1997 1

APO AE 09789

QC000000

45TH MED CO (AA)UH-60-97-ASAM-11 ONE TIME INSP OF M/RBLADE CUFFS TO INCREASE FATIGUE LIFEFOR CERTAIN PN# & TYPE, COMPLIED WITH @1941.6 ACFT HRS (LG0000)

19-Mar-1997 1

APO AE 09789

QC000000

45TH MED CO (AA)LATE ENTRY UH-60-97-ASAM-1 INSP OF MAINSUPPORT BRIDGE TO ESTAB MAOT FOR PTMFG BY AIR INDUSTRIES COMPLIED WITH @1941.0 ACFT HRS (LG0000)

19-Mar-1997 2

APO AE 09789

QC000000

B CO 7/159TH AVNRESTORATION OF SERVICE LIFE OF THE T/RINBOARD RETENTION PLATES P/N 70358-06612-042 MFG BY FENN N/A THIS ACFT.(SC2163)

28-Apr-1997 1

APO AE 09182

QC000000

AVSCOM OCM SECJACE PERFORMED AT COLEMANN BRKS, GEAT ACFT HRS.1972.1 BY T. (AL0000)

15-May-1997 1

ST LOUIS, MO

QC000000

2-502 AVN REGTUH-60-97-ASAM-13 ONE TIME INSPECTION OFM/R SPHERICAL BEARING FOR EXISTENCE OFINNER SLEEVE TEFLON BEARINGCOMPLETED AT 1972.1 ACFT HRS. (LR0000)

09-Jun-1997 1

APO AE 09028

QC000000

DYNCORP-E OLR,DURING INSTALL OF MWO 50-74, STUDBACKED OUT OF RH FUEL SELECTOR VALVE,REPAIRED PER REVISED MERA EN-3739A AT1972.1 ACFT HRS. (MB0000)

01-Jul-1997 1

APO AE 09028

QC000000

2-502 AVN REGTPMS-2 #4 COMPLETED AT 1972.1 ACFT HRSNEXT PMS-2 #5 DUE AT 2472.1 ACFT HRS.(GK0000)

30-Jul-1997 1

APO AE 09028

QC000000

2-502 AVN REGTUH-60-97-ASAM-14 INSPECTION OFBELLCRANK SUPPORT P/N 70400-08158-101FOR SPECIFIC CAGE CODE (1W160)COMPLETED AT 1973.6 ACFT HRS-ASAM-14(BV1063)

06-Aug-1997 1

APO AE 09028

QC000000

2-502 AVN REGTUH-60-97-ASAM-15 INSPECTION OF LOWERP/C LINK ROD END FOR P/N 70400-08202-101WITH CAGE 40137 COMPLETED AT 1973.6ACFT HRS (BV1063)

06-Aug-1997 2

APO AE 09028

QC000000

2-502 AVN REGTUH-60-97-ASAM-16 INSPECTION OF LATERALSWASHPLATE LINK P/N -050 FOR CAGE CODE2A622 COMPLETED AT 1973.6 ACFT HRS(BV1063)

06-Aug-1997 3

APO AE 09028

QC000000



8.7.DATE

6.REMARKS

4. 5.



2-502 AVN REGTUH-60-97-ASAM-17 INSPECTION OF INTERNALRESCUE HOIST BRACKET COMPLETED 1979.1ACFT HOURSAGE 78286 OR LOCALLY MFG'DPART; REMOVAL OF BRACKET P/N 70800-02508-046 TO CHECK FOR WEAR OR CRACKS@ BL 34.50 BEAM COMPLIED WITH AT 2228.5ACFT HRS (BV1063)

14-Aug-1997 1

APO AE 09028

QC000000

2-502 AVN REGTUH-60-97-ASAM-18 ONE TIME INSP ANDREMOVAL OF CERTAIN S/N SWASHPLATEASSY COMPLETED AT 1981.6 ACFT HRS(BV1063)

10-Sep-1997 1

APO AE 09028

QC000000


UH-60-97-ASAM-19 ONE TIME INSP OFANVIS/HUD POWER SUPPLY COMPLIED WITHAT 1982.8 ACFT HRS (BV1063)

30-Sep-1997 1

APO AE 09180

QC000000


UH-60-98-ASAM-01 ONE TIME INSP OFHISTORICAL RECORDS FOR MAIN ROTORSHAFT EXTENSION MFG'D BY FENN ORPURDY CORP COMPLIED WITH AT 1990.1ACFT HRS (BV1063)

08-Oct-1997 1

APO AE 09180

QC000000


UH-60-98-ASAM-02 ONE TIME INSP FORPUSHRODS MFG'D BY VERSATILE MACHININGINC. CAGE 6S522 COMPLIED WITH AT 1992.2ACFT HRS. (BV1063)

14-Oct-1997 1

APO AE 09180

QC000000


UH-60-98-ASAM-03 ONE TIME INSP OFSWASHPLATE LINK ASSY PN 70400-08100-054MFG BY TEK CAGE 65780 COMPLIED WITH AT1996.6 ACFT HRS. (AJ1671)

05-Nov-1997 1

APO AE 09180

QC000000


AWR 580 SMDIM, DCIU,PDDS AND OCDCI(AWR590) (MJ3055)

09-Nov-1997 1

APO AE 09180

QC000000


AWR 554 TRIMBLE GLOBAL POSITIONINGSYSTEM (GPS) (AWR554) (MJ3055)

14-Jan-1998 1

APO AE 09180

QC000000


AWR 548 HAVE QUICK II (HQII) (AWR548)(MJ3055)

14-Jan-1998 2

APO AE 09180

QC000000


AWR 543 EMERGENCY LOCATORTRANSMITTER (ELT)(AWR543 (MJ3055)

16-Jan-1998 1

APO AE 09180

QC000000


AWR 524 PERSONNEL LOCATOR SYSTEM(PLS) (AWR 524) (MJ3055)

28-Jan-1998 1

APO AE 09180

QC000000

D 2-501UH-60-98-SOF-01 UH/EH-60 ACFT RISKMANAGEMENT OF 230 GALLON EXT TANKMANAGEMENT (JM1943)

31-Jan-1998 1

APO AE 09165

QC000000

236TH MEDICALCOMPANY

AWR 570 BAMBI WATER BUCKET (AWR570)(MJ3055)

13-Mar-1998 1

APO AE 09180

QC000000


UH-60-98-ASAM-04 ONE TIME INSP FORLOOSE HUCK BOLTS ON OVERHAULEDPRIMARY SERVOS COMPLIED WITH @ 2046.5ACFT HRS. (WJ8557)

08-Apr-1998 1

APO AE 09180

QC000000



8.7.DATE

6.REMARKS

4. 5.




UH-60-98-ASAM-05 ONE TIME INSP OF AFTSWASHPLATE LINK ASSY FOR SPECIFICCAGE CODE COMPLETED AT 2071.3 ACFTHRS (GR2306)

15-May-1998 1

APO AE 09180

QC000000


AWR 757 MILES/AGES II ON UH-60L (AWR757)(MJ3055)

14-Jun-1998 1

APO AE 09180

QC000000


AWR 764 VIP II ICS (AWR764) (MJ3055) 20-Jun-1998 1

APO AE 09180

QC000000


AWR 587 MILES/AGES PDDS, SMODIM & DCIU(AWR5870 (MJ3055)

13-Aug-1998 1

APO AE 09180

QC000000


UH-60-98-ASAM-07 ONE TIME INSP OFARGENTCORD MFG'D LEFT TIE ROD FORSPECIFIC CAGE CODE (3R021) & P/NCOMPLETED AT 2160.2 ACFT HRS (GR2306)

16-Sep-1998 1

APO AE 09180

QC000000


UH-60-98-ASAM-06 INFORMATIONAL ALLEH/MH AND UH-60L/K ACFT T700-GE-700ENGINE ODV FLAME OUTS, N/A THIS ACFT(GR2306)

17-Sep-1998 1

APO AE 09180

QC000000


AWR 813 MILES/AGES ON UH-60A WITHOUTESSS (AWR813) (MJ3055)

02-Oct-1998 1

APO AE 09180

QC000000


AWR 554 TRIMBLE GLOBAL POSITIONINGSYSTEM (GPS) (AWR554) (MJ3055)

02-Oct-1998 2

APO AE 09180

QC000000


UH-60-99-ASAM-02 INSP OF ACFT WITHPROVISIONS TO INSTALL EXTERNAL HOIST,N/A THIS ACFT COMPLIED WITH @ 2209.3ACFT HRS. (GT1986)

06-Nov-1998 1

APO AE 09180

QC000000


JACE/CPCE PERFORMED AT 2209.0 ACFT HRSAT LANDSTUHL, GERMANY (EA0000)

08-Nov-1998 1

APO AE 09180

QC000000


UH-60-99-ASAM-01 INSP OF ACFT FORMS ANDRECORDS FOR SPEC SWASHPLATE LINK,COMPLIED WITH @ 2208.3 ACFT HRS (GT1986)

08-Nov-1998 2

APO AE 09180

QC000000


UH-60-99-ASAM-03 ONE TIME INSPECTION OFT700-GE- 700 ENGINE RECORDS COMPLIEDWITH AT 2209.3 ACFT HRS (AJ1611)

30-Nov-1998 1

APO AE 09180

QC000000


AWR 548 HAVE QUICK II(HQII)(AWR 548)(MJ3055)

02-Dec-1998 1

APO AE 09180

QC000000


UH-60-99-ASAM-05 ONE TIME INSP OFSPINDLE BEARING PN SB 5203-202 C/W @2216.1 ACFT HRS (GT1986)

10-Dec-1998 1

APO AE 09180

QC000000


UH-60-99-ASAM-04 INFORMATIONAL ALLEH/MH UH60L/K T700-GE-701C ENGINE ODVRELATED FLAME OUTS, NA THIS ACFT(GT1986)

10-Dec-1998 2

APO AE 09180

QC000000



8.7.DATE

6.REMARKS

4. 5.




UH-60-99-ASAM-06 ONE TIME INSP OF PITCHHORNS FOR SPECIFIC SERIAL NUMBERS C/W@ 2218.4 ACFT HRS. (GR2306)

22-Dec-1998 1

APO AE 09180

QC000000


AWR 534 PERSONNEL LOCATOR SYSTEM(PLS) (AWR524) (MJ3055)

12-Jan-1999 1

APO AE 09180

QC000000


AWR 543 EMERGENCY LOCATORTRANSMITTER (ELT) FOR THE UH-60A/L(AWR543) (MJ3055)

15-Jan-1999 1

APO AE 09180

QC000000


UH-60-99-ASAM-07 REVISED INSPECTIONCRITERIA FOR HUB NDI OF 11 O'CLOCK BOLTHOLE FOR DAMPER BRACKET COMPLETEDAT 2255.8 ACFT HRS/2256 HUB HOURS(GT1986)

24-Mar-1999 1

APO AE 09180

QC000000


UH-60-99-ASAM-08 REVISED RETIREMENTLIFE OF BELL- CRANK SUPPORT ASSY. P/N70400-08162-042/0433/045 WITH CAGE 8L513C/W @ 2307.1 ACFT HRS (RC3243)

17-Jun-1999 1

APO AE 09180

QC000000

AMCOM-E OLR,JACE/CPCE PERFORMED AT 2319 ACFT HRSAT LANDSTUHL GE BY S. (SH6234)

14-Jul-1999 1

HUNTSVILLE,AL

QC000000

236TH MED CO(AA)UH-60-99-ASAM-10 ONE TIME INSP OFNUMBER TWO CROSSFEED FUEL LINEBREAKAWAY VALVE FOR LEAKAGE (JM1943)

09-Aug-1999 1

APO AE 09180

QC000000

236TH MED CO(AA)UH-60-99-ASAM-11 ONE TIME INSP OF T700-GE-700 ENGINES HISTORICAL RECORDS FORUPDATED SERVICE AND RETIREMENT LIFEC/W @ 2343.4 ACFT HRS (RC3243)

20-Aug-1999 1

APO AE 09180

QC000000

236TH MED CO(AA)UH-60-99-ASAM-12 INSP INTERVAL CHANGEFOR HAMILTON STANDARD HYDOMECHANICAL UNITS P/N4046T52G01/04/06/09/11 USED ON T700-GE700ENGINES C/W AT ACFT HRS BY SSG J.MITSCHT.I. (JM1943)

30-Aug-1999 1

APO AE 09180

QC000000

236TH MED CO(AA)UH-60-99-ASAM-09 ONE TIME INSP FOR M/RBLADE PINS FOR "OUTER" SEGMENTSWITHOUT EXPANSION SLOTS OR HAVING PN70103-08107-101. (GR2306)

31-Aug-1999 1

APO AE 09180

QC000000

236TH MED CO(AA)UH-60-00-ASAM-01/TB1-1520-237-20-215CHANGE TO M/R HUB NDI FROM 100 HR TO200 HR RECURRING INSPECTION C/W @ 2403ACFT HRS (JM1943)

03-Dec-1999 1

APO AE 09180

QC000000

236TH MED CO(AA)AWR ELT AWR FOR EMERGENCY LOCATORTRANSMITTER(ELT) INSTALLATION ANDTESTING PROCEDURES ON ALL US ARMYAIRCRAFT INCORPORATING ELTS (MJ3055)

17-Dec-1999 1

APO AE 09180

QC000000

236TH MED CO(AA)UH-60-00-ASAM-02/TB 1-1520-237-20-216 ONETIME INSP OF PILOT/COPILOTS CYCLIC STICKWIRING BUNDLES C/W @ 2406.2 ACFT HRS(GR2306)

20-Dec-1999 1

APO AE 09180

QC000000

236TH MED CO(AA)UH-60-00-ASAM-03/TB 1-1520-237-20-217 ONETIME INSP AND REMOVAL OF SUSPECTPRIMARY SERVO ASSEMBLI C/W @ 2406.2ACFT HRS (GR2306)

03-Jan-2000 1

APO AE 09180

QC000000



8.7.DATE

6.REMARKS

4. 5.



236TH MED CO(AA)UH-60-00-ASAM-04/TB 1-1520-237-20-218 ALL H-60 ACFT INSP OF T/L/G SHOCK STRUT ASSYFOR MISSING BEARING RETENTION PIN C/W@ 2412.9 ACFT HRS (AJ1671)

01-Mar-2000 1

APO AE 09180

QC000000

236TH MED CO(AA)UH-60-00-ASAM-05/TB 1-1520-237-20-219 ONETIME INSP OF FIRE EXTINGUISHER WIRINGC/W @ 2432.9 ACFT HRS (PD3396)

23-May-2000 1

APO AE 09180

QC000000

AMCOM-E OLRJACE/CPCE PERFORMED AT 2439.5 ACFT HRSAT LANDSTUHL, GE BY MEMBER CC (IK3963)

12-Jun-2000 1

HUNTSVILLE AL

QC000000

236TH MED CO (AA)UH-60-00-ASAM-06 / TB 1-1520-237-20-219 CH1REVISION TO UH-60-00-ASAM-05 ADDING TAIL#91-26318 THRU 91-26367 NA THIS ACFT(PD3396)

26-Jun-2000 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-00-SOF-01 INSPECTION OF M/RSPINDLE LUGS C/W AT 2443.8 ACFT HRS(CL1490)

12-Jul-2000 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-00-SOF-02 REMOVAL OF INPUT MODGEARBOX ASSY WITH POTENTIALLY BEVELGEARS C/W @ 2450.5 ACFT HRS (RC3243)

10-Aug-2000 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-00-ASAM-07 / TB1-1520-237-20-224 ONETIME INSP OF WIRE HARNESS CONNECTINGNO.1 AND NO.2 JUNCTION BOXES C/W @2458.2 ACFT HRS (PD3396)

05-Sep-2000 1

APO AE 09180

QC000000

2-502 AVNN REGTUH-60-01-SOF-01 / TB1-1520-237-20-255 DRAGBEAM ASSEMBLY C/W AT 2471.7 ACFT HRS(EW2953)

13-Nov-2000 1

APO AE 09028

QC000000

2-502 AVNN REGTUH-60-01-SOF-02 / TB1-1520-237-20-255REVISION TO UH-60-01-01 INITIAL ANDRECURRING INSP OF M/L/G DRAG BEAM ASSYC/W @2471.7 ACFT HRS (EW2953)

02-Jan-2001 1

APO AE 09028

QC000000

2-502 AVNN REGTUH-60-01-SOF-03 / TB1-1520-237-20-229REMOVAL OF PURDY LATERAL BELLCRANKASSY C/W AT 2471.7 AFT HRS (EW2953)

08-Jan-2001 1

APO AE 09028

QC000000

2-502 AVNN REGTPMS-2 COMPLETED @ 2471.7 ACFT HRS, NEXTPMS-2 DUE AT 2971.7 ACFT HRS (EW2953)

08-Jan-2001 2

APO AE 09028

QC000000

2-502 AVNN REGTUH-60-01-SOF-04 / TB1-1520-237-20-228 RISKMANAGEMENT OF 230 GAL EXTERNAL TANKFLIGHT OPNS. AND FOR FUEL MONITORINGSYS MWO 1-1520-237-50-78. NA THIS ACFT.ACFT HAS SOFT POINTS, C/W @ 2471.7 ACFTHRS (EW2953)

09-Jan-2001 1

APO AE 09028

QC000000

236TH MED CO (AA)AWR944 UH-60L PERFORMANCE PLANNINGCARD (PPC) (AWR944) (EW2953)

16-Mar-2001 1

APO AE 09180

QC000000

236TH MED CO (AA)AWR893R3 AIRWORTHINESS RELEASE FORUH-60A/L HELICOPTERS WITH VERTICALSUPPORT PYLON FAIRING MODIFICATIONS(MJ3055)

19-Mar-2001 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-01-SOF-06 / TB1-1520-237-20-231 INSPSAS ACTUATORS FOR INSTALLATION OFSAFETY CABLE AND POSSIBLE DAMAGE,COMPLETED @ 2480.7 ACFT HRS (DH6609)

27-Mar-2001 1

APO AE 09180

QC000000



8.7.DATE

6.REMARKS

4. 5.



236TH MED CO (AA)UH-60-01-SOF-05 / TB1-1520-237-20-230ULTRASOUND INSPECTION OF MAIN ROTORSPINDLE LUGS C/W AT 2482.2 ACFT HRS(JM1238)

06-Apr-2001 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-01-SOF-07 INSPECTION OF M/R FLIGHTCONTROL SELF LOCKING BOLTS COMPLIEDWITH AT 2504.1 ACFT HRS (CL1490)

07-Jun-2001 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-01-SOF-08 REVISION TO UH-60-01-07,INSPECTION OF M/R FLIGHT CONTROL SELFLOCKING BOLTS C/W @ 2504.1 ACFT HRS(CL1490)

08-Jun-2001 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-01-SOF-09 INSPECTION OF M/REXPANDABLE PINS COMPLIED WITH @ 2511.8ACFT HRS (CL1490)

11-Jun-2001 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-01-SOF-10 TB1-1520-237-20-234 ONETIME INSP OF MAIN ROTOR BLADEEXPANDABLE PINS C/W @ 2511.8 ACFT HRS(RC3243)

19-Jul-2001 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-01-SOF-11 TB1-1520-237-20-235 INSPM/R HUB C/W AT 2524.6 ACFT HRS (JM1943)

24-Aug-2001 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-01-SOF-12 TB1-1520-237-20-236 INSPEXPANDABLE PINS C/W @ 2524.6 ACFT HRS(JM1943)

24-Aug-2001 2

APO AE 09180

QC000000

236TH MED CO (AA)AWR920 BAMBI WATER BCKET INCLUDINGCH3 (AWR920) (MJ3055)

06-Sep-2001 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-02-ASAM-01 / TB1-1520-237-20-239 INSPT/R BLADE FAIRING ASSY C/W @ 2565.3 ACFTHRS (JM1943)

19-Nov-2001 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-02-SO-01 / TB1-1520-237-20-240 INSP OILCOOLER FAN SHAFT ASSY FWD MOUNTFLANGE C/W @ 2565.3 ACFT HRS (JM1943)

20-Nov-2001 1

APO AE 09180

QC000000

AMCOM-E OLRACE/CPCE PERFORMED AT 2569.0 ACFT HRSAT LANDSTUHL GERMANY BY CC & KK(RR2743)

04-Dec-2001 1

HUNTSVILLE, AL

QC000000

236TH ME CO (AA)UH-60-02-SOF-02 TB1-1520-237-20-237INSPECT M/R HUB FOR ELIGIBILITY FORREWORK C/W @ 2512.0 ACFT HRS (RR2743)

10-Dec-2001 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-SOF-03 TB1-1520-237-20-241INSPECT M/R FLIGHT CONTROL PITCH TRIMC/W @ 2532.0 ACFT HRS (RR2743)

11-Dec-2001 1

APO AE 09180

QC000000

236TH ME CO (AA)AWR917R3 FOR FM IMMUNE AN/ARN-147VOR/ILS RECEIVERS 622-6376-020 IN THESTANDARD CONFIGUTATION AND FM IMMUNEAN/ARN-147 VOR/ILS RECEIVERS PIN 622-6376-020 WITH THE VIM-123 ADAPTER TRAYMOUNT IN AN/ARN-123 CONFIGURED UH-60A/L (RR2743)

21-Dec-2001 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-SOF-04 TB1-1520-237-20-242 INSPAPU SHROUD FOR PROPER GROMMET @2573.0 ACFT HRS SPU SN876079 (SC1642)

28-Jan-2002 1

APO AE 09180

QC000000

236TH ME CO (AA)AWR999 UH-60A/L HELICOPTERS TOCONDUCT OPERATIONS ABOARD LHA 1CLASS SHIPS (MJ3055)

02-Feb-2002 1

APO AE 09180

QC000000



8.7.DATE

6.REMARKS

4. 5.



236TH ME CO (AA)UH-60-02-SOF-05 TB1-1520-237-20-243 INSPM/R EXPANDABLE PINS C/W @ 2576.5 ACFTHRS (RC3243)

07-Feb-2002 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-ASAM-02 TB1-1520-237-20-246 INSPFLIGHT CONTROL ROD JAMNUTS C/W @2577.5 ACFT HRS (RC3243)

08-Feb-2002 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-ASAM-03 TB1-1520-237-20-245 INSPENGINE PCL QUADRANT C/W @ 2577.5 ACFTHRS (RM6604)

20-Feb-2002 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-ASAM-04 TB1-1520-237-20-244 INSPALL SEAT RESTRAINT SYSTEMS C/W @ 2594.6ACFT HRS (RM6604)

20-Mar-2002 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-ASAM-05 TB1-1520-237-20-251 INSPALL MAIN ROTOR SPINDLE ASSY C/W @2597.6 ACFT HRS (RM6604)

28-Mar-2002 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-SOF-06 REVISION TO MAIN ROTORHHUB NDI PROCEDURES UH-60-02-06 TB1-1520-237-20-23-1 DOES NOT REQUIRECOMPLIANCE AND ENTERED ON TM 1-1520-237-23-1 (RR9167)

23-Apr-2002 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-ASAM-06 INSP SWAGE/COLLAR PINSON COLL/ YAW BOOST SERVOS C/W @ 2625.9ACFT HRS (JM1943)

30-Apr-2002 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-SOF-07 TB1-1520-237-20-255 INSPACFT MAIN MOD HISTORICALS C/W @ 2625.9ACFT HRS (RM6604)

06-May-2002 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-SOF-09 TB1-1520-237-20-258 MAINMOD PLANETARY CARRIER ASSEMBLY C/W @2626.3 ACFT HRS (RM6604)

30-May-2002 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-SOF-10 TB1-1520-237-20-258 MAINMOD PLANETARY CARRIER ASSEMBLY C/W @2626.3 ACFT HRS (JM1943)

08-Jun-2002 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-ASAM-08 INSPECT ARC-220 WIRINGC/W @ 2631.4 ACFT HRS (JM1943)

21-Jun-2002 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-ASAM-09 INSPECT TAIL ROTORQUADRANT HDWR C/W @ 2631.4 ACFT HRS(JM1943)

21-Jun-2002 2

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-ASAM-10 INSP AERIAL REFUELPROBE NOZZLES NA THIS ACFT (JM1943)

25-Jun-2002 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-SOF-11 INSP M/R BLADE CUFF C/W@ 2641.7ACFT HRS (RB6944)

10-Aug-2002 1

APO AE 09180

QC000000

236TH ME CO (AA)UH-60-02-SOF-12 INSP M/R BLADE CUFFREVISION C/W@ 2641.7 ACFT HRS (RB6944)

13-Aug-2002 1

APO AE 09180

QC000000

AMCOM-E OLRACE/CPCE PERFORMED AT 2648.4 AIRCRAFTHRS @ LANDSTUHL GERMANY BY MEMBERCC (IK3963)

15-Aug-2002 1

HUNTSVILLE, AL

QC000000

236TH MED CO (AA)UH-60-02-ASAM-11 INSP OF ARC-220 WIRINGC/W @ 2654.3 ACFT HRS (RB6944)

30-Sep-2002 1

APO AE 09180

QC000000



8.7.DATE

6.REMARKS

4. 5.



236TH MED CO (AA)AWR980 FOR USE OF FOREST PENETRATORIN UH-60 SERIES HELICOPTERS DTD 21DEC01(JM1943)

04-Oct-2002 1

APO AE 09180

QC000000

236TH MED CO (AA)AWR967 FOR USE OF FM IMMUNE AN/ARN-123VOR/ILS IN UH-60 SERIES HELICOPTERS DTD25MAY01 (JM1943)

04-Oct-2002 2

APO AE 09180

QC000000

236TH MED CO (AA)AWR524 FOR USE OF PLS IN UH-60 SERIESHELICOPTERS DTD 12JAN99 (JM1943)

04-Oct-2002 3

APO AE 09180

QC000000

236TH MED CO (AA)AWR543 FOR USE OF ELT IN UH-60 SERIESHELICOPTERS DTD 15JAN99 (JM1943)

04-Oct-2002 4

APO AE 09180

QC000000

236TH MED CO (AA)AWRFOR USE OF TACAN IN UH60 SERIESHELICOPTERS DTD 25NOV91 (JM1943)

04-Oct-2002 5

APO AE 09180

QC000000

236TH MED CO (AA)AWR FOR USE OF CEP ON UH-60 SERIESHELICOPTERS DTD 14JUL99 (JM1943)

04-Oct-2002 6

APO AE 09180

QC000000

236TH MED CO (AA)AWR1054 AIRWORTHINESS RELEASE (AWR)FOR UH-60A/L HELICOPTERS EQUIPPED WITHSEI INDUSTRIES BAMBI WATER BUCKETS(MJ3055)

23-Oct-2002 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-03-SOF-01 MAIN MOD PLANETARYCARRIER APPLIED@ 2675.0 ACFT HRS(JC1421)

20-Nov-2002 1

APO AE 09180

QC000000

236TH MED CO (AA)AWR980R3 AIRWORTHINESS RELEASE FORUSE OF FOREST PENETRATOR, SURVIVOR*SSLING, SKED RESCUE SYSTEM, RESCUE NET,AND RESCUE STROP WITH UH-60A/L UH-60QAND HH-60L HELICOPTERS EQUIPPED WITHRESCUE HOIST SYSTEM KIT (MJ3055)

03-Dec-2002 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-03-ASAM-01 BELLCRANK FWDSUPPORT @ 2687.5 ACFFT HRS (JC1421)

10-Dec-2002 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-03-ASAM-02 T/R SERVO @ 2688.7 ACFTHRS (RB6944)

12-Dec-2002 1

APO AE 09180

QC000000

236TH MED CO (AA)GEN-03-ASAM-01 SINGARS ARC-201 BATTERYBOX (RR9167)

17-Dec-2002 1

APO AE 09180

QC000000

236TH MED CO (AA)GEN-03-ASAM-01 INSP OF BATTERY BOX CY-85815 C/W @ 2695.4 ACFT HRS (RB6944)

18-Dec-2002 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-03-SOF-01 INSP AND NDI OF MAINTRANSMISSION PLANETARY CARRIER ASSYC/W (AK6390)

01-Jan-2003 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-03-ASAM-03 PERFORMANCE PLANNINGDURING DESERT COMBAT OPERATIONS(JC1421)

18-Feb-2003 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-03-SOF-03 MAIN MOD PLANETARYCARRIER RETIREMENT LIFE C/W @ 2711.5ACFT HRS (JC1421)

18-Feb-2003 2

APO AE 09180

QC000000

236TH MED CO (AA)EXTENSION FOR FLIGHT CONTROL RODINSPECTION GRANTED @ 06FEB03 2699.6ACFT HRS; LETTER OF EXTENSION WILL BEMAINTAINING IN HISTORICAL FILES (JC1421)

18-Feb-2003 3

APO AE 09180

QC000000



8.7.DATE

6.REMARKS

4. 5.



236TH MED CO (AA)UH-60-03-SOF-04 REVISION OG UH-60-03-03MAIN MOD PLANETARY CARRIER ASSYRETIREMENT LIFE C/W @ 2800.2 ACFT HRSNOT APPLICABLE THIS ACFT (JC1421)

29-May-2003 1

APO AE 09180

QC000000

236TH MED CO (AA)INSP A665 FLIGHT CONTROL RODINSPECTION COMPLETED@ 2800.2 ACFT HRS20030530 (BG1476)

30-May-2003 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-03-SOF-02 INSPECTION OF MAINROTOR BLADE CUFF ASSY (JM1943)

15-Jun-2003 1

APO AE 09180

QC000000

236TH MED CO (AA)AWR1111R1 AIRWORTHINESS RELEASE FORUH-60A/L DESERT COMBAT OPERATIONSWITH THE PILOT AND COPILOTS DOORSREMOVED (AWR1111) (MJ3055)

01-Jul-2003 1

APO AE 09180

QC000000

236TH MED CO (AA)ACE/CPCE PERFORMED AT 2803.4 ACFT HRSBY KK AT LANDSTUHL GERMANY (RR2743)

23-Jul-2003 1

APO AE 09180

QC000000

236TH MED CO (AA)INSP A669 CABIN TUB INSPECTIONCOMPLETED @ 2803.4 ACFT HRS (BG1476)

30-Jul-2003 1

APO AE 09180

QC000000

236TH MED CO (AA)AWR1127 FOR UH-60A/L HELICOPTERS TOCONDUCT HELLASKET OPERATIONS WITHELECTRIC LONG LINE (RR9167)

08-Aug-2003 1

APO AE 09180

QC000000

236TH MED CO (AA)AWR1119R1 AIRWORTHINESS RELEASE FORUH-60A/L OPERATIONS DURING DESERTCOMBAT OPERATIONS (MJ3055)

12-Aug-2003 1

APO AE 09180

QC000000

236TH MED CO (AA)AWR1124R0 AIRWORTHINESS RELEASE FORUH-60A/L TO CONDUCT OPERATIONSABOARD LHA CLASS SHIPS (RR9167)

15-Aug-2003 1

APO AE 09180

QC000000

236TH MED CO (AA)AWR 911R4 AIRWORTHINESS RELEASE FORUH-60A/L HELICOPTERS EQUIPPED WITHAUXILIARY POWER UNIT (APU) INLETBARRIER FILTERS (MJ3055)

15-Aug-2003 2

APO AE 09180

QC000000

236TH MED CO (AA)AWR1128R0 AIRWORTHINESS RELEASE FORUH-60A/L HELICOPTERS TO PERFORM HIGHAMBIENT TEMPERATURE ENGINE STARTS INDESERT COMBAT OPERATIONS (RR9167)

20-Aug-2003 1

APO AE 09180

QC000000

236TH MED CO (AA)LATE ENTRY UH-60-04-SOF-01 ALL UH-60AAND UH-60Q SERIES AIRCRAFT, FORWARDBELLCRANK SUPPORT INSTALLATIONHARDWARE (RR9167)

03-Oct-2003 1

APO AE 09180

QC000000

236TH MED CO (AA)AWR 548 NO LONGER REQUIRED RMVD FROMACFT AS PER UH-60 PMO (AK6390)

23-Oct-2003 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-04-ASAM-01 ALL UH-60A/L AIRCRAFT,GLARE SHIELD LIGHTING CIRCUIT BREAKERREPLACEMENT AT NEXT PMS2 BUT NLT31JAN05 (RR9167)

30-Jan-2004 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-04-MIM-06 CHANGE IN COMPONENTLIFE TRACKING FROM THE SHOCK STRUTASSEMBLY TO THE PISTON CYLINDER ASSY(RR9167)

08-Mar-2004 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-04-ASAM-02 TAILL ROTOR DRIVEFLANGE NUT C/W @ 2878.1 ACFT HRS(AK6390)

01-Apr-2004 1

APO AE 09180

QC000000



8.7.DATE

6.REMARKS

4. 5.



236TH MED CO (AA)UH-60-04-ASAM-03 ALL H-60 SERIES ACFT,FUEL SYSTEM INTEGRITY CHECKS NLT15APR06 (RR9167)

08-Apr-2004 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-04-SOF-02 DISABLING OF COCKPITAIRBAG SYSTEM COMPLIED WITH ON10JUN2004 (MJ3055)

10-Jun-2004 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-04-SOF-04 MAIN ROTOR HUBSUBASSEMBLY REWORK COMPLETED @2933.1 ACFT HRS (TM9308)

12-Aug-2004 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-05-ASAM-01 REVISION OF FUELSYSTEM INTEGRITY CHECKS C/W @ 2933.1ACFT HRS (TM9308)

04-Jan-2005 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-02-ASAM-03 INSP AND MODIFICATIONOF PCL QUADRANT (DH4124)

15-Feb-2005 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-05-ASAM-02 BLUE FORCE TRACKER(BFT) NA THIS ACFT (DF9665)

03-Mar-2005 1

APO AE 09180

QC000000

236TH MED CO (AA)EMC CHECK COMPLETED FOR THE HAVEQUICK II AWR DTD 02JUN1998 ON 16FEB2005ON LIKE MODEL ACFT 8223753 @ 3315.4 ACFTHRS (DF9665)

09-Mar-2005 1

APO AE 09180

QC000000

236TH MED CO (AA)EMC CHECK COMPLETED FOR THE TACANIAW AWR DTD 23JUN1999 ON 16FEB2005 ONLIKE MODEL ACFT 8223753 @ 3315.4 ACFTHRS (BS4235)

09-Mar-2005 2

APO AE 09180

QC000000

236TH MED CO (AA)EMC CHECK COMPLETED FOR THE PLS IAWAWR DTD 12JAN1999 ON 16FEB2005 ON LIKEMODEL ACFT 8223753 @ 3315.4 ACFT HRS(BS4235)

09-Mar-2005 3

APO AE 09180

QC000000

236TH MED CO (AA)EMC CHECK COMPLETED FOR THE GPS IAWAWR DTD 02DEC1998 ON 16FEB2005 ON LIKEMODEL ACFT 8223753 @ 3315.4 ACFT HRS(BS4235)

09-Mar-2005 4

APO AE 09180

QC000000

236TH MED CO (AA)EMC CHECK COMPLETED FOR THE FMIMMUNE IAW AWR DTD 25MAY2001 ON16FEB2005 ON LIKE MODEL ACFT 8223753 @3315.4 ACFT HRS (BS4235)

09-Mar-2005 5

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-05-ASAM-03 AIRCREW RESTRAIINTSYSTEM COMPATABILITY C/W @ 3932.3 ACFTHRS (AG3649)

07-Apr-2005 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-05-ASAM-04 TAIL LANDING GEAR YOKEASSEMBLY C/W @ 3932.3 ACFT HRS (AG3649)

07-Apr-2005 2

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-05-ASAM-05 RIGHT TIE RODINSPECTION COMPLETED ON 20050426(AG3649)

21-Apr-2005 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-04-SOF-04 M/R HUB MODIFIED ATTT:3402 HRS IAW S.O.#DK005296 ANDENGINEERING #70700-10046. MODIFIED PN:70103-08112-041 TO 70070-10046-055SIKORSKY AIRCRAFT. ARTHUR RUSSELL(AG3649)

22-Apr-2005 1

APO AE 09180

QC000000

236TH MED CO (AA)UH-60-05-ASAM-06 TROOP RESTRAINTBUCKLE C/W @ 2932.00 ACFT HRS (TM8433)

27-Apr-2005 1

APO AE 09180

QC000000



8.7.DATE

6.REMARKS

4. 5.



DYNACORP-E OLRUH-60-05-ASAM-06 TROOP RESTRAINTBUCKLE C/W @ 2932.00 ACFT HRS (SH0481)

27-Jun-2005 1

APO AE 09058

QC000000

2-502 AVN REGTUH-60-05-SOF-02 ENHANCED SCHEDULEDMAINTENANCE PROGRAM (ESM) @ 2933.1ACFT HRS (TM9308)

25-Jul-2005 1

APO AE 09058

QC000000

2-502 AVN REGTPMS-II COMPLETED @ 2933.1 ACFTHOURS.PARTS REPLACED M/R HUB ASSY,MAIN TRANSMISSION MODULE, #2 ENG HIGHSPEED SHAFT, ENG. ANTI-ICING VALVE, 2EAM/R DAMPERS, R/H TIE ROD, 4EA BALL BRNGANNUAL, 2EA SPHERICAL BRNGS, T/R PITCHCHANGE SHAFT, COLD SECTION MODULE, &POWER TURBINE MODULE, NEXT PMI-1 @3282.1 ACFT HRS (TM9308)

01-Aug-2005 1

APO AE 09058

QC000000

2-502 AVN REGTUH-60-05-ASAM-09 CRASHWORHTYEXTERNAL FUEL SYSTEM (CEFS)INSTALLATION BOLTS. NA THIS AIRCRAFTC/W @ 2933.1 ACFT HRS (TM9308)

02-Aug-2005 1

APO AE 09058

QC000000

2-502 AVN REGTUH-60-05-ASAM-10 COMPLETED @ 2936.6AIRCRAFT HRS #1 AND #2 ENGINE OUTPUTSHAFT INSPECTION (TM9308)

15-Aug-2005 1

APO AE 09058

QC000000

2-502 AVN REGTUH-60-05-ASAM-07 AIR INTRUSION OFHYDRAULIC SYSTEM C/W @ 2933.1 ACFTHRSDURING PMS-2 29JUL05 (DL3855)

25-Aug-2005 1

APO AE 09058

QC000000

2-502 AVN REGTUH-60-05-SOF-01 COCKPIT AIRBAG SYSTEM(CABS) REACTIVATION , NA THIS ACFT @2933.1 ACFT HRS DURING PMS-2 29JUL05(DL3855)

25-Aug-2005 2

APO AE 09058

QC000000

2-502 AVN REGTUH-60-04-SOF-04 CRASHWORHTY EXTERNALFUEL SYSTEM DOES NOT APPLY @ 2933.1ACFT HRS DURING PMS-2 24JUN05 (DL3855)

25-Aug-2005 3

APO AE 09058

QC000000

2-502 AVN REGTUH-60-05-ASAM-08 TIE ROD ASSYREINSPECTION C/W @ 293.1 2-502COMPLETED DURING PMS-2 16JUN05 (DL3855)

25-Aug-2005 4

APO AE 09058

QC000000

45TH MED CO (AA)LATE ENTRY - UH-60-97-ASAM-10 FATIGUELIFE FOR THE MAIN SUPPORT BRIDGE PN70400-0811-048 NA THIS ACFT 2 2943.5 ACFTHRS (DL3855)

06-Sep-2005 1

APO AE 09250

QC000000

45TH MED CO (AA)LATE ENTRY - UH-60-02-SOF-08 MAIN MODPLANETARYY CARRIER ASSEMBLY NA THISACFT @ 2943.5 ACFT HRS (DL3855)

06-Sep-2005 2

APO AE 09250

QC000000

45TH MED CO (AA)UH-60-02-ASAM-04 H-60 SERIES HELICOPTERSRESTRAINT SYSTEM INSPECTION C/W 22943.5 ACFT HRS (DL3855)

06-Sep-2005 3

APO AE 09250

QC000000

159TH MED CO (AA)ACFT LOGBOOK AND HISTORICALINFORMATION WAS TRANSFERED OVERFROM ULLS-A SCP5 TO ULLS-A SCP6(AG3649)

02-Nov-2005 1

APO AE 09096

QC000000

159TH MED CO (AA)UH-60-05-ASAM-11 UH-60 ACFT WIRINGHARNESS CHAFFING C/W @ 2960.4 ACFT HRS(DW1719)

06-Dec-2005 1

APO AE 09096

QC000000

159TH MED CO (AA)UH-60-06-ASAM-01 TAIL LANDING GEARSHOCK STRUT C/W @ 2963.2 ACFT HRS(TM8433)

15-Dec-2005 1

APO AE 09096

QC000000



8.7.DATE

6.REMARKS

4. 5.



159TH MED CO (AA)UH-60-06-SOF-01 MAIN ROTOR HUBINSPECTION C/W @ 2963.2 ACFT HRS (TM8433)

22-Dec-2005 1

APO AE 09096

QC000000

159TH MED CO (AA)BALLASTIC ARMOR PROTECTION SYSTEM(BPS) INSTALLED BY AVUM MAINTENANCEON 20060208 (AG3649)

10-Feb-2006 1

APO AE 09096

QC000000

159TH MED CO (AA)DESERT BLUE FORCE TRACKER, COMMONMISSLE WARNING SYSTEM AND EIBF TOINCLUDE HIGH PERFORMANCE HOIST POWERON EMC CHECKS COMPLETD (AG3649)

11-Feb-2006 1

APO AE 09096

QC000000

159TH MED CO (AA)EMC COMPLETED FOR SATCOM SYSTEM IAWAWR DTD 5SEP03ON 15MAR06 ON LIKE ACFT8926146, 2794.2 ACFT HRS (DW1719)

20-Mar-2006 1

APO AE 09096

QC000000

159TH MED CO (AA)SATCOM INSTALLED IAW AWR DTD 5SEP03(DW1719)

20-Mar-2006 2

APO AE 09096

QC000000

159TH MED CO (AA)TAIL ROTOR GEARBOX CHIP DECTECTORILLUMINATED IN FLIGHT. UPON ARRIVAL OFTHE AIRCRAFT, THE CHIP DETECTOR WASPULLED AND PARTICLES ON THE CHIPDETECTOR WERE OBSERVED. QUALITYCONTROL DETERMINED THAT THE T/RGEARBOX WAS GOOD, AND TO PERFORM A15 MINUTE GROUND RUN TO SEE IF CHIPLIGHT ILLUMINATES AGAIN. GEARBOX WASRETURNED TO SERVICE AT 3006.7ACFT HRS(DW1719)

05-Apr-2006 1

APO AE 09096

QC000000

159TH MED CO (AA)UH-60-06-ASAM-02 COMPLETED ON THISDATE @ 3031.4 ACFT HRS (DW1719)

27-Apr-2006 1

APO AE 09096

QC000000

159TH MED CO (AA)DOOR OFF MWO APPLIED IAW AWR 1279 DTD6JUL05 (AG3649)

03-Jun-2006 1

APO AE 09096

QC000000

159TH MED CO (AA)UH-60-06-ASAM-04 ACFT COCKPIT AIRBAGSYSTEM ELCTRONIC CRASH SENSOR, NATHIS ACFT (AG3649)

24-Jun-2006 1

APO AE 09096

QC000000

159TH MED CO (AA)UH-60-06-SOF-02 DISABLING OF COCKPITAIRBAG SYSTEM NA THIS ACFT (AG3649)

24-Jun-2006 2

APO AE 09096

QC000000

159TH MED CO (AA)UH-60-06-ASAM-03 C/W @ 3100.5 ACFT HRSTHIS DATE PLAY WAS .002 INCH (DF9665)

13-Jul-2006 1

APO AE 09096

QC000000

159TH MED CO (AA)INSTALLATION OF HOIST CABLE GUARDDEFLECTOR IAW ISAQ-103 (DW1719)

31-Jul-2006 1

APO AE 09096

QC000000

159TH MED CO (AA)UH-60-06-ASAM-05 BLUE FORCE TRACKERHARDWARE INSTALLATION COMPLIED WITH@ 3142.8 ACFT HRS (DW1719)

15-Aug-2006 1

APO AE 09096

QC000000

159TH MED CO (AA)LATE ENTRY ACFT ARRIVED TOAFGHANISTAN ON 5FEB06 @2964.0 ACFT HRS(AG3649)

10-Nov-2006 1

APO AE 09096

QC000000

159TH MED CO (AA)WHITE ENGINE/AIRFRAME HARNESSASSEMBLY ON BOTH #1 AND #2 ENGREQUIRES RELOCATION IAW UH-60-07-ASAM-01 COMPLIED WITH (DW1719)

22-Dec-2006 1

APO AE 09096

QC000000

159TH MED CO (AA)UH-60-07-ASAM-03 COMPLIED WITH ON22DEC2006 (AG3649)

22-Dec-2006 2

APO AE 09096

QC000000



8.7.DATE

6.REMARKS

4. 5.



159TH MED CO (AA)WHITE ENGINE/AIRFRAME HARNESSASSEMBLY ON BOTH #1 AND #2 ENGREQUIRES RELOCATION IAW UH-60-07-ASAM-02 COMPLIED WITH (AG3649)

27-Dec-2006 1

APO AE 09096

QC000000

159TH MED CO (AA)UH-60-07-ASAM-04 COMPLIED WITH ON 29DEC 2006 (AG3649)

29-Dec-2006 1

APO AE 09096

QC000000

C CO 3/82 GSABPMI-1 COMPLETED @ 3293 ACFT HRS, NEXTPMI-2 DUE @ 3653.0 ACFT HRS (JD9782)

29-Jan-2007 1

BAGRAM,AFGHANISTAN

QC000000

DCO 3-82 GSABAIRCRAFT HISTORICAL RECORDS ANDLOGBOOK ENTERED FROM ULLS-A SCP6 TOULLS-A SCP5 ON THIS DATE (RH4586)

03-Feb-2007 1

APO AE 09354

QC000000

D CO 3-82 GSABUH-60-07-ASAM-05, H-60 ARC-220/KY100START UP PROCEDURES C/W THIS DATE.

20-Feb-2007 1

FT. BRAGG, NC 28310

JS544833

DCO 3-82 GSABMAIN TRANSMISSION REPLACED AT 3352ACFT HRS. M/R RIG COMPLETED AT THISTIME, READINGS ARE AS FOLLOWS; RED 10.0,BLUE 10.1, YEL 10.2, BLK 10.1, LOW COLL:90/10.0, 180/-.5, 270/-11.4, 0/-.4, TTL/-2.3, AVG/-.575. HIGH COLL: 90/21.4, 180/12.2, 270/8.7,0/18.1, TTL/60.4, AVG/15.1. FWD CYC/HIGHCOLL: 90/-1.4, 270/33.0, TTL/34.4. AFTCYC/HIGH COLL90/24.2, 270/4.9, TTL/19.3. LEFTCYC/LOW COLL: 180/9.3, 0/5.9, TTL/15.2. RTCYC/LOW COLL: 180/6.0, 0/9.5, TTL/15.5.(RH4586)

07-Apr-2007 1

APO AE 09354

QC000000

DCO 3-82 GSABCONTINUED M/R RIG COMPLETED AT THISTIME, READINGS ARE AS FOLLOWS; PRIMARYSERVO CONTROL ROD BIAS: FWD:LENGTHENED 3/4 TURN AFT: SHORTENED 3/4TURN LAT: SHORTENED 1/2 TURN (RH4586)

07-Apr-2007 2

APO AE 09354

QC000000

C CO 3-82 GSABUH-60-07-AMAM-01 CMWS INSTALLATIONINSP C/W ON THIS DATE AT 3357.0 ACFT HRS(JD9782)

21-Apr-2007 1

BAGRAM,AFGHANISTAN

QC000000

C CO 3-82 GSABUH-60-07-ASAM-07 N/A TO THIS ACFT 3391ACFT HRS (CEFS FUEL LINE BONDINGJUMPERS) (JD9782)

14-May-2007 1

APO AE 09354

QC000000

C CO 3/82 GSABUH-60-07-ASAM-08 CERTAIN HMU P/NS C/WTHIS DATE (JD9782)

19-Jul-2007 1

BAGRAM,AFGHANISTAN

QC000000

C CO 3/82 GSABUH-60-07-ASAM-09 CERTAIN DEC S/NS C/WTHIS DATE (JD9782)

26-Jul-2007 1

BAGRAM,AFGHANISTAN

QC000000

L-3 VERTEXMEC LE-BAL016-0150 (INPUT MODULECORROSION) APPLIED TO THIS ACFT THISDATE AT 3555.0 ACFT HRS. INSPECTIONREQ*D AT EACH PMI FOR PITTINGPROGRESSION. (KC8146)

06-Aug-2007 1

BAGRAM,AFGHANISTAN

QC000000

C CO 3/82 GSABUH-60-07-ASAM-10 MANIFOLD FUEL SUPPLYLINE C/W THIS DATE AT 3557 ACFT HRS(JD9782)

17-Aug-2007 1

BAGRAM,AFGHANISTAN

QC000000



8.7.DATE

6.REMARKS

4. 5.



L-3 VERTEX CFTOTR 2007-20 REPAIR OF CORROSION ONVERTICAL FIN ANTENNA COMPLETED20071006 AT 3633.9 ACFT HRS (RT8352)

06-Oct-2007 1

BAGRAM,AFGHANISTAN

QC000000

L-3 VERTEX CFTOPTION II (MAVEN) CABIN HEATER MODINSTALLED 20071006 AT 3633.9 ACFT HRS(RT8352)

06-Oct-2007 2

BAGRAM,AFGHANISTAN

QC000000

L-3 VERTEX CFT701D ENGINE MOD INSTALLED 20071006 AT3633.9 ACFT HRS (RT8352)

06-Oct-2007 3

BAGRAM,AFGHANISTAN

QC000000

L-3 VERTEX CFTM/R RIG COMPLETED THIS DATE 3633.9 ACFTHRS. READINGS ARE AS FOLLOWS: RED 9.2,BLUE 9.2, YLW 9.1, BLK 9.2; LOW COLL: 90/9.2,180/-1.2, 0/0.1, TTL/2.2, AVG/-,550; HIGH COLL:90/19.9, 180/11.3, 270/10.3, 0/18.5, TTL/60,AVG/15.00; FWD CYC/HIGH COLL: 90/-2.2,270/31.1, TTL/33.3; AFT CYC/HIGH COLL:90/25.2, 270/4.6, TTL/20.6; LEFT CYC/LOWCOLL: 180/-9.1, 0/6.3, TTL/15.4; RIGHTCYC/LOW COLL: 180/7.5, 0/-7.3, TTL/14.8;(RT8352)

08-Oct-2007 1

BAGRAM,AFGHANISTAN

QC000000

L-3 VERTEX CFTCONTINUED M/R RIG COMPLETED AT THISDATE, READINGS ARE AS FOLLOWS;PRIMARY CONTROL ROD BIAS: FWD:SHORTENED 5 FLATS AFT: LENGTHENED 5FLATS LAT: 0 TURNS (RT8352)

08-Oct-2007 2

BAGRAM,AFGHANISTAN

QC000000

L-3 VERTEX CFTT/R RIG COMPLETED THIS DATE; BIAS INFOAS FOLLOWS:RED; START:5.180, FINISH:4.850,DIFF: .33 BLUE;START:4.450, FINISH:4.160,DIFF: .29 YLW; START:5.140, FINISH:4.820,DIFF: .32 BLK; START:4.520, FINISH:4.180,DIFF: .34 CABLE TENSION: L/H 136 R/H 135TEMP:21 DEG CELCIUS (RT8352)

08-Oct-2007 3

BAGRAM,AFGHANISTAN

QC000000

L-3 VERTEX CFTPMI-2 COMPLETED @ 3633.9 ACFT HRS, NEXTPMI-1 DUE @ 3993.9 ACFT HRS (RT8352)

10-Oct-2007 1

BAGRAM,AFGHANISTAN

QC000000

L-3 VERTEX CFTUH-60-08-ASAM-01 TROOP SEATS INSP C/WTHIS DATE AT 3633.9 ACFT HRS (RT8352)

12-Oct-2007 1

BAGRAM,AFGHANISTAN

QC000000

D CO 3-82 GSABT/R CABLE TENSION STABILIZED: L/H 130 R/H130 TEMP 18 DEGREES AVG 130 (SS6660)

17-Oct-2007 1

BAGRAM,AFGHANISTAN

QC000000

L-3 VERTEX CFTUH-60-08-AMAM-01 MAIN LANDING GEARSHOCK STRUTS, INSP C/W 20071022 AT 3642.9ACFT HRS (RT8352)

22-Oct-2007 1

BAGRAM,AFGHANISTAN

QC000000

L-3 VERTEX CFTACFT EXPERIENCED HARD LANDING20071016, HARD LANDING INSP COMPL20071023 IAW TM1-1520-237-23-12M/R HUBAND 4EA SPINDLE ASSY REPLACED DUE TOBLADES DROOPING, LARGE HOLE REPAIREDIN ACFT BELLY SKIN NEAR QUAD BAYANTENNA (RT8352)

23-Oct-2007 1

BAGRAM,AFGHANISTAN

QC000000



8.7.DATE

6.REMARKS

4. 5.



D CO 3-82 GSABH-60-08-ASAM-02 COMPLIED WITH @ 3686.9ACFT HRS (GD3161)

16-Nov-2007 1

BAGRAM,AFGHANISTAN

QC000000

D CO 3-82 GSABUH-60-08-AMAM-02 SUSPECT T/R O/B RETPLATE C/W THIS DATE (JD9782)

30-Nov-2007 1

BAGRAM,AFGHANISTAN

QC000000

D CO 3-82 GSABUH-60-08-ASAM-05 T/R QUADRANT SPRINGASSY TBO C/W THIS DATE (JD9782)

18-Dec-2007 1

BAGRAM,AFGHANISTAN

QC000000

D CO 3-82 GSABUH-60-08-ASAM-04 PILOT SEAT RAIL CHAFINGC/W THIS DATE (JD9782)

22-Dec-2007 1

BAGRAM,AFGHANISTAN

QC000000

D CO 3-82 GSABUH-60-08-AMAM-03 SUSPECT ENGINE OIL C/WTHIS DATE (JD9782)

23-Dec-2007 1

BAGRAM,AFGHANISTAN

QC000000

D CO 3-82 GSABUH-60-08-ASAM-03 FUEL INTEGRITY CHECKC/W THIS DATE AT 3737 ACFT HRS (JD9782)

04-Jan-2008 1

BAGRAM,AFGHANISTAN

QC000000

D CO 3-82 GSABAIRCRAFT RETURNED TO CONUS HOMESTATION AT FT BRAGG, NC FROMAFGHANISTAN OEF VIII ON 20080227 (JD9782)

27-Feb-2008 1

BAGRAM,AFGHANISTAN

QC000000

D CO 3-82 GSABH-60-08-AMAM-05 CERTAIN HOISTS SN/PN C/WTHIS DATE AT 3750.8 ACFT HRS (JD9782)

28-Feb-2008 1

BAGRAM,AFGHANISTAN

QC000000

D CO 3-82 GSABH-60-08-AMAM-06 CMWS SEQUENCER WIRINGC/W THIS DATE AT 3750.8 ACFT HRS (JD9782)

28-Feb-2008 2

BAGRAM,AFGHANISTAN

QC000000

D CO 3-82 GSABH-60-08-SOF-01 BLADE PIN INSP C/W THISDATE AT 3750.8 ACFT HRS (JD9782)

28-Feb-2008 3

BAGRAM,AFGHANISTAN

QC000000

D CO 3/82AWR 1479 MAIN MODULE ASSEMBLYEQUIPPED WITH THE IMPROVED PLANETARYCARRIER ASSEMBLY P/N 70351-08100-075APPLIED TO THIS AIRCRAFT AT 3555.0 HOURS

03-Apr-2008 1

FT BRAGG, NC 28310

RC048900

ALMB/DS2COMPLIED WITH REQUIREMENTS OF H-60-08-ASAM-06 (MAIN ROTOR PYLON SLIDINGFORWARD FAIRING) THIS DATE AT 3751.9ACFT HRS. UNIT COMPLETED

09-Apr-2008 1

FT BRAGG, NC

CH402079

DS2/OLRACE COMPLETED @ 3751.9 ACFT HRS BYTEAM MEMBERS "EE & VV".

11-Apr-2008 1

FT BRAGG, NC

JS544833

ALMB/DS2COMPLIED WITH REQUIREMENTS OF H-60-08-AMAM-04 (COCKPIT DOOR JETTISONABLEWINDOWS) THIS DATE AT 3751.9 ACFT HRS.REQUEST NEW SEALS

16-Apr-2008 1

FT BRAGG, NC

CH402079

ALMB/DS2H-60-08-ASAM-08 SELF-RETAINING FLIGHTCONTROL BOLTS COMPLIED WITH THIS DATEAT 3751.9 ACFT HRS. THIS ASAM DOES NOTAPPLY TO THIS AIRFRAME

16-Apr-2008 2

FT BRAGG, NC

CH402079



8.7.DATE

6.REMARKS

4. 5.



DS2/OLRREPAIRED BL34.5R WL 262 WEB CRACK IAWMEC#F75567

05-May-2008 1

FT BRAGG, NC

RP769187

ALMB/DS2H-60-08-AMAM-08, FLIGHT CONTROLSRIGGING UPDATE COMPLIED WITH THIS DATEAT 3751.9 ACFT HRS. CURRENTCOMPONENTS MEETS STANDARDSINDICATED IN MESSAGE.

19-May-2008 1

FT BRAGG, NC

CH402079

ALMB/DS2COMPLIED WITH REQUIREMENTS &MODIFICATION IAW TB1-1520-237-20-193 AT3751.9 ACFT HRS

19-May-2008 2

FT BRAGG, NC

CH402079

ALMB/DS2COMPLIED WITH AUTHORIZED REPLACEMENTOF ENGINE DRIVESHAFT KIT 2835-01-123-7648FOR NEW ENGINE DRIVESHAFT KIT 4920-01-526-4112 BY UH-60 PMO DATED 24 APR 2007AT 3751.9 ACFT HRS.

20-May-2008 1

FT BRAGG, NC

CH402079

ALMB/DS2COMPLIED WITH AUTHORIZED REPLACEMENTOF MAIN LANDING GEAR DRAG BEAM P/N70250-12105-043 FOR NEW DRAG BEAM 1620-01-523-0905 BY UH-60 PMO DATED 24 APR2007 AT 3751.9 ACFT HRS.

21-May-2008 1

FT BRAGG, NC

CH402079

ALMB/DS2UH-60A/L RESET INSPECTION AND TESTCRITERIA FOR THE AN/AAR-57 (V3) COMMONMISSILE WARNING SYSTEM (CMWS) NOTCOMPLIED WITH. TEST EQUIPMENT NOT ON-SITE

27-May-2008 1

FT BRAGG, NC

CH402079

ALMB/DS2UH-60A/L RESET INSPECTION AND TESTCRITERIA FOR THE BLUE FORCES TRACKING-AVIATION (BFT/AVN) NOT COMPLIED WITH.TEST EQUIPMENT NOT ON-SITE

27-May-2008 2

FT BRAGG, NC

CH402079

ALMB/DS2COMPLY WITH REQUIREMENTS OF TB1-1500-200-20-31, AIRCRAFT DESERT OPERATIONCLEANING REQUIREMENT DATED 10 AUG2004 (ATTACHMENT 2), AT 3751.9 ACFT HRS.

28-May-2008 1

FT BRAGG, NC

CH402079

D CO 3-82ND GSABH-60-08-ASAM-09 ALL H-60M SERIESAIRCRAFT, SPINDLE LUG ULTRASONICINSPECTION, NOT APPLICABLE TO THIS MDS

01-Jun-2008 1

FT. BRAGG, NC 28310

SB740025

ALMB/DS2COMPLIED WITH REQUIREMENTS OF TB1-1520-237-30-1( DESERT THEATER OF OPERATION )THIS DATE AT 3751.9 ACFT HRS. FUEL CELLSREMOVED AND REPLACED DURING THISMAINTENANCE OPERATION (RESET)

12-Jun-2008 1

FT BRAGG, NC

CH402079

ALMB/DS2H-60-08-ASAM-05 TAIL ROTOR QUADRANTSPRING CAPSULE ASSY. REPLACED THISDATE AT 3751.9 ACFT HRS. NEXTREPLACEMENT DATE SEE 2408-18.

16-Jun-2008 1

FT BRAGG, NC

CH402079



8.7.DATE

6.REMARKS

4. 5.



ALMB/DS2RESET MAINTENANCE COMPLETED THISDATE AT 3751.9 ACFT HRS. NEXT PMI-1 DUEAT 4111.9 ACFT HRS. MAIN ROTOR AND TAILROTOR RIGGED IAW CURRENT TM ANDULLSA(E) PROGRAM. MAIN ROTOR RIGGEDAS FOLLOWS: L.O.C: 90=9.9, 180=-1.3, 270=-11.3, 0=0, TOTAL=-2.7, AVG= -0.675. PRIMARYSERVO: FWD=SHORTEN 1/2 TURN, AFT=LENGHTEN 1/2 TURN, LATERAL: NOADJUSTMENT. TAIL ROTOR BIAS: RED=BEFORE 4.840, AFTER 5.170, DIF:.330, BLACK=BEFORE 4.220, AFTER 4.520, DIF: .300,YELLOW=BEFORE 4.850, AFTER 5.180, DIF:.330, BLUE=BEFORE 4.140, AFTER 4.470, DIF:.330. T/R CABLE TENSION: 23C, L/H- 155, R/H-154. FOR MORE INFO SEE ATTACHED MAINROTOR RIG WORKSHEET IN HISTORICALRECORDS.

16-Jun-2008 2

FT BRAGG, NC

CH402079

D CO 3-82ND GSABH-60-08-AMAM-11 MAIN ROTOR BLADEANGLE, -15 ENTRY NOT REQUIRED

20-Jun-2008 1

FT. BRAGG, NC 28310

SB740025

ALMB/DS2AUTHORIZED REPLACEMENT OF MAIN ROTORBLADE PINS 5315-01-329-0707 FOR NEWBLADE PINS 5315-01-537-4652 BY UH-60 OMODATED 24 APR 2007, PINS REPLACED THISDATE AT 3756.4 ACFT HRS

23-Jun-2008 1

FT BRAGG, NC

CH402079

ALMB/DS2COMPLIED WITH H-60-08-AMAM-07 (AN/ASN-128B/D DOPPLER GPS NAVIGATION SET(DGNS) ) THIS DATE AT 3758 ACFT HRS. SDCCHANGE TWICE TO CONFORM WITHREQUIREMENT. SYSTEM CHECK OK

24-Jun-2008 1

FT BRAGG, NC

CH402079

D CO 3-82ND GSABH-60-08-ASAM-10 INSPECTION OF ALL H-60SERIES AIRCRAFT FOR, ELECTRICAL WIRECHAFE ISSUES COMPLETED@ 3762.4 ACFTHOURS 28 JULY 2008

28-Jul-2008 1

FORT BRAGG, N

SB740025

D CO 3-82 GSABH-60-08-ASAM-11, H-60A FLIGHT CONTROLINSPECTION COMPLIED WITH @ 3774.1 ACFTHRS.

21-Aug-2008 1

FT. BRAGG, NC 28310

JS544833

D CO 3-82 GSABOPERATION OF GOODRICH INTERNALRESCUE HOIST IAW AWR 1308 DTD 12 MAY 08

08-Sep-2008 1

FT. BRAGG, NC 28310

JS544833

D CO 3-82 GSABH-60-08-ASAM-12 INSPECTION OF PARKERAEROSPACE AIR TURBINE STATERSCOMPLIED @ 3781.6 ACFT HRS.

17-Sep-2008 1

FT. BRAGG, NC 28310

JS544833

D CO 3-82 GSABH-60-08-AMAM-12 MAIN TRANSMISSION OILGAGE TUBE ASSEMBLY INSPECTION N/A THISMDS AIRCRAFT

17-Sep-2008 2

FT. BRAGG, NC 28310

JS544833

DCO 3-82 GSABH-60-08-ASAM-13 FIRE EXTIGUISHER TUBEUNION RING INSPECTION COMPLIED WITH @3781.6 ACFT HRS

22-Sep-2008 1

FT. BRAGG, NC 28310

MM582344

D CO 3-82 GSABH-60-08-ASAM-14 INSPECTION FOR SUSPECTENGINE HARNESSES COMPLIED WITH @3781.6 ACFT HRS.

24-Sep-2008 1

FT. BRAGG, NC 28310

JS544833

D CO 3-82 GSABUH-60-07-ASAM-06, INTERNAL RESCUE HOISTCABLE (GUARD) DEFLECTOR C/W DURINGRESET.

30-Sep-2008 1

FT. BRAGG, NC 28310

JS544833



8.7.DATE

6.REMARKS

4. 5.



D CO 3-82 GSABAWR 1324 OPERATION OF COMMON MISSILEWARNING SYSTEM(CMWS) AND IMPROVEDCOUNTER MEASURES DISPENSER(ICMD) ONUH-60A/L HELICOPTERS

02-Oct-2008 1

FT. BRAGG, NC 28310

JS544833

D CO 3-82 GSABAWR 1347 UH-60A/L HELICOPTERS EQUIPEDWITH THE ELECTRONIC DATAMANAGER(EDM) AND BLUE FORCETRACKER(BFT) SYSTEM (QUAD BAY INSTALL

02-Oct-2008 2

FT. BRAGG, NC 28310

JS544833

D CO 3-82 GSABAWR 1037 UH-60A/L WITH HARRIS AN/PRC-117F SATELLITE COMMUNICATIONS(SATCOM) RADIO INSTALLED

02-Oct-2008 3

FT. BRAGG, NC 28310

JS544833

D CO 3-82 GSABAWR 1453 FOR INSTALLATION OF AIRWARRIOR(AW) BLOCK I ON UH-60A/LHELICOPTERS APPLIED

02-Oct-2008 4

FT. BRAGG, NC 28310

JS544833

D CO 3-82 GSABAWR 1467 FOR UH-60A/L HELICOPTERSEQUIPPED WITH THE DOPPLER GLOBALPOSITIONING SYSTEM NAVIGATION SYSTEM(DGNS) PREPLANNED PRODUCTIMPROVEMENT (DGNS-P31), AN/ASN-128D A-KIT AND B-KIT APPLIED

02-Oct-2008 5

FT. BRAGG, NC 28310

JS544833

D CO 3-82 GSABISAQ 107 FOR UH-60A/L, UH-60M, UH-60Q NADHH60L HELICOPTERS EQUIPPED WITHIMPROVED ENGINE DRIVESHAFTS APPLIED

02-Oct-2008 6

FT. BRAGG, NC 28310

JS544833

D CO 3-82 GSABISAQ 110 FOR UH-60A/L HELICOPTERSEQUIPPED WITH THE MATERIAL VALUEENGINEERING (MAVEN) IMPROVED HEATINGSYSTEM (OPTION II KIT) APPLIED

02-Oct-2008 7

FT. BRAGG, NC 28310

JS544833

D CO 3-82 GSAB ISAQ 127 FOR ALL H-60 SERIESHELICOPTERS EQUIPPED WITH THE MAINROTOR SOLID BLADE PIN PART NUMBER70103-08108-041 APPLIED.

02-Oct-2008 8

FT. BRAGG, NC 28310

JS544833

D CO 3-82 GSABISAQ 105 FOR UH-60A/L HELICOPTERSEQUIPPED WITH THE STANDARDINSTALLATION AN/ARC-220(V) 1 HF RADIOAPPLIED.

02-Oct-2008 9

FT. BRAGG, NC 28310

JS544833

D CO 3-82 GSABAWR 1334 FOR UH-60A HELICOPTERS TOOPERATE WITH T700-GE-701D/CC ENGINESWITH OR WITHOUT AUTO RELIGHT ANDTRANSIENT DROOP IMPROVEMENT TDIAPPLIED.

02-Oct-2008 10

FT. BRAGG, NC 28310

JS544833

D CO 3-82 GSABH-60-09-SOF-01 INSPECT FOR SUSPECTHYDRO-MECHANICAL UNIT (HMU) COMPLIEDWITH @ 3790.0 ACFT HRS.

23-Oct-2008 1

FT. BRAGG, NC 28310

JS544833

D CO 2-82 AVN REGTCOMPLIED WITH H-60-09-SOF-02 ALL H-60REMOVAL OF AN/ALQ-144 B-KIT @ 3817.1ACFT HRS

10-Nov-2008 1

SAAF, FT BRAGG, NC28310

MA985970

D CO 2-82 AVN REGTCOMPLIED WITH H-60-09-SOF-03 COMPONETLIFE CHANGE @ 3820.5 ACFT HRS.

16-Nov-2008 1

SAAF, FT BRAGG, NC28310

MA985970

DS2/OLRAWR 1494 DATED 9 MAY 2008 R2 COMMONMISSLE WARNING SYSTEM 5TH SENSOR(CMWS 5S) IN EFFECT

17-Dec-2008 1

FT. BRAGG, NC 28310

SG909797



8.7.DATE

6.REMARKS

4. 5.



D CO. 3/82 GSABH-60-09-ASAM-03 UTILITY MODULE HYDRALICPRESSURE/RETURN LINES N/A TO UH-60AAIRCRAFT

23-Feb-2009 1

FT. BRAGG, NC 28310

SB740025

D CO 3-82 AVN REGTH-60-09-ASAM-05 UPDATE TO LIFE LIMITCHANGE OF TR QUADRANT COMPLIED WITH@ 3919.6 ACFT HRS

04-Mar-2009 1

FT. BRAGG, NC 28310

MC374951

DCO 3-82AVN REGTACFT SHIPPED THROUGH FT. BRAGG, NC TOAFGHANISTAN.

21-Apr-2009 1

FT. BRAGG, NC 28310

KW701924

D CO 3-82ND AVN REGTH-60-09-SOF-04 MAIN TRANSMISSION MODULEPLANETARY CARRIER ASSEMBLY NOTAPPLICABLE THIS AIRFRAME

02-May-2009 2

KANDAHAR, AF APO AE09355

RC048900

D CO 3/82 AVN REGH-60-09-ASAM-09 REVISION TO H-60-09-ASAM-07 FIRE EXTINGUISHER WIRING COMPLIEDWITH 15 MAY 09 @ 3943.0 ACFT HRS

15-May-2009 1

KANDAHAR AB,AFGHANISTAN

RC048900

D CO 3/82 AVN REGH-60-09-ASAM-07 FIRE EXTINGUISHER WIRING(BREAKAWAY THREAD) COMPLIED WITH 15MAY 09 @ 3943.0 ACFT HRS

15-May-2009 2


RC048900

D CO 3-82 AVN REGTH-60-09-ASAM-10 SPINDLE LUG ULTRASONICINSPECTION DOES NOT APPLY TO THIS ACFT

30-May-2009 1


MC374951

D CO 3-82 AVN REGTH-60-09-ASAM-08 ENGINE COWLING WEIGHTRESTRICTION COMPLIED WITH 14 MAY 09 @3943.0 ACFT HRS

30-May-2009 2


MC374951

D CO 3-82 AVN REGTH-60-09-ASAM-11 CARGO DOOR WINDOWEMERGENCY JETTISON HANDLE ASSEMBLYCOMPLIED WITH 29 JUN 09 @ 3994.8 ACFTHRS

30-Jun-2009 1


MC374951

D CO 3-82 AVN REGTH-60-09-AMAM-03 SWASHPLATE RETIREMENTLIFE INCREASE DOES NOT APPLY TO THISACFT

13-Jul-2009 1


MC374951

D CO 3-82 AVN REGTH-60-09-ASAM-12 CENTER CONSOLERECONFIGURATION DOES NOT APPLY TOTHIS ACFT

05-Aug-2009 1


MC374951

D-CO 3/82ND AVN REGT3' BIAS FOR REPLACEMENT OF T/RRED/YELLOW BLADE S/N: A009-01021 @4064.1 ACFT HRS ON 12 AUG 09RED BLADEB 4.78 A 5.10, YELLOW BLADE B 4.77A 5.1 BLACK BLADE B 4.15 A 4.48BLUE BLADE B 4.10 A 4.43

13-Aug-2009 1


TW219145

D CO. 3/82H-60-09-ASAM-13 FLIGHT DIRECTOR/DISPLAYCONTROL PANEL (FD/DCP) DOES NOT APPLYTO THIS ACFT

19-Aug-2009 1


IB733386

D CO 3-82 AVN REGTH-60-09-SOF-05 TARGET TORQUE VALUE(TTV) CHARTS DOES NOT APPLY TO THISACFT

24-Aug-2009 1


MC374951

D CO 3/82NDH-60-09-AMAM-05 MAIN ROTOR BLADE ANGLERIG CHECK MANUAL CHANGES. TM CHANGEONLY

24-Aug-2009 2


RC048900



8.7.DATE

6.REMARKS

4. 5.



D CO 3-82 AVN REGTH-60-09-AMAM-04 CO-PILOT SEATINTERFERENCE WITH THE ARMY AIRBORNECOMMAND AND CONTROL SYSTEMCOMPLIED WITH 25 AUG 09 @ 4075.0 ACFTHRS

25-Aug-2009 1


MC374951

D CO 3-82 AVN REGTGEN-09-AMAM-03 ULLS-A (E) INTEGRATEDMATERIAL MANAGEMENT CENTER (IMMC)LCF CHANGE 60 REQUIREMENTS COMPLIEDWITH 25 AUG 09 @ 4075.0 ACFT HRS

25-Aug-2009 2


MC374951

D. CO 3/82H-60-09-AMAM-06 CARGO HOOK CARTRIDGEACTUATED DEVICE LIFE REDUCTIONCOMPLIED WITH 01 SEP 09 @ 4075.0 ACFTHRS

01-Sep-2009 1


IB733386

D CO 3-82 AVN REGTPMI 1 COMPLETED 02 SEPT 09 @ 4075.0 ACFTHRS

02-Sep-2009 1


MC374951

D CO 3-82 AVN REGT3 DEGREE BIAS COMPLETED INCONJUNCTION WITH PMI 1 @ 4075.0 ACFTHRS. READINGS ARE AS FOLLOWS:COLOR1ST 2NDDIFFBLUE 4.144.47 0.33BLACK4.18 4.520.34YELLOW 4.875.21 0.34RED4.91 5.23 0.32

02-Sep-2009 2


MC374951

D CO 3-82 AVN REGTT/R CABLE TENSION CK COMPLETED INCONJUNCTION WITH PMI 1 @ 4075.0 ACFTHRS. READINGS ARE AS FOLLOWS:TEMP = 32DEGREES CELCIUSL/H = 176R/H = 176

02-Sep-2009 3


MC374951

D CO 3-82 AVN REGTIAW AWR1346 IVHUMS INSTALLED. OILCOOLER BEARING PART NUMBERS: 70361-03005-107, 52E15-1 OILCOOLER AXIAL FANASSEMBLIES, CONTAINING PART NUMBER210SFFC0129, 210SFFC-3, 210SFFC, ORZ33C32 FAN BEARINGS, RETIREMENT LIFEINCREASED TO 3240 HOURS

04-Sep-2009 1


KW701924

D CO 3-82 AVN REGTM/R RIG COMPLETED IN CONJUNCTION WITHPMI @ 4079.0 ACFT HRS. READINGS ARE ASFOLLOWS:CONTROL POSITION 90180 270 0TOTAL AVGLOW COLL ANGLE7.6 -1.5 -9.1 -0.3 -3.3 -.825HIGH COLL ANGLE18.1 11.7 11.518 59.3 14.825FWD CYCLICANGLE 2.731.1 33.8AFT CYCLICANGLE 24.45.1 19.3LEFT CYCLICANGLE -8.66.4 15RIGHT CYCLIC ANGLE7.4 -8.2 15.6

11-Sep-2009 1


MC374951

D CO 3-82 AVN REGTH-60-10-ASAM-01 HAMILTON-SUNSTRANDHYDRO-MECHANICAL UNITS COMPLIED WITH01 OCT 09 @ 4115.0 ACFT HRS

03-Oct-2009 1


MC374951



8.7.DATE

6.REMARKS

4. 5.



D CO 3-82 AVN REGTH-60-10-AMAM-02 REDESIGNED PLANETARYGEAR CARRIER RETIREMENT LIFE COMPLIEDWITH 06 OCT 09 @ 4130.8 ACFT HRS

17-Oct-2009 1


MC374951

D CO 3/82H-60-10-ASAM-02 DOES NOT APPLY TO THISACFT

06-Nov-2009 1


IB733386

D CO 3/82ND AVNH-60-10-AMAM-03 "COCKPIT AIRBAG SYDTEMDEACTIVATION" DOES NOT APPLT TO THISAIRCRAFT, IT IS FOR UH-60L ONLY

11-Nov-2009 1


RC048900

D CO 3/82NDCOMPLIED WITH REQUIREMNETS OF H-60-10-ASAM-03 "FIRE BOTTLE DISCHARGE LINESAND NOZZLES" ON 15 NOV 09 @ 4173.9 ACFTHOURS IN CONJUNCTION WITH PMI

15-Nov-2009 1


RC048900

D CO 3/82NDH-60-10-AMAM-04 "ASN-128B/C DOPPLERGLOBAL POSITIONING SYTEM GPSNAVIGATION SET" NOT APPLICABLE THISAIRCRAFT. MWO 1-1520-237-50-92 APPLIED TOTHIS AIRFRAME (ASN-128D)

18-Nov-2009 1


RC048900

D CO 3/82NDCOMPLIED WITH H-60-10-AMAM-05 "ULLS-A-EINTEGRATED MATERIAL MANAGEMENTCENTER (IMMC) LEGITIMATE CODE FILE (LCF)CHANGFE 60B REQUIREMENTS" ON 23 NOV09.

23-Nov-2009 1


RC048900

D CO 3-82 AVN REGTH-60-10-ASAM-04 "STABILITY AUGMENTATIONSYSTEM (SAS) LINKS" COMPLIED WITH 25NOV 09 @ 4186.3 ACFT HRS

25-Nov-2009 1


MC374951

D CO 3/82NDH-60-10-AMAM-07 AIRCRAFT MEDICAL ANDONBOARD OXGEN GENERATORS(AMOGS/OBOGS) DOES NOT APPLY THISAIRCRAFT. HH-60 ONLY

18-Dec-2009 1


RC048900

TF AVCRADA3T EVALUATION COMPLETED @ 4239.3 ACFTHRS ON 23JAN10 BY TF AVCRAD AND ACEINSPECTORS F & MM.

23-Jan-2010 1


RR854614

D CO 3/82NDAIRCRAFT ARE NOT IN COMPLIANCE WITHGEN-10-AMAM-02. LAPTOP COMPUTERS ARENOT ON HAND. 28 JAN 2010.

28-Jan-2010 1


RC048900

D CO 3/82Aircraft transferred from C co 3/82nd to C co6/101st on 16 March 2010 in Kandahar,Afghanistan @4321.7 ACFT HRS.

16-Mar-2010 1


JD071308

DCO 6-101 AVNCOMPLIED WITH H-60-10-ASAM-07 (STABHINGE INSP)

17-May-2010 1

KANDAHARAFGHANISTAN 09355

JF843426

DCO 6-101 AVNCOMPIED WITH H-60-10-AMAM-12 (IMPROVEDDRAG BEAM)

17-May-2010 2


JF843426

D CO 6-101 AVNAVCRAD COMPLETED REPAIR OF STA 308TEE WL 206 DAMAGED BY SMALL ARMS FIREBETWEEN BL 14L AND 15L, 1" HOLE WITHAPPROX 5" CRACK OF TEE RADIUS.REPAIRED IAW MEC F106648 A

28-May-2010 1


JF843426



8.7.DATE

6.REMARKS

4. 5.



DCO 6-101 AVNUNIT WILL CONDUCT AN INSPECTION OF THEREPAIR AND THE HILOK FASTENERS FORLOOSENESS OR WORKING FASTENERS ORCRACKS ARE REQUIRED AT EVERY PHASEINSPECTION AND AFTER EVERY SLING LOADFLIGHT.RESET- RE-INSPECT THE REPAIR INTHE MEC F106648A AND INSTALL NEW BEAMINTO AIRCRAFT PER SIKORSKY DRAWINGS.

28-May-2010 2


JF843426

D CO 6-101 AVNCOMPLIED WITH H-60-10-ASAM-06 (TDI ANDAUTO RELIGHT)

07-Jun-2010 1


MH664811

DCO 6-101 AVNCOMPLIED WITH H-60-10-ASAM-08 (APUCHAFFING)

09-Jun-2010 1


JF843426

D CO 6-101 AVNCOMPLIED WITH H-60-10-AMAM-16 (CMWSGUARDED DISPENSE SWITCH)

04-Jul-2010 1


MH664811

B 96ASB/101 CABPMI 2 COMPLETED 10JUL 10 @ 4409.0 ACFTHRS NEXT PMI 1 DUE @ 4769.0 ACFT HRS

09-Jul-2010 1


AK626390

B CO. 96TH ASBUH60-10-SOF-02 SPINDLE NDI COMPLETED 10-Jul-2010 1

KANDAHAR, AFGAN

AK626390

B CO. 96TH ASBMWO 1-1520-237-30-3 AUTO RELIGHT ANDTRANSIENT DROOP IMPROVEMENT FOR T700-GE-701D APPLIED THIS DATE

11-Jul-2010 1

FORT CAMPBELL

DS716004

DCO 6-101COMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-12. ALL H60 T700 SERIES COMPONENTRETIREMENT CHANGE.

05-Aug-2010 1


CZ787658

D CO 6-101 AVNCOMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-11 (COMMON COMPONENTRETIREMENT CHANGE TIMES UPDATE).

05-Aug-2010 2


MH664811

D CO 6-101ST AVNCOMPLIED WITH H-60-10-ASAM-15 (ESSSFUEL SYSTEM VENT ELBOW) (PASSED INSP)

16-Aug-2010 1


MG602513

DCO 1-101ST CAB(LATE ENTRY) H-60-ASAM-15 ESS FUELSYSTEM VENT ELBOW COMPLIED WITH ON 24SEP 10 @4469.2 ACFT HOURS. INSP

24-Sep-2010 1

TERIN KOWT AFG, APOAE 09308

TV374830

D 1-101ST CABH-60-11-AMAM-03 OIL COOLER FAN AXIALBEARING COMPLIED WITH ON 31 OCT 10 @1791.3 ACFT HOURS.

31-Oct-2010 1


TV374830

D/1-101 CABH-60-11-ASAM-03, ALL H-60A SERIESAIRCRAFT, HAMILTON STANDARD HYDRO-MECHANICAL UNITS (HMU) COMPLIED WITHON 01 DEC 10 @ 4513.4 ACFT HOURS

01-Dec-2010 1


SK713578

DCO 6-101 AVN FORTCAMPBELL, KY

LATE ENTRY H-60-09-ASAM-06 ( MIKE MODLEONLY)

09-Dec-2010 1


JF843426



8.7.DATE

6.REMARKS

4. 5.




LATE ENTRY H-60-10-ASAM-05 (MIKE MODLEONLY)

09-Dec-2010 2


JF843426


LATE ENTRY H-60-10-ASAM-09 (HH AND MIKEMODLE ONLY)

09-Dec-2010 3


JF843426


LATE ENTRY H-60-10-ASAM-10 (L MODLEONLY)

09-Dec-2010 4


JF843426


LATE ENTRY H-60-10-ASAM-13 (HH AND MIKEMODLE ONLY)

09-Dec-2010 5


JF843426


LATE ENTRY H-60-10-ASAM-14 (CHANGE TOBLADE DEICE PROCEDURE)

09-Dec-2010 6


JF843426


LATE ENTRY H-60-08-AMAM-09 (SOLID BLADEPIN CORROSION)

09-Dec-2010 7


JF843426


LATE ENTRY H-60-08-AMAM-10 (CLEANINGPROCEDURES FOR ENGINE START CONTROLVALVES)

09-Dec-2010 8


JF843426


LATE ENTRY H-60-09-AMAM-01 (APUREDUCTION DRIVE HOUSING)

09-Dec-2010 9


JF843426


LATE ENTRY H-60-09-AMAM-02 (OIL COOLERVIBRATION CHECKS)

09-Dec-2010 10


JF843426


LATE ENTRY H-60-10-AMAM-01 (FLIGHTCONTROL RIGGING PROCEDURES)

09-Dec-2010 11


JF843426


LATE ENTRY H-60-10-AMAM-06 (PHASEDMAINTENANCE INSPECTIONS CHECKLISTCHANGE)

09-Dec-2010 12


JF843426


LATE ENTRY H-60-10-AMAM-08 (MAGNETICVARIATION EXPIRATION/UPDATE)

09-Dec-2010 13


JF843426



8.7.DATE

6.REMARKS

4. 5.




LATE ENTRY H-60-10-AMAM-09 (MIKE MODLEONLY)

09-Dec-2010 14


JF843426

DCO 6-101 AVNFORTCAMPBELL, KY

LATE ENTRY H-60-10-AMAM-10 (HH MODLEONLY)

09-Dec-2010 15


JF843426


LATE ENTRY H-60-10-AMAM-14 ( MIKE MODLEONLY)

09-Dec-2010 16


JF843426


LATE ENTRY H-60-10-AMAM-13 (CHANGES TOREQUIRED MAINTENANCE AND INSPECTIONS)

09-Dec-2010 17


JF843426


LATE ENTRY H-60-10-AMAM-15 (HOIST CADTEST SET)

09-Dec-2010 18


JF843426


LATE ENTRY H-60-10-AMAM-17 (PRIMARYSERVO REPLACEMENT TM CHANGE)

09-Dec-2010 19


JF843426


LATE ENTRY H-60-10-AMAM-18 (IBIT CHIPDETECTOR CHANGE CH1)

09-Dec-2010 20


JF843426


LATE ENTRY H-60-10-AMAM-19 (NDI TRAININGREQUIREMENTS)

09-Dec-2010 21


JF843426


LATE ENTRY H-60-11-AMAM-02 (MANUALCHANGE TO FLIGHT CONTROL RIGGINGPROCEDURE)

09-Dec-2010 22


JF843426

DCO 1-101 CABH-60-11-AMAM-04 CODE FILE CHANGE 61COMPLIED WITH ON 11 DEC 10 @ 4524.6 ACFTHOURS

11-Dec-2010 1


TV374830

DCO 1-101 CABCOMPLIED WITH H-60-11-ASAM-04 TACANRECEIVER BEARING ERROR @ 4541.2 ACFTHRS.

20-Dec-2010 1


TV374830


COMPLIED WITH H-60-11-AMAM-05 (MIKEMODLE ONLY)

20-Dec-2010 2


JF843426

D CO. 6-101 GSABH-60-11-ASAM-06 (CYCLIC STICK STOPBOLTS) COMPLIED WITH.

07-Feb-2011 1


GM660936



8.7.DATE

6.REMARKS

4. 5.



D CO. 6-101 GSABH-60-11-ASAM-08 COMPLIED WITH (LOS / IFFANTENNA AND IVHMS ACCELEROMETERCONNECTORS SAFETY WIRE)

07-Feb-2011 2


GM660936

D CO. 6-101 GSABCOMPLIED WITH REQUIREMENTS OF H-60-11-ASAM-09. IAFTS NOT INSTALLED.

16-Jun-2011 1

FORT CAMPBELL, KY42223

GM660936

D CO. 6-101 GSABCOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-09. (19-3 REPORTING)

16-Jun-2011 2


GM660936

D CO. 6-101 GSABCOMPLIED WITH REQUIREMEMNTS OF H-60-11-AMAM-06. (MEDEVAC CARSOULES)

16-Jun-2011 3


GM660936

D CO. 6-101H-60-11-AMAM-14 (INTERNAL FUEL TUBESWAGING) COMPLIED WITH. N/A THIS ACFT

28-Jun-2011 1


GM660936

DELTA COMPANY 6-101H-60-11-AMAM-13 NOT APPLICABLE TOAIRCRAFT (EXTERNAL RESCUE HOIST MOUNTFITTINGS)

07-Jul-2011 1


JC246510

D CO 6-101 AVN REGTH-60-11-SOF-01 COMPLIED WITH 22-Jul-2011 1


JV111420

D CO 6-101 AVN REGTH-60-11-ASAM-13 COMPLIED WITH 26-Jul-2011 1


JV111420

DCO 6-101COMPLIED WITH H-60-11-ASAM-14 (ENGINECOWLING RESTRICTIONS

16-Aug-2011 1


JC246510

DCO 6-101 GSABH-60-11-AMAM-15 IVHMS COMPLIED WITH 13-Sep-2011 1


JC246510

DCO 6-101 GSABMR RIG COMPLETED LOW COLLECTIVEANGLE AVG -0.43, HIGH COLLECTIVE AVG15.38, COLL ANGLE SPREAD AVG 15.81, FWDCYCLIC ANGLE TOTAL 33.00, AFT CYCLICANGLE TOTAL 20.78, LEFT CYCLIC ANGLE15.02, RT CYCLIC ANGLE 14.76. PRIMARYSERVO BIAS ADJUSTMENTS AS FOLLOWSFWD 1 WRENCH FLAT CLOCKWISE, AFT 1WRENCHFLAT COUNTER CLOCKWISE, LAT 1WRENCHFLAT CLOCKWISE.

15-Sep-2011 1


JC246510

DCO 6-101 GSABH-60-11-ASAM-15 N/A MIKE MODLE ONLY 20-Sep-2011 1


JC246510

DCO 6-101 GSABH-60-11-AMAM-18 N/A MIKE MODLE ONLY 20-Sep-2011 2


JC246510

DCO 6-101 GSABH-60-11-AMAM-20 (AMPS SOFTWAREUPGRADE) COMPLIED WITH

26-Sep-2011 1


JC246510



8.7.DATE

6.REMARKS

4. 5.



L-3 COMMUNICATIONSRASM-E

OCM/ACE PERFORMED AT 4633.4 ACFT HRSBY TEAM MEMBERS J AND N AMCOM AFMA

05-Oct-2011 1

FT. CAMPBELL, KY42223-5000

LH369501

RESET UH-60 DYNCORPCOMPLIED WITH H-60-12-SOF-01,EMERGENCY, ALL H-60 SERIES AIRCRAFT,TAIL ROTOR INTERMEDIATE GEARBOX,PASSED

11-Oct-2011 1


RM008701

WGLED0COMPLIED WITH THE REQUIREMENTS OF H-60-12-SOF-02 (12-SOF-01 REVISION)

11-Oct-2011 2


CC749505

DYNCORP UH-60 RESETCOMPLIED WITH H-60-11-AMAM-17, TAILROTOR INBOARD/ OUTBOARD RETENTIONPLATE SHIMS, PASSED

17-Oct-2011 1


RM008701

DYNCORP UH-60 RESETMEC NUMBER: F134639. REPAR OF SPLICECRACK AT FS:379

18-Oct-2011 1


RM008701

DYNCORP RESET UH-60COMPLIED WITH REQUIREMENTS OF H-60-12-SOF-03, TAIL ROTOR INTERMEDIATEGEARBOX

19-Oct-2011 1


RM008701

DYNCORP RESET UH-60VANEAXIAL FAN (OIL COOLER FAN) PARTNUMBER 70361-03005-107 CONTAINING PARTNUMBER 210SFFC3 FAN BEARINGS SHALLHAVE THEIR TIME BEFORE OVERHAUL (TBO) /RETIREMENT LIFE (RC) INCREASED TO 3240HOURS IAW AWR 1346 R18 DATED 15 SEP2011

24-Oct-2011 1


RM008701

DYNCORP UH-60 RESETMEC NUMBER: F135416. REPAIR OVERSIZED/DAMAGED HOLE BY THE INSTALLATION OF AFREEZE PLUG ON R/H BEADED PANEL RIVETHOLE

25-Oct-2011 1


RM008701

DYNCORP RESET UH-60COMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-01, TAIL ROTOR OUTPUT BEVEL GEARNON-DESTRUCTIVE INSPECTION, PASSED

02-Nov-2011 1


RM008701

DYNCORP UH-60 RESETMEC NUMBER: F136346. REPAIR 3EAELONGATED/ DAMAGED HOLES BY THEINSTALLATION OF FREEZE PLUGS ON L/HBEADED PANEL RIVET HOLES

10-Nov-2011 1


RM008701

DYNCORP UH-60 RESETMEC NUMBER: F136774. REINSTALLED THECONTROL ATTACHMENT PAD OUTBOARDNAS537B8P-55 BUSHING IN THE FS 327FRAME

21-Nov-2011 1


RM008701

DYNCORP UH-60 RESETMAIN ROTOR SYSTEM COMPLETE RIGCOMPLETED DURING RESET I/A/W TM 1-1520-237-23-9, WP 1036 00 AT 4633.4 ACFT HOURS

08-Dec-2011 1


RM008701



8.7.DATE

6.REMARKS

4. 5.



DYNCORP UH-60 RESETTAIL ROTOR SYSTEM COMPLETE RIGCOMPLETED IN RESET I/A/W TM 1-1520-237-23-9, WP 1038 00 AT 4633.4 ACFT HOURS. (RED:INITIAL 4.650 - BIAS 4.940= DIFF 0.290)(BLUE:INITIAL 3.900 - BIAS 4.220= DIFF0.320)(YELLOW: INITIAL 3.750 - BIAS 4.040=DIFF 0.290)(BLACK: INITIAL 3.920 - BIAS 4.250=DIFF 0.330)

08-Dec-2011 2


RM008701

DYNCORP UH-60 RESETCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-02, DRAG BEAM REPLACEMENT.PASSED

13-Dec-2011 1


RM008701

DYNCORP UH-60 RESETINSTALLATION OF 50-5 AND 50-7, AS PERMEC# F134025

15-Dec-2011 1


RM008701

DYNCORP UH-60 RESETCOMPLIED WITH THE REQUIREMENTS OF TB 1-1500-200-20-31, AIRCRAFT DESERTOPERATIONS CLEANING REQUIREMENTS AT4633.4 ACFT HOURS

15-Dec-2011 2


RM008701

DYNCORP UH-60 RESETCOMPLIED WITH THE REQUIREMENTS OF TB 1-1500-237-30-1, AIRCRAFT DESERTOPERATIONS SPECIAL INSPECTION ANDCLEANING REQUIREMENTS AT 4633.4 ACFTHOURS

15-Dec-2011 3


RM008701

DYNCORP UH-60 RESETPMI #1, #2 AND RESET COMPLETED AT 4633.4ACFT HOURS

15-Dec-2011 4


RM008701

RASM-E AFMA L3COMMUNICATIONS

MWO 1-1520-237-50-97 IMPROVEDCOUNTERMEASURE DISPENSER SYSTEM(ICMD) COMMON MISSILE WARNING SYSTEM(CMWS) MODERNIZED (P3I) ON UH-60 A/LCOMPLETED AT 4633.4 ACFT HOURS

16-Dec-2011 1


RM787005


MWO 1-1520-237-50-84 INSTALLATION OFAN/APX-118 MODE S TRANSPONDER (CXP) ONUH-60 A/L COMPLETED AT 4633.4 ACFTHOURS

16-Dec-2011 2


RM787005


COMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-03 TANSPONDER AND COMMONMISSILE WARNING SYSTEM INSTALLATIONON 16 DEC 2011, 4633.4 ACFT HOURS

16-Dec-2011 3


RM787005


MEC F137625 RELOCATION OF NUTPLATE TOCOMPLETE INSTALLATION OF CMWS ECUTRAY IAW MWO 1-1520-237-50-97 (CMWS P3I)

16-Dec-2011 4


RM787005



8.7.DATE

6.REMARKS

4. 5.



DYNCORP UH-60 RESETMEC NUMBER F138143. UH-60A, 82-23745,4633.4 ACFT HRS: DURING THE RESETINSPECTION A PREVIOUS BATTLE DAMAGEREPAIR WAS FOUND IN THE CABIN TUB ATSTATION 308 (COVERED BY MEC NO.F106648). THE MEC INCLUDES AN ADDENDUMTHAT REQUIRED RE-INSPECTION OF THEREPAIR, AND INSTALLATION OF A NEW BEAMIAW SIKORSKY DRAWINGS DURING RESET.REQUEST ENGINEERING DISPOSITION FORRETAINING THE ORGINAL BEAM WITH THECURRENT REPAIR. ENGINEERINGDISPOSITION : THE TEE-CAP REPAIR OF THETRANSVERSE FLOOR FORMER AT STA 308HAS BEEN REVIEWED AND IS FOUNDSATISFACTORY AS A PERMANENT REPAIR.REPLACEMENT OF THE FLOOR FORMER ISNOT REQUIRED BECAUSE THE REPAIR ISMORE THAN ADEQUATE.THICKNESSCONFORMS TO THE ORIGINAL BEAM TEE-CAPTHICKNESS. THE FORWARD AND AFT SIDESPLICE ANGLES UNDER THE CAP ON BOTHTHE LEFT AND RIGHT SIDES OF THE TEEFITTING WERE INSTALLED TO DMWRSTANDARD FOR SPLAICE REPAIR. ADEQUATEFASTENERS PAST EACH SPLICE POINT WITH4 TO 5 FASTENERS PITCH LENGTH ON EACHSIDE OF THE SPLAICE FOR ALL 4 SPLICEANGLES. THIS TEE-CAP REPAIR FOR THETRANSVERSE FLOOR AT STA 308 CAN BERETAINED IN SERVICE

20-Dec-2011 1


RM008701

DYNCORP UH-60 RESETAWR 1425 R15 DATED 9 SEP 11 (CMWS),(ICMD) AND (P3I), FCC HAS BEENSUCCESSFULLY COMPLETED ON ANOTHERSPECIFIED AIRCRAFT, UH-60A / 82-23688

28-Dec-2011 1


RM008701

DYNCORPMEC NUMBER F138755PROBLEM: REQUESTPERMISSION TO REPLACE THE CANNON PLG(OLD STYLE) ON SPAN A.DISPOSITION:AUTHORIZATION IS GRANTED TO REPLACETHE DE-ICE ELECTRICAL CONNECTOR ONSPAN A OF T/R BLADE S/N A009-08171 PERTHE PROCEDURES OF DMWR 1-1615-287AUTHORIZED BY CLARK D. LEMONS, DSN635-7966 [email protected]

06-Jan-2012 1


MB009185

DCO 6-101 GSABCOMPLIED WITH H-60-12-ASAM-03 14-Jan-2012 1


JC246510

WGLED0POST DATED ENTRY 04 OCT 11 "COMPLIEDWITH REQUIREMENTS OF H-60-11-AMAM-19"

03-Feb-2012 1


CC749505

WGLED0REQUIREMENTS OF H-60-12-AMAM-06 NOTAPPLICABLE TO THIS MDS (H-60M ONLY)

21-Feb-2012 1


CC749505

WGLED0COMPLIED WITH REQUIREMENTS OF H-60-12-SOF-04 BREEZE EASTERN HOIST (GOODRICHHOIST UTILIZED)

21-Feb-2012 2


CC749505



8.7.DATE

6.REMARKS

4. 5.



D CO 6-101 AVNRIG COMPLETED: LOW COLLECTIVE ANGLE 1-.075/ COLL ANGLE SPREAD 15.8/ FWD CYCANGLE -1.9-31.9-33.8/ AFT CYC ANGLE 26.3-4.7-21.6/LEFT CYCLIC ANGLE 8.3-7.8-16.1/RIGHTCYCLIC ANGLE 6.8-7.4-14.2

29-Feb-2012 1


JV111420

WGLED0H-60-12-ASAM-04 NOT APPLICABLE TO THISMDS

14-Mar-2012 1


CC749505

WGLED0H-60-12-ASAM-05 NOT APPLICABLE TO THISMDS (H-60M FM2 CONNECTION)

15-Mar-2012 1


CC749505

WGLED0COMPLIED WITH THE REQUIREMENTS OF H-60-12-ASAM-06 (UPPER FUEL BREAKAWAYVALVE SEALANT APPLICATION)

15-Mar-2012 2


CC749505

WGLED0REQUIREMENTS OF H-60-12-AMAM-01 NOTAPPLICABLE TO THIS MDS (H-60M CEFS FUELMOMENTS CHANGE)

16-Mar-2012 1


CC749505

WGLED0REQUIREMENTS OF H-60-12-AMAM-04 NOTAPPLICABLE TO THIS MDS (H-60M)

21-Mar-2012 1


CC749505

WGLED0REQUIREMENTS OF H-60-12-AMAM-05 NOTAPPLICABLE TO THIS MDS (HH-60 LITTERCONVERTERS)

21-Mar-2012 2


CC749505

DOL ALMD FT DRUM,NY13602

NOTIFIED PC OF LOST TOOL OVER THEWEEKEND. RED 25 FOOT EXTENSION CHORDCAME UP MISSING. CHORD NOT FOUND.

26-Jun-2012 1

HAAF, GA

JS542747

YULISTA AVIATION, INC.COMPLIED WITH MWO 1-1520-237-50-106,PILOT/COPILOT M4 MOUNT.

26-Jun-2012 2

HAAF, GA

MC195346

YULISTA AVIATION, INC.COMPLIED WITH MWO 1-1520-237-20-95,CREWCHIEF/DOOR GUNNER M4 MOUNT.

26-Jun-2012 3

HAAF, GA

MC195346

YULISTA AVIATION, INC.COMPLIED WITH AWR 1615CREWCHIEF/DOOR GUNNER M4 CARBINEMOUNT SYSTEM, 14MAR12.

26-Jun-2012 4

HAAF, GA

MC195346

YULISTA AVIATION, INC.COMPLIED WITH AWR 1667 VERTICAL PILOTAND COPILOT M4 CARBINE MOUNT SYSTEM,3MAY12.

26-Jun-2012 5

HAAF, GA

MC195346

L-3ACE COMPLETED AT 4836.7 A/C HRS. BY ACETEAM MEMBERS B/G. AFMA, RASM-E,AMCOM.

14-Sep-2012 1

HAAF, GA

JG389608

D CO 2/3 AVNCOMPLETED AND COMPLIED WITH H-60-12-AMAM-09 @4871.5 AIRCRAFT HOURS(HYDRAULIC LINE CHAFFING DUE TO MISSINGCLAMPS).

30-Oct-2012 1

HAAF, GA

MY626146

D CO 2-3 GSABH-60-13-AMAM-03 (DECU/EDECU TGT BIAS)C/W 12 DEC 2012.

12-Dec-2012 1

KAF

VD373747

D CO 2-3 GSABLATE ENTRY COMPLIED WITH REQUIREMNTSOF H-60-13-AMAM-04 CHANGE 63

13-Dec-2012 1

HAAF, GA

JC674882



8.7.DATE

6.REMARKS

4. 5.



D CO 2-3 GSABLATE ENTRY COMPLIED WITHREQUIREMENTS OF H-60-12-ASAM-09(RESCUE HOIST CAD ELEC CONN) N/A THISAIRCRAFT

13-Dec-2012 2

HAAF, GA

VD373747

D CO 2-3 GSABCOMPLIED WITH H-60-13-ASAM-01 (ANTI-COLLISION POWER SUPPLY) THIS DATE;PASSED INSPECTION.

13-Dec-2012 3

KAF

VD373747

D CO 2-3 GSABCOMPLY WITH REQUIRMENTS OF H-60-13-ASAM-02 HONTEK BLADES. N/A THIS ACFT.H60M ONLY

14-Feb-2013 1

KANDAHAR,AFGHANISTAN

JC674882

D CO 2-3 GSABCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-06 (CEFS) N/A THIS ACFT.

20-Feb-2013 1


VD373747

D CO 2-3 GSABCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-05 (WHEEL BRAKE ASSY) PASSED

26-Mar-2013 1


VD373747

D CO 2-3 GSABCOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-04 (PLASTIC MEDIA BLAST(PMB) ANDOXIDE FLAKE RESIDUE)

29-Mar-2013 1


GA676486

D CO 2-3 GSABCOMPLIED WITH REQUIRMENTS OF H-60-13-AMAM-07 LDS CABLE CLEARANCE (PASS)

02-Apr-2013 1


JC674882

D CO 2-3 GSABCOMPLIED WITH REQUIRMENTS OF H-60-13-ASAM-05. BREEZE EASTERN HOIST. NA THISACFT

09-Apr-2013 1


JC674882

DCO 2-3 GSABCOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-06 (PMI CHECKLIST CHANGES)

09-May-2013 1


JC591557

D CO 2-3 GSABCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-09 (NUMBER 6R STRINGER); N/A THISACFT

01-Jun-2013 1


VD373747

DYNCORP INTL, KAF,APO AE 09355

COMPLIED WITH REQUIREMENTS OF H-60-13-SOF-01 ATTITUDE HEADING REFERENCE SET(AHRS)

02-Jun-2013 1

ALAM 1325

ER802103


COMPLETE MAIN ROTOR RIG COMPLETED AT4989.5 ACFT HRS BLADE ANGLES ARE ASFOLLOWS:LOW COL 9.6, -1.3, -10.7, 0.0AVG -0.598HIGH COL 20.0, 12.3, 10.5, 18.4AVG 15.3FWD CYC -1.8, 31.4 TOTAL 33.2AFTCYC 26.1, 4.8 TOTAL 21.3LEFT CYC 8.2, 7.2TOTAL 15.4RIGHT CYC 6.6 8.0 TOTAL14.7ADDITIONAL BIAS SET AS FOLLOWSFWDLENGHTHEN 2.5 FLATSAFT SHOERTEN 2.5FLATSLAT SHORTEN 4 FLATS

08-Jun-2013 1

ALAM 1325

ER802103


COMPLETE TAIL ROTOR RIG COMPLETED AT4989.5 ACFT HRS BIAS SET AS FOLLOWS:SET DIM A DIM B DIFF FINALRED0.0 4.800 5.100 .300 3.0BLACK 0.54.100 4.400 .300 3.0YELL 0.04.800 5.100 .300 3.0BLUE 1.14.100 4.400 .300 3.0

08-Jun-2013 2

ALAM 1325

ER802103



8.7.DATE

6.REMARKS

4. 5.




COMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-01 FLIGHT CONTROL RIGGING

08-Jun-2013 3

ALAM 1325

ER802103


COMPLY WITH REQUIREMENTS OF H-60-13-AMAM-09 (6R STRINGER) N/A THIS ACFT.H60M ONLY

12-Jun-2013 1

ALAM 1325

ER802103


PMI-1 COMPLETED 12JUN2013 AT 4989.5ACFT HRS

12-Jun-2013 2

ALAM 1325

ER802103

D C0 2-3 GSABCOMPLIED WITH REQUIRMENTS OF H-60-13-AMAM-10. CHANGE 64

23-Jun-2013 1


TASM-O/DYNCORPA3T INSP. COMPLETED AT ACFT HRS 5003.4 25-Jun-2013 1


WC643445

D CO 2-3 GASBCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-11 NLT 15 JUL 13 (MAIN TRANSMISSIONFILTER BOWL ATTACHMENT HARDWAREREPLACEMENT) NOT INST

07-Jul-2013 1


JC674882

D CO 2-1 GASBOperate within limitations and restrictionsspecified in AWR 1037 R10, DTD 20 SEP 13 (HARRIS AN/PRC-117F SATELLITECOMMUNICATIONS (SATCOM) RADIOINSTALLED)

24-Sep-2013 1


JK954169

D 2-1 AVN (GSAB)COMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-15 (CEFS RIGHT HAND FUEL CELLCOVER PLATE) ON 10 OCT 2013.

10-Oct-2013 1


JK954169

D.CO. 2-1 GSABCOMPLYED WITH REQUIREMENTS OF H-60-14-AMAM-01 (TRANSPONDER ACFTREGISTRATION NUMBER) NOT APPLICABLETO THIS ACFT

29-Oct-2013 1


BK944665

D.CO. 2-1 GSABCOMPLYED WITH H-60-14-ASAM-01 (MAINTRANSMISSION MOD) ACFT IN COMPLIANCE

29-Oct-2013 2


BK944665

D.CO. 2-1 GSABCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-01 (TRANSPONDER REGISTRATIONCODE) NOT APPLICABLE THIS AIRFRAME

01-Nov-2013 1


BK944665

D 2-1 AVN (GSAB)COMPLIED WITH REQUIREMENTS OF H-60-14-SOF-01 (BREEZE EASTERN EXTERNALRESCUE HOIST INSTALLATION) N/A TO THISAIRCRAFT

02-Nov-2013 1


JK954169

D CO 2-1 GASBOPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1357 R4DATED 24 SEP 13 (Helicopters in Support ofCombat Operations to Conduct AlternateMethod (Ground) Maximum Power Checks)

22-Nov-2013 1


JK954169

D-CO 2-1 GSABOPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1750 R2DTD 29 MAR 13(AVS-6 NVG)

24-Nov-2013 1


JL085789



8.7.DATE

6.REMARKS

4. 5.



D CO 2-1 GSABOPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1692 R5DTD 24 JAN 13 (NEW T/R DE-ICE)

24-Nov-2013 2


JL085789

D CO 2-1 GSABOPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1529 R3DTD 30 OCT 2013 (FOGS)

24-Nov-2013 3


JL085789

D CO 2-1 GSABOPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1445 R4DTD 30 SEP 2013 ((AFCS PANEL)

24-Nov-2013 4


JL085789

D CO 2-1 GSABOPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1223 R7DTD 18 JUN 13 (IR ANTI-COLLISION LIGHT)

24-Nov-2013 5


JL085789

D CO 2-1 GSABOPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1119 R6DTD 06 JULY 2012 (DESERT COMBAT OPS)

24-Nov-2013 6


JL085789

D CO 2-1 GSABOPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 996 R6 DTD26 SEP 2013 (FUEL SAMPLE ACCESSORYBOX)

24-Nov-2013 7


JL085789

D CO 2-1 GSABCOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-02 (HUMS ACCELEROMETERS) DTD 21NOV 2013

24-Nov-2013 9


JL085789

D CO 2-1 GSABCOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-02 (HUMS ACCELEROMETERS) DTD 21NOV 2013

24-Nov-2013 10


JL085789

D.CO. 2-1 GSABCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-03 ( DISCREPANT CONNECTING LINKS),DATED 231245Z DEC 13, ACFT PASSEDINSPECTION

28-Dec-2013 1


BK944665

D CO 2-1 GSABCOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-03 (EIBF)BRACKET REMOVAL, DATED301230Z DEC 13, ACFT PASSED

31-Dec-2013 1


JL085789

D CO 2-1 GSABOperate within limitations and restrictionsspecified in AWR 1037 R12, dated 3 Jan 14 ( UH-60A/L with Harris AN/PRC-117F SatelliteCommunications (SATCOM) Radio Installed ).

14-Jan-2014 1


JK954169

TASM-O/DYNCORPAVIATION

A3T INSP COMPLETED AT ACFT HRS. 5177.4BY TEAM MEMBER "S"

21-Jan-2014 1


WC643445

D CO 2-1 GSABCOMPLIED WITH REQUIREMENTS OF H-60-14-SOF-02 DTD 24 JAN 14 (TAIL ROTOR PITCHCHANGE SHAFT ASSEMBLY).

31-Jan-2014 1


JL085789

D CO 2-1 GSABCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-05 ( ULLS-A(E)ALC Legitimate CodeFile(LFC) Change 65 Requirements ) ON 07MAR 14.

09-Mar-2014 1


JK954169

D.CO. 2-1 GSABMAIN MOD FILTER BOWL POPPED SECONDTIME WITHIN 200 FLIGHT HOURS CURRENTACFT HOURS 5213.1

19-Mar-2014 1


BK944665



8.7.DATE

6.REMARKS

4. 5.



L3 RASM EASTCOMPLY WITH REQUIREMENTS OF AWR 1520R25, DATED 26 MAR 14 (SPONSON MOUNTEDFLIR SYSTEM ON SPECIFIED UH60-A/LHELICOPTERS)

27-Mar-2014 1

HAAF, GA

JD132412

L3 RASM EASTOPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN THE ENCLOSEDAWR 1520 R25, DATED 26 MAR 14 (SPONSONMOUNTED FLIR SYSTEM ON SPECIFIED UH60-A/L HELICOPTERS)

27-Mar-2014 2

HAAF, GA

JD132412

D 2-1 GSABCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-09 (MAIN TRANSMISSION FILTER BOWLAND CHIP DETECTOR ATTACHMENTHARDWARE) ON 29 MAR 14

29-Mar-2014 1


JK954169

D.CO. 2-1 GSABCOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-04 (MR ASSY)

30-Mar-2014 1


BK944665

D CO 1-52 AVNCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-10 (HONTEK COATED MAIN ROTORBLADE)

10-Apr-2014 1


MM231326

D CO 1-52 GSABMEC: F182428 AUTHORIZATION IS GRANTEDTO 2-53 GSAB IN KANDAHAR, AFGHANISTAN,TO EXTEND THE LIFE OF THE #2 CROSSFEEDVALVE (PN: 70307-03006-103, S/N: 057)INSTALLED ON UH-60A BY 98.9 HOURS.

17-Apr-2014 1


LN334741

D CO 1-52COMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-06 (FLIGHT CONTROL MIXERASSEMBLY)

24-Apr-2014 1


LN334741

D CO 1-52 AVNCOMPLIED WITH H-60-14-AMAM-12 (M/RSPINDLE NUT RETIREMENT LIFE)

27-Apr-2014 1


LN334741

D CO. 1-52 AVNLATE ENTRY; COMPLIED WITH H-60-09-ASAM-01

18-May-2014 1


MP779328


18-May-2014 2


MP779328

D CO. 1-52 AVNLATE ENTRY; COMPLIED WITH H-60-09-AMAM-07

18-May-2014 3


MP779328

D CO. 1-52 AVNLATE ENTRY; COMPLIED WITH H-60-10-SOF-01 18-May-2014 4


MP779328


18-May-2014 5


MP779328


18-May-2014 6


MP779328



8.7.DATE

6.REMARKS

4. 5.




18-May-2014 7


MP779328

D CO. 1-52 AVNLATE ENTRY; COMPLIED WITH H-60-12-SOF-05 18-May-2014 8



18-May-2014 9


MP779328


18-May-2014 10


MP779328


18-May-2014 11


MP779328


18-May-2014 12


MP779328

D CO 1-52 AVNLATE ENTRY; COMPLIED WITH H-60-12-AMAM-15

18-May-2014 13


MP779328


18-May-2014 14


MP779328


18-May-2014 15


MP779328


18-May-2014 16


MP779328


18-May-2014 17


MP779328


18-May-2014 18


MP779328


18-May-2014 19


MP779328


18-May-2014 20


MP779328


18-May-2014 21


MP779328



8.7.DATE

6.REMARKS

4. 5.



D CO 1-52 AVNCOMPLIED WITH 60-14-SOF-03 ON 28 JUN 14. 28-Jun-2014 1


AR807262

D CO, 1-52LATE ENTRY COMPLIED WITH H-60-14-AMAM-14 ON 27 JUN 14. (IVHMS CABLING)

28-Jun-2014 2


AR807262

D CO 1-52 GSABCOMPLIED WITH REQUIREMENTS H-60-14-AMAM-16 (ATTITUDE HEADING REFERENCEUNIT)

15-Jul-2014 1


AP999711

DYNCORP TASM OMEC NUMBER F187165 AUTHORIZATION ISGRANTED TO B CO. 46TH ASB AND/ORDYNCORP IN KANDARHAR AFGHANISTAN TOREPAIR THE MAIN ROTOR HUB (P/N) 70070-10046-055, SN A308-00238), LOWER LINER (P/N70103-08002-113) IAW THE "REPAIR BONDEDLINER" PROCEDURE FROM TM 1-1520-BLACKHAWK WP 0557 00.

27-Jul-2014 1


JB609325

DYNCORP TASM OCOMPLIED WITH THE REQUIREMENTS OF H-60-14-ASAM-08 (HYDRO-MECHANICAL UNITQUICK DISCONNECT PINS) ON 05 AUG 14,HYDRO-MECHANICAL UNITS PASSEDINSPECTIONS

06-Aug-2014 1


JB609325

DYNCORP TASM 0PMI-1 AND PMI-2 COMPLETED AT 5349.5 ACFTHRS, PMI-1 DUE AT 5709.5 ACFT HRS

09-Aug-2014 1


JB609325

DYNCORP TASM OTAIL ROTOR SYSTEM COMPLETE RIGCOMPLETED 09 AUG 14 AT 5349.5 ACFT HRSIAW H-60-13-AMAM-01 ADDENDUM 1: BIASDIM A; RED 4.749, BLACK 4.039, YELLOW4.800, BLUE 4.035. DIM B; RED 5.071, BLACK4.333, YELLOW 5.112, BLUE 4.348. DIFF; RED0.322, BLACK 0.294, YELLOW 0.312, BLUE0.313. BLADE SET ANGLE RED; -1.56, FINAL3.0, BLACK SET -1.69, FINAL 3.0, YELLOW SET-1.24, FINAL 2.9, BLUE SET -0.56, FINAL 2.9.

09-Aug-2014 2


JB609325

DYNCORP TASM OTAIL ROTOR CABLE TENSION CHECKCOMPLETED 09 AUG 14 AT 5349.5 ACFT HRSIN CONJUNCTION WITH TAIL ROTOR SYSTEMCOMPLETE RIG. LEFT CABLE TENSION 167LBS, RIGHT CABLE TENSION 165 LBS @ 27DEG CEL.

09-Aug-2014 3


JB609325

DYNCORP TASM OMAIN ROTOR SYSTEM COMPLETE RIGCOMPLETED 09 AUG 14 AT 5349.5 ACFT HRS.IAW H-60-13-AMAM-01 ADDENDUM 1: L0WCOLL ANGLES; 90 RT 9.5 180 FWD -2.0, 270LFT -10.3, 0 AFT 0.6, TOTAL -2.2, AVG -0.548.HIGH COLL; 90 20.7, 180 FWD 11.0, 270 LFT10.9, 0 AFT 19.1, TOTAL 61.7, AVG 15.43. FWDCYCL; 90 -1.8,270 31.3, TOTAL 33.13. AFTCYCL; 90 26.3, 270 5.2,TOTAL 21.14 LEFTCYCL; 180 FWD -8.2, 0 AFT 7.5, TOTAL 15.65.RT CYCL; 180 FWD 6.9, 0 AFT -7.6 TOTAL 14.46.

09-Aug-2014 4


JB609325

DYNCORP AVIATIONCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-17(MAIN ROTOR BLADE HEATER MATELECTRICAL ARCING), N/A THIS MDS

10-Aug-2014 1


DM937925



8.7.DATE

6.REMARKS

4. 5.



DYNCORP AVIATIONCOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-09 (ENGINE OUTUT SHAFT) BOTHSHAFTS ARE IMPROVED SHAFTS

10-Aug-2014 2


DM937925

D CO 1-52 AVNCOMPLY WITH H-60-AMAM-14 NLT 30-NOV-14 20-Aug-2014 1


DR604724

D C0 1-52 AVNCOMPLIED WITH H-60-14-SOF-04 (TM 1-1520-237-CL UPDATE) 31 AUG 14

31-Aug-2014 1


MM231326

D CO 1-52 AVNT/R RIG COMPLETED READINGS ASFOLLOWS:RED: SET 2.97, 1ST 3.0, 2ND 3.01,FINAL 2.99RED: DIM A: 4.78, DIM B: 5.07, DIFF:0.29BLACK: SET 2.72, 1ST 2.99, 2ND 3.03,FINAL 2.97BLACK: DIM A: 4.05, DIM B: 4.35,DIFF: 0.30YELLOW: SET 2.95, 1ST 3.01, 2ND3.01, FINAL 2.97YELLOW: DIM A: 4.79, DIM B:5.11, DIFF: 0.32BLUE: SET 2.85, 1ST 3.0, 2ND3.0, FINAL 3.0BLUE: DIM A: 4.05, DIM B: 4.35,DIFF: 0.30CABLE TENSION: L/H 161 LBS R/H162 LBS @ 26 DEG CELCIUS

03-Sep-2014 1


LN334741

D CO 1-52 AVNCOMPLIED WITH H-60-14-ASAM-10 (MAINTRANSMISSION PLANETARY CARRIERASSEMBLY) ON 3 SEP 14

03-Sep-2014 2


DR604724

D CO 2-501STLATE ENTRY: H-60-14-AMAM-14 (IVHMSCABLING) COMPLETED

15-Dec-2014 1

FT. BLISS, TX 79916

AS862253

L3/AFM(LATE ENTRY) PREVIOUSLY COMPLIED WITHH-60-10-ASAM-16 ON 10 OCT 10 (RESCUEHOIST)

28-Jan-2015 1

FT. BRAGG, NC

JR956316

L3/AFM(LATE ENTRY) PREVIOUSLY COMPLIED WITHH-60-11-ASAM-02 ON 16 OCT 10 (T/R SERVOHARDWARE)

28-Jan-2015 2

FT. BRAGG, NC

JR956316

L3/AFM(LATE ENTRY) PREVIOUSLY COMPLIED WITHH-60-11-AMAM-11 ON 28 JUN 10 (AWRRELEASE)

28-Jan-2015 3

FT. BRAGG, NC

JR956316

L3/AFM(LATE ENTRY) PREVIOUSLY COMPLIED WITHH-60-11-AMAM-13 ON 7 JUL 11 (EXTERNALHOIST MOUNT FITING)

28-Jan-2015 4

FT. BRAGG, NC

JR956316

L3/AFM(LATE ENTRY) PREVIOUSLY COMPLIED WITHH-60-12-ASAM-07 ON 12 DEC 12 (ELECTRICALWIRE CHAFE)

28-Jan-2015 5

FT. BRAGG, NC

JR956316

L3/AFM(LATE ENTRY) PREVIOUSLY COMPLIED WITHH-60-14-AMAM-09 ON 29MAR14 (MAIN XMSNFILTER BOWL HWDR)

28-Jan-2015 6

FT. BRAGG, NC

JR956316

L3/AFM(LATE ENTRY) PREVIOUSLY COMPLIED WITHH-60-14-AMAM-19 ON 20 AUG 14 (ULLS-ACODE CHANGE)

28-Jan-2015 7

FT. BRAGG, NC

JR956316

L3/AFM(LATE ENTRY) PREVIOUSLY COMPLIED WITHH-60-13-AMAM-02 ON 12 DEC 12 (AHRS)

28-Jan-2015 8

FT. BRAGG, NC

JR956316

L3/AFM(LATE ENTRY) PREVIOUSLY COMPLIED WITHH-60-13-AMAM-06 ON 27MAR13 (CEFS)

28-Jan-2015 9

FT. BRAGG, NC

JR956316



8.7.DATE

6.REMARKS

4. 5.



L3/AFM(LATE ENTRY) PREVIOUSLY COMPLIED WITHH-60-15-ASAM-01ON 3 DEC 14 (LED-CAP)

28-Jan-2015 10

FT. BRAGG, NC

JR956316

L-3 RASM-E, AMCOMACE COMPLETED @ 5428.2 ACFT HRS BY ACETEAM MEMBERS "D" AND "L" L-3 RASM-E,AMCOM

06-Feb-2015 1

FT. BRAGG, NC

SD928779

L-3/AFMCOMPLIED WITH H-60-15-AMAM-05 (AHRS) AT5428.2 ACFT HRS

10-Feb-2015 1

FT. BRAGG, NC

GM706809

L-3/AFMCOMPLIED WITH H-60-15-SOF-01 (OIL COOLERFAN AXIAL BEARING) AT 5428.2 ACFT HRS

10-Feb-2015 2

FT. BRAGG, NC

GM706809

L-3/AFMCOMPLIED WITH H-60-15-AMAM-06 (ASE) AT5428.2 ACFT HRS

12-Feb-2015 1

FT. BRAGG, NC

GM706809

L-3/AFMDURING RESET INSPECTION THE RIGHT HANDTEXAS PATCH WAS FOUND CRACKED ANDWAS REPLACED I/A/W MEC# F195301 AT5428.2 ACFT HRS

04-Mar-2015 1

FT. BRAGG, NC

GM706809

L-3/AFMDURING RESET INSPECTION THE RIGHT HANDMAIN LANDING GEAR FITTING P/N 70219-02526-042 OTBD LUG BORE WAS GROOVED 0.010AND WAS REPAIRED I/A/W MEC# F195676 AT5428.2 ACFT HRS. THE FITTING P/N ISCHANGED TO P/N AF-058-1B I/A/W DMWR 1-1520-237-1 WP 0136 00.

04-Mar-2015 2

FT. BRAGG, NC

GM706809

L-3/AFMDURING DRY RIG THE CO-PILOTS LOW STICKSTOP HAD TO BE SET TO 0.730 IAW WP 107700 STEP 14 D

24-Mar-2015 1

FT. BRAGG, NC

GM706809

L-3/AFMMAIN ROTOR RIGGED IAW ADDENDUM 1 TO H-60-15-AMAM-03 BLADE ANGLES: LOW COLL= -0.525, HIGH COLL= 15.225, FWD CYC= +33.3,AFT CYC= 22.2, LEFT CYC= 16.0, RIGHT CYC=14.3. THE PRIMARY SERVO CONTROL RODSWERE ADJUSTED AS FOLLOWS AFTER BIASWAS SET:FWD SHORTENED 1.5 FLATS, AFTLENGTHENED 1.5 FLATS, LAT SHORTENED 3FLATS.COMPLETED AT 5428.2 ACFT HRS

26-Mar-2015 1

FT. BRAGG, NC

GM706809

L-3/AFMTAIL ROTOR RIGGED IAW ADDENDUM 1 TO H-60-15-AMAM-03 BLADE ANGLES: BLADESET DIM A DIM B DIFF FINALANGLERED -0.2 4.798 5.119 .3213.0 DEGBLK -1.3 4.025 4.337 .3123.0 DEGYEL -0.3 4.737 5.060 .3233.0 DEGBLU -0.6 3.982 4.296 .3143.0 DEGTAIL ROTOR CABLE TENSIONCOMPLETED TEMP 22C, LEFT 158, RIGHT 160.COMPLETED AT 5428.2 ACFT HRS

26-Mar-2015 2

FT. BRAGG, NC

GM706809

L-3/AFMRESET INSPECTION COMPLIED WITH IAW TB 1-1500-200-20-31 AND TB 1-1520-237-30-1 @5428.2 AIRCRAFT HOURS. NEXT PMI ISDUE @5788.2 ACFT HRS

01-Apr-2015 1

FT. BRAGG, NC

GM706809

L-3/AFMAWR 744/R9 DTD 16 JAN 15 (TOW PLATES)APPLIED AT 5428.2 ACFT HRS

01-Apr-2015 2

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1037/R12 DTD 3 JAN 14(SATCOM)APPLIED AT 5428.2 ACFT HRS

01-Apr-2015 3

FT. BRAGG, NC

GM706809



8.7.DATE

6.REMARKS

4. 5.



L-3/AFMAWR 1279/R5 DTD 13 JUN 14(OPERAT WITHDOORS/WINDOWSREMOVED) APPLIED AT5428.2 ACFT HRS

01-Apr-2015 4

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1309/R8 DTD 14 APR 14(UH/HH-60 A/L/MHELICOPTERS EQUIPED WITH OREGON AEROSEAT CUSHIONS) APPLIED AT 5428.2 ACFTHRS

01-Apr-2015 5

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1425/R18 DTD 18 SEP 14(OPERATECMWS,ICMD,P3I ON UH-60 A/L) APPLIED AT5428.2 ACFT HRS

01-Apr-2015 6

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1444/R7 DTD 14 APR 14(HELICOPTERSEQUIPPED WITH SINGLE AHRS/AHRU)APPLIED AT 5428.2 ACFT HRS

01-Apr-2015 7

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1452/4 DTD 12 APR 13(UH/HH-60A/LEQUIPPED WITH DIGITALCHONOMETER)APPLIED AT 5428.2 ACFT HRS

01-Apr-2015 8

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1455/R5 DTD 28 OCT 14(UH/EH-60A/LHELICOPTERS EQUIPPED WITH THEBATTELLE CAP) APPLIED AT 5428.2 ACFT HRS

01-Apr-2015 9

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1566/R4 DTD 13 MAR 15(HOIST CABLEGUARD) APPLIED AT 5428.2 ACFT HRS

01-Apr-2015 10

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1648/R3 DTD 28 MAR 14(UH/HH-60A/L/MOPERATE MAGNUS LAPTOP ONBOARD)APPLIED AT 5428.2 ACFT HRS

01-Apr-2015 11

FT. BRAGG, NC

GM706809

L-3/AFMAWR1656/R3 DTD 8 JAN 15(PHOENIX DRIPPAN) APPLIED AT 5428.2 ACFT HRS

01-Apr-2015 12

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1682/R16 DTD 19 DEC 14(701D FOR UH-60A) APPLIED AT 5428.2 ACFT HRS

01-Apr-2015 13

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1694/R4 DTD 6 JAN 14(UH/HH-60A/LEQUIPPED WITH DSC)APPLIED AT 5428.2ACFT HRS

01-Apr-2015 14

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1738/R2 DTD 23 JAN 15 (UH-60AEQUIPPED WITHAN/APX-118 CPX)APPLIED AT5428.2 ACFT HRS

01-Apr-2015 15

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1753/R5 DTD 30 JAN 15(UH-60A/L AND EH-60A EQUIPPED WITH DGNS AN/ASN-128B/D)APPLIED AT 5428.2 ACFT HRS

01-Apr-2015 16

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1787/R1 DTD 28 AUG 13(UH-60A/LEQUIPPED WITH AN/ARN-123VOR/ILS)APPLIED AT 5428.2 ACFT HRS

01-Apr-2015 17

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1788/R5 DTD 23 DEC 14(AN/ARN-123VOR/ILS TRAY MOUNT)APPLIED AT 5428.2ACFT HRS

01-Apr-2015 18

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1800/R3 DTD 16 JUL 14(BFT)APPLIED AT5428.2 ACFT HRS

01-Apr-2015 19

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1833/R4 DTD 29 DEC 14(UH-60A/L WITHAN/APX-123 TRANSPONDER)APPLIED AT5428.2 ACFT HRS

01-Apr-2015 20

FT. BRAGG, NC

GM706809

L-3/AFMAWR 1967/R1 DTD 28 JAN 15(UH-60A/LEQUIPPED WITH FLIR)APPLIED AT 5428.2ACFT HRS

01-Apr-2015 21

FT. BRAGG, NC

GM706809



8.7.DATE

6.REMARKS

4. 5.



L-3/AFMISAQ 110/R2 DTD 30 MAR 06 (UH-60A/LEQUIPPED WITH MAVEN HEATING SYSTEMOPTION II)APPLIED AT 5428.2 ACFT HRS

01-Apr-2015 22

FT. BRAGG, NC

GM706809

L-3/AFMCOMPLIED WITH H-60-15-AMAM-02 (IVHMS) AT5428.2 ACFT HRS

02-Apr-2015 1

FT. BRAGG, NC

GM706809

L-3/AFMCOMPLIED WITH H-60-15-ASAM-03(TROOP/GUNNER SEAT ENERGYATTENUATORS) AT 5432.2 ACFT HRS

09-Apr-2015 1

FT. BRAGG, NC

GM706809

PAEH-60-15-AMAM-10 AV-DEC GASKETINSPECTION. COMPLETED @ 5459.2 ACFTHRS. AV-DEC NOT INSTALLED.

11-May-2015 1

FORT IRWIN, CA

RT110477

PAEMODE S ADDRESS FOR UH-60A 8223745 IS:53407242

01-Jun-2015 1

FORT IRWIN, CA

RT110477

PAEH-60-15-AMAM-11, MODE-S TRANSPONDERADDRESS REVIEW, COMPLETED @ 5461.2ACFT HRS.

01-Jun-2015 2

FORT IRWIN, CA

RT110477

PAEACE COMPLETED @5463.3 ACFT HRS AT THISLOCATION BY TEAM MEMBERS JJ&T.

19-Jun-2015 1

FT. IRWIN, CA

WG084807

PAELATE ENTRY, ACFT TRANSFERRED TO FT.IRWIN, CA, APRIL 2015

06-Jul-2015 1

FORT IRWIN, CA

RT110477

PAEH-60-15-AMAM-14, LCF CHANGE 67REQUIREMENTS COMPLETED AT 5501.8AIRCRAFT HOURS

24-Aug-2015 1

FT. IRWIN, CA

JG116242

PAETAIL ROTOR GEARBOX CHIP DETECTORLIGHT ILLUMINATED IN FLIGHT AT 5501.8ACFT HRS. INSPECTION RREVEALED ONEFINE HAIR LIKE PARTICLE.

25-Aug-2015 1

FT. IRWIN, CA

FN113208

PAEH-60-15-SOF-02 N/A THIS AIRCRAFT 25-Sep-2015 1

FORT IRWIN, CA

FN113208

AFMA RASM-P / PAETECHNICAL SERVICES

AWR 1858/R4 DTD 15 MAY 15 (OPERATION OFUH-60A/L HELICOPOTERS WITHTELEPHONICS ENCRYPTED AIRCRAFTWIRELESS INTERCOM SYSTEM (EAWIS)INSTALLED

28-Oct-2015 1

FORT IRWIN, CA

RB117980

PAEH-60-15-AMAM-18 N/A THIS AIRCRAFT 29-Oct-2015 1

FT. IRWIN, CA

FN113208

PAEH-60-16-AMAM-01 N/A THIS ACFT 29-Oct-2015 2

FORT IRWIN, CA

MP115695

PAEH-60-16-ASAM-01 INBOARD RETENTIONPLATE TORQUE CHECKS COMPLIED WITH

13-Nov-2015 1

FORT IRWIN, CA

JG116242

PAEH-60-16-AMAM-03 PERSONNEL LOCATOR SETCOMPLIED WITH

23-Nov-2015 1

FORT IRWIN, CA

MP115695

PAEH-60-16-ASAM-02, DEFECTIVE FUEL HOSES,COMPLIED WITH AT 5582.1 ACFT HRS. N/ATHIS AIRCRAFT.

05-Jan-2016 1

FORT IRWIN, CA

FN113208

PAEH-60-16-AMAM-04, T-CLIPS INSTALLATION,COMPLIED WITH AT 5582.1 ACFT HRS. N/ATHIS AIRCRAFT.

05-Jan-2016 2

FORT IRWIN, CA

FN113208



8.7.DATE

6.REMARKS

4. 5.



PAE TECHNICALSERVICES JBLM WA98433

AWR 1859 DATED 08 JAN 16 R7 ACFTMODIFIED WITH WULFSBERG FLEXCOMM IISYSTEM INSTALLED

29-Jan-2016 1

FORT IRWIN, CA

GS110789

PAEH-60-16-AMAM-06 T-CLIP INSTALLATIONADDITIONAL TAIL NUMBERS: NOTAPPLICABLE

18-Apr-2016 1

FORT IRWIN, CA

AL117738

PAEH-60-16-ASAM-05 MAIN ROTOR BLADEDEBONDING COMPLIED WITH, NOTAPPLICABLE TO THIS AIRCRAFT.

18-May-2016 1

FORT IRWIN, CA

AL117738

PAEAVIATION MAINTENANCE ACTION MESSAGE(AMAM), MAINTENANCE MANDATORY,TRANSPONDER BATTERY REPLACEMENT,GEN-16-AMAM-04 COMPLIED WITH

31-May-2016 1

FORT IRWIN, CA

CR118106

PAE TSCOMPLIANCE OF H-60-16-AMAM-09COMPLETED

09-Jun-2016 1

FORT IRWIN, CA

MP115695

PAESOF MSG UH-60-16-SOF-01 TECHNICAL,UPPER CABIN STATION (STA) 379 FRAMECRACKING, COMPLIED WITH, NO CRACKSINDICATED AT 5684.8 ACFT HOURS

21-Jun-2016 1

FORT IRWIN, CA

CR118106

PAE JBLMACE PERFORMED AT 5687.9 A/C HRS @DAGGETT CA BY ACE TEAM MEMBERS JJ & D(WG552700)

14-Jul-2016 1

FORT IRWIN, CA

KG403888

PAEH-60-16-AMAM-10 ULLS-A(E) PHASE LCFUPDATES COMPLIED WITH 21 JULY 2016

22-Jul-2016 1

FORT IRWIN, CA

AL117738

PAECOMPLIED WITH H-60-16-SOF-02, RESCUEHOIST OPERATIONAL RESTRICTIONS, NOTAPPLICABLE TO THIS AIRCRAFT.

16-Aug-2016 1

FORT IRWIN, CA

CH111144

PAEH-60-16-ASAM-06, IMPROVED TAIL ROTORQUADRANT SUPPORT

23-Aug-2016 1

FORT IRWIN, CA

RT110477

PAEH-60-17-ASAM-01 ULLS-A(E) CADS MODULECOMPLIED WITH

11-Oct-2016 1

FORT IRWIN, CA

JG116242

P A ECOMPLIED WITH H-60-17-AMAM-01,ULLS-A(E)LCF CHANGE 68 REQUIRMENTS

31-Oct-2016 1

FORT IRWIN, CA

EK119162

PAECOMPLY WITH H-60-17-ASAM-02, TAIL ROTORSERVO PILOT INPUT ARM ASSEMBLY BEFORE5752.6 ACFT HRS, BUT NOT TO EXCEED 5 DEC16, PREVIOUSLY COMPLETED ON [email protected] ACFT HOURS BY EK119162, ON -13,DAMAGE FOUND. (JM115963)

22-Dec-2016 1

FORT IRWIN, CA

JM115963

PAECOMPLY WITH H-60-15-ASAM-04, MAIN ROTORBLADE DEBONDING, BEFORE 5468.2 HOURS,BUT NOT TO EXCEED 3 JULY 15, PREVIOUSLYCOMPLIED 07-MAY-15 @5459.2 ACFT HOURS -13 BY CR118106. (JM115963)

23-Dec-2016 1

FORT IRWIN, CA

JM115963

PAECOMPLY WITH H-60-15-ASAM-07, MAIN ROTORBLADE DEBONDING AND TIP RIB CRACKING,BEFORE 5788.2 ACFT HOURS, BUT NOT TOEXCEED 10 AUG 16, PREVIOUSLY COMPLIEDWITH ON 07 AUG 16 @5711.9 ACFT HOURS -13BY MP115695. (JM115963)

23-Dec-2016 2

FORT IRWIN, CA

JM115963



8.7.DATE

6.REMARKS

4. 5.



PAEH-60-17-ASAM-04, AIRFRAME STRUCTURALPARTS C/W @ AC HOURS 5758.2

04-Jan-2017 1

FORT IRWIN, CA

JG116242

PAETRANSFER STATEMENT: AIRCRAFTTRANSFERRED TO BEST PROGRAM ON 20JAN 2017 FOR ARMY/BEST PROGRAM BY ACO. 2916TH AVN BN AT 5759.5 ACFT HRS.DATA PLATE REMAINED INSTALLED.RT110477, PAE, (760) 380-0231.

18-Jan-2017 1

FORT IRWIN, CA

RT110477

SCIENCE ANDENGINEERINGSERVICES LLC

H-60-17-SOF-01 NOT COMPLIED WITH. 25-Jan-2017 1

HUNTSVILLE

JH902419

SCIENCE ANDENGINEERINGSERVICES, LLC.

H-60-17-ASAM-05 NOT COMPLIED WITH. 22-Feb-2017 1

HUNTSVILLE, AL.

TM902492


DATE AC HRS SHAFT VERTICAL REASON FOR VIB CHECKLONGITUDINALLATERAL

IPS READINGS4.

8223745HELICOPTER, UTILITYUH-60A3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Report Date: 19-Jan-2017 1/5

POST RESET GMTF REQUIREMENTS.16-Jun-2008 # 1 ENGINE 0.14003751.9

100HR INSP01-Jan-2001 #1 ENGINE 0.0099999997002570

100HR INSP01-Jan-2001 #2 ENGINE 0.1099999994002570

GIMBAL REPLACEMENT17-Jul-2002 #2 ENGINE 0.2199999988002625

ENGINE REPLACEMENT18-Oct-2002 #1 ENGINE 0.1800000071002665.699

T/R OUTPUT SEAL REPLACED18-Oct-2002 TAIL ROTOR 0.0799999982002665.699

RMVD/REINST T/R PADDLES14-Nov-2002 TAIL ROTOR 0.1099999994002674.600

100HR INSP17-Sep-2003 #1 ENGINE 0.2800000011002828.600

100HR INSP17-Sep-2003 #2 ENGINE 0.2599999904002828.600

100HR INSP17-Sep-2003 TAIL ROTOR 0.0700000002002828.600

100HR INSP17-Sep-2003 OIL COOLER 0.14000000050.460000008302828.600

ENG REPLACEMENT26-May-2004 #1 ENGINE 0.1899999976002913.699

PMS-2 COMPLETION01-Aug-2005 #1 ENGINE 0.3100000023002933.100

PMS-2 COMPLETION01-Aug-2005 #2 ENGINE 0.0700000002002933.100

PMS-2 COMPLETION01-Aug-2005 OIL COOLER 0.10000000140.519999980902933.100

PMS-2 COMPLETION01-Aug-2005 TAIL ROTOR 0.0799999982002933.100

DEPLOYMENT08-Feb-2006 TAIL ROTOR 0002965

120 HR VIBE CHECKS27-Apr-2006 #1 ENGINE 0.3199999928003032.399

120 HR VIBE CHECKS27-Apr-2006 #2 ENGINE 0.0299999993003032.399

120 HR VIBE CHECKS27-Apr-2006 OIL COOLER 0.15000000590.490000009503032.399

120 HR VIBE CHECKS27-Apr-2006 TAIL ROTOR 0.2000000029003032.399

120 HR VIBE CHECKS18-Aug-2006 #1 ENG 0.1500000059003144

120 HR VIBE CHECKS18-Aug-2006 #2 ENG 0.0199999995003144

120 HR VIBE CHECKS18-Aug-2006 OIL COOLER 0.10000000140.490000009503144

120 HR VIBE CHECKS18-Aug-2006 TAIL ROTOR 0.0599999986003144

120 HR VIBE CHECKS24-Nov-2006 #1 ENGINE 0.0199999995003251.399

120 HR VIBE CHECKS24-Nov-2006 #2 ENGINE 0.0500000007003251.399

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

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


IPS READINGS4.



120 HR VIBE CHECKS24-Nov-2006 OIL COOLER 0.10000000140.469999998803251.399

120 HR VIBE CHECKS24-Nov-2006 TAIL ROTOR 0.0399999991003251.399

120HR INSP17-May-2007 #1 ENGINE 0.0799999982003484

120HR INSP17-May-2007 #2 ENGINE 0.1199999973003484

120HR INSP17-May-2007 OIL COOLER 0.109999999400.20999999343484

120HR INSP17-May-2007 T/R 0.1000000014003484

#1 ENG REPLACEMENT04-Jun-2007 #1 ENGINE 0.4300000071003448.699

120HR INSP20-Jul-2007 #1 ENGINE 0.1800000071003528.699

120HR INSP20-Jul-2007 #2 ENGINE 0.1899999976003528.699

120HR INSP20-Jul-2007 OIL COOLER 0.1199999973003528.699

120HR INSP20-Jul-2007 TAIL ROTOR 00.029999999303528.699

POST RESET GMTF REQUIREMENTS.16-Jun-2008 # 2 ENGINE 0.1003751.9

POST RESET GMTF REQUIREMENTS.16-Jun-2008 OIL COOLER 00.09603751.9

POST RESET GMTF REQUIREMENTS.16-Jun-2008 TAIL ROTOR 0.08003751.9

120 HR INSP INCONJUCTION WITH IVHUMS MOD06-Jan-2009 OIL COOLER 0.080.3403868.1

120 HR INSP INCONJUCTION WITH IVHUMS MOD06-Jan-2009 #1 ENGINE 0.28003868.1

120 HR INSP INCONJUCTION WITH IVHUMS MOD06-Jan-2009 #2 ENGINE 0.09003868.1

120 HR INSP INCONJUCTION WITH IVHUMS MOD06-Jan-2009 TAIL ROTOR 0.05003868.1

120 HR21-Jun-2009 OIL COOLER 0.110.2103985.9

120 HR21-Jun-2009 #1 ENGINE 0.49003985.9

120 HR21-Jun-2009 #2 ENGINE 0.19003985.9

120 HR21-Jun-2009 TAIL ROTOR 0.02003985.9

T/R PADDLE REPLACEMENT13-Aug-2009 TAIL ROTOR 00.0704064.1

PMI 102-Sep-2009 TAIL ROTOR 00.104075

PMI 102-Sep-2009 OIL COOLER 0.270.0904075

PMI 102-Sep-2009 #1 ENGINE 0.09004075

PMI 102-Sep-2009 #2 ENGINE 0.22004075




IPS READINGS4.



120 HR INSP.25-Nov-2009 TAIL ROTOR 0.07004186.3

120 HR INSP.25-Nov-2009 OIL COOOLE 0.070.2204186.3

120 INSP.25-Nov-2009 #1 0.23004186.3

120 INSP.25-Nov-2009 #2 ENG 0.27004186.3

120 HR VIBE CHECK02-Mar-2010 T/R 00.1104306.3

120 HR VIBE CHECK02-Mar-2010 #1 ENG 00.2804306.3

120 HR VIBE CHECK02-Mar-2010 #2 ENG 00.2204306.3

120 HR VIBE CHECK02-Mar-2010 OL COOLER 0.4900.094306.3

ENGINE REMOVAL/REINSTALLATION10-Nov-2010 #1 HSS 0.09004494.7

ENGINE REMOVAL/REINSTALLATION10-Nov-2010 #2 HSS 0.2004494.7

POST RESET05-Jan-2012 #1 HSS 0.22004641.5


POST RESET05-Jan-2012 OIL COOLER 0.1100.064641.5

POST RESET05-Jan-2012 T/R 00.0604641.5

POST RESET18-Jan-2012 T/R 00.1504643.5



POST RESET18-Jan-2012 OIL COOLER 0.3800.114643.5

POST 9-11HR TQ CHECKS FOR INBOARD RETENT30-Jan-2012 T/R 00.12046447

120 HR VIBES24-Oct-2012 OIL COOLER 0.0060.2504871.5

120 HR VIBES24-Oct-2012 #1 ENG 0.18004871.5

120 HR VIBES24-Oct-2012 #2 ENG 0.35004871.5

TBC WHEN COMING OUT OF 120HR INSP24-Oct-2012 TAIL ROTOR 0.33004871.5

POST 120HR. WITHIN ADVISORY LIMITS.30-Oct-2012 TAIL ROTOR 0.25004873.1

PREPHASE MTF20-May-2013 #1 ENG 0.26004984.3

PREPHASE MTF20-May-2013 #2 ENG 0.36004984.3

PREPHASE MTF20-May-2013 OIL COOLER 0.040.404984.3




IPS READINGS4.



PREPHASE MTF20-May-2013 TAIL ROTOR 0.2004984.3

POST PMI-115-Jun-2013 #1 ENG 0.29004989.5

POST PMI-115-Jun-2013 #2 ENG 0.36004989.5

POST PMI-115-Jun-2013 OIL COOLER 0.030.3304989.5

POST PMI-115-Jun-2013 TAIL ROTOR 0.05004989.5

120 VIBES10-Oct-2013 T/R 0.1005109.5

120 VIBES10-Oct-2013 O/C 0.260.3405109.5

120 VIBES10-Oct-2013 #1 HSS 0.26005109.5

120 VIBES10-Oct-2013 #2 HSS 0.36005109.5

TAIL ROTOR TRACK & BALANCE VERIFICATION03-Mar-2014 T/R 0.02005202

120 VIBES30-Mar-2014 T/R 0.09005224.1

120 VIBES30-Mar-2014 O/C 0.070.405224.1

120 VIBES30-Mar-2014 #1 HSS 0.26005224.1

120 VIBES30-Mar-2014 #2 HSS 0.31005224.1

POST PMI19-Aug-2014 #1 HSS 0.04005349.5

POST PMI19-Aug-2014 #2 HSS 0.27005349.5

POST PMI19-Aug-2014 T/R 0.05005349.5

POST PMI19-Aug-2014 O/C 0.110.2705349.5

T/R BALANCE FOR T/R REMOVAL30-Aug-2014 TAIL ROTOR 0.08005369.5

T/R BALANCE FOR T/R REMOVAL03-Sep-2014 TAIL ROTOR 0.01005379.6

T/R BAL FOR T/R UNFOLD23-Dec-2014 TAIL ROTOR 0.07005406.7

POST RESET03-Apr-2015 #1 ENG 0.15005428.2

POST RESET03-Apr-2015 #2 ENG 0.2005428.2

POST RESET03-Apr-2015 OIL COOLER 0.030.2905428.2

POST RESET03-Apr-2015 TAIL ROTOR 0.03005428.2

#1 ENG REPLACEMENT27-Jun-2015 #1 ENG 0.29005465.1

120 HR CHECK10-Nov-2015 #2 ENG 0.49005545.4




IPS READINGS4.



120 HR CHECK10-Nov-2015 #1 ENG 0.1005545.4

120 HR CHECK10-Nov-2015 OIL COOLER 00.32305545.4

120 HR VIB CK10-Nov-2015 TAIL ROTOR 0.03005545.4

120 HRS27-May-2016 #1 ENG 0.39005663.1

120 HRS27-May-2016 #2 ENG 0.44005663.1

120 HRS27-May-2016 T/R 0.1005663.1

120 HRS27-May-2016 OIL COOLER 00.2905663.1

IN CONJUNCTION WITH TRACK AND BALANCE12-Aug-2016 TAIL ROTOR 0.02005714.3

6. Remarks



Report Date: 22-Feb-2017 1/4

8223745HELICOPTER, 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

A012 16 Feb 201771-1520-237-PMDPMD INSPECTION DUE 09 Feb 2017D

A020 5769.510TM 1-1520-237-PMDPERFORM M/R SPINDLE LUGS,M/R CUFF, TIP CAPSINSPECTION

5759.5H

A022 14 Feb 201714TM 1-1520-237-23-914 DAY FLYABLE STORAGEENGINE RUN UP

31 Jan 2017D

A045 5798.240H-60-11-AMAM-03REQUIRE DOWNLOAD ANDTRANSMIT OF IVHMS FULL RAWDATA

5758.2H

A092 16 Feb 201730TM 11-6140-203-23&P30 DAY SLAB BATTERYINSPECTION (D8565/11-1)

17 Jan 2017D

A100 15 Feb 201730DA PAM 738-751#1 ENGINE HISTORY RECORDERREADING DUE

16 Jan 2017D

A101 15 Feb 201730DA PAM 738-751#2 ENGINE HISTORY RECORDERREADING DUE

16 Jan 2017D

A110 5798.240TM 1-1520-237-PMSPMS 40 HOUR INSPECTION 5758.2H

A115 11 Mar 201730TM 1-1520-237-23-12LUBE REQUIRMENTS 09 Feb 2017D

A115 5819.940TM 1-1520-237-23-12LUBE REQUIRMENTS 5779.9H

A116 5989.9360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

5629.9H

A116 03 Apr 201712H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

03 Apr 2016M

A117 5989.9360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 5629.9H

A117 03 Apr 201712H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 03 Apr 2016M

A140 5783.9120AWR 1346R16, IVHMSIN ACF

DOWNLOAD AND REVIEW IVHMSDATA

5663.9H

A160 11 Apr 201790TM 1-1520-237-23-1290 DAY CORROSIONINSPECTION

11 Jan 2017D

A177 18 Apr 201790AR 95-190 DAY REVIEW/UPDATE OF 365-4 ENTRIES

18 Jan 2017D

A210 5783.9120TM 1-1520-237-23-12120 HOUR INSPECTIONREQUIREMENTS

5663.9H

A211 5989.9360H-60-10-AMAM-11APU OIL SAMPLE 5629.9H

A211 03 Apr 201712H-60-10-AMAM-11APU OIL SAMPLE 03 Apr 2016M

A213 5783.1120TM 1-2840-248-23ENGINE COMPRESSORCLEANING

5663.1H

A214 5783.1120TM 1-1520-237-23-12CLEAN TAIL WHEEL ADAPTER 5663.1H

A222 24 Mar 2017360TM 1-1680-377-13&PAMSS SURVIVAL KITINSPECTION

29 Mar 2016D

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

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

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



7. FREQUENCY 4.




INSP

A230 20 Mar 2017120MWO 1-1520-237-50-77INSPECT BATTERYCOMPARTMENT FORCORROSION (SLAB)

20 Nov 2016D

A295 5788.2360TM 1-1520-237-23-12STABILATOR ACTUATOR ASSYLUBE

5428.2H

A296 5788.2360TM 1-1520-237-23-12STABILATOR INSPECTION 5428.2H

A298 5987.9360TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 5627.9H

A298 31 Mar 201712TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 31 Mar 2016M

A299 5987.9360TM 1-1520-237-23-12SWASHPLATE LUBE 5627.9H

A299 31 Mar 201712TM 1-1520-237-23-12SWASHPLATE LUBE 31 Mar 2016M

A320 5788.2360TM 1-2840-248-23ENGINE INSPECTION &CLEANING

5428.2H

A400 5788.2720TM 1-1520-237-PMIPMI-1 5068.2H

A401 6148.2720TM 1-1520-237-PMIPMI-2 5428.2H

A408 6148.2720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-2, AREA 5 AND 6)

5428.2H

A410 5788.2720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-1, AREA 1 THRU 4)

5068.2H

A415 6148.2720H-60-10-AMAM-11MAIN GEARBOX OIL SAMPLE-PART # 073, 074, 076

5428.2H

A440 6148.2720TM 1-1520-237-23-12CLEAN TAIL WHEEL LOCKPIN 5428.2H

A470 6849.51500TM 1-1520-237-23-12REPLACE NUMBER TWOCROSSFEED VALVE

5349.5H

A471 6793.42160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

4633.4H

A472 6793.42160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

4633.4H

A473 6793.42160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

4633.4H

A476 9633.45000TM 1-1520-237-23-12REPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

4633.4H

A477 10428.25000TM 1-1520-237-23-12REPLACEMENT OF STABILATORACTUATOR BOLTS

5428.2H

A480 9633.45000TM 1-1520-237-23-12REPLACE PIVOT BOLT 70400-08159-101,102,103,104

4633.4H

A485 9633.45000TM 1-1520-237-23-12REPLACE BELLCRANK BOLT70400-08159-105,106,107,108

4633.4H

A496 09 Aug 20176TM 1-1500-204-23-1CF3BR FIRE EXTINGUISHERWEIGHT TEST & INSPECTION

09 Feb 2017M

A501 30 Mar 20176TM 1-1520-237-23-12MAIN ROTOR BLADE PRESSURECHECK

30 Sep 2016M






7. FREQUENCY 4.




INSP

A502 09 Mar 20176TM 1-1520-237-23-12INSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

09 Sep 2016M

A530 21 Jan 201712DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

21 Jan 2016M

A532 03 Apr 201712TM 1-1500-204-23-4COMPASS SWING / RMI 03 Apr 2016M

A533 31 Mar 201712TM 1-1520-237-23-12PITOT STATIC SYSTEMINSPECTION

31 Mar 2016M

A534 01 Jan 201812TM 1-1500-204-23-1FIRST AID KIT INSPECTION 01 Jan 2017M

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

31 Mar 2016M

A541 31 Mar 201712TM 1-1520-237-23, C4REPLACE DIGITAL CLOCKBATTERY

31 Mar 2016M

A550 31 Mar 201712AWR1346R16IVHUMS BATTERYREPLACEMENT

31 Mar 2016M

A553 31 Mar 201712AR 95-1AIRCRAFT WEIGHINGINVENTORY (365-1)

31 Mar 2016M

A580 31 Mar 201724TM 11-6140-203-23&PRETURN SLAB TO AVIM FORCAPACITY CHECK (VEREY 24MONTH)

31 Mar 2015M

A621 31 Mar 201724AR 95-1AIRCRAFT WEIGHING CLASS 2 31 Mar 2015M

A625 01 Jun 201960TM 11-6140-203-23&PREPLACEMENT OF SLABBATTERY (SLAB)

01 Jun 2014M

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

01 Jan 2010M

A633 01 Jun 2020114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Dec 2010M

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

01 Jun 2010M

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

01 Jan 2010M

A641 08 Oct 202296TB 9-1300-385RESERVE FIRE BOTTLE #2,CARTRIDGE DODIC MT20

08 Oct 2014M

A648 16 Jun 2023180TM 1-1520-237-23REPLACE T/R SPRING CAPSULEASSY

16 Jun 2008M

A660 01 Oct 201872TB 9-1300-385REPLACE THRUSTEREMERGENCY RELEASE CARGOHOOK, MJ20

01 Oct 2012M

A665 31 Mar 201948H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

31 Mar 2015M

A670 31 Mar 201948TM 1-1520-237-23-1CABIN TUB INSPECTION 31 Mar 2015M

A673 31 Mar 201948TM 1-1520-237-23-12FUEL CELL CORROSIONINSPECTION

31 Mar 2015M

A675 31 Mar 201948TM 1-1520-237-23-12FLIGHT CONTROL ROD INSP 31 Mar 2015M






7. FREQUENCY 4.




INSP

A695 6148.2720H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

5428.2H

A695 31 Mar 201948H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

31 Mar 2015M

A755 14428.29000H-60-10-ASAM-11PC LINK TO SWASHPLATEBOLTS REPLACEMENT

5428.2H

E330 11 Dec 20186AWR1346R16UNDER WATER ACOUSTICBEACON BATTERYREPLACEMENT

11 Dec 2012Y

E351 01 Apr 2017180TM 11-5895-1841-13PREPLACE APX-118TRANSPONDER BATTERY

03 Oct 2016D




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: 1/1123-Feb-2017

82237451520010350266 00HELICOPTER, UTILITY

156001113021502C12D

5350535082237450809601

70219-05001-044TAIL CONE FITTING CCCC COND COND

162001231183103A01

4385428BEM286070250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001231183103A01

15034633IA0128570250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001421089003B01

10655359333013088L70250-13101-044SHOCK ABSORBER (TAIL) CCCC COND COND

165001285302405A01Z

28715780A106-0357570106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z

27815780A106-0443670106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z

24845780A1060193170106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z

21745780WG1060163070106-08100-046DAMPER ASSY, M/R CCCC COND COND

531501537465205A02H

13685780B9411284070103-08108-041SOLID BLADE PIN CCCC COND COND

531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


161501199764605A03A

2781578015152-151670104-08000-050SWASHPLATE ASSY CCCC COND COND

161501383899206A11

61145780A258-0153370351-08080-045ACCESSORY MODULE CCCC COND COND

161501383899206A11

32445780A258-0579470351-08080-045ACCESSORY MODULE CCCC COND COND

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

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

h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






161501503311506A

50265780A2650004070351-08100-076MAIN TRANSMISSIONMODULE

CCCC COND COND

161501353382506E

19175780A264-0758470351-08001-049INPUT MODULE CCCC COND COND

161501353382506E

19175780A264-0762570351-08001-049INPUT MODULE CCCC COND COND

168001074515206F

01972A005-0142970357-06300-042INTERMEDIATE GEARBOX CCCC COND COND

161501376508906G01

03293A006-0330070358-06600-046TAIL ROTOR GEARBOXASSY

CCCC COND COND

161501524780506H04 #2 ENGINE

03752C845-0214670361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501524780506H04

8814633C8450411870361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501081277506H06

0999A271-0116870361-03001-045SHAFT ASSY, T/R DRV SEC1

CCCC COND COND

161501158951706H08 OIL COOLER

03752WG30027-00088

70361-03009-047SHAFT ASSY, T/R DRV SEC2

CCCC COND COND

161501158952206H09

04633WG30049-00088

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

CCCC COND COND

161501158952206H09

04633WG30049-00375

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

CCCC COND COND

161501158952206H09

04633WG30050-00002

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

CCCC COND COND

161501083295306H11


CCCC COND COND

161501158578806H12


CCCC COND COND

432001207722807A01

258957804008236ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01

12665780K5494ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01

20345359272849ABR70652-02300-050PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

481001102247307B05A

16954633150653213850-3-1VALVE, SOLENIOD CCCC COND COND

481001102247307B05A

29495428B1290-1685370306-02107-104VALVE, SOLENIOD CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






165001250376707B11

32374460C401-010070204-0004ACCUMULATOR CCCC COND COND

168001342049608B20

054285509100-601561-000PANEL INDICATOR (PDU) CCCC COND COND

168001342049608B20

28054285546100-601561-000PANEL INDICATOR (PDU) CCCC COND COND

168001566036608F01

76646335130279-0302IVHMU (CBM MONITORSYSTEM)

CCCC COND COND

611501114969609A01

19175780106-A292128B302-8-DMGENERATOR CCCC COND COND

611501114969609A01

18305780111-A048828B302-8-DMGENERATOR CCCC COND COND

168001310225911C21

05350B9950165170400-02300-048MIXER ASSEMBLY CCCC COND COND

168001261204411D25 LOWER

17734409B2920045470400-06641-117STABILATOR ACTUATOR CCCC COND COND

168001261204411D25 UPPER

179944092697DL2155M20STABILATOR ACTUATOR CCCC COND COND

599601547345211D26

0522052391011445-1-002STABILATOR AMPLIFIER(DUAL)

CCCC COND COND

299501496368615A04

0449529484504587ENGINE SEQUENCINGUNIT

CCCC COND COND

599601188333219D01F

04633986BB622-6545-003AMPLIFIER, RADIOFREQUENC

CCCC COND COND

584101421416219E05A CO PILOT

053500998AAHG7209AD01RECEIVER-TRANSMITTER,RADAR

CCCC COND COND

584101245909319E05C

0542829BBA3060591INDICATOR HEIGHT CCCC COND COND

660501503528419E06A

053441736765100-20ATTITUDE HEADINGREFERENCE UNIT

CCCC COND COND

661001490516852A

178355272521202825050-1-001AUTOMAT FLT CONTCOMPUTER

CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






SIGNIFICANT HISTORICAL EVENTS7.




kjigfdcbaRMVL HR RMVL HRS

NOMEN HRS)COMPO/HO/HLOCATIONNSNWUC

he (ACFTLIFESINCEPRESER NO.ANDAND

INST HRSP/N DUEREPLACE

INST HRSTIMENO.COMPONENTNOMENCLATURE

NOMEN REP.O/H OCOMP6.

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

Report Date:

TIME CHANGE COMPONENTS5/1123-Feb-2017

00

156001081924402C15J20170

A496-01089 1802197270209-06051-043TAIL PYLON FITTING RCRC20000

161501450483405A01A9120

15152-00958 1760578070103-08112-047HUB, M/R ROTOR ASSY RCRC5100

161501442692605A01I11119

A001-08106 1061578070102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501442692605A01I10851

D001-01134 1329578070102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501442692605A01I10759

E001-00374 1421578070102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501442692605A01I10759

E001-00454 1421578070102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501074515105A01L16999

A286-01128 2781578070351-08186-043MAIN ROTOR SHAFTEXTENDER

RCRC14000

161501127738805A01T18027

AIM00292 753578070107-08400-046BIFILAR, M/R ROTORASSY

RCRC13000

161501113818805B027024

A00904494 8404542870101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501113818805B0213484

A00908705 1944542870101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501083681206G01B12956

A25702825 2337329370102-11101-042O/B RETENTION PLATE(T/R)

RCRC12000

414101329342806H237153

C51200332 3414463370361-03005-107FAN AXIAL 022520

156001129125607A2415956

B112-03650 2654561070410-02500-049SAS ACTUATOR 0013000

156001129125607A2417029

C11203756 1330535970410-02500-049SAS ACTUATOR RCRC13000

156001129125607A24 ROLL17075

C11205793 558463370410-02500-049SAS ACTUATOR RCRC13000

161501141753211C23 n/a6398

B233-02123 3321578070400-06100-042TAIL ROTOR PITCHCHANGE SHAFT

154212160

165001305695411C2515516C30004574 91254282227000-17TAIL ROTOR SERVO

ASSYRCRC

11000

165001143122611D0129104B30301503B 7245428274000-1031MAIN ROTOR PRIMARY

SERVORCRC

24400

165001143122611D0129527B30316234 3015428274000-1031MAIN ROTOR PRIMARY

SERVORCRC

24400

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

EDITION MAY 67 IS OBSOLETE

AIRCRAFT COMPONENT HISTORICALRECORD

DA FORM 2408-16-E, OCT 91


kjigfdcbaRMVL HR RMVL HRS

NOMEN HRS)COMPO/HO/HLOCATIONNSNWUC

he (ACFTLIFESINCEPRESER NO.ANDAND

INST HRSP/N DUEREPLACE

INST HRSTIMENO.COMPONENTNOMENCLATURE

NOMEN REP.O/H OCOMP6.

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

Report Date:

TIME CHANGE COMPONENTS6/1123-Feb-2017

00

165001143122611D0124977B30304179B 4851542870410-02820-054MAIN ROTOR PRIMARY

SERVORCRC

24400

156001158968511D0415999C343-02318 2781578070400-08102-045AFT BELLCRANK RCRC

13000

156001164416111D0520752A39101850 0375270400-08112-045AFT TIE ROD SUPT

FITTINGRCRC

17000

168001164416011D066220MM00255 1760578070400-08111-042AFT TIE ROD ASSY RCRC

2200

156001286887011D077399390-01930 2781578070400-08117-049AFT BELLCRANK SPT

ASSYRCRC

4400

304001287243811D0815238

1515202834 1158578070400-08151-061LATERAL SWASHPLATELINK

RCRC11000

161501158965811D0915622E289-00029 4623578070400-08150-045LATERAL SERVO

BELLCRANKRCRC

5500

168001158965311D116657E346-00008 2781578070400-08104-048AFT WALKING BEAM RCRC

11000

156001289269711D137599344-01985 2781578070400-08115-046LEFT TIE ROD ASSY RCRC

4600

156001296948611D14787028800410 1410578070400-08114-051RIGHT TIE ROD ASSY RCRC

3500

168001158965211D1517999646 2781578070400-08101-046FORWARD BELLCRANK RCRC

15000

156001221261911D168599B367-03938 2781578070400-08162-042FWD BELLCRANK SPT

ASSYRCRC

5600

SIGNIFICANT HISTORICAL EVENTS7.

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

EDITION MAY 67 IS OBSOLETE

AIRCRAFT COMPONENT HISTORICALRECORD

DA FORM 2408-16-E, OCT 91

ji kgfdcbaRMVL HRSRMVL HRSCOMPO/HNOMENWUC

HRS)O/HLOCATIONNSN

AND he SINCELIFE (ACFT

PREVSER NO. OAND

NOMENCLATURE PN TIMEINST HRS DUEREPLACE

INST HRSNO.COMPONENTNOMEN REP.O/H ORCOMP6.

1520010350266HELICOPTER,UTILITY

UH-60A 8223745 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 7 of 11

23-Feb-2017

COND COND

156001113021502C12D

53505350TAIL CONE FITTING 8223745080960170219-05001-044 CCCC

20000 20170

156001081924402C15J

18021972TAIL PYLON FITTING A496-0108970209-06051-043 RCRC

COND COND

162001231183103A01

4385428FWD FIXED GEARSHOCK

BEM286070250-12051-045 CCCC

COND COND

162001231183103A01


IA0128570250-12051-045 CCCC

COND COND

162001421089003B01

10655359SHOCK ABSORBER(TAIL)

333013088L70250-13101-044 CCCC

5100 9120

161501450483405A01A

17605780HUB, M/R ROTOR ASSY 15152-0095870103-08112-047 RCRC

6400 11119

161501442692605A01I

10615780MAIN ROTOR SPINDLEASSY

A001-0810670102-08200-069 RCRC

6400 10851

161501442692605A01I


D001-0113470102-08200-069 RCRC

6400 10759

161501442692605A01I


E001-0037470102-08200-069 RCRC

6400 10759

161501442692605A01I


E001-0045470102-08200-069 RCRC

14000 16999

161501074515105A01L

27815780MAIN ROTOR SHAFTEXTENDER

A286-0112870351-08186-043 RCRC

13000 18027

161501127738805A01T

7535780BIFILAR, M/R ROTORASSY

AIM0029270107-08400-046 RCRC

COND COND

165001285302405A01Z

28715780DAMPER ASSY, M/R A106-0357570106-08100-046 CCCC

COND COND

165001285302405A01Z


COND COND

165001285302405A01Z

24845780DAMPER ASSY, M/R A1060193170106-08100-046 CCCC

COND COND

165001285302405A01Z

21745780DAMPER ASSY, M/R WG1060163070106-08100-046 CCCC

COND COND

531501537465205A02H

13685780SOLID BLADE PIN B9411284070103-08108-041 CCCC

COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


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

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


HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 8 of 11

23-Feb-2017

COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

161501199764605A03A

27815780SWASHPLATE ASSY 15152-151670104-08000-050 CCCC

10000 7024

161501113818805B02

84045428TAIL ROTOR BLADEASSY

A0090449470101-31000-043 RCRC

10000 13484

161501113818805B02


A0090870570101-31000-043 RCRC

COND COND

161501383899206A11

61145780ACCESSORY MODULE A258-0153370351-08080-045 CCCC

COND COND

161501383899206A11


COND COND

161501503311506A

50265780MAIN TRANSMISSIONMODULE

A2650004070351-08100-076 CCCC

COND COND

161501353382506E

19175780INPUT MODULE A264-0758470351-08001-049 CCCC

COND COND

161501353382506E


COND COND

168001074515206F

01972INTERMEDIATEGEARBOX

A005-0142970357-06300-042 CCCC

COND COND

161501376508906G01

03293TAIL ROTOR GEARBOXASSY

A006-0330070358-06600-046 CCCC

12000 12956

161501083681206G01B

23373293O/B RETENTION PLATE(T/R)

A2570282570102-11101-042 RCRC

COND COND

1615015247805 #2 ENGINE06H04

03752DRIVESHAFT ASSYENGINE

C845-0214670361-08014-041 CCCC

COND COND

161501524780506H04


C8450411870361-08014-041 CCCC

COND COND

161501081277506H06

0999SHAFT ASSY, T/R DRVSEC 1

A271-0116870361-03001-045 CCCC

COND COND

1615011589517 OIL COOLER06H08


WG30027-0008870361-03009-047 CCCC

COND COND

161501158952206H09

04633SHAFT ASSY, T/R SEC3,4,5

WG30049-0008870361-05001-051 CCCC

COND COND

161501158952206H09


WG30049-0037570361-05001-051 CCCC

COND COND

161501158952206H09


WG30050-0000270361-05001-051 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 9 of 11

23-Feb-2017

COND COND

161501083295306H11


A273-0050170361-05002-045 CCCC

COND COND

161501158578806H12


A274-0048370361-06002-047 CCCC

2520 7153

414101329342806H23

34144633FAN AXIAL C5120033270361-03005-107 02

COND COND

432001207722807A01

25895780PUMP MODULE ASSY,HYDRAUL

4008236ABR53023-06 CCCC

COND COND

432001207722807A01


K5494ABR53023-06 CCCC

COND COND

432001207722807A01


272849ABR70652-02300-050 CCCC

13000 15956

156001129125607A24

26545610SAS ACTUATOR B112-0365070410-02500-049 00

13000 17029

156001129125607A24

13305359SAS ACTUATOR C1120375670410-02500-049 RCRC

13000 17075

1560011291256 ROLL07A24


COND COND

481001102247307B05A

16954633VALVE, SOLENIOD 150653213850-3-1 CCCC

COND COND

481001102247307B05A

29495428VALVE, SOLENIOD B1290-1685370306-02107-104 CCCC

COND COND

165001250376707B11

32374460ACCUMULATOR C401-010070204-0004 CCCC

COND COND

168001342049608B20

05428PANEL INDICATOR (PDU) 5509100-601561-000 CCCC

COND COND

168001342049608B20


COND COND

168001566036608F01

7664633IVHMU (CBM MONITORSYSTEM)

5130279-0302 CCCC

COND COND

611501114969609A01

19175780GENERATOR 106-A292128B302-8-DM CCCC

COND COND

611501114969609A01


COND COND

168001310225911C21

05350MIXER ASSEMBLY B9950165170400-02300-048 CCCC

2160 6398

1615011417532 n/a11C23

33215780TAIL ROTOR PITCHCHANGE SHAFT

B233-0212370400-06100-042 15421

11000 15516165001305695411C25

9125428TAIL ROTOR SERVOASSY

C300045742227000-17 RCRC

24400 29104165001143122611D01

7245428MAIN ROTOR PRIMARYSERVO

B30301503B274000-1031 RCRC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 10 of 11

23-Feb-2017

24400 29527165001143122611D01


B30316234274000-1031 RCRC

24400 24977165001143122611D01


B30304179B70410-02820-054 RCRC

13000 15999156001158968511D04

27815780AFT BELLCRANK C343-0231870400-08102-045 RCRC

17000 20752156001164416111D05

03752AFT TIE ROD SUPTFITTING

A3910185070400-08112-045 RCRC

2200 6220168001164416011D06

17605780AFT TIE ROD ASSY MM0025570400-08111-042 RCRC

4400 7399156001286887011D07

27815780AFT BELLCRANK SPTASSY

390-0193070400-08117-049 RCRC

11000 15622304001287243811D08

11585780LATERAL SWASHPLATELINK

151520283470400-08151-061 RCRC

5500 6657161501158965811D09

46235780LATERAL SERVOBELLCRANK

E289-0002970400-08150-045 RCRC

11000 13999168001158965311D11

27815780AFT WALKING BEAM E346-0000870400-08104-048 RCRC

4600 7599156001289269711D13

27815780LEFT TIE ROD ASSY 344-0198570400-08115-046 RCRC

3500 7870156001296948611D14

14105780RIGHT TIE ROD ASSY 2880041070400-08114-051 RCRC

15000 17999168001158965211D15

27815780FORWARD BELLCRANK 64670400-08101-046 RCRC

5600 8599156001221261911D16

27815780FWD BELLCRANK SPTASSY

B367-0393870400-08162-042 RCRC

COND COND

1680012612044 LOWER11D25

17734409STABILATOR ACTUATOR B2920045470400-06641-117 CCCC

COND COND

1680012612044 UPPER11D25

17994409STABILATOR ACTUATOR 2697DL2155M20 CCCC

COND COND

599601547345211D26

05220STABILATOR AMPLIFIER(DUAL)

52391011445-1-002 CCCC

COND COND

299501496368615A04


29484504587 CCCC

COND COND

599601188333219D01F

04633AMPLIFIER, RADIOFREQUENC

986BB622-6545-003 CCCC

COND COND

5841014214162 CO PILOT19E05A

05350RECEIVER-TRANSMITTER, RADAR

0998AAHG7209AD01 CCCC

COND COND

584101245909319E05C

05428INDICATOR HEIGHT 29BBA3060591 CCCC

COND COND

660501503528419E06A

05344ATTITUDE HEADINGREFERENCE UNIT

1736765100-20 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 11 of 11

23-Feb-2017

COND COND

661001490516852A

17835527AUTOMAT FLT CONTCOMPUTER

2521202825050-1-001 CCCC

7. SIGNIFICANT HISTORICAL DATA




HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM2860 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

22-Feb-2017

9000 13990

165001125090703A01A

00PISTON, MAIN L/GEARSTR

BEM286070250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM2860 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

22-Feb-2017





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 IA01285 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

22-Feb-2017

9000 12130

165001125090703A01A

12791279PISTON, MAIN L/GEARSTR

IA0748170250-12067-102 RCRC


