uh-60a helicopter, utility 8423935 - gsa auctions€¦ · uh-60a helicopter, utility 8423935 1. ......

NUMBERLOCATIONPIDENTRYORGANIZATION

8.7.DATE

6.REMARKS

4. 5.

UH-60A 8423935HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL

Report Date: of 9901-Dec-2015

F CO 1/160TH SOAR(ABN)

PMS-2 INSP COMPLETED AT 1984.0 ACFT HRSUH-60-94-SOF-05, UH-60-ASAM-95-03COMPLETED(SH1310)

25-Jan-1995 1

FT CAMPBELL, KY

QC000000

For use of this form, see DA PAM 738-751; the proponent agency is DCSLOGEDITION OF JAN 64 IS OBSOLETE

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


8.7.DATE

6.REMARKS

4. 5.



1106TH TASMGR/H AND L/H FS 34.5 BEAMS RECIEVED 50-7MODS BY 1106TH TASMG IAW MEC #F181652,@ 5332.2 ACFT HRS.

08-May-2014 2

MARANA, AZ 85653

SD718109

1106TH TASMGR/H FS 308 BEAM INBOARD AND OUTBOARDTABS REPAIRED BY 1106TH TASMG IAW MEC#F181652, @ 5332.2 ACFT HRS.

08-May-2014 1

MARANA, AZ 85653

SD718109




8.7.DATE

6.REMARKS

4. 5.



1108TH AVCRADACFT PLASTIC MEDIA DEAD BLASTED ANDPAINTED IAW TM 55-1500-23 BY UNCCONTRACTOR ON SITE. 2065.9 HRS(HS0516)

21-Sep-1995 2

GULFPORT MS

QC000000

1108TH AVCRADUH-60-95-ASAM-08 AVIATION SAFETY ACTIONMESSAGE ONE-TIME INSP TO IDENTIFYSUSPECT ENGINES WITH GG TURBINE ROTORBLADES THAT ARE UNDAMPNED.(HS0516)

21-Sep-1995 1

GULFPORT MS

QC000000

1108TH AVCRADUH-60-04-SOF-04 H-60 MAIN ROTOR HUBSUBASSEMBLY REWORK. C/W 3433.2 ACFTHRS(KS2668)

12-Aug-2004 2

GULFPORT, MS. 39505

QC000000

1108TH AVCRADUH-60-04-ASAM-04 REVISION TO UH-60-04-ASAM-03 FUEL SYSTEM INTEGRITY CHECKS.C/W 3433.2 ACFT. HRS.(KS2668)

12-Aug-2004 1

GULFPORT, MS. 39505

QC000000

1108TH AVCRADUH-60-04-ASAM-05 RESTRAINT SYSTEMINSPECTION. C/W 3433.2 ACFT. HRS.(KS2668)

22-Sep-2004 1

GULFPORT, MS. 39505

QC000000

1108TH AVCRADUH-60-05-ASAM-01 ALL H-60 SERIESAIRCRAFT, REVISION OF FUEL SYSTEMINTEGRITY CHECKS. C/W 3433.2 ACFT.HRS.(KS2668)

04-Jan-2005 1

GULFPORT, MS. 39505

QC000000

1108TH AVCRADPMS-2 #7 COMPLETED AT 3433.2 ACFT. HRS.NEXT PMS-2 IS #8 DUE AT 3933.2 ACFT.HRS.(KS2668)

25-Jan-2005 1

GULFPORT, MS. 39505

QC000000




8.7.DATE

6.REMARKS

4. 5.



1108TH AVCRAD (LSI)PAINT REMOVED BY PMB & PAINTED I/A/W TM55-1500-345-23 CONTRACT #F34601-97-D-0423.3433.2 ACFT. HRS.(KS2668)

20-Jan-2005 1

GULFPORT, MS.

QC000000




8.7.DATE

6.REMARKS

4. 5.



1109TH AVCRADCOMPLIED WITH H-60-10-ASAM-12 T700 ENGCOMP RC TIME

03-Aug-2010 1

GROTON,CT

1109TH AVCRADCOMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-15 (ESSS VENT TUBE REQUIRESREPLACEMENT)

11-Aug-2010 1

GROTON,CT

1109TH AVCRADCOMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-16 (RESCUE HOIST CABLE CUT CONN)

08-Sep-2010 1

GROTON,CT

1109TH AVCRADH-60-11-AMAM-03 COMPLETE(N/A THISAIRCRAFT)

26-Oct-2010 3

GROTON,CT

1109TH AVCRADH-60-10-ASAM-04 COMPLIED WITH @4498 A/CHOURS

26-Oct-2010 2

GROTON,CT

1109TH AVCRADH-60-10-ASAM-08 APU MOD COMPLETE 26-Oct-2010 1

GROTON,CT

1109TH AVCRADUPON INSPECTION OF AREA AROUND MAINMOD AFTER REMOVAL FOR MAINTENENCE,FOUND SEVERAL DRILL STARTS IN THE R/HAND L/H CORNERS OF THE AFTTRANSMISSION BEAM, DAMAGE FOUND NOTTO BE NEGLEGABLE BY ADAN GARCIA,AMCOM LAR

23-Nov-2010 2

GROTON,CT

1109TH AVCRADUPON INSPECTION OF AREA AROUND MAINMOD AFTER REMOVAL FOR MAINTENENCE,FOUND SEVERAL DRILL STARTS IN THE R/HAND L/H CORNERS OF THE FWDTRANSMISSION BEAM, IAW MEC#F118371 THETRANSMISSION BEAM CAN REMAIN INSERVICE AFTER ALODINE, PRIME AND PAINTON THE AFFECTED AREAS

23-Nov-2010 1

GROTON,CT


24-Nov-2010 1

GROTON,CT

1109TH AVCRADH-60-11-ASAM-04 COMPLIED WITH @4498 A/CHOURS, N/A THIS AIRCRAFT

02-Dec-2010 1

GROTON,CT

1109TH AVCRADT/R CABLE TENSION CHECK [email protected] A/C HOURS L/H 140 LBS; R/H 140LBS; TEMP 69 DEG F

09-Dec-2010 3

GROTON,CT

1109TH AVCRADT/R RIG COMPLETE @ 4498.2 A/C HOURS, T/RBIAS SETTINGS: RED 4.940/5.271 DIF. .331,BLUE 4.211/4.534 DIF. .323, BLACK 4.192/4.530DIF. .332, YELLOW 4.875/5.207 DIF. .332.

09-Dec-2010 2

GROTON,CT

1109TH AVCRADM/R RIG COMPLETED @ 4498.2 A/C HOURS 09-Dec-2010 1

GROTON,CT

1109TH AVCRADR/H PYLON STABILATOR ATTACH FITTINGREPLACED IAW MEC#116576

20-Dec-2010 2

GROTON,CT

1109TH AVCRADMULTIPLE IMPROPER REPAIRS ON TAILPYLON REPAIRED ON MEC 114934

20-Dec-2010 1

GROTON,CT


22-Dec-2010 1

GROTON,CT




8.7.DATE

6.REMARKS

4. 5.



AASFPMS 2 COMPLETED AT2445.3 ACFT HRS.NEXT DUE AT 2945.3 G. GRAY TI(GG6692)

09-Oct-1998 1

JACKSON MS

QC000000

AASFSOF UH-60-01-01 TB 1-1520-237-20-225 INITIALAND RECURRING INSP. OF MAIN LANDINGGEAR DRAG BEAM WAVER C/W(JL8322)

04-Dec-2000 1

JACKSON MS

QC000000

AASFSOF UH-60-01-05 TB 1-1520-237-20-230 INSPM/R SPINDLE ASSY.IAW UH-60-01-05C/W(JL8322)

06-Mar-2001 1

JACKSON MS

QC000000

AASFSOF UH60-01-07 TB 1-1520-237-20-232INSPECT FLIGHT CONTROL SELF LOCKINGBOLTS C/W(JL8322)

29-May-2001 1

JACKSON MS

QC000000

AASFSOF UH-60-01-08 TB 1-1520-237-20-232 INSP.M/R FLIGHT CONTROL SELF LOCKING BOLTS,REVISION TO UH-60-01-07 C/W(JL8322)

02-Jul-2001 1

JACKSON MS

QC000000

AASFAWR FOR ELT INSTALLATION ALL ARMYAIRCRAFT ISSUED 17 DEC 99(SS6692)

13-Sep-2001 1

JACKSON MS

QC000000

AASFUH60-02-ASAM-01 TB 1-1520-237-20-239 INSP.OF T/R BLADE FATING ASSY'S C/W AT 2923ACFT HRS(JL8322)

16-Nov-2001 1

JACKSON MS

QC000000

AASFSOF UH-60-02-01 INSP OF PROPER HDW ONFAN SHAFT MOUNT FLANGE(GS6692)

17-Nov-2001 1

JACKSON MS

QC000000

AASFSOF UH-60-02-03 ONE TIME INSP OF FLIGHTCONTROL SYSTEM PITCH TRIMASSY.(HK6028)

12-Dec-2001 1

JACKSON MS

QC000000

AASFSOF UH-60-02-04 APU FUEL LINES FORPROPER GROMMET AT APU SHROUD ASSY.C/W AT 2936.9 ACFT HRS(JL8322)

29-Jan-2002 1

JACKSON MS

QC000000

AASFUH-60-02-ASAM-02 INSPECT CONTROL RODJAMNUTS C/W. (JL8322)

12-Feb-2002 1

JACKSON,MS. 39209

QC000000

AASFUH-60-02-ASAM-04 (TB 1-1520-237-20-244)INSP. OF ALL UH-660 RESTRAINT SYSTEM'SC/W.(JL8322)

20-Mar-2002 1

JACKSON,MS 39209

QC000000

AASFINSPECT SWAGE PIN/COLLARS ON BOOSTSERVO ASSEMBLIES IAW UH-60-02-ASAM-06(TB 1-1520-237-20-252) WITHIN THE NEXT 10FLIGHT HOURS, BUT NLT 2 MAY 2002(BS9249)

18-Apr-2002 1

JACKSON MS. 39209

QC000000

AASFSOF UH-60-02-08 TB 1-1520-237-02-08 INSP. OFMAIN MODULE CARRIER ASSY. C/W(SH2609)

07-May-2002 1

JACKSON MS

QC000000

AASFUH-60-02-ASAM-09 TB 1-1520-237-20-257 INSPT/R QUADRANT INSTALLATION HARDWARE.C/W(SH2609)

13-Jun-2002 2

JACKSON MS

QC000000

AASFUH-60-02-ASAM-08 TB 1-1520-237-20-256 INSP.ARC-220 WIRING FOR CHAFING. C/W(SH2609)

13-Jun-2002 1

JACKSON MS

QC000000

AASFPMS2 COMPLETED AT 2936.9 ACFT HRS NEXTDUE 3436.9 JAMES LUNDSTROM TI(JL8322)

17-Jun-2002 1

JACKSON MS

QC000000

AASFUH-60-02-ASAM-11 (TB 1-1520-237-20-261)INSP AR/ARC-220 WIRING C/W(SH2609)

03-Oct-2002 1

JACKSON,MS

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASFUH-60-03-ASAM-02 RETIREMENT CHANGELIFE LIMITS FOR ALL TAIL ROTOR SERVOSC/W (SH2609)

13-Dec-2002 2

JACKSON, MS.

QC000000

AASFUH-06-03-ASAM-01 BELLCRANK SUPPORTASSY. RETIREMENT LIFE. C/W(SH2609)

13-Dec-2002 1

JACKSON, MS.

QC000000

AASFGEN-03-ASAM-01 SINGARS ARC 201.1 HRS 220BATTERY BOX C/W (PS9249)

20-Dec-2002 1

JACKSON MS

QC000000

AASFSOF UH-60-04-01 FWD. BELLCRANK SUPPORTINSTALLATION HARDWARE C/W(JL8322)

03-Oct-2003 1

JACKSON MS

QC000000

AASFSOF UH-60-04-02 UH-60A/L AND OH-58DSERIES HELICOPTERS, DISABLING COCKPITAIRBAG SYSTEM C/W.(JL8322)

14-Jun-2004 1

JACKSON, MS.

QC000000

AASFAWR 1189 ELT FOR ALL UH-60A/L/Q AND HH-60L AIRCRAFT INSTALLATION AND TESTINGPROCEDURES ISSUED 14JUN04/R1.

16-Jun-2004 1

JACKSON,MS.

AASFUH-60-06-ASAM-04 (CABS) (ECSU) DRAINPLUG INSPECTION COMPLIED WITH(SH192609)

23-Jun-2006 1

JACKSON, MS

AASFAWR 1374 UH-60A/L HELICOPTERS WITH FASTROPE INSERTION/EXTRACTION (FRIES)EQUIPMENT INSTALLED. DATED 28SEP06.

02-Oct-2006 1

JACKSON,MS.

AASFAWR 1189 ELT FOR ALL UH-60 A/L/Q AND HH-60L AIRCRAFT INSTALLED AND TESTINGPROCEDURES ISSUED 26MAR07/R3.

30-Apr-2007 1

JACKSON,MS.

AASFUH-60-07-ASAM-07 INSTALLATION OF STATICBONDING JUMPERS FOR CEFS C/W.

09-May-2007 1

JACKSON,MS

AASFAWR 1054R6, BAMBI WATER BUCKET ISSUED01JUN 07.

10-Jun-2007 1

JACKSON,MS.

AASFAWR 1054R7, BAMBI WATER BUCKET ISSUED08JUN07.

11-Jun-2007 1

JACKSON,MS.

AASFH-60-09-SOF-01 C/W. (HMU) 21-Oct-2008 1

JACKSON, MS 39209-3436

AASFMEC F101907 ON TAILCONE ACCESS PANELCOMPLIED WITH ON 9 DEC 2009. AIRCRAFTHOURS: 4359.4. AASF JACKSON,MS. 39209

10-Dec-2009 1





8.7.DATE

6.REMARKS

4. 5.



AASFUH-60-06-ASAM-01 TAIL LANDING SHOCKSTRUT C/W. (JL8322)

14-Dec-2005 1

JACKSON,MS.

QC000000

AASFH-60-09-SOF-02 C/W ( ALQ-144) 07-Nov-2008 1





8.7.DATE

6.REMARKS

4. 5.



AASF # 1 FTIGCOMPLIED W/ REQUIREMENTS OF H-60-11-ASAM-08 @ 4519.8 ACFT HRS (LOS/IFFANTENNA & IVHMS ACCELEROMETERCONNECTORS SAFETY WIRE)

10-Feb-2011 1

BLDG 19-101ANNVILLE,PA 17003

DK708878




8.7.DATE

6.REMARKS

4. 5.



AASF #1SOF MSG UH-60-01-01 INSPECTION OF MAINLANDING GEAR DRAG BEAM AND DECREASETORQUE DN NUT (TB 1-1520-237-20-225)(HC5747)

06-Nov-2000 1

JACKSON MS

QC000000

AASF #1CORRECTED COPY, SOF MSG UH-60-01-01MAIN LANDING GEAR DRAG BEAMINSPECTION (TB 1-1520-237-20-225)(HC5747)

07-Nov-2000 1

JACKSON MS

QC000000

AASF #1SOF MSG UH-60-01-02REVISION TO UH-60-01-01, MAIN LANDING GEAR DRAG BEAMINSPECTION (TB 1-1520-237-20-225)(HC5747)

28-Dec-2000 1

JACKSON MS

QC000000

AASF #1SOF MSG UH-60-01-04 REVISION TO UH-60-98-01,RISK MANAGEMENT OF 230 GALLONEXTERNAL TANK OPERATIONS (TB 1-1520-237-20-220)(HC5747)

05-Jan-2001 2

JACKOSN MS

QC000000

AASF #1SOF MSG UH-60-01-03, INSP. AND RMVL OFLATERAL SERVO BELLCRANKASSY, (KFG.PURDY MACHINE CO.), CAGE CODE 15152, (TB1-1520-237-20-229)(HC5747)

05-Jan-2001 1

JACKSON MS

QC000000

AASF #1SOF MSG UH-60-01-03 TB 1-1520-237-20-229INSPECTION AND REMOVAL OF LATERALSERVO BELLCRANK MANUFACTURED BY THEPURDY MACH. CO. C/W 09JAN01(CL8322)

09-Jan-2001 1

JACKSON MS

QC000000

AASF #1SOF MSG UH-60-01-02 TB 1-1520-237-20-225REVISION TO UH-60A-01-01 MAIN LANDINGGEAR DRAG BEAM C/W (JL8322)

10-May-2001 1

JACKSON MS

QC000000

AASF #1UH-60-04-ASAM-02 INSP. OF T/R DRIVE SHAFTFLANGE NUTS C/W(BS9249)

01-Apr-2004 1

JACKSON MS

QC000000

AASF #1UH-60-05-ASAM-04 CORRECTED COPYC/W(SH2609)

08-Apr-2005 4

JACKSON, MS.

QC000000

AASF #1UH-60-05-ASAM-04 TAIL LANDING GEARYOKE ASSY. C/W(SH2609)

08-Apr-2005 3

JACKSON, MS.

QC000000

AASF #1UH-60-05-ASAM-03 AIRCREW RESTRAINTSYWTEM C/W(SH2609)

08-Apr-2005 2

JACKSON, MS.

QC000000

AASF #1UH-60-05-ASAM-06 TROOP SEAT RESTRAINTBUCKLE C/W.(JL8322)

01-May-2005 1

JACKSON MS.

QC000000

AASF #1UH-60-05-ASAM-07 AIR INTRUSION OFHYDRAULIC SYSTEM C/W(BS9249)

19-May-2005 1

JACKSON MS

QC000000

AASF #1AIRCRAFT PLACED ON ESM JUN 29, 2005ACFT HRS 3604.3 PMI 2 DUE 3738.2(GG6692)

29-Jun-2005 1

JACKSON MS

QC000000

AASF #1UH-60-05-ASAM-09 (CEFS) BOLTSC/W(BS9249)

02-Aug-2005 1

JACKSON MS

QC000000

AASF #1UH-60-05-ASAM-10 ENG OUTPUT SHAFTC/W(SH2609)

08-Aug-2005 1

JACKSON, MS.

QC000000

AASF #1AWR 1054 FOR UH-60A/L/Q AND HH-60LHELICOPTERS EQUIPPED WITH SEIINDUSTRIES WATER BUCKETS AWR1054R3(SH2609)

08-Sep-2005 1

JACKSON, MS

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF #1COMPLY WITH REQUIREMENTS OF AWRDATED 08 MAR 06(SH2609)

08-Mar-2006 1

JACKSON, MS

QC000000

AASF #1PMI-2 COMPLETED AT 3778.2 ACFT HOURS 16-May-2006 1

JACKSON MS

AASF #1COMPLY WITH REQUIREMENTS OF AWRDATED 28 SEP 06(SH2609)

28-Sep-2006 1

JACKSON, MS

QC000000

AASF #1"TEXAS PATCH" APPLIED TO LEFT HANDBELLY STRAP BY 1108TH AVCRAD. 25 OCT 063888.5 ACFT. HRS

02-Nov-2006 1

JACKSON, MS.

AASF #1UH-60-07-ASAM-04 AUTOROTATIONAL RPMCHARTS. C/W (SH192609.

25-Jan-2007 1

JACKSON, MS

AASF #1UH-60-07-ASAM-05 (ARC-220/KY-100 START-UPPROCEDURES). C/W. (SH192609)

30-Jan-2007 2

JACKSON, MS.

AASF #1UH-60-07-ASAM-05 (ARC-220/KY-100 START-UPPROCEDURES).C/W

30-Jan-2007 1

JACKSON, MS.

AASF #1UH-60-07-ASAM-06 INTERNAL RESCUE HOISTCABLE (GUARD) DEFLECTOR C/W (SH192609).

09-Feb-2007 1

JACKSON, MS

AASF #1H60-08-ASAM-14, SUSPECT ENGINE HARNESS. 22-Sep-2008 1

JACKSON, MS

AASF #1MEC # F85845 LEFT HAND MAIN LANDINGGEAR BRAKE FLANGE SPACERS DISBONDED.ONE TIME AUTHORIZATION FOR DEVIATIONFROM THE TECH MANUAL TO USE LORD 506ADHESIVE, NSN 01-170-3599 INSTEAD OFVERSALOK 204 ADHESIVE NSN 01-160-9551.PERMISSION GRANTED BY DALE A. MILLERAEROSPACE LIASON ENGINEER, RDECOM,MAINTENANCE ENGINEERING DIVISION,1108TH AVCRAD GULFPORT MS 228.214.1375DSN 293.

17-Dec-2008 1


AASF #1H60-09-ASAM-01, T701C GAS GENERATOR (GGROTOR) ASSEMBLIES.

12-Jan-2009 1

JACKSON, MS

AASF #1H60-09-ASAM-11, CARGO DOOR WINDOWEMERGENCY JETTISON HANDLE ASSY. C/W

25-Jun-2009 1

JACKSON, MS

AASF #1AWR 1428 R2 MULTI-BAND AIRBORNEFRREQUENCY MODULATED TRANSCEIVERRADIOS TDFM-6148 DTD 14 JUL 09 APPLIED

14-Jul-2009 1


MD663566

AASF #1H60-10-ASAM-01, HAMILTON SUNDSTRANDHYDROMECHANICAL UNITS. COMPLIED WITH.

01-Oct-2009 1

JACKSON , MS

AASF #1H60-10-AMAM-02, REDESIGNED PLANETARYGEAR CARRIER. COMPLIED WITH.

09-Oct-2009 1

JACKSON, MS

AASF #1AWR 1479 R1 IMPROVED PLANETARYCARRIER ASSEMBLY MAIN MODULE DTD 4JAN 10 APPLIED

04-Jan-2010 1


MD663566




8.7.DATE

6.REMARKS

4. 5.



AASF #1AWR 1661 OPERATION OF MH-60AHELICOPTERS MODIFIED TO UH-60ACONFIGURATION DTD 10 FEB 10 APPLIED

10-Feb-2010 1


MD663566

AASF #1H-60-10-AMAM-12 (IMPROVED DRAG BEAM)C/W

29-Apr-2010 1


RH542424

AASF #1AWR 1279 R3 OPERATIONS WITH COCKPITDOORS/WINDOWS AND/OR CABINDOORS/WINDOWS REMOVED DTD 11 JUN 10APPLIED

11-Jun-2010 1


MD663566

AASF #1H-60-10-ASAM-12 ENGINE COMMONCOMPONENT RETIREMENT CHANGE TIMESCOMPLIED WITH

05-Aug-2010 1


MD663566

AASF #1AWR 1539 R1 AFS APU INLET BARRIERFILTERS DTD 30 AUG 10 APPLIED

30-Aug-2010 1


MD663566

AASF #1AWR 1516 R6 ELT DTD 29 OCT 11 APPLIED 29-Oct-2010 1


MD663566

AASF #1AWR 1738 AN/APX-118 CXP DTD 1 FEB 11APPLIED

01-Feb-2011 1


MD663566

AASF #1AWR 1054 R10 BAMBI WATER BUCKETS DTD 9MAR 11 APPLIED

09-Mar-2011 1


MD663566

AASF #1AWR 1750 AN/AVS-6 SERIES NVG DTD 25 MAR11 APPLIED

25-Mar-2011 1


MD663566

AASF #1AWR 1347 R15 EDM AND BFT DTD 28 JUL 11APPLIED

28-Jul-2011 1


MD663566

AASF #1AWR 980 R7 FOREST PENETRATOR DTD 5AUG 11 APPLIED

05-Aug-2011 1


MD663566

AASF #1AWR 1753 R1 (DGNS) DTD 31 AUG 11 APPLIED 31-Aug-2011 1


MD663566

AASF #1H-60-11-AMAM-19, ULLSA(E) LCF CHANGE 62REQUIREMENTS, COMPLIED WITH

21-Oct-2011 1


RH542424

AASF #1AWR 1800 EDM AND/OR BFT DTD 30 NOV 11APPLIED

30-Nov-2011 1


MD663566

AASF #1AWR 1308 R9 GOODRICH INTERNAL RESCUEHOIST DTD 23 DEC 11 APPLIED

23-Dec-2011 1


MD663566




8.7.DATE

6.REMARKS

4. 5.



AASF #1AWR 1452 R2 LC-6 DIGITAL CHRONOMETERDTD 20 JAN 12 APPLIED

20-Jan-2012 1


MD663566

AASF #1AWR 1750 R1 DTD 27 MAR 12, AN/AVS-6 NIGHTVISION GOGGLES, APPLIED

30-Mar-2012 1


RH542424




8.7.DATE

6.REMARKS

4. 5.



AASF #1SOF MSG UH-6-01-03 REVISION TO UH-60-01-03,RMVL OF LATERAL SERVO BELLCRANKASSY, (MFG. PURDY MACHINE CO.), CAGECODE 151512, (TB 1-1520-237-20-229)(HC5747)

08-Jan-2001 1

JACKSON MS

QC000000

AASF #1AWR 1054 FOR UH-60A/L/Q AND HH60LHELICOPTERS EQUIPPED WITH SEIINDUSTRIES BAMBI WATER BUCKETS AWR1054 R4(SH2609)

22-Sep-2005 1

JACKSON, MS

QC000000

AASF #1UH-60-07-AMAM-01 COMMON MISSILEWARNING SYSTEM (CMWS). C/W (SH192609)

03-Apr-2007 1

JACKSON, MS.

AASF #1H-60-10-AMAM-03 COMPLIED WITH, CABSSYSTEM NOT INSTALLED

12-Nov-2009 1


AASF #1H-60-10-SOF-02, SPINDLE LUG NDI ANDRETIREMENT LIFE CHANGES, COMPLIEDWITH

22-Jun-2010 1


RH542424

AASF #1AWR 1566 R2 RESCUE HOIST CABLE GUARDDTD 18 MAR 11 APPLIED

18-Mar-2011 1


MD663566

AASF #1AWR 1787 FM IMMUNE AN/ARN-123 VOR/ILSRECEIVER DTD 26AUG11 APPLIED

26-Aug-2011 1


MD663566




8.7.DATE

6.REMARKS

4. 5.



AASF #1 FTIG, PAH-60-11-AMAM-13, EXTERNAL RESCUE HOISTMOUNT FITTING COMPLIED WITH. NOTINSTALLED ON ACFT

15-Jun-2011 1


MD663566

AASF #1 FTIG, PALATE ENTRY: PMI 2 COMPLETED @ 4498.2ACFT HRS. PMI 2 WAS COMPLETED ATGROTON, CT

08-Jul-2011 1


MD663566

AASF #1 FTIG, PAXMSN MAIN MOD FILTER BUTTON POPPED @4682.7 ACFT HRS. 1 AUG. 2011. FILTERSREPLACED AND OIL RECIRCULATEDTHROUGH TSU @ 3 MICRONS.

02-Aug-2011 1


MD663566




8.7.DATE

6.REMARKS

4. 5.



AASF #1 FTIGH-60-10-ASAM-16 RESCUE HOIST SAFETYINSP C/W

09-Sep-2010 1


RH542424

AASF #1 FTIGH-60-11-AMAM-06, MEDEVAC CAROUSELREFURBISHMENT, COMPLIED WITH

08-Feb-2011 1


RH542424

AASF #1 FTIGH-60-11-AMAM-09, HISTORY RECORDERREADINGS, COMPLIED WITH

18-Apr-2011 1


RH542424

AASF #1 FTIGH-60-11-AMAM-11, AWR STATUS UPDATES,COMPLIED WITH

19-Apr-2011 1


RH542424

AASF #1 FTIGH-60-11-ASAM-11, ANTI ICE START BLEEDVALVE SHAFT INSPECTION, COMPLIED WITH.

23-Jun-2011 1


RH542424

AASF #1 FTIGH-60-11-ASAM-13, INLET ANTI ICE VALVE, C/W 20-Jul-2011 1


RH542424

AASF #1 FTIGH-60-11-SOF-01, HEXAGON NUTS, C/W 21-Jul-2011 1


RH542424

AASF #1 FTIGH-60-11-ASAM-14, ENGINE COWLING DOORS,COMPLIED WITH

11-Oct-2011 3


RH542424

AASF #1 FTIGH-60-12-SOF-02, TAIL ROTOR INTERMEDIATEGEARBOX, COMPLIED WITH

11-Oct-2011 2


RH542424


11-Oct-2011 1


RH542424


18-Oct-2011 1


RH542424

AASF #1 FTIGH-60-12-AMAM-03. TRANSPONDER ANDCOMMON MISSILE WARNING SYSTEMINSTALLATION, COMPLIED WITH

08-Nov-2011 1


RH542424

AASF #1 FTIGH-60-12-ASAM-02, MLG DRAG BEAMASSEMBLIES, COMPLIED WITH

06-Dec-2011 1


RH542424

AASF #1 FTIGH-60-12-SOF-04, BREEZE EASTERN HOISTOPS, COMPLIED WITH

17-Feb-2012 1


RH542424

AASF #1 FTIGAWR 1346 R20 DTD 31 JAN 12, IVHUMSSYSTEM, APPLIED

07-Mar-2012 1


RH542424




8.7.DATE

6.REMARKS

4. 5.



AASF #1 FTIGCOMPLY WITH REQUIREMENTS OF H-60-12-SOF-05 NLT 23 APR 12

10-Apr-2012 1


RH542424

AASF #1 FTIGH-60-12-ASAM-02, R/H AND L/H DRAG BEAMINSPECTION, COMPLIED WITH AND DRAGBEAMS REPLACED

13-Apr-2012 3


RH542424

AASF #1 FTIGH-60-12-ASAM-01, T/ OUTPUT BEVEL GEARNDI INSPECTION, COMPLIED WITH ANDCOMPLETED

13-Apr-2012 2


RH542424

AASF #1 FTIGH-60-11-AMAM-17, T/R PADDLE LABELS,COMPLIED WITH

13-Apr-2012 1


RH542424

AASF #1 FTIGTAIL ROTOR RIG CHECK AS FOLLOWS:REDBLADE INIT: 4.609 BIAS: 4.946 DIFF:.337BLACK BLADE INIT: 4.157 BIAS: 4.496DIFF: .312YELLOW BLADE INIT: 4.526 BIAS:4.855 DIFF: .329BLUE BLADE INIT: 4.196 BIAS:4.509 DIFF: .313T/R SERVO PISTONTRAVEL:EXTENDED WITH HIGH COLL FULLLEFT YAW: 3.50RETRACTED WITH LOW COLLFULL RIGHT YAW: .016

08-May-2012 1


RH542424

AASF #1 FTIGPMI-1 COMPLETED AT 4858.3 AIRCRAFTHOURS. NEXT PMI-2 DUE AT 5218.3 AIRCRAFTHOURS

19-May-2012 1


RH542424

AASF #1 FTIGH-60-12-AMAM-12, COMMON COMPONENTRETIREMENT, COMPLIED WITH

12-Jul-2012 1


RH542424

AASF #1 FTIGH-60-12-AMAM-15, TRIM ACTUATOR,COMPLIED WITH

06-Sep-2012 1


RH542424

AASF #1 FTIGH-60-12-ASAM-11, HMU TBO TIMES, COMPLIEDWITH

07-Sep-2012 1


RH542424




8.7.DATE

6.REMARKS

4. 5.



AASF #1 FTIG PAH-60-12-ASAM-10, ENGINE ANTI-ICE/STARTBLEED VALVE, COMPLIED WITH

10-Sep-2012 1





8.7.DATE

6.REMARKS

4. 5.



AASF #1 FTIG, PAH-60-10-ASAM-07 STABILATOR HINGEFITTINGS COMPLIED WITH

23-Apr-2010 1


MD663566




8.7.DATE

6.REMARKS

4. 5.



AASF #1 MSARNGJACE/CPC PERFORMED AT 2445 ACFT HRS BYTEAM MEMBER "N" AMCOM OLR/MWOBRANCH HUNTSVILLE, AL DON ESCHROEDER(DS5651)

28-May-1998 1

JACKSON, MS

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF #1 PAACFT TRANSFERED TO THE EAATS (W7QNAA)FORT INDIANTOWN GAP, ANNVILLE PA 17003-5005. AT 4369.4 ACFT HRS.

06-Jan-2010 1


RB509919




8.7.DATE

6.REMARKS

4. 5.



AASF #1,H60-09-ASAM-04, RESCUE HOIST CARTRIDGEACTIVATION DEVICE (CAD). C/W

26-Feb-2009 1

JACKSON, MS




8.7.DATE

6.REMARKS

4. 5.



AASF 1ACE/CPCE PERFORMED AT 2885 ACFT HRSBY TEAM MEMBERS K&W AMCOM OLR/MWOBRANCH KILLEEN TEXAS(JP2527)

12-Dec-2000 1

JACKSON MS

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF 1 FTIGH-60-12-ASAM-09 BREEZE EASTERNEXTERNAL RESCUE HOIST CARTRIDGEACTUATED DEVICE (CAD) ELECTRICALCONNECTOR COMPLIED WITH

22-Aug-2012 1





8.7.DATE

6.REMARKS

4. 5.



AASF 1, MS ARNGUH-60-97-ASAM-05, ONE-TIME INSPECTIONFOR REMOVAL AND REWORK OF CERTAINVISCOUS DAMPER BEARING SUPPORTASSY.(HS0516)

15-Jan-1997 1

JACKSON, MS

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF FTIGM/R TRACK AND BALANCE ADJUSTMENTS:YELLOW TRIM +12; RED TRIM -2; BLACK TRIM-2; RED P/C -1; BLACK P/C -1; YELLOW P/C-5

08-Apr-2010 1


RH542424




8.7.DATE

6.REMARKS

4. 5.



AASF MS ARNGREMOVAL OF LOWER PITCH CHANGE RODEND BEARING MFR. BY ISLANDENGINEERING. CAGE4D137 UH-60-97-ASAM-15(HS0516)

12-Aug-1997 2

JACKSON MS

QC000000

AASF MS ARNGREMOVAL OF BELLCRANK SUPPORTS MFR.BY AMERICAN GENERAL. CAGE 2A622 UH-60-97-ASAM-14(HS0516)

12-Aug-1997 1

JACKSON MS

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF MSARNGUH-60-99-ASAM-05 TB 1-1520-237-20-209 ONETIME INSPECTION OF THE MAIN ROTORSPINDLE BEARING ASSY FOR THE EXISTENCEOF SLEEVE BEARING P/N SB5203-202COMPLETED 28DEC98 K LANCASTER ACFTTI(KL0973)

28-Dec-1998 1

JACKSON, MS

QC000000

AASF MSARNGUH-60-99-ASAM-06 TB 1-1520-237-20-210INSPECTION AND REVISED RETIREMENT LIFEOF MAIN ROTOR PITCH HORN P/N 70102-08111-047 COMPLETED K LANCASTER ACFTTI(KL0973)

05-Jan-1999 1

JACKSON, MS

QC000000

AASF MSARNGMIM UH-60-99-001 ESTABLISHMENT OF LIFELIMIT (RETIREMENT) OF 9000 HRS FOR MAINLANDING GEAR STRUT(KL0973)

13-May-1999 1

JACKSON, MS

QC000000

AASF MSARNGUH-60-99-ASAM-08 (TB 1-1520-237-20-211)REVISION OF RETIREMENT LIFE OFBELLCRANK SUPPORT ASSEMBLY P/N 70400-08162-042/043/045, MANUFACTURED BY AIRINDUSTRIES(KL0973)

28-Jun-1999 1

JACKSON, MS

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF#1AIRCRAFT, GLARE SHEILD, LIGHTING CIRCUITBREAKER REPLACEMENT, UH-60-04-ASAM-01COMPLIED WITH.(GG6692)

05-Apr-2004 1

JACKSON, MS.

QC000000

AASF#1UH-60-05-SOF-01 (CABS) C/W(SH2609) 15-Mar-2005 1

JACKSON, MS.

QC000000

AASF#1UH-60-05-SOF-02 ESM PROGRAMC/W(SH2609)

08-Apr-2005 1

JACKSON, MS.

QC000000

AASF#1ACE/CPCE PERFORMED AT 3888.5 ACFT HRSBY TEAM MEMBERS K&W AMCOM PROJECTOLR GG606692

03-Oct-2006 1

JACKSON, MS

AASF#1AED HAS ISSUED A MAINTENANCEENGINEERING CALL (MEC) FOR L MODEL AFTSUPPORT BRIDGE/STRUT/BASE TO BEOPERATED ON THIS ACFT UNTIL THE NEXTPMI. A SPECIAL 120 HR INSP WILL BEPERFORMED I/A/W TM 1-1520-237-PMI PARA6.14. AED POC IS DALE MILLER AED MECNUMBER F57811.

19-Jan-2007 1

JACKSON, MS.

AASF#1UH-60-07-ASAM-01 REVISED BY UH-60-07-ASAM-02 C/W ENGINE WHITE CABLES.

25-May-2007 1

JACKSON, MS

AASF#1COMPLY WITH REQUIREMENTS OF AWR1374R1 DATED 14 SEP 07 "FRIES BAR"

01-Oct-2007 1

JACKSON, MS

AASF#1H-60-08-AMAM-01 COMPLIED WITH. (MLGSHOCK STRUTS)

17-Oct-2007 1

JACKSON, MS

AASF#1H-60-08-ASAM-02 COMPLIED WITH. (PCLSPRING CLIP)

06-Nov-2007 1

JACKSON, MS

AASF#1H-60-08-ASAM-01 TROOP/GUNNERS UPPERENERGY ATTENUATING WIRES C/W

27-Nov-2007 1

JACKSON,MS

AASF#1H-60-08-ASAM-04 PILOTS LOWER SEAT RAILCHAFING ELECTRICAL HARNESS. C/W

04-Dec-2007 1

JACKSON, MS

AASF#1H-60-08-ASAM-05 T/R QUADRANT SPRINGCAPSULE. C/W

18-Dec-2007 1

JACKSON, MS

AASF#1H-60-08-ASAM-03 CHANGES TO CURRENTFUEL SYSTEM INTEGRITY CHECKS C/W.

09-Jan-2008 1

JACKSON, MS

AASF#1H-60-08-AMAM-02 TAIL ROTOR OUTBOARDRETENTION PLATE SHIMS C/W.

15-Jan-2008 1

JACKSON, MS

AASF#1H-60-08-SOF-01 ALL H-60 AIRCRAFT, MAINROTOR BLADE EXPANDABLE PIN INSPECTIONCHANGE C/W.

30-Jan-2008 1

JACKSON, MS

AASF#1H-60-08-AMAM-05 GOODRICH INTERNALRESCUE HOIST. C/W

04-Feb-2008 1

JACKSON, MS

AASF#1H-60-08-AMAM-06, COMMON MISSILEWARNING SYSTEM (CMWS) SEQUENCERSC/W

06-Feb-2008 1

JACKSON, MS

AASF#1H-60-08-ASAM-06 MAIN ROTOR PYLONSLIDING FORWARD FAIRING C/W.

31-Mar-2008 1

JACKSON, MS




8.7.DATE

6.REMARKS

4. 5.



AASF#1H-60-08-AMAM-07 C/W (DOPPLR/GPS) 20-May-2008 1

JACKSON, MS

AASF#1H-60-08-AMAM-08 FLIGHT CONTROL RIGGINGUPDATE C/W

19-Jun-2008 1

JACKSON, MS

AASF#1H-60-08-AMAM-04 C/W COCKPIT DOORJETTISONABLE WINDOW.

08-Jul-2008 1


AASF#1OPERATE IAW AWR 1522 DATED 27 AUG 08R1. (MH-60A TO UH-60A MOD)

27-Aug-2008 1


AASF#1H-60-08-ASAM-11 C/W (FLIGHT CONTROLS) 04-Sep-2008 1


AASF#1H-60-08-ASAM-12 C/W. (ENGINE STARTERS) 10-Oct-2008 1


AASF#1H-60-08-ASAM-13 C/W. (FIRE EXT TUBEUNION RING)

17-Oct-2008 1


AASF#1MEC # F5834 A TEMPORARY REPAIR OF TAILROTOR BLADE DE-ICE CABLE. CABLESHROUD BROKEN, WIRES IN TACT, MANUALREQUIRES REPLACEMENT OF OLD STYLE T/RDE-ICE SLIP-RING. MEC GRANTS ONE TIMEREPAIR OF TAIL ROTOR DE-ICE CABLE USINGPRO-SEAL UNTIL SLIP RING CAN BEREPLACED. PERMISSION GRANTED BY DALEA. MILLER AEROSPACE LIASON ENGINEER,RDECOM, MAINTENANCE ENGINEERINGDIVISION, 1108TH AVCRAD GULFPORT MS228.214.1375 DSN 293.

17-Dec-2008 2


AASF#1PMI-1 COMPLETED AT 4138.2 ACFT HRS 19-Dec-2008 1


AASF#1H-60-09-ASAM-05 (LIFE LIMIT ON T/RCAPSULES) C/W

04-Mar-2009 1


AASF#1M/R RIG COMPLETED FOR 48 MONTH FLIGHTCONTROL ROD INSPECTION: LOW COLLANGLE -0.625, HIGH COLL ANGLE 15.150, FWDCYCLIC ANGLE 34.1, AFT CYCLIC ANGLE 19.2,LEFT CYCLIC ANGLE 15.0, RIGHT CYCLICANGLE 14.1 PRIMARY SERVO ADJUSTMENTSFWD: SHORTENED 1 FLATAFT: LEGNTHENED 1 FLATLAT: SHORTENED 0.5 FLAT

17-Mar-2009 1


AASF#1H-60-09-ASAM-07 FIRE EXTINGUISHER WIRING(BREAKAWAY THREAD) C/W

16-Apr-2009 1





8.7.DATE

6.REMARKS

4. 5.



AASF#1H-60-09-ASAM-09 FIRE EXTINGUISHERSYSTEM WIRING LOOP C/W.

28-May-2009 1


AASF#1H-60-09-ASAM-08 ENGINE COWLING WEIGHTRESTRICTION C/W.

09-Jun-2009 1


AASF#1COMPLIED WITH REQUIREMENTS OF H-60-09-AMAM-06

25-Aug-2009 1


AASF#1COMPLIED WITH REQUIREMENTS OF H-60-09-AMAM-04 (A2C2S SYSTEM NOT INSTALLED)

26-Aug-2009 1


AASF#1T/R BIAS SET AS FOLLOWS: RED A. 4.73 - B.5.06 DIFF .330, BLACK A. 4.0 - B. 4.33 DIFF .330,YELLOW A 4.68 - B 5.01 DIFF .330, BLUE A. 4.03- B. 4.36 DIFF .330

16-Oct-2009 1


AASF#1H-60-09-AMAM-07 HALON HAND HELD FIREEXTINGUISHERS. C/W

20-Oct-2009 1


AASF#1T/R BIAS SETTINGS: RED 4.73/5.05 DIF. .320,BLUE 4.03/4.35 DIF. .320, BLACK 4.05/4.38 DIF..330, YELLOW 4.65/4.98 DIF. .330.

21-Oct-2009 1


AASF#1H-60-10-ASAM-03 (FIRE BOTTLE DISCHARGETUBES) COMPLIED WITH

12-Nov-2009 3


AASF#1H-60-10-AMAM-04 (ASN128B) COMPLIED WITH 12-Nov-2009 2


AASF#1COMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-04 (SAS LINKS NDI)

20-Nov-2009 1


AASF#1H-60-10-AMAM-16 CMWS GUARDED DISPENSESWITCH, COMPLIED WITH

25-Jun-2010 1


TW642993




8.7.DATE

6.REMARKS

4. 5.



AASF#1UH-60-06-SOF-02 DISABLING OF COCKPITAIRBAG SYSTEM (CABS) C/W. (JL178322)

23-Jun-2006 2

JACKSON,MS.

AASF#1H-60-09-SOF-03 (POSSIBLE RETIREMENT LIFEOVERFLIGHT) C/W

13-Nov-2008 1


AASF#1H-60-08-ASAM-10 ELECTRICAL WIRE CHAFEISSUES C/W.

09-Jan-2009 1





8.7.DATE

6.REMARKS

4. 5.



AASF#1 FTIGH-60-10-ASAM-11 COMMON COMPONENT TIMELIFE CHANGES COMPLIED WITH

16-Jul-2010 1


RH542424

AASF#1 FTIGH-60-12-ASAM-08, CARGO HOOK MANUALRELEASE SPRING ASSY, COMPLIED WITH

20-Jul-2012 1





8.7.DATE

6.REMARKS

4. 5.



AASF#1 FTIG,PAH-60-10-AMAM-05 LCF CHANGE 60BCOMPLIED WITH

18-Nov-2009 1


AASF#1 FTIG,PAH-60-11-AMAM-04 LCF CHANGE 61B-CORRECTED COPY COMPLIED WITH

25-Oct-2011 1





8.7.DATE

6.REMARKS

4. 5.



AASF#1 PATAIL ROTOR RIG CHECK AS FOLLOWS:REDBLADE INIT: 4.667 BIAS: 5.003 DIFF:.336BLACK BLADE INIT: 4.006 BIAS: 4.348DIFF: .342YELLOW BLADE INIT: 4.636 BIAS:4.980 DIFF: .344BLUE BLADE INIT: 4.021 BIAS:4.344 DIFF: .323

05-Jun-2012 1





8.7.DATE

6.REMARKS

4. 5.



AASF#1-FTIGH-60-11-AMAM-20, AN/ASN-128D DOPPLERAND AMPS SOFTWARE UPGRADE, COMPLIEDWITH

18-Jul-2012 1


HC523489

AASF#1-FTIGH-60-12-ASAM-07, ELECTRICAL WIRINGCHAFE, COMPLIED WITH

07-Sep-2012 2


HC523489




8.7.DATE

6.REMARKS

4. 5.



AASF, MS ARNGUH-60-96-ASAM-07 REPLACEMENT OFSPINDLE ASS'S WITH CERTAIN S/N RETAININGRODS INSTALLED.(HS0516)

20-Aug-1996 1

JACKSON, MS

QC000000

AASF, MS ARNGUH-60-96-ASAM-10, ALL H-60 SERIESAIRCRAFT, SPINDLE ASSY AND SPINDLEELASTROMERIC BEARINGS(HS0516)

16-Sep-1996 1

JACKSON, MS

QC000000

AASF, MS ARNGUH-60-96-ASAM-11, INCREASE IN FATIGUELIFE OF FENN MANUFACTURED MAIN ROTORBLADE CUFFS.(HS0516)

25-Sep-1996 1

JACKSON, MS

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF, MSARNGUH-60-9-ASAM-07, REPLACEMENT CRITERIAFOR TROOP GUNNER SEAT ATENUATORWIRES AND EXPLICIT SHIMMINGPROCEDURES FOR ATTENUATORROLLERS(HS0516)

27-Sep-1995 1

JACKSON MS

QC000000

AASF, MSARNGSOF UH-60-96-01, CHANGE IN RETIREMENT OFFWD BELLCRANK SUPPORT ASSY.(HS0516)

08-Nov-1995 1

JACKSON MS

QC000000

AASF, MSARNGSOF UH-60-96-02, TB 1-1520-237-20-173INSPECTION FOR SUSPECT TAIL ROTORINBOARD RETENTION PLATES.(HS0516)

28-Nov-1995 1

JACKSON, MS

QC000000

AASF, MSARNGSOF UH-60-95-03, CHANGE IN RETIREMENTLIFE OF MAIN ROTOR BLADE CUFF.(HS0516)

08-Dec-1995 1

JACKSON, MS

QC000000

AASF, MSARNGSOF UH-60-96-04, REMOVAL OF SPECIFIC S/NAFT BELLCRANK SUPPORT ASSY.(HS0516)

13-Dec-1995 1

JACKSON, MS

QC000000

AASF, MSARNGUH-60-96-ASAM-03, REVISION TO UH-60-96-ASAM-02(HS0516)

11-Jan-1996 1

JACKSON, MS

QC000000

AASF, MSARNGUH-60-96-ASAM-04, REVISION TO AWR FORFRIES BAR. LIMITED TO 1300 LBS PERSIDE(HS0516)

26-Jan-1996 1

JACKSON, MS

QC000000

AASF, MSARNGAIRWORTHINESS RELEASE, DTD 23OCT95ISSUED TO AASF, MSARNG, JACKSON FORMH-60A AIRCRAFT WITH SPECIAL MISSIONEQUIPMENT INSTALLED.(HS0516)

27-Feb-1996 1

JACKSON, MS

QC000000

AASF, MSARNGACE/AACCE PERFORMED AT 2165 ACFT HRS.BY DYN CORP FT HOOD TX, OLR PROFILER"N"(HS0516)

24-Jul-1996 1

JACKSON, MS

QC000000

AASF, MSARNGUH-60-96-ASAM-05 INCREASE IN FATIGUELIFE ON FWD SUPPORT ASSY.(HS0516)

06-Aug-1996 1

JACKSON, MS

QC000000

AASF, MSARNGUH-60-96-ASAM-08 INCREASE IN FATIGUELIFE OF CERTAIN S/N T/R INBOARDRETENTION PLATES.(HS0516)

23-Aug-1996 1

JACKSON, MS

QC000000

AASF, MSARNGUH-60-97-ASAM-02, ONE-TIME INSPECTION OFTAIL DRIVE FLEX COUPLINGCONNECTIONS(HS0516)

01-Nov-1996 1

JACKSON MS

QC000000

AASF, MSARNGUH-60-97-ASAM-08, AIRCRAFT WITHCONNECTING LINK P/N: 70400-08155-056.MANUFACTURED BY PURDY MACHINECO.(HS0516)

21-Jan-1997 1

JACKSON MS

QC000000

AASF, MSARNGJACE PERFORMED AT 2299 ACFT HRS. BYJACE TEAM MEMBER "K". ATCOM OLR/MWOBRANCH ST. LOUIS MO(HS0516)

01-May-1997 1

JACKSON MS

QC000000

AASF, MSARNGUH-60-98-ASAM-04 TB 1-1520-237-20-205INSPECTION OF OVERHAULED PRIMARYSERVOS, COLLECTIVE BOOST SERVOS, YAWBOOST SERVOS, AND TAIL ROTOR SERVOSFOR LOOSE HUCK BOLTSCOMPLETED(KL0973)

15-Apr-1998 1

JACKSON, MS

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF, MSARNGTB 1-1520-237-20-167 INSPECTION ANDREPAIR OF STATION 635 FRAME ASSEMBLYFOR TAIL WHEEL STRUT INSTA TURBINEROTOR BLADES VERIFIED BY VISUALINSP(KL0973)

15-Sep-1998 1

JACKSON, MS

QC000000




8.7.DATE

6.REMARKS

4. 5.



AASF-1 FTIGH-60-10-AMAM-11, H-60 SERIES AIRCRAFT, OILSAMPLING SCHEDULE CHANGES COMPLIEDWITH.

03-Feb-2010 1


AT562754

AASF-1 FTIGH-60-10-ASAM-06, ALL H-60A SERIESAIRCRAFT, AUTO-IGNITION AND TRANSIENTDROOP IMPROVEMENT (TDI) MODIFICATIONCOMPLIED WITH.

12-Feb-2010 1


AT562754

AASF-1 FTIGH-60-11-AMAM-15, INTEGRATED VEHICLEHEALTH MANAGEMENT SYSTEM, C/W

02-Aug-2011 2


AT562754

AASF-1 FTIGAUTHORITY IS GRANTED BY MEC #F127275DATED 23MAY2011 TO REMOVE THE ALQ-144SHOCK MOUNTS AND FAIRING.

01-May-2012 1


AT562754

AASF-1 FTIGH-60-12-ASAM-06, UPPER BULKHEAD FUELSYSTEM BREAKAWAY VALVE AND FIREEXTINGUISHING SYSTEM DIRECTIONALVALVE, COMPLIED WITH.

08-May-2012 2


AT562754

AASF-1 FTIGH-60-12-AMAM-09, HYDRAULIC LINE CHAFEDUE TO MISSING CLAMPS, COMPLIED WITH

14-Jun-2012 1


AT562754




8.7.DATE

6.REMARKS

4. 5.



AASF-1 FTIGH-60-11-ASAM-09, ALL H-60A/L SERIESAIRCRAFT, INTERNAL AUXILLARY FUELTRANSFER SYSTEMS (IAFTS) COMPLIEDWITH.

07-Apr-2011 1


AT562754




8.7.DATE

6.REMARKS

4. 5.



AASF-FTIGGEN-10-AMAM-02 DISTRIBUTION OF NEWAIRCRAFT LOGBOOK. (MAGNUS TABLET)

05-Feb-2010 1





8.7.DATE

6.REMARKS

4. 5.



AFMA PAE JBLM WA98433

ACE COMPLETED AT SILVERBELL AHPMARANA AZ @ 5322.3 A/C HRS BY ACE TEAMMEMBERS JJ & T (WG4807)

26-Mar-2014 1

MARANA, AZ 85653

WG084807




8.7.DATE

6.REMARKS

4. 5.



AFMA RASM-PACE PERFORMED @ 5482.7 ACFT HRS ATMARANA, AZ 85653 BY TEAM MEMBERS JJ&T.

06-May-2015 1

MARANA, AZ 85653

WG084807




8.7.DATE

6.REMARKS

4. 5.



AMCOM FT HOODPROJECT OLR

ACE/CPCE PERFORMED AT 4118 AIRCRAFTHOURS BY TEAM MEMBERS K & Q.

05-Nov-2008 1





8.7.DATE

6.REMARKS

4. 5.



ARMY AVIATIONSUPPORT FACILITY

UH-60-97-ASAM-17 ALL H-60 SERIES WITHTHE INTERNAL RESCUED HOIST BRACKETASSEMBLY P/N 70800-02508-346 INSTALLED.BRACKET NOT INSTALLED IN THISAIRCRAFT(SA0342)

25-Aug-1997 1

JACKSON MS. 39209-3436

QC000000


UH-60-98-ASAM-01 MAIN ROTOR SHAFTEXTENSION ASSY SERVICE LIFE OF SUBJECTCOMPONENTS IS REVISED TO THE ORIGINAL14,000 HRS(SA0342)

03-Oct-1997 1

JACKSON MS 39209

QC000000


UH-60-98-ASAM-02 ALL H-60 AIRCRAFT WITHPUSHRODS P/N 70400-08155-050 AND 051MANUFACTURED BY VERSATILE MACHINEINC., CAGE CODE 6S522. (TB 1-1520-237-20-197C) COMPLIED WITH(SA0342)

14-Oct-1997 1

JACKSON MS 39209-3436

QC000000


UH-60-97-ASAM-19, M/UH-60A/L AIRCRAFT,ONE TIME INSPECTION OF ANVIS/HUD POWERSUPPLY (TB 1-1520-237-20-204) COMPLIEDWITH(SA0342)

17-Oct-1997 1

JACKSON MS 39209-3436

QC000000


UH-60-98-ASAM-03 TB 1-1520-237-20-203 ALLH-60 AIRCRAFT WITH THE SWASHPLATE LINKASSEMBLY P/N 70400-08110-054,MANUFACTURED BY TEK CAGE CODE 65780IS COMPLETEED(SA0342)

13-Nov-1997 1

JACKSON MS 39209

QC000000


UH-60-98-ASAM-05 ALL H-60 AIRCRAFT WITHTHE SWASHPLATE LINK ASSEMBLY, P/N70400-08110-045/-061 MANUFACTURED BYTEK (CAGE CODE 65780)(UH-60-98-ASAM-05)(TB 1-1520-237-20-20)(SA0342)

15-May-1998 1

JACKSON, MS

QC000000


UH-60-98-ASAM-07, ALL H-60 HELICOPTERSLEFT TIE ROD P/N 70400-08115-043, NSN 1560-01-083-2954, MANUFACTURED BYARGENCORD (CAGE CODE 3R021) TB 1-1520-237-20-206 COMPLETED 26SEP90(SA0342)

26-Sep-1998 2

JACKSON MS 39209

QC000000


UH-60-99-ASAM-02 ALL H-60 HELICOPTERSWITH PROVISION TO INSTALL EXTERNALHOIST AND ALL EXTERNAL HOISTMANUFACTURED BY BREEZE EASTERNCOMPLETED 18 NOV 98 ACFT TI S.ASKEW(SA0342)

26-Sep-1998 1

JACKSON MS 39209

QC000000


UH-60-99-ASAM-03 ALL UH-60A AND EH-60ASERIES HELICOPTER, ONE TIME INSPECTIONOF ALL T700-GE-700 ENGINE RECORDSCOMPLETED 18 NOV 98 ACFT TI S.ASKEW(SA0342)

18-Nov-1998 2

JACKSON MS 39209

QC000000


UH-60-99-ASAM-01 ALL H-60 AIRCRAFT,RESTORATION OF FULL SERVICE LIFE ONSWASHPLATE LINK ASSEMBLY P/N 70400-08110-054/-061 MANUFACTURED BY TEKCAGE CODE 65780 COMPLETED 18 NOV 98ACFT TI S. ASKEW(SA0342)

18-Nov-1998 1

JACKSON MS 39209

QC000000


UH-60-99-ASAM-02 ALL H-60 HELICOPTERSWITH PROVISION TO INSTALL EXTERNALHOIST AND ALL EXTERNAL HOISTMANUFACTURED BY BREEZE EASTERNCOMPLETED 18 NOV 98 ACFT TI S.ASKEW(SA0342)

19-Nov-1998 1

JACKSON MS 39209

QC000000




8.7.DATE

6.REMARKS

4. 5.




OPERATE IAW AWR 980 R5 DATED 29 AUG2008. (MISSION EQUIPMENT)

05-Sep-2008 1





8.7.DATE

6.REMARKS

4. 5.



AVCRADINSTALLATION OF RESCUE HOIST "A" KITCOMPLETED BY GL2479 AT 1108TH AVCRADGPT. MS

25-Aug-2006 1

GULFPORT MS




8.7.DATE

6.REMARKS

4. 5.



AVSCOMOCM/ACE PERFORMED AT 0834 ACFT HRS ATFT CAMPBELL, KY BY ACE TEAM MEMBER RHAVSCOM OCMSEC. ST. LOUIS, MO(RH0000)

21-Nov-1988 2

ST LOUIS, MO

QC000000

AVSCOMOCM/ACE PERFORMED AT 0834 ACFT HRS ATFT CAMPBELL, KY BY ACE TEAM MEMBER RHAVSCOM OCMSEC, ST. LOUIS, MO(RH0000)

08-Nov-1989 1

ST LOUIS, MO

QC000000




8.7.DATE

6.REMARKS

4. 5.



AVSCOMOCM/ACE PERFORMED AT 1111 ACFT HRS ATFT CAMPBELL, KY BY ACE TEAM MEMBER SPARKER AVSCOM OCMSEC, ST LOUIS,MO(SP0000)

29-Jan-1991 1

ST. LOUIS, MO

QC000000




8.7.DATE

6.REMARKS

4. 5.



AVSCOM/DYNCORPACE/AACE PERFORMED AT 1769 ACFT HRSAT FT CAMPBELL KY BY ACE TEAM MEMBERV AVSCOM ACE/OCM SECTION, ST LOUIS,MO(VV0000)

06-Jan-1994 1

ST LOUIS, MO

QC000000




8.7.DATE

6.REMARKS

4. 5.



C CO 1/160THONE TIME INSPECTION FOR PROPERHARDWARE ON PEDAL ADJUSTER IAW UH-60-93-ASAM-04 C/W BY C CO 1/160TH SOAR(ABN) FTCKY 42223 SSG JPLOEGSTRA(JP0000)

21-Dec-1992 1

FT CAMPBELL,KY

QC000000

C CO 1/160THONE TIME INSPECTION OF T/R PITCH CHANGEASSY P/N 70103-11001-041 IAW UH-60-93-ASAM-06 C/W BY C CO 1/160TH SOAR (ABN)FTCKY 42223 SSG J PLOEGSTRA(JP0000)

22-Dec-1992 2

FT CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



C CO 1/160THT700-GE-700-G/G ROTOR CLEARING/FAILURERE-READ UH-60-93-ASAM-02 C/W BY C CO1/160TH SOAR (ABN) FTCKY 42223 SSG JPLOEGSTRA(JP0000)

20-Oct-1992 1

FT CAMPBELL, KY

QC000000

C CO 1/160THONE TIME INSPECTION OF T/R DRIVESHAFTVISCOUS DAMPER BEARINGS I/A/W UH-60-93-ASAM-05 C/W BY C CO 1/160TH SOAR (ABN)FTCKY 42223 SSG J PLOEGSTRA(JP0000)

22-Dec-1992 1

FT CAMPBELL, KY

QC000000

C CO 1/160THREVISION OF T/R G/B SERVO CORROSIONLIMITS IAW UH-60-93-ASAM-07 C/W BY C CO1/160TH SOAR (ABN) FTCKY 42223 SSG JPLOEGSTRA(JP0000)

29-Dec-1992 2

FT CAMPBELL, KY

QC000000

C CO 1/160THONE TIME INSPECTION AND REPLACEMENTOF M/R BLADE PINS I/A/W UH-60-93-ASAM-03C/W BY C CO 1/160TH SOAR (ABN) FTCKY42223 SSG J PLOEGSTRA(JP0000)

29-Dec-1992 1

FT CAMPBELL, KY

QC000000

C CO 1/160THONE TIME AND RECURRING INSP OF ESSSLINES IAW UH-60-93-ASAM-10 C/W BY C CO1/160TH SOAR (ABN) FTCKY 42223 SSG JPLOEGSTRA(JP0000)

08-Apr-1993 1

FT CAMPBELL, KY

QC000000

C CO 1/160THSOF MESSAGE UH-60-93-02 NOT APPLICABLE,VERIFIED BY SSG J PLOEGSTRA CO C1/160TH SOAR (ABN) FT CAMPBELL, KY 42223-5000(JP0000)

16-Apr-1993 1

FT CAMPBELL, KY

QC000000

C CO 1/160THONE TIME INSPECTION AND REPLACEMENTOF CREW RESTAINT, BUCKLE/CROTCHASSEMBLIES I/A/W UH-60-93-ASAM-11 (TB 1-1520-237-20-142), C/W B C CO 1/160TH SOAR(ABN) FTCKY 42223 SSG JPLOEGSTRA(JP0000)

28-Apr-1993 1

FT CAMPBELL, KY

QC000000

C CO 1/160TH3 DEGREES BIAS OF T/R ASSY IAW UH-60-93-ASAM-08 TB 1-1520-237-20-138 C/W BY CO C1/160TH SOAR (ABN) FTCKY 42223 SSG JPLOEGSTRA(JP0000)

04-May-1993 1

FT CAMPBELL, KY

QC000000

C CO 1/160THONE TIME INSP TO DETERMINE COMPLIANCEW/ SYSTEM MWO IAW UH-60-93-ASAM-09 C/WBY C CO 1/160TH SOAR (ABN) FTCKY 42223SSG J PLOEGSTRA(JP0000)

06-May-1993 1

FT CAMPBELL, KY

QC000000

C CO 1/160THADVISORY OF ABRUPT VIBRATION CHANGESIN THE MAIN ROTOR SYSTEM I/A/W UH-60-93-ASAM-12 C/W BY C CO 1/160TH SOAR (ABN)FTCKY 42223 SSG J PLOEGSTRA(JP0000)

14-May-1993 1

FT CAMPBELL, KY

QC000000

C CO 1/160THREVISION TO TM 55-1520-237-10 FOR ESSSAND ERF'S MISSION KITS IAW UH-60-93-ASAM-13 C/W BY C CO 1/160TH SOAR (ABN) FTCKY42223 SSG J PLOEGSTRA

08-Jun-1993 1

FT CAMPBELL, KY

QC000000

C CO 1/160THONE TIME INSPECTION OF HYDRAULIC PUMPMODULE KNURLES BLEED/RELIEF KNOBSECURING PIN TAIL UH-60-93-ASAM-16 C/WBY C CO 1/160TH SOAR (ABN) FTCKY 42223SSG WAYNE CAMPBELL, TI(WC0000)

03-Sep-1993 1

FT CAMPBELL, KY

QC000000

C CO 1/160THINSP/MODIFY MASTER WARNING PANELS IAWUH-60-94-ASAM-01 C/W BY C CO 1/160THSOAR (ABN) FTCKY 42223 SSG WAYNECAMPBELL, TI (WC3552)

10-Nov-1993 1

FT CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



C CO 1/160THUH-60-94-ASAM-03 INSP OF SPINDLE THRUSTBEARINGS C/W BY C CO 1/160TH SOAR (ABN)FTCKY 42223(CC7160)

01-Feb-1994 1

FT CAMPBELL, KY

QC000000

C CO 1/160THUH-60-94-ASAM-04 INSP OF TAIL ROTORPITCH BEAM ASSY C/W BY C CO 1/160THSOAR (ABN) FTCKY 42223(CC7160)

07-Feb-1994 1

FT CAMPBELL, KY

QC000000

C CO 1/160THUH-60-94-ASAM-05 TAIL ROTOR GEARBOXOUTPUT SHAFT C/W BY C CO 1/160TH SOAR(ABN) FTCKY 42223(CC7160)

09-Feb-1994 1

FT CAMPBELL, KY

QC000000

C CO 1/160THUH-60-94-ASAM-07 INSP OF HISTORICALRECORDS TBO AND MOAT C/W BY C CO1/160TH SOAR (ABN) FTCKY 42223(CC7160)

13-Mar-1994 1

FT CAMPBELL, KY

QC000000

C CO 1/160THUH-60-94-ASAM-08 INSP OF HISTORICALRECORDS ASSITION TO -07 C/W BY C CO1/160TH SOAR (ABN) FTCKY 42223(CC7160)

15-Mar-1994 1

FT CAMPBELL, KY

QC000000

C CO 1/160THUH-60-94-ASAM-06 INSP OF RESTRAINTSYSTEM STANDARDIZATION C/W BY C CO1/160TH SOAR (ABN) FTCKY 42223(CC7160)

30-Mar-1994 1

FT CAMPBELL, KY

QC000000

C CO 1/160THUH-60-94-ASAM-09 INSP OF PRIMARY SERVOS/N C/W BY C CO 1/160TH SOAR (ABN) FTCKY42223(CC7160)

12-Apr-1994 1

FT CAMPBELL, KY

QC000000

C CO 1/160THUH-60-94-ASAM-03 REVISION OF UH-60-94-ASAM-03 C/W BY C CO 1/160TH SOAR (ABN)FTCKY 42223(CC0011)

26-Apr-1994 1

FT CAMPBELL, KY

QC000000

C CO 1/160THUH-60-94-ASAM-11 MAIN ROTOR DEICEHEATER MAT RESISTANCE MEASUREMENTSTEST C/W BY C CO 1/160TH SOAR (ABN)FTCKY 42223(CC0011)

10-May-1994 1

FT CAMPBELL, KY

QC000000

C CO 1/160THONE TIME INSP AND CONVERSION OF FORMSAND RECORDS FOR T700-GE-700/701C SERIESENGINES I/A/W TB 1-2840-248-20-2 COMPLIEDWITH(JS1430)

27-Sep-1994 1

FT CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



C CO 1/160THUH-60-95-ASAM-02 OPERATE WITH THE FUELBOOST PUMPS ON AT ALL TIMES WITH ALLFUELS(CB3774)

27-Oct-1994 2

FT CAMPBELL, KY

QC000000

C CO 1/160THUH-60-95-ASAM-01 RESTRICTION OF AERIALRECOVERY OF UH-60/EH-60 ESSS FIXEDPROVISIONED HELICOPTERS USING THE FWDFUSELAGE MOUNTED TIEDOWN(CB3774)

27-Oct-1994 1

FT CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



C CO 1/160TH SOAR(ABN)

UH-60-95-ASAM-03 T/R BLADE PIVOTBEARING SERIAL NUMBER CHECK(CB3774)

28-Oct-1994 1

FT CAMPBELL, KY

QC000000


ACFT EXPOSED TO SALT WATER FORAPPROX 30 DAYS CORROSION INSPECTIONCOMPLETED I/A/W NDI FOR CORROSIONCONTROL RECOVERY OPS BY LTC ARICHARDSON DATED 3OCT94(CG3383)

01-Nov-1994 1

FT CAMPBELL, KY

QC000000


UH-60-95-SOF-01 ONE TIME HISTORICALRECORDS CHECK FOR OUTPUT BEVEL GEARP/N 70358-06620-101(KB8029)

08-Dec-1994 1

FT CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



C CO 101/160TH TASKFORCE

SOF MSG UH-60A-84-14 (TB 55-1520-237-20-58)ONE TIME INSP. OF TAIL ROTOR CABLES FORPROPER ROUTING AND PROPER TENSION.COMPLETED BY C CO 101/160 FTCKY ALBERTHERNANDEZ, SSG, TI(AH0000)

02-Nov-1984 1

FT CAMPBELL KY

QC000000


SOF MSG UH-60A-84-17 (TB 55-1520-237-20-59)INSP OF MAIN MODULE DOWEL PINS (5) EACHTO ASSURE DOWEL PINS ARE SECURE C/WC CO 101/160 FTCKY CARL S RADFORD SSG,TI(CR0000)

02-Jan-1985 1

FT CAMPBELL KY 42223

QC000000


SOF MSG UH-60A-85-02 ONE TIME INSP OFROTOR TACHOMETER COMPLETED BY CO C101/160 FTCKY ALBERT HERNANDEZ, SSG,TI.(AH0000)

26-Feb-1985 1


QC000000


SOF MSG UH-60A-85-03 TB 55-1520-237-20/60DTD 28 FEB 85 ONE TIME INSP OF STAB AMPSCO C 101/160 FTCKY ALBERT HERNANDEZ,SSG, TI.(AH0000)

01-Mar-1985 1


QC000000


SOF MSG UH-60A-85-06 TB 55-1520-237-20/61ONE TIME INSP OF MAIN ROTOR PRIMARYSERVO CO C 101/160 FTCKY MARK STEVENSSSG, TI.(MS0000)

22-Mar-1985 1


QC000000


SOF MSG UH-60A-85-07 AND 08 ONE TIMEINSP OF UH-60A FLIGHT CONTROLS CO C101/160 FTCKY MARK STEVENS SSG,TI.(MS0000)

06-Apr-1985 1


QC000000


SOF MSG UH-60A-85-10 DTD 22APR85 TB 55-1520-237-20/64 ONE TIME INSP. CO C 101/160FTCKY MARK STEVENS SSG, TI.(MS0000)

22-Apr-1985 1


QC000000


SOF MSG UH-60A-85-11 TB 55-1520-237-20/65MAIN ROTOR SPINDLE INSP. COMPLETED30APR85 CO C 101/160 FTCKY MARKSTEVENS SSG, TI.(MS0000)

30-Apr-1985 1


QC000000


SOF MSG UH-60A-85-14 TB 55-1520-237-20/68ONE TIME INSP. OFUH-60A RECORDS FOR N/RSHAFT PN'S CO C 101/160 FTCKY MARKSTEVENS SSG TI.(MS0000)

03-Jun-1985 1


QC000000


OCM/ACE PERFORMED AT 0216 ACFT HRS ATFT CMPBL KY BY TEAMMEMBER K AVSCOMOCM SEC. ST. LOUIS MO(CR0000)

04-Jun-1985 2


QC000000


SOF MSG UH-60A-85-15 TB 55-1520-237-20/69ONE TIME INSP. OFUH-60A RECORDS FOR M/RHUB BY SN AND PN: CO C 101/160 FTCKYCARL S RADFORD, SSG, TI.(CR0000)

04-Jun-1985 1


QC000000


ONE TIME INSP AND MODIFICATION FO UH-60A IAW SOF MSG UH-60A-85-18 TB 55-1520-237-20-70 COMPLETED BY C101/160 FTCKYMARK STEVENS SFC TI(MS0000)

26-Jul-1985 2


QC000000


ONE TIME INSP. OF UH-60A VISCOUS DAMPERI/A/W SOF MSG UH-60A-85-23 TB 55-1520-237-20-71 COMPLETED BY C101/160 FTCKYALBERT HERNANDEZ SSG, TI(AH0000)

26-Jul-1985 1


QC000000




8.7.DATE

6.REMARKS

4. 5.




RELEASE OF A/C WITH MRC BEARINGS OVER100 HRS IAW SOF MSG UH-60A-85-24COMPLETED BY C101/160 TF FTCKY MARKSTEVENS SSG, TI.(MS0000)

02-Aug-1985 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



C/CO 101/160TH TFONE TIME INSP. OF M/R SPINDLE PITCH ARMATTACTCHING BOLTS I/A/W SOF UH60-84-12TB-55-1520-237-20/55 COMPLETED BY C CO.160TH TF FTCKY 42223 ALET H, SSG,TI(AH0000)

02-Aug-1984 1

FT CAMPBELL KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



C/CO 160TH TASKFORCE

AIRCRAFT CLEARED FOR FLIGHT IAW SOFMSG UH-60A-86-07 PARA. #9 COMPLETED BYC CO TF 160TH FT CPBL KY WESLEY BSTRUDWICK SSG TI(NS0000)

30-Apr-1986 1


QC000000


ONE TIME INSP OF STABILATOR ACTUATORSFOR PART#'S IAW SOF MSG UH60A-86-08COMPLETED 8MAY86 C/W BY C CO 101/160THFT CPBL KY 42223 STEVEN M CLOUD SSGTI(SC0000)

09-May-1986 1


QC000000


ONE TIME INSP AND STAKING OF YAWCONTROL LEVER IAW SOF MSG UH60A-86-10COMPLETED BY C160TH T LYSLON TI(TL0000)

13-Jun-1986 1


QC000000


OCE/ACE PERFORMED AT 0409 ACFT HRS ATFT CAMPBELL BY ACE TEAM MEMBER J MPILKIT AVSCOM OCM SEC, ST LOUIS,MO(SC0000)

24-Jun-1986 1


QC000000


ONE TIME INSP AND REPLACEMENT OF EYEBOLT NUTS IAW SOF MSG UH60A-86-13COMPLETED BY 160TH T LYSLON, TI(TL0000)

30-Jul-1986 2


QC000000


ONE TIME INSP OF YAW SERVO ASSY BY SN#IAW SOF MSG UH60A-86-120 COMPLETED BY160TH T LYSLON, TI(TL0000)

30-Jul-1986 1


QC000000


ONE TIME INSP OF #1 AND #2 DRIVE SHAFTSINPUT AND OUTPUT IAW UH60A-86-20COMPLETED BY C CO 160TH RICHARD DULL,SFC, TI(RD0000)

07-Nov-1986 1


QC000000


ONE TIME INSP OF CREW SEATS IAW SOFUH60A-86-21 COMPLETED BY C CO 160TH TLYSLON, TI(TL0000)

09-Dec-1986 1


QC000000


ACFT RELEASED FROM SOF MSG UH60A-86-18 AND 18A IAW TWX# 31213020OCT86 BY CCO 160TH AT FT CPBL, KY 42223 STEVENCLOUD SSG, TI(SC0000)

15-Jan-1987 1


QC000000


ONE TIME AND RECURRING INSPECTION OFFIRST THREE (3) T/R D/S SPLINE COUPLINGSIAW PARA 9 SOF MSG UH-60A-87-03COMPLETED BY C CO 160TH SOAG (ABN) FTCAMPBELL, KY 42223 STEVEN CLARK, SSG,TI(SC0000)

14-Mar-1987 1


QC000000


ONE TIME REPETITIVE INSP. OF TIE DOWNEYE BOLTS IAW SOF MSG UH60A-87-04COMPLIED WITH BY C CO 160TH SOAG ABNFT CAMPBELL, KY 42223 STEVEN CLOUD SSGTI(SC0000)

01-Apr-1987 1


QC000000


ONE TIME AND RECURRING INSP OF OILCOOLER SPLINES IAW SOF MSG UH60A-87-06COMPLIED WITH BY C CO 160TH SOAG ABNFT CAMPBELL, KY 42223 STEVEN CLOUD SSGTI(SC0000)

06-May-1987 1


QC000000




8.7.DATE

6.REMARKS

4. 5.




ONE TIME AND RECURRING INSP OF 2 LONG/1LAT LINK ASSYS BEARING INNER RACE FORCRACKS IAW SOF MSG UH60A-87-07 C/W BY CCO 160TH SOAR ABN FT. CPBL KY 42223STEVEN CLOUD TI(SC0000)

16-May-1987 1


QC000000


ONE TIME INSPECTION OF ACFT HISTORICALRECORDS FOR ID OF LOCALLY PURCHASEDTIME CHANGE COMPONENT PARTS IAW SOFMSG GEN 87-02 COMPLIED WITH PER PARA 9AND 10 BY CO C 160TH FTCKY, SSG STEVENSMITH, TI(SC0000)

30-Jun-1987 1


QC000000


ONE TIME INSP OF MID SECTION BELLCRANKASSEMBLIES IAW SOF MSG UH60A-87-08 C/WBY C CO 160TH SOAR ABN FT. CPBL KY 42223STEVEN CLOUD TI(SC0000)

01-Jul-1987 1


QC000000


ONE TIME INSP OF INPUT FLANGE ASSY TAWSOF MSG UH60A-87-10 C/W BY C CO 160THSOAR ABN FT. CPBL KY 42223 E RAMSEYTI(ER0000)

15-Oct-1987 1


QC000000


SOF MSG UH-60A-88-02 ONE TIME INSP OFTAIL ROTOR GEARBOX OUTPUT SHAFT C/WBY M. FRAZIER ACFT RECORDS CLERK CCADCRPC TX(MF0000)

10-Apr-1988 6


QC000000


SOF MSG UH-60A-88-01 ONE TIME INSP FORCERTAIN S/N TAIL ROTOR BLADEASSEMBLIES C/W BY M FRAZIER ACFTRECORDS CLERK CCAD CRPC TX(MF0000)

10-Apr-1988 5


QC000000


SOF MSG UH-60A-87-12 ONE TIME INSP FORT700-GE-700/701 ENGINE POWER TURBINEMODULES C/W BY M FRAZIER ACFT RECORDSCLERK CCAD CRPC TX(MF0000)

10-Apr-1988 4


QC000000


TB 55-1520-237-20-93 ONE TIME ANDRECURRING INSP. OF ENGINE COWLING C/WBY M FRAZIER ACFT RECORDS CLERK CCADCRPC TX(MF0000)

10-Apr-1988 3


QC000000


SOF MSG UH60A-87-11 ONE TIME INSP OFCARGO DOOR UPPER AND LOWER ROLLERSUPPORT ASSY C/W BY M. FRAZIER ACFTRECORDS CLERK CCD CRPC TX(MF0000)

10-Apr-1988 2


QC000000


ONE TIME NSP OF CYCLIC STABILATOR SLEWSWITCH IAW SOF MSG UH60A-09 C/W BY C CO160TH SOAG ABN FT. CPBL KY 42223 DAVID DFRANCIS SSG TI(DF0000)

10-Apr-1988 1


QC000000




8.7.DATE

6.REMARKS

4. 5.



CCADDRAWING # 70070-20103 SPAR MODIFICATIONE HERNANDEZ, ACFT RECORDS CLERK,CCAD, CORPC, TX(EH0000)

09-Aug-1984 20

CORPUS CHRISTI TX

QC000000

CCADCOMPLIED WITH INSTRUCTIONS FOR FIELDINSTALLATION OF FORWARD SPARINSPECTION HOLES IN STABILATOR. EHERNANDEZ, ACFT RECORDS CLERK, CCAD,CORPC, TX(EH0000)

09-Aug-1984 19

CORPUS CHRISTI TX

QC000000

CCADTB 55-1520-237-20-56 INSP OFLONGITUDINAL/LATERAL LINK ASSEMBLIESFOR CRACKED BRNG INNER RACE, C/W. EHERNANDEZ, ACFT RECORDS CLERK, CCAD,CORPC, TX(EH0000)

09-Aug-1984 18

CORPUS CHRISTI TX

QC000000

CCADAN/URC 101-110 SAT. COMM., C/W. EHERNANDEZ, ACFT RECORDS CLERK, CCAD,CORPC, TX(EH0000)

09-Aug-1984 17

CORPUS CHRISTI TX

QC000000

CCADMWO 55-1520-H60-50-41 INST OF D-7 AUXFUEL SYSTEM, C/W. E HERNANDEZ, ACFTRECORDS CLERK, CCAD, CORPC, TX(EH0000)

09-Aug-1984 16

CORPUS CHRISTI TX

QC000000

CCADMWO 55-1520-H60-50-40 INST OF MODACCUMULATOR PUMP HANDLE. C/W EHERNANDEZ, ACFT RECORDS CLERK, CCAD,CORPC, TX(EH0000)

09-Aug-1984 15

CORPUS CHRISTI TX

QC000000

CCADMWO 55-1520-H60-50-39 INST OF STABILATORBEEFED UP FWD SPAR. C/W EHERNANDEZ, ACFT RECORDS CLERK, CCAD,CORPC, TX(EH0000)

09-Aug-1984 14

CORPUS CHRISTI TX

QC000000

CCADMWO 55-1520-H60-50-38 INST OF LTN-211OMEGA C/W E HERNANDEZ, ACFTRECORDS CLERK, CCAD, CORPC, TX(EH0000)

09-Aug-1984 13

CORPUS CHRISTI TX

QC000000

CCADMWO 55-1520-H60-50-37 INST OF DIGITAL RMI,C/W E HERNANDEZ, ACFT RECORDSCLERK, CCAD, CORPC, TX(EH0000)

09-Aug-1984 12

CORPUS CHRISTI TX

QC000000

CCADMWO 55-1520-H60-50-34 INST OF AN/ARC 186VHF, C/W. E HERNANDEZ, ACFT RECORDSCLERK, CCAD, CORPC, TX(EH0000)

09-Aug-1984 11

CORPUS CHRISTI TX

QC000000

CCADMWO 55-1520-H60-50-29 INST OF GLASSCENTER WINDSHELD, C/W. E HERNANDEZ,ACFT RECORDS CLERK, CCAD, CORPC,TX(EH0000)

09-Aug-1984 10

CORPUS CHRISTI TX

QC000000

CCADMWO 55-1520-H60-50-20 INST OF FAST ROPEBAR, C/W. E HERNANDEZ, ACFT RECORDSCLERK, CCAD, CORPC, TX(EH0000)

09-Aug-1984 9

CORPUS CHRISTI TX

QC000000

CCADMWO 55-1520-H60-50-17 INST OF COVERTLIGHTING, C/W E HERNANDEZ, ACFTRECORDS CLERK, CCAD, CORPC, TX(EH0000)

09-Aug-1984 8

CORPUS CHRISTI TX

QC000000

CCADMWO 55-1520-H60-50-14 INST. OF TOWPLATES: STEP, P/C/W E HERNANDEZ, ACFTRECORDS CLERK, CCAD, CORPC, TX(EH0000)

09-Aug-1984 7

CORPUS CHRISTI TX

QC000000

CCADMWO 55-1520-H60-50-10 HF VOLUMECONTROL: SECURE VOICE, C/W EHERNANDEZ, ACFT RECORDS CLERK, CCAD,CORPC, TX(EH0000)

09-Aug-1984 6

CORPUS CHRISTI TX

QC000000




8.7.DATE

6.REMARKS

4. 5.



CCADMWO 55-1520-H60-50-8 INST OF DIGITALCLOCK, C/W. E HERNANDEZ, ACFTRECORDS CLERK, CCAD, CORPC, TX(EH0000)

09-Aug-1984 5

CORPUS CHRISTI TX

QC000000

CCADMWO 55-1520-H60-50-7 NVG COCPITLIGHTING. C/W. E HERNANDEZ, ACFTRECORDS CLERK, CCAD, CORPC, TX(EH0000)

09-Aug-1984 4

CORPUS CHRISTI TX

QC000000

CCADMWO 55-1520-H60-50-6 INSTALLATION OFCONTROLLABLE SEARCHLIGHT. P/C/W EHERNANDEZ, ACFT RECORDS CLERK, CCAD,CORPC, TX(EH0000)

09-Aug-1984 3

CORPUS CHRISTI TX

QC000000

CCADMWO 55-1520-H60-50-5 RADAR ALTIMETERDIMMIING CAPABILITIES (APN-209). C/W. EHERNANDEZ, ACFT RECORDS CLERK, CCAD,CORPC, TX(EH0000)

09-Aug-1984 2

CORPUS CHRISTI TX

QC000000

CCADACFT PROCESSED AT CCAD AND SPECIALMISSION EQUIPMT AT 23.7 A/C HRSHERNANDEZ, ACFT RECORDS CLERK, CCAD,CORPC, TX(EH0000)

09-Aug-1984 1

CORPUS CHRISTI TX

QC000000

CCADTB 55-1500-200-20/24 SOF GEN 85-01 ONETIME INSP. OF MS 25224 SWITCH GUARDSAND 2 POSITION SWITCHES. C/W M. FRAZIERACFT RECORDS CLERK, CCAD, CORPC,TX(MF0000)

15-Jan-1986 4

CORPUS CHRISTI TX

QC000000

CCADTB 55-1500-200-20/68 SOF GEN 85-19CORRECTION TO ONE TIME RECORDS INSP.OF M/R SHAFT UH-60A-85-14 P/C/W M.FRAZIER ACFT RECORDS CLERK, CCAD,CORPC, TX(MF0000)

15-Jan-1986 3

CORPUS CHRISTI TX

QC000000

CCADTB 55-1520-237-20/69 SOF MSG UH60A-85-16CORRECTION TO ONE TIME RECORD INSP. OFMAIN ROTOR HUB, P/C/W M. FRAZIER ACFTRECORDS CLERK, CCAD CORPC, TX(MF0000)

15-Jan-1986 2

CORPUS CHRISTI TX

QC000000

CCADACFT COMPLETED STRUCTURAL REPAIR ATCCAD AT 329.5 ACFT HRS IAW PROJECTDIRECTIVE 68ARJ3-363-00D DTD 5DEC85 M.FRAZIER ACFT RECORDS CLERK, CCADCORPC, TX(MF0000)

15-Jan-1986 1

CORPUS CHRISTI TX

QC000000

CCADONE TIME INSP FOR TAIL ROTOR FLEXCPLING MOUNT BOLTS AND DAMPERSUPPORT AND OIL COOLER FOR PROPERTORQ. BEFORE NEXT 10HR/14DAY OR ACFTSTATUS WILL BE CHANGED TO A RED XSTATUS IAW SOF MSG UH60A-86-03COMPLETED BY C/CO 101/160TH FT CPBL KY42223 CARL S. RADFORD SSG TI(CR0000)

24-Feb-1986 3

CORPUS CHRISTI TX

QC000000

CCADONE TIME INSP OF TAIL ROTORDRIVESHAFTFLEX COUPLIN MOUNT BOLTSFOR PROPER TORQUE BEFORE NEXT10HR/14DAY OR ACFT STATUS WILL BECHANGED TO A RED X STATUS IAW SOF MSGUH60A-86-02. COMPLETED BY C/CO101/160TH FT CPBL KY 42223 CARL SRADFORD SSG TI(CR0000)

24-Feb-1986 2

CORPUS CHRISTI TX

QC000000




8.7.DATE

6.REMARKS

4. 5.



CCADONE TIME INSP OF TAIL ROTOR VISCOUSDAMPERS (4 EA) FOR SERIAL# AND PART#581138-101 MUST BE REPLACED WITHIN 100A/C HRS OR90 DAYS WHICHEVER OCCURSFIRST IAW SOF MSG UH60A-86-01COMPLETED BY C101/160TH FT CPBL KY42223 CARL S RADFORD SSG, TI(CR0000)

24-Feb-1986 1

CORPUS CHRISTI TX

QC000000

CCADINSPECTION AND REWORK OF THE MEDEVACPROVISION POWER RECEPTACLE TB 55-1520-237-20-114 C/W J RODRIGUEZ, DAC, CC,TX(JR0000)

12-Jan-1993 1

CORPC, TX

QC000000

CCADONE TIME OPERATIONAL CHECK OF THETRANSMISSION AND GEARBOX CHIPDETECTOR SYSTEM UH-60-93-ASAM-01 C/W SSHULTZ,DAC, CC, TX(SS0000)

13-Jan-1993 1

CORPC, TX

QC000000




8.7.DATE

6.REMARKS

4. 5.



CNDR AMCOMTB 1-1520-237-20-218 INSP TAIL LANDINGGEAR SHOCK STRUT ASSEMBLY FORMISSING BEARING RET, PIN 2741.1 ACHRS(JF3097)

27-Feb-2000 1

REDSTONE ARSENAL,AL

QC000000




8.7.DATE

6.REMARKS

4. 5.



CO C 1/160THINSP OF PILOT AND CO-PILOTS SEAT BUCKLECROTCH STRAP ASSY IAW UH-60-94-ASAM-02C/W BY C CO 1/160TH SOAR (ABN) FTCKY42223 SSG WAYNE CAMPBELL, TI(WC3552)

13-Jan-1994 1

FT CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



CO C 160TH SOAG ABNONE TIME INSPECTION OF MAIN MODULE IAWSOF MSG UH60A-88-03 COMPLETED BY CO C160TH SOAG ABN SSG ALBERT HEMP(AH0000)

13-May-1988 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME INSPECTION OF APU IAW SOF MSGUH-60A-88-05 COMPLETED BY CO C 160THSOAG ABN FT CAMPBELL, KY 42223 SGT TOMCOLEMAN, TI(TC0000)

15-Jun-1988 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME INSPECTION OF APU XMSN OILCOOLER BLOWER IAW SOF MSG UH-60A-88-06 COMPLETED BY CO C 160TH SOAG ABN FTCAMPBELL, KY 42223 SSG ALBERT HEMP(AH0000)

12-Jul-1988 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME INSPECTION OF A.R.A. SEATS PN:D3801-H2 IAW SOF MSG UH-60A-88-09COMPLETED BY CO C 160TH SOAG ABN FTCAMPBELL, KY 42223 SSG ALBERTHEMP(AH0000)

04-Aug-1988 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME INSPECTION OF ACFT PORTABLEFIRE EXTING IAW SOF MSG GEN-88-02COMPLETED BY CO C 160TH SOAG ABN FTCAMPBELL, KY 42223 SSG ALBERTHEMP(AH0000)

22-Sep-1988 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME INSP OF TROOP/GUNNER SEATBARS IAW SOF MSG UH-60A-88-10COMPLETED BY CO C 160TH SOAG ABN FTCAMPBELL, KY 42223 SGT KURT VHENRY(KH0000)

24-Oct-1988 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME INSP OF MAIN ROTOR BLADEEXPANDABLE PINS IAW SOF MSG UH-60A-88-13 COMPLETED BY CO C 160TH SOAG ABN FTCAMPBELL, KY 42223 DANIEL DFRANK(DF0000)

21-Nov-1988 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME INSP OF MAIN ROTOR SPINDLERETENTION NUT IAW SOF MSG UH-60A-89-03/04 COMPLETED BY CO C 160TH SOAG ABNFT CAMPBELL, KY 42223 ALBERTHENRY(AH0000)

31-Mar-1989 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME INSP OF WIRE STRIKE PROTECTIONSYSTEM IAW SOF MSG UH-60A-89-05COMPLETED BY CO C 160TH SOAG ABN FTCAMPBELL, KY 42223 SGT JIM KCOLE(JC0000)

13-Jun-1989 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME INSP OF L/H AND R/H RELAYPANELS IAW SOF MSG UH-60A-89-06/07COMPLETED BY CO C 160TH SOAG ABN FTCAMPBELL, KY 42223 SGT KURT VHENRY(KH0000)

18-Jul-1989 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME INSP OF FUEL BOOST PUMP HOSEAT ATTACH IAW SOF MSG UH-60A-89-08COMPLETED BY CO C 160TH SOAR ABN FTCAMPBELL, KY 42223 SGT KURT VHENRY(KH0000)

10-Aug-1989 1

FT CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



CO C 160TH SOAG ABNCORRECTION OF RETIREMENT LIFESCHEDULE FOR H-60 COMPONENTS IAW SOFMSG UH-60A-89-08 COMPLETED BY 160THSOAR ABN FT CAMPBELL, KY 42223 SGTKURT V HENRY(KH0000)

19-Aug-1989 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME INSP OF OIL COOLER AXIAL FANASSY IAW SOF MSG UH-60A-89-12COMPLETED BY CO C 160TH SOAR ABN FTCAMPBELL, KY 42223 SGT KENTBREWER(KB0000)

23-Nov-1989 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME INSP OF GAS GENERATOR ROTORAND STATOR IAW SOF MSG UH-60A-89-10P/C/W BY CO C 160TH SOAR ABN FTCAMPBELL, KY 42223 SGT JON CROCK,TI(JC0000)

09-Feb-1990 3

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME INSP OF GAS GENERATOR STATORIAW SOF MSG UH-60A-89-01/02 COMPLETEDBY CO C 160TH SOAR ABN FT CAMPBELL, KY42223 SGT JON CROCK, TI(JC0000)

09-Feb-1990 2

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNNEW OVERHAUL/RETIREMENT LIFESCHEDULE FOR H-60 RETIREMENT LIFECOMPONENTS IAW TB 55-1520-237-20-104 W/CHG 1 COMPLIED WITH BY CO C 160TH SOAR(ABN) FT CAMPBELL, KY SGT JON K CROCK,TI(JC0000)

09-Feb-1990 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME AND RECURRING INSP OF MAINROTOR BLADE EXPANDABLE PINS IAW SOFMSG UH-60A-90-01 TB 55-1520-237-20-113COMPLIED WITH BY C CO 160TH SOAR (ABN)FT CAMPBELL, KY 42223 JON CROCK,TI(JC0000)

12-Apr-1990 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAG ABNONE TIME AND RECURRING INSP OF TAILROTOR PITCH BEAM RETAINING WASHERAND RETAINING NUT I/A/W SOF MSG UH60-90-02 (TB 55-1520-237-20-128) C/W BY C CO160TH SOAR (ABN) FT CAMPBELL, KY 42223JON CROCK, TI(JC0000)

22-Aug-1990 1

FT CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



CO C 160TH SOAR ABNONE TIME REPLACEMENT AND 30 HRRECURRING INSP FO THE T/R PITCH BEAMRETAINING WASHER IAW SOF MSG UH-60-91-ASAM-01 (TB 55-1520-237-20-119) C/W BY COCO 1/160TH SOAR (ABN) FT CAMPBELL, KY42223 JON CROCK, SSG TI(JC0000)

28-Jan-1991 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAR ABNONE TIME INSPECTION FOR (4)INSERVICEABLE SPINDLE ASSY'S IAW SOFMSG UH-60-91-ASAM-05 (TB 55-1520-237-20-122) C/W BY CO CO 1/160TH SOAR (ABN) FTCAMPBELL, KY 42223 JON CROCK, SSG,TI(JC0000)

21-Feb-1991 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAR ABNCHS 80 ENHANCEMENT PHASE II MH-60A/LCOMPLETED IAW ROCKWELL DWG TOINCLUDE UPDATED PILOTS AND CO-PILOTSCCO'S AND SCC# AND SCC#2 ALSO UPDATED286 AND 1504 RADIOS INSTALLED BYDYNCORP LARRY L KATX, CIV, TI DYNCORPTM 10-16 FT CAMPBELL KY, 42223-5000(LK0362)

01-Apr-1991 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAR ABNONE TIME INSP FIRE EXTINGUISHINGSYSTEMS IAW UH-60-91-ASAM-08COMPLETED BY CO C 160TH SOAR ABN FTCAMPBELL, KY 42223 SSG KENT BREWER,TI(KB0000)

08-Apr-1991 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAR ABNONE TIME INSP OF CARGO HOOK INTERNALWIRE BUNDLE ROUTING IAW UH-60-91-ASAM-06 (TB 1-1520-237-20-124 C/W BY CO C 1/160THSOAR ABN FT CAMPBELL, KY 42223-5000 SGTDENNIS L HAYWOOD, TI(DH0000)

19-Apr-1991 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAR ABNONE TIME INSP FOR THREE (3)UNSERVICEABLE SPINDLES IAW UH-60-92-ASAM-01 (TB 1-1520-237-20-129) C/W BY CO C1/160TH SOAR ABN FT CAMPBELL, KY 42223-5000 SSG WAYNE CAMPBELL, TI(WC0000)

14-Jan-1992 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAR ABNONE TIME INSP AND REPLACEMENT OF MAINLANDING GEAR BRAKE ASSY PISTONINSULATOR IAW UH-60-91-ASAM-10 C/W BYCO C 1/160TH SOAR ABN FT CAMPBELL, KY42223-5000 SSG KURT BRUNELL, TI(KB0000)

05-Mar-1992 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAR ABNPMS#2 NO.2 COMPLETED AT 1000.0 ACFT HRSON 24JAN90 C/160TH SOAG(A) FT CAMPBELL,KY42223-5000 VERIFIED BY SSG KURTBRUNELL THE SPC MONITOR CURTISBAKER(CB0000)

09-Mar-1992 2

FT CAMPBELL, KY

QC000000

CO C 160TH SOAR ABNPMS #2 NO. 1 COMPLETED AT 500.0 ACFT HRSON 8JAN87 C/160TH SOAG (A) FT CAMPBELL,KY 42223-5000 VERIFIED BY SSG KURTBRUNELL THE SPC MONITOR CURTISBAKER(CB0000)

09-Mar-1992 1

FT CAMPBELL, KY

QC000000

CO C 160TH SOAR ABNONE TIME INSP FOR ENGINE OUTPUT SHAFTBOLT TORQUE AND VIB LEVEL IAW UH-60-92-ASAM-02 C/W BY C 1/160T FT CAMPBELL, KY42223-5000 SSG WAYNE CAMPBELL,TI(WC0000)

12-May-1992 1

FT CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



CO C 160TH SOAR ABNONE TIME INSP OF AN/ALQ-144A(V)1REQUIRED IAW SOF MSG (CECOM91-12-01)C/W BY CO C 1/160TH SOAR ABN FTCAMPBELL, KY 42223-5000 SSG WAYNECAMPBELL, TI(WC0000)

18-Jun-1992 1

FT CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



CO F 160TH SOAR ABNPMS-2 #3 COMPLETED AT 1500.0 ACFT HRSBY F CO 1/160TH SOAR (A) FT CAMPBELL, KY42223 VERIFIED BY DANIEL D FRANK(DF0000)

27-Aug-1992 1

FT CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



COMPUTER SCIENCECORP.

AIRCRAFT REWIRED TO STANDARD UH-60ACONFIGURATION BY COMPUTER SCIENCECORP. (CSC) CONTRACT TASK ORDER # CR-1018/CR-1018PWS, GOVT. TASK ORDER # TO0110.

01-Jul-2008 2

FT. WORTH, TEXAS




8.7.DATE

6.REMARKS

4. 5.



CSCACE COMPLETED AT 4488.4 ACFT HRS. BYACE TEAM MEMBERS B/G. AFMA RASM-E,AMCOM

29-Jul-2010 1


CSCACE COMPLETED AT 4682.7 A/C HRS. BY ACETEAM MEMBERS B/G. AFMA, RASM-E,AMCOM.

02-Aug-2011 3





8.7.DATE

6.REMARKS

4. 5.



D2 1/185TH AVNTB 1-1615-351-23 MAIN ROTOR BLADEEROSION PROTECTION KITSINSTALLED(KL0973)

26-Jul-1999 1

FSGA

QC000000




8.7.DATE

6.REMARKS

4. 5.



DYNA CORP OLRACE-CPCE PERFORMED AT 2911 A/C HRS BYTEAM MEMBERS "K" AND "II" AMCOM OLRMWO BRANCH KILEEN, TX LARRYLEWIS(LL2629)

02-Nov-2001 1

JACKSON MS

QC000000




8.7.DATE

6.REMARKS

4. 5.



DYNCORPJACE/CPCE PERFORMED AT 2476 ACFT HRSBY TEAM MEMBER "H" AT FT HOOD(JP2527)

04-Mar-1999 1

FT HOOD TX

QC000000

DYNCORPUH-60-99-ASAM-07 M/R HUB NDI RECURRINGINSPECTION COMPLIED WITH AT 2475.6 ACFTHRS(GD6707)

12-Mar-1999 1

FT HOOD TX

QC000000

DYNCORPACE/CPCE PERFORMED AT 3032 ACFT. HRS.BY TEAM MEMBERS K&W. AMCOM PROJECTOLR KILLEEN, TX. JERRY D. PARKS(JP2527)

26-Nov-2002 1

KILLEEN, TX

QC000000

DYNCORPACE/CPCE PERFORMED AT 3092 ACFT HRSBY TEAM MEMBERS K & I AMCOM PROJECTOLR KILLEEN TX(JL7296)

06-Jun-2003 1

KILLEEN TX

QC000000

DYNCORPACE/CPCE PERFORMED AT 3715 ACFT. HRS.BY TEAM MEMBERS K & W. AMCOM PROJECTOLR JACKSON MS.(JP2527)

08-Dec-2005 1

KILLEEN, TX

QC000000




8.7.DATE

6.REMARKS

4. 5.



DYNCORP OLRACE/CPCE PERFORMED AT 3433 ACFT. HRS.BY TEAM MEMBERS K & W. AMCOM PROJECTOLR GULFPORT, MS.(JP2527)

14-Oct-2004 1

KILLEEN, TX.

QC000000




8.7.DATE

6.REMARKS

4. 5.




UH-60-95-ASAM-05: CHANGE IN RETIREMENTLIFE FOR SERVO BEAM RAILINGS(EH1318)

26-Jan-1995 1

FT CAMPBELL, KY

QC000000


UH-60-95-SOF-02 CHANGE TO RETIREMENTLIFE FOR CERTAIN MAIN ROTOR BLADECUFFS(EH1318)

14-Feb-1995 1

FT CAMPBELL, KY

QC000000


UH-60-95-ASAM-06 INSP OF MAIN XMSNBEAMS, UPPER DECK SKIN, AND FRAME FORCRACKS AND IMPLEMENTATION OF 100HRRECURRING INSP.(EH1318)

22-Jun-1995 1

FT CAMPBELL, KY

QC000000


UH-60-95-ASAM-04 REDUCTION OF TORQUEOF SELF RETAINING PIVOT BOLTS(PA1318)

22-Nov-1995 1

FT CAMPBELL, KY

QC000000




8.7.DATE

6.REMARKS

4. 5.



FT HOOD AFMAAIRCRAFT 8423935 ACE COMPLETED AT 4328ACFT HRS AT JACKSON, MS BY TEAMMEMBERS RR & W

27-Oct-2009 1





8.7.DATE

6.REMARKS

4. 5.



INTERCONNECT WIRINGL. P.

AIRCRAFT REWIRING PRODUCED ANDMANUFACTURED BY INTERCONNECT WIRINGL. P. INTERCONNECT JOB # 00121862, GOVT.TASK ORDER # TO 0110.

01-Jul-2008 3

FT. WORTH, TEXAS




8.7.DATE

6.REMARKS

4. 5.



IWLP/TEXAS AVIATIONSERVICES

LIST OF REWIRED MWO'S APPLIED BYINTERCONNECT/ TEXAS AVIATIONSERVICES:1-1520-237-50-26 CHIP DETECTORWIRING.1-1520-237-50-34 DIRECTIONALCONTROL CABLE.1-1520-237-50-39 MODIFYENGINE CONTROL LEVERS.1-1520-237-50-46INCORPORATION OF STABILATOR SLEW-UPSWITCH.1-1520-237-50-54 STABILATORACTUATOR GROUNDING STRAP.1-1520-237-50-56 AVIATORS NIGHT VISION IMAGINGSYSTEM (ANVIS LIGHTING UPGRADE)1-1520-237-50-59 EME PROTECTION.1-1520-237-50-66IMPROVED FIRE EXT. CIRCUIT AND HELLFIRECONNECTOR.1-1520-237-50-68 INSTALLATIONOF DUAL AN/ARC-186-AN/ARC-201(V) FMRADIO SYS/HARDWIRING OF TSEC KY-58.1-1520-237-50-70 ELECTRICALLY HEATEDCENTER WINDSHIELD, UH-60A HELICOPTER.1-1520-237-50-75 AN/ASN-128B DOPPLER/GPSNAVIGATION SYSTEM, UH-60A/LHELICOPTER.1-1520-237-50-76 AN/ARC-220 HFCOMMUNICATION SYSTEM.1-1520-237-50-77INSTALLATION OF SEALED LEAD-ACIDBATTERY AND RELOCATION OF UTILITYLIGHT POWER.1-1520-237-50-62INSTALLATION OF THE HEADS UP DISPLAY(HUD) AN/AVS-7.

01-Jul-2008 5

FT. WORTH, TEXAS




8.7.DATE

6.REMARKS

4. 5.



OCM SECTIONOCM/ACE PERFORMED AT 2033 ACFT HRS ATFT CAMPBELL KY BY U (AB0000)

23-Mar-1995 1

ST LOUIS, MO

QC000000




8.7.DATE

6.REMARKS

4. 5.



PAEAWR 1682 DATED 26 FEB 2014 COMPLIEDWITH (AUTO RELIGHT).

18-Sep-2014 1

MARANA, AZ 85653

DW462311




8.7.DATE

6.REMARKS

4. 5.



RASM P URS JBLM, WAACE PERFORMED @ 5061 A/C HRS AT WAATSMARANA, AZ 85653 BY TEAM MEMBERS JJ &T.

15-Mar-2013 1

MARANA, AZ 85653




8.7.DATE

6.REMARKS

4. 5.



RAYTHEON CFTSOF-UH-60-00-01 TB 1-1520-237-20-221 ONETIME RECURRING INSP.OF M/R SPINDLE LOGSCOMPLETED 12 JULY 00 2836.4 ACFTHRS(RH7188)

12-Jul-2000 1

CAMP DOHA, KUWAIT

QC000000

RAYTHEON CFTSOF UH-60-00-02 TB 1-1520-237-222 ONE TIMEINSP OFTHE INPUT MODULE GEARBOXASSEMBLY RECORDS C/W AT 2849.4 ACFTHRS 4 AUG 00(RH7188)

04-Aug-2000 1

CAMP DOHA, KUWAIT

QC000000




8.7.DATE

6.REMARKS

4. 5.



SCIENCE ANDENGINEERINGSERVICES LLC

ACFT TRANSFERED TO SESI HUNTSVILLEFOR INDUCTION INTO B.E.S.T. PROGRAM

21-Nov-2015 1

HUNTSVILLE

TM729539




8.7.DATE

6.REMARKS

4. 5.



SIKORSKYPERSUANT TO MOD P00072 THECONTRACTOR HAS INSTALLED ECP-0252WITH THE EXCEPTION OF THE DAMPENINGTO THE AIRSPEED INDICATING SYSTEM ASDESCRIBED ON NEO 21519 AND 21541ATTATCHED TO THE A/C LOG BOOK. THECONTRACTOR WILL PROMPTLY RETROFITTHE NEW RESTRICTOR TO COMPLY WITH THEECP REQUIREMENTS AT NO DIRECT COST TOTHE GOVT.NOTE: ALL SAFETY OF FLIGHTMESSAGES RECV'D THROUGH NUMBER UH-60A-84-08 HAVE BEEN COMPLIED WITH INPRODUCTION AS APPLICABLE(HS0516)

13-Jun-1984 6

SIKORSKY

QC000000

SIKORSKYUH60A -84-08 (TB55-1520-237-20-50) ONE TIMEINSP. OF AEROQUIP CARGO HOOKPRESSURE CARTRIDGE ASSY P/N FE7590-6COMPLIED WITH(HS0516)

13-Jun-1984 5

SIKORSKY

QC000000

SIKORSKYUH60A-84-07 (TB55-1520-237-20-53) INSP OFENGINE OUTPUT SHAFT P/N 70351-08004-042AND 043. BOLTS INSTALLED AND INSPECTEDPER UH-60-84-07 COMPLIED WITH.(HS0516)

13-Jun-1984 4

SIKORSKY

QC000000

SIKORSKYUH-60A-84-02 (TB55-1520-237-20-48)ONE TIMEINSP OF WIRING HARNESS FOOTING FORFEEDER HARNESS BETWEEN #1 AND #2JUNCTION BOXES COMPLIED WITH(HS0516)

13-Jun-1984 3

SIKORSKY

QC000000

SIKORSKYUH60A-84-01 (TB55-1520-237-50-1) ONE TIMEINSP OF M/R SHAFT P/N 70351-08131-044 AND045 COMPLIED WITH(HS0516)

13-Jun-1984 2

SIKORSKY

QC000000

SIKORSKYUH60A-83-12 (TB55-1520-237-20-46) INSP OFTAIL ROTOR ASSY FOR BENT SERVO VALVEINPUT STEM COMPLIED WITH.(HS0516)

13-Jun-1984 1

SIKORSKY

QC000000




8.7.DATE

6.REMARKS

4. 5.



SIKORSKYAIRCRAFT M/R HEAD RIGGED INACCORDANCE WITH SA DWG 70400-00003REV E SYSTEM CONTROLS HAVE BEENBIASED I/A/W A. AFT CONTROL SERVOINPUT ROD HAS BEEN LENGTHENED TURN.B. LATERAL CONTROL INPUT ROD HAS BEENSHORTENED 1/8 TURN. C. FWD CONTROLSERVO INPUT ROD HAS BEEN SHORTENDTURN.NOTE: WHEN AIRCRAFT RIGGING ISBIASED RIGGING PIN HOLES ARETEMPORARILY LOSTAT THE ABOVE THREEPNTS.(HS0516)

09-May-1984 1

SIKORSKY

QC000000




8.7.DATE

6.REMARKS

4. 5.



SIKORSKY SUPPORTSERVICES

TAIL CONE REPAIRED AT SIKORSKYSUPPORT SERVICES, INC. TROY, ALINACCORDANCE WITH CONTRACT DAAJ09-90-P-1437 REPALCED FRAME P/N 70211-05008-041, FRAME P/N 70211-05009-041 DECK P/N70211-05010-041 SKIN P/N 70211-05001-101,SKIN P/N 70210-05001-102 MICHAEL S GALT,Q.A. FOREMAN(MG0000)

05-Sep-1990 2

TROY, AL

QC000000

SIKORSKY SUPPORTSERVICES

TAIL PYLON REPAIRED AT SIKORSKYSUPPORT SERVICES, INC. TROY, AL INACCORDANCE WITH CONTRACT DAAJ09-90-P-1436 REPALCED TAIL PYLON DECK P/N 70201-06152-041. TAIL PYLON FITTING 70209-06051-043 S/N D496-00516 TIME SINCE NEW 0 HRSMICHAEL S GALT Q.A. FOREMAN(MG0000)

05-Sep-1990 1

TROY, AL

QC000000




8.7.DATE

6.REMARKS

4. 5.



TEXAS AVIATIONSERVICES

AIRCRAFT STRIPPED AND PAINTED IAW TM 55-1500-345-23 BY TEXAS AVIATION SERVICES.

01-Jul-2008 6

FT WORTH, TEXAS


AIRCRAFT WIRING INSTALLED BY TEXASAVIATION SERVICES (TAS) WORK ORDER NO.016580. GOVT. TASK ORDER # TO 0110.

01-Jul-2008 4

FT. WORTH, TEXAS


AIRCRAFT WIRING REPLACED TO BASELINECONFIGURATION (REF. BY ACFT 89-26173EFF. 1214) WITH ALL MWO'S APPLIED.

01-Jul-2008 1

FT. WORTH, TEXAS




8.7.DATE

6.REMARKS

4. 5.



TF 151 AVNAIRCRAFT DEPLOYED TO EROSIVE AND SALTWATER ENVIRONMENT (SOUTHWEST ASIA)AT 2566.9 ACFT FLT HOURS(KL0973)

15-Aug-1999 1

CAMP DOHA, KUWAIT

QC000000

TF 151 AVNUH-60-99-ASAM-11 (TB 1-284-248-23) ONE TIMEINSPECTION OF T700-GE-700/701/701CENGINES. ENG SERIAL NUMBER INSPECTED:GE-E-306551 AND GE-E-306736(KL0973)

16-Aug-1999 3

CAMP DOHA, KUWAIT

QC000000

TF 151 AVNUH-60-99-ASAM-10 (TB 1-1520-237-20-213)INSP AND PREVENTATIVE MAINTENANCE OFNUMBER TWO CROSS FEED BREAKAWAYVALVE, PN 70307-03006-103(KL0973)

16-Aug-1999 2

CAMP DOHA, KUWAIT

QC000000

TF 151 AVNUH-60-99-ASAM-09 ONE TIME INSP OF MAINROTOR EXP PIN P/N 70103-08107-101/102/103.SERIAL NUMBERS OF PINS INSPECTED: E416-2911, E416-02917, E416-02902, E416-01692,E416-02140, E416-02282, E416-01638, E416-01637 (TB 1-1520-237-20-214)(KL0973)

16-Aug-1999 1

CAMP DOHA, KUWAIT

QC000000

TF 151 AVNUH-60-99-ASAM-12 INSPECTION INTERVALCHANGE FOR HAMILITON STANDARD HMUSPECIFIC PART NUMBERS, ENGINE AND HMUINSPECTED BY SERIAL NUMBER:AND ENG GE-E-306736 HMU SN:J7406 PN:4046T52G11ENGGE-E-306551 HMU SN: UDAJ2689 PN:4046T52G09(KL0973)

28-Aug-1999 1

CAMP DOHA, KUWAIT

QC000000

TF 151 AVNUH-60-00-ASAM-01 CHANGE IN INTERVALFOR MAIN ROTOR HUB NDIINSPECTION(GH3963)

11-Nov-1999 1

CAMP DOHA, KUWAIT

QC000000

TF 151 AVNULLS-A CHANGES THROUGH CHANGE NO 45DATED NOV 1999 LOADED IN DATABASE(KL0973)

15-Dec-1999 1

CAMP DOHA, KUWAIT

QC000000

TF 151 AVNUH-60-00-ASAM-02 TB 1-1520-237-20-216COMPLIED WITH CYCLIC STICK WIRINGBUNDLE RELOCATION(KL0973)

19-Dec-1999 1

CAMP DOHA, KUWAIT

QC000000

TF 151 AVNUH-60-00-ASAM-04 TB 1-1520-237-20-217INSPECTION AND REMOVAL OF SUSPECTPRIMARY SERVO ASSEMBLY(KL0973)

04-Jan-2000 1

CAMP DOHA, KUWAIT

QC000000

TF 151 AVNUH-60-00-ASAM-05 INSP. OF FIRE EXT.WIRING COMPLETED AT 2807.0 ACFTHRS(RS6124)

29-May-2000 1

CAMP DOHA, KUWAIT

QC000000




8.7.DATE

6.REMARKS

4. 5.



WAATSACFT TRANSFERED FROM EAATS, FTIG, PATO WAATS, MARANA, AZ @4961.6 ACFT HRS;ALL ACCEPTANCE INSPECTIONS COMPLETEDI/A/W TM 1-1500-328-23

14-Sep-2012 1

MARANA, AZ 85653

JK495821

WAATSAWR 1428 R3 EQUIPPED WITH MULTI-BANDAIRBORN FREQUENCY MODULATEDTRANSCEIVER HOIST UPDATE COMPL

21-Nov-2012 8

MARANA, AZ 85653

AH928217

WAATSAWR 1479 R2 EQUIPPED WITH IMPROVEDPLANETARY CARRIER ASSEMBLY HOISTUPDATE COMPL

21-Nov-2012 7

MARANA, AZ 85653

AH928217

WAATSAWR 1279 R4 EQUIPPED WITH COCKPITDOORS/WINDOWS AND /OR CABINDOOR/WINDOW RMVD, UPDATE COMPL

21-Nov-2012 6

MARANA, AZ 85653

AH928217

WAATSAWR 1539 R2 EQUIPPED WITH AFS, (APU)INLET BARRIER FILTERS UPDATE COMPL

21-Nov-2012 5

MARANA, AZ 85653

AH928217

WAATSAWR 1516 R7 EQUIPPED WITH A EBC406 (ELT)UPDATE COMPL

21-Nov-2012 4

MARANA, AZ 85653

AH928217

WAATSAWR 1054 R12 EQUIPPED WITH A SEI UPDATECOMPL

21-Nov-2012 3

MARANA, AZ 85653

AH928217

WAATSAWR 980 R 8 EQUIPPED WITH A RESCUEHOIST UPDATE COMPL

21-Nov-2012 2

MARANA, AZ 85653

AH928217

WAATSAWR 1800 R1 EDM AND/OR BFT DTD 20 JUL 12APPLIED

21-Nov-2012 1

MARANA, AZ 85653

AH928217

WAATSN/A THIS AIRCRAFT H-60-13-AMAM-02 NLT 05DEC 12 (AHRS WIRING HARNESSES)AT 5007.3AIRCRAFT HOURS

26-Nov-2012 1

MARANA, AZ 85653

JL613055

WAATSH-60-13-ASAM-01 (ANTI-COLLISION LIGHTSPOWER SUPPLY) COMPLIED WITH AT 5011.1ACFT HRS

29-Nov-2012 1

MARANA, AZ 85653

TT187443

WAATSH-60-13-AMAM-03 (TGT BIAS) COMPLIED WITH 04-Dec-2012 1

MARANA, AZ 85653

TT187443

WAATSH-60-13-AMAM-04 (ULLS-A(E)- (ALC)- (LCF)CHANGE 63) COMPLIED WITH AT ACFT HRS5013.6

18-Dec-2012 1

MARANA, AZ 85653

EF717865

WAATSH-60-13-AMAM-05 (BRAKES) COMPLIED WITHAT 5020.0 AIRCRAFT HOURS

22-Jan-2013 1

MARANA, AZ 85653

JL613055

WAATSH-60-13-AMAM-06 CRASHWORTHY EXTERNALFUEL SUSTEM COMPLETED(NOT INST)

13-Feb-2013 1

MARANA, AZ 85653

AH928217

WAATSH-60-13-ASAM-04 (PLASTIC MEDIA BLAST ANDOXIDE FLAKE RESIDUE ) COMPLIED WITH AT5086.1 ACFT. HRS.

26-Mar-2013 1

MARANA, AZ 85653

RB764735

WAATSH-60-13-ASAM-05 COMPLY WITH (N/A HOISTNOT INSTL)

09-Apr-2013 1

MARANA, AZ 85653

AH928217




8.7.DATE

6.REMARKS

4. 5.



WAATSMAIN ROTOR RIGGING COMPL. ADDENDUM 1TO H-60-13-AMAM-01 WORKSHEET LOW COLLANGLE/90RT=#1 8.7-#2 8.8-#3 8.8-#48.7/180FWD= -0.3/270LFT= -10/0AFT=0.8/TOTAL= -2.4/AVG=-.6HIGH COLANGLE/90RT=+20.6/180FWD=+12.7/270LFT=+9.8/0 AFT=+17.7/TOTAL=60.8/AVG=15.2FWDCYCLIC ANGLE 90RT=-1.6/270LFT=+31.4/TOTAL=33.0AFT CYCLICANGLE 90RT= +24.4/ 270LFT=+5.6/TOTAL=19.3LEFT CYCLI ANGLE 180FWD= -8.4/0 AFT= 6.5/TOTAL=15.4RIGHT CYCLIC ANGLE180FWD=7.1/ 0 AFT=7.2/TOTAL=14.3PRI SERVCONTROL ROD BIAS:FWD ADDITIONALADJUSTMENT= +2 FLTSAFT ADDITIONALADJUSTMENT= +2 FLTSLAT ADDITIONALADJUSTMENT= +3 FLTST/R CABLETENSION:L/H 145, R/H 141. TEMP 78.4T/R SERVPISTON TRAVEL:EXTENDED INTIAL=3.60, HIGHCOLL FULL LT YAW=3.53RETRACTEDINTIAL=0.0, LOW COLL FULL RIGHT YAW=.052T/R BIAS MEASUREMENTS:BLADEBLADE SET(DEG) DIM A DIM BDIFF FINAL ANGLE(DEF)RED.6 5.555 5.9300.375 30BLK .04.814 5.184 0.370 30YEL.9 5.433 5.7940.361 30BLU .44.940 5.312 0.37230REMARKS: NONE

30-Apr-2013 1

MARANA, AZ 85653

AH928217

WAATSCOMPLIED WITH H-60-13-ASAM-06 PMICHECKLIST CHANGES AT 5094.9 ACFT HRS

08-May-2013 1

MARANA, AZ 85653

TT187443

WAATSH-60-13-SOF-01 (AHRS) COMPLIED WITH AT5114.2 ACFT HRS

31-May-2013 1

MARANA, AZ 85653

EF717865

WAATSH-60-13-AMAM-11 COMPLY WITH AND FAIL, 12POINT BOLT NOT INSTALLED.

01-Jul-2013 1

MARANA, AZ 85653

AH928217

WAATSH-60-13-AMAM-10 LEGITIMATE CODE FILE(LCF) COMPLIED WITH

10-Sep-2013 1

MARANA, AZ 85653

AH928217

WAATSCOMPLIED WITH H-60-13-AMAM-15 (CEFS R/HFUEL CELL COVER PLATE) AT 5218.2 ACFTHRS

25-Sep-2013 1

MARANA, AZ 85653

TT187443

WAATSH-60-14-SOF-01 (EXTERNAL HOIST) COMPLIEDWITH AT 5218.2 ACFT HRS.

31-Oct-2013 2

MARANA, AZ 85653

RB764735

WAATSPMI-2 COMPLETED AT 5218.2 ACFT. HRS.NEXT PMI - PMI-1 DUE AT 5578.2 ACFT. HRS.

31-Oct-2013 1

MARANA, AZ 85653

RB764735




8.7.DATE

6.REMARKS

4. 5.



WAATSH-60-13-AMAM-01( FLIGHT CONTROL RIGGINGPROCEDURES) COMPLIED WITH AT 5218.2ACFT. HRS. 90RT180FWD 270LFT 0AFTTOTAL AVGLOW COLL ANGLE 1 9.7-0.5 -10.6 -0.7-2.1 -0.525 LOW COLL ANGLE 29.7LOW COLL ANGLE 3 9.7HIGH COLLANGLE 19.3 12.811.1 17.4 60.615.15FWD CYCLIC ANGLE -1.731.3 33.0AFT CYCLIC ANGLE 24.95.4 19.5LEFTCYCLIC ANGLE 8.56.6 15.1 7.55RT CYCLICANGLE 7.36.8 14.1 7.05

01-Nov-2013 2

MARANA, AZ 85653

RB764735

WAATSH-60-13-AMAM-01 FLIGHT CONTROL RIGGINGPROCEDURES-CONT.PRIMARY SERVOCONTROL ROD BIAS ; FWD: CW 3 FLATS AFT:CCW 3 FLATS LAT: CW 5 FLATSTAIL ROTORBIAS CHECK RED- I: 4.538 B:4.861 D: 0.323BLUE- I: 3.859 B:4.194 D: 0.335 YELLOW- I:4.629 B:4.953 D:0.324 BLACK- I: 3.828 B: 4.172D: 0.344TAIL RPTOR CABLE TENSION: L/H 154R/H 155 TEMP 71.6 AVG 154.5 DIFF-1.00 TAILROTOR PISTON TRAVEL OUT: 3.530 IN:0.000

05-Nov-2013 1

MARANA, AZ 85653

RB764735

WAATSH-60-14-ASAM-02 ( IV HUMS ACCEL. )COMPLIED WITH AT 5218.2 ACFT. HRS. - N/ATHIS ACFT.

25-Nov-2013 1

MARANA, AZ 85653

RB764735

WAATSH-60-14-ASAM-04 (MAIN ROTOR HUBASSEMBLY) COMPLIED WITH AT 5218.2 ACFTHRS

02-Jan-2014 2

MARANA, AZ 85653

JK495821

WAATSH-60-14-AMAM-03 (SWASHPLATECONNECTING LINKS) COMPLIED WITH AT5218.2

02-Jan-2014 1

MARANA, AZ 85653

PO676911

WAATSH-60-14-ASAM-03 (EIBF BRACKETS)COMPLIED WITH AT 5218.2 ACFT HOURS

07-Jan-2014 1

MARANA, AZ 85653

PO676911

WAATSH-60-13-AMAM-11 ( MAIN XMSN. FILTER BOWLATTACHMENT HARDWARE REPLACEMENT)COMPLIED WITH ON 09 JAN 14 @ 5218.9 ACFT.HRS.

09-Jan-2014 1

MARANA, AZ 85653

RB764735

WAATSH-60-14-AMAM-08 (AN/ASC-15ECOMMUNICATION CONSOLE CIRCUITBREAKER PROTECTION) COMPLIED WITH @5298.8 ACFT. HRS. - N/A THIS ACFT.

04-Mar-2014 1

MARANA, AZ 85653

RB764735

WAATSH-60-14-AMAM-10 (HONTEK COATED MAINROTOR BLADE) COMPLIED WITH AT 5332.2ACFT HRS

08-Apr-2014 1

MARANA, AZ 85653

TT187443

WAATSH-60-14-AMAM-05 (LCF CHANGE 65)COMPLIED WITH AT 5332.2 ACFT HRS

18-Apr-2014 1

MARANA, AZ 85653

TT187443

WAATSH-60-14-AMAM-12 (M/R SPINDLE NUTRETIREMENT LIFE) COMPLIED WITH AT 5332.2ACFT HOURS

21-Apr-2014 1

MARANA, AZ 85653

JK495821




8.7.DATE

6.REMARKS

4. 5.



WAATSH-60-14-ASAM-06 (FLIGHT CONTROL MIXERASSY.) COMPLIED WITH @ 5332.2 ACFT. HRS.

15-May-2014 1

MARANA, AZ 85653

RB764735

WAATSH-60-14-AMAM-14 (IVHMS CABLING )COMPLIED WITH @ 5332.2 ACFT. HRS.

29-May-2014 1

MARANA, AZ 85653

RB764735

WAATSH-60-14-SOF-03( DISCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS) COMPLIED WITH @5335.3 ACFT. HRS

26-Jun-2014 1

MARANA, AZ 85653

RB764735

WAATSH-60-14-ASAM-09 (ENGINE OUTPUT SHAFTS)COMPLIED WITH @ 5350.3 ACFT. HRS.

05-Aug-2014 1

MARANA, AZ 85653

RB764735

WAATSH-60-14-AMAM-16 (AHRU 2410 TRACKING)COMPLIED WITH @ 5352.8 ACFT. HRS.

11-Aug-2014 1

MARANA, AZ 85653

RB764735

WAATSH-60-14-ASAM-10 (MAIN XMSN. PLANETARYCARRIER) COMPLIED WITH @ 5367.7 ACFT.HRS.

03-Sep-2014 1

MARANA, AZ 85653

RB764735

WAATSH-60-14-SOF-04 (OPERATORS ANDCREWMEMBERS CHECKLIST) COMPLIEDWITH AT 5380.4 ACFT HRS

18-Sep-2014 2

MARANA, AZ 85653

TT187443

WAATSH-60-15-AMAM-02 ( IVHMS WIRINGMANAGEMENT ) COMPLIED WITH @ 5406.3ACFT. HRS.

21-Oct-2014 1

MARANA, AZ 85653

RB764735

WAATSH-60-15-SOF-01 (OIL COOLER FAN AXIALBEARING) COMPLIED WITH @ 5418.2AIRCRAFT HOURS

28-Oct-2014 1

MARANA, AZ 85653

RB764735

WAATSH-60-15-ASAM-01 LIGHT EMITTING DIODE(LED) CAUTION ADVISORY PANEL COMPLIEDWITH @ 5455.2 ACFT. HRS.

25-Nov-2014 1

MARANA, AZ 85653

RB764735

WAATSH-60-14-AMAM-19 ULLS-A(E) LEGIMATE CODEFILE CHANGE 66 REQUIREMENTS COMPLIEDWITH @ 5455.2 ACFT. HRS.

26-Nov-2014 1

MARANA, AZ 85653

RB764735

WAATSH-60-15-AMAM-05 ( AHRS EMER. PROCED.)COMPLIED WITH @ 5471.8 ACFT. HRS.

20-Jan-2015 1

MARANA, AZ 85653

RB764735




8.7.DATE

6.REMARKS

4. 5.



WAATSM/R RIG COMPLETED @ 5471.8 ACFT HRS.LOW COLL:90: 9.1, 180= -0.4, 270= -10.4, 0= -0.6, TOTAL= , AVG= -0.575. HIGH COLL:90= 20,180= 12.6, 270= 10.3, 0= 17.6, TOTAL= 60.5, AVG= 15.125. FWD CYCLIC:90= -1.9, 270= 31.7,TOTAL = 33.6. AFT CYCLIC 90=6, 270= 25,TOTAL = 19. LEFT CYCLIC 180=6.8, 0= 8.3,TOTAL= 15.1. RIGHT CYCLIC 180= 7.4, 0= 7.1,TOTAL=14.5. FORWARD PRIMARY SERVO:3.5CW. AFT PRIMARY SERVO: 3.5CCW. LATPRIMARY SERVO: 3 CW. COMPLETEDBY:RV240103, RV240103, RV240103, , T/R BIASCOMPLETED AT 5471.8 ACFT HOURS.READINGS ARE AS FOLLOWS:BLADEBLADE SET DEGREE DIM A DIM BDIFF FINAL ANGLE DEGREERED 14.535 4.861 0.326 3BLK 0.93.737 4.087 0.35 2.9YEL 0.94.533 4.876 0.343 3BLU 1.13.868 4.174 0.306 2.9T/R RIGCOMPLETED AT 5471.8 ACFTHOURS.READINGS ARE AS FOLLOWS: T/RCABLE: L/H CABLE=146, R/H CABLE= 146,AVG= 146, DIFF=0, TEMP= 87 DEGREES F.T/R SERVO PISTON: INITIAL HIGHCOLL/FULL LEFT YAW LOW COLL/FULLRIGHT YAW EXTENDED: 3.5253.483 XRETRACTED: 0 X0.03

23-Mar-2015 1

MARANA, AZ 85653

RB764735

WAATSH-60-15-AMAM-06 (IDENTIFICATION OF ASEEQUIPMENT) COMPLIED WITH @ 5471.8 ACFT.HRS.

26-Mar-2015 1

MARANA, AZ 85653

RB764735

WAATSH-60-15-AMAM-10 (AV-DEC GASKET INSP.)COMPLIED WITH @ 5503.5 ACFT. HRS.

22-May-2015 1

MARANA, AZ 85653

RB764735

WAATSH-60-15-ASAM-03 (TROOP/GUNNER SEATENERGY ATTENUATORS) COMPLIED WITH @5503.5 ACFT. HRS.

29-May-2015 1

MARANA, AZ 85653

RB764735

WAATSH-60-15-AMAM-11 ( MODE S TRANSPONDER )COMPLIED WITH @ 5503.5 ACFT. HRS.MODE SADDRESS 53405526

08-Jun-2015 1

MARANA, AZ 85653

TM874804

WAATSH-60-15-AMAM-14 LEGITIMATE CODE FILE(LCF) CHANGE 67 REQUIREMENTS COMPLIEDWITH @ 5545.4 ACFT. HRS.

27-Aug-2015 1

MARANA, AZ 85653

RB764735

WAATSH-60-15-SOF-02(FRIES RELEASE CABLE)COMPLIED WITH @ 5560.4 ACFT. HRS.

24-Sep-2015 1

MARANA, AZ 85653

RB764735

WAATSH-60-15-AMAM-18 (MEDEVAC CAROUSEL)COMPLIED WITH @ 5561.1 ACFT. HRS.

13-Oct-2015 1

MARANA, AZ 85653

RB764735

WAATSCOMPLIED WITH H-60-16-AMAM-01. N/A THISAIRCRAFT.

26-Oct-2015 1

MARANA, AZ 85653

PO676911

WAATSH-60-16-ASAM-01 (INBOARD RETENTIONPLATE TORQUE CHECKS) COMPLIED WITH @5561.1 ACFT HRS

10-Nov-2015 1

MARANA, AZ 85653

TT187443




8.7.DATE

6.REMARKS

4. 5.



WAATSAIRCRAFT TRANSFERRED TO BESTPROGRAM ON 18 NOV 15 FOR ARMY / BESTPROGRAM BY WESTERN ARMY AVIATIONTRAINING SITE W7V0AA @ 5571.1 ACFT HRS,DATA PLATE REMAINED INSTALLED

20-Nov-2015 1

MARANA, AZ 85653

TT187443




8.7.DATE

6.REMARKS

4. 5.



WAATS MARANA AZ,85653

H-60-13-AMAM-07 ( LOAD DEMAND SPINDLECABLE CLEARANCE) COMPL IAW AMAM...."PASS"

02-May-2013 2

MARANA, AZ 85653

AH928217




8.7.DATE

6.REMARKS

4. 5.



WAATS, MARANA AZ85653

MEC # F164496 COMPLETED IAW MEC BY UR (FUSELAGE STRUCTURE REPAIR ON 34.5BEAM AT THE INTERNAL HOIST MOUNTPOINT)

02-May-2013 1

MARANA, AZ 85653

AH928217



DATE AC HRS SHAFT VERTICAL REASON FOR VIB CHECKLONGITUDINALLATERAL

IPS READINGS4.

8423935HELICOPTER, UTILITYUH-60A3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Report Date: 01-Dec-2015 1/3

NO REMARKS07-Mar-1994 #1 ENGINE 000.51800


NO REMARKS07-Mar-1994 OIL COOLER 0.4500.351800


NO REMARKS27-Jan-1995 #1 ENGINE 000.191984

NO REMARKS27-Jan-1995 #2 ENGINE 000.031984

NO REMARKS27-Jan-1995 OIL COOLER 0.6700.361984

NO REMARKS23-Jul-1996 OIL COOLER 0.2200.442165

NO REMARKS23-Jul-1996 #2 ENGINE 000.332165

100 HR18-Mar-1997 #2 ENG O/P 000.282267.6

100 HR18-Mar-1997 #1 ENG O/P 000.122267.6

100 HR18-Mar-1997 OIL COOLER 0.330.602267.6

100 HR26-Jan-1998 #2 ENGINE 000.362365.9

100 HR27-Jan-1998 #1 ENGINE 000.172365.9

100 HR27-Jan-1998 OIL COOLER 0.240.5502365.9

COMPLETION OF PMS II25-Sep-1998 OIL COOLER 0.450.4902445.3

COMPLETION OF PMS II25-Sep-1998 #2 ENGINE 000.052445.3

COMPLETION OF PMS II25-Sep-1998 #1 ENGINE 000.092445.3

CHG OF HARDWARE20-Nov-1998 #2 ENGINE 000.132447

100 HR05-Nov-1999 OIL COOLER 0.380.3802637

100HR INSPECTION05-Nov-1999 #2 ENGINE 000.352637

100 HR INSPECTION05-Nov-1999 #1 ENGINE 000.062637

100 HR16-Jul-2000 ENGINE #1 000.112836.9

100 HR16-Jul-2000 ENGINE #2 000.22836.9

100 HR16-Jul-2000 OIL COOLER 0.480.702836.9

100 HR17-Jul-2000 TAIL ROTOR 000.172836.9

100HR11-Apr-2003 NO 1 ENG. 000.213032.3

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

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


IPS READINGS4.



100HR11-Apr-2003 NO 2 ENG. 000.333032.3

100HR11-Apr-2003 OIL COOLER 0.260.5103032.3

100HR11-Apr-2003 TAIL ROTOR 000.263032.3

100HR04-Feb-2004 NO 1 ENG. 000.23220.9

100HR04-Feb-2004 NO 2 ENG. 000.373220.9

100HR04-Feb-2004 OIL COOLER 0.220.503220.9

100HR04-Feb-2004 TAIL ROTOR 000.053220.9

100HR17-May-2004 NO 1 ENG. 000.33326

100HR17-May-2004 NO 2 ENG. 000.413326

100HR17-May-2004 TAIL ROTOR 000.073326

100HR17-May-2004 OIL COOLER 0.220.5203326

100HR02-Jun-2005 NO 1 ENG. 000.233532.8

100HR02-Jun-2005 NO 2 ENG. 000.393532.8

100HR02-Jun-2005 OIL COOLER 0.550.7503532.8

100HR02-Jun-2005 TAIL ROTOR 000.023532.8

120 HR22-Sep-2005 NO 1 ENG. 000.433653.6

120 HR22-Sep-2005 NO 2 ENG. 000.283653.6

120 HR22-Sep-2005 OIL COOLER 0.440.0103653.6

120 HR22-Sep-2005 TAIL ROTOR 000.063653.6

120 HR31-Jan-2007 T/R 000.143888.5

REPLACED T/R BOOT30-Apr-2007 T/R 000.14047.7

120 HR18-Dec-2008 T/R 000.084136.1

REMOVAL OF #1 DRIVE SHAFT30-Jan-2009 OIL COOLER 00.6804195

3 M/R SERVOS REPLACED26-Mar-2009 T/R 0.11004195

DUST BOOT R/R01-May-2009 TAIL ROTOR 0.14004201

ENG REPLACEMENT27-May-2009 #2 ENG 0.32004220

120 HR02-Jul-2009 T/R 0.03004247.1




IPS READINGS4.



120 HR02-Jul-2009 #1 ENG 0.12004247.1

120 HR02-Jul-2009 #2 ENG 0.39004247.1

120 HR02-Jul-2009 OIL COOLER 00.3604247.1

REPLACEMENT OF #1 HSS06-Apr-2010 #1 HSS 0.33004369.4

REPLACEMENT OF T/R CONTROL CABLES06-Apr-2010 T/R 0.04004369.4

120 HR27-Apr-2010 #1 ENG 0.13004378.4

120 HR27-Apr-2010 #2 ENG 0.43004378.4

120 HR27-Apr-2010 OIL COOLER 00.8204378.4

120 HR27-Apr-2010 T/R 0.02004378.4

120 HR06-Sep-2011 #1 ENG HSS 0.29004738.4

120 HR06-Sep-2011 #2 ENG HSS 0.09004738.4

120 HR06-Sep-2011 OIL COOLER 00.1404738.4

120 HR06-Sep-2011 TAIL ROTOR 0.15004738.4

REPAIR OF BLADE SKIN09-Sep-2011 TAIL ROTOR 0.09004738.4

REPLACEMENT OF A AXIS SEAL17-Jul-2012 #1 ENG HSS 0.34004896.1

REPLACEMENT OF A AXIS SEAL17-Jul-2012 #2 ENG HSS 0.33004896.1

23-Apr-2015 #1 ENG HSS 0.13005475.2

23-Apr-2015 #2 ENG HSS 0.32005475.2

23-Apr-2015 OIL COOLER 00.2205475.2

23-Apr-2015 T/R 0.08005475.2

INSTALLATION OF T 700-GE70001-Oct-2015 #1 ENG HSS 0.19005560.4

INSTALLATION OF T700-GE70001-Oct-2015 #2 ENG HSS 0.32005560.4

6. Remarks




8423935HELICOPTER, UTILITY UH-60A

7. FREQUENCY 4.

5. ITEMS TO BE INSPECTED

2. MODEL 3. SERIAL NUMBER 1. NOMENCLATURE

8. NEXTNO DUE 6. REFERENCE 9. COMPLETED AT

INSP

A020 5571.110TM 1-1520-237-PMDPERFORM M/R SPINDLE LUGS,M/R CUFF, TIP CAPSINSPECTION

5561.1H

A022 Nov 26 201514TM 1-1520-237-23-914 DAY FLYABLE STORAGEENGINE RUN UP

Nov 12 2015D

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

Oct 24 2015D

A100 Dec 15 201530DA PAM 738-751#1 ENGINE HISTORY RECORDERREADING DUE

Nov 15 2015D

A101 Dec 15 201530DA PAM 738-751#2 ENGINE HISTORY RECORDERREADING DUE

Nov 15 2015D

A103 Dec 9 201530TM 1-1500-344-23AIRCRAFT WASH DUE Nov 9 2015D

A110 5600.440TM 1-1520-237-PMSPMS 40 HOUR INSPECTION 5560.4H

A115 Dec 9 201530TM 1-1520-237-23-12LUBE REQUIRMENTS Nov 9 2015D

A115 5601.140TM 1-1520-237-23-12LUBE REQUIRMENTS 5561.1H

A116 5865.2360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

5505.2H

A116 Jun 17 201612H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

Jun 17 2015M

A117 5865.2360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 5505.2H

A117 Jun 17 201612H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE Jun 17 2015M

A160 Dec 28 201590TM 1-1520-237-23-1290 DAY CORROSIONINSPECTION

Sep 29 2015D

A177 Dec 30 201590AR 95-190 DAY REVIEW/UPDATE OF 365-4 ENTRIES

Oct 1 2015D

A200 5572.2120H-60-08-ASAM-11120 HOUR INSPECTIONREQUIREMENTS ON DOWEL PIN

5452.2H

A210 5572.2120TM 1-1520-237-23-12120 HOUR INSPECTIONREQUIREMENTS

5452.2H

A211 5865.2360H-60-10-AMAM-11APU OIL SAMPLE 5505.2H

A211 Jun 17 201612H-60-10-AMAM-11APU OIL SAMPLE Jun 17 2015M

A230 Nov 17 2015120MWO 1-1520-237-50-77INSPECT BATTERYCOMPARTMENT FORCORROSION (SLAB)

Jul 20 2015D

A295 5578.2360TM 1-1520-237-23-12STABILATOR ACTUATOR ASSYLUBE

5218.2H

A296 5578.2360TM 1-1520-237-23-12STABILATOR INSPECTION 5218.2H

A298 5863.5360TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 5503.5H

A298 May 15 201612TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING May 15 2015M

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

A299 5831.8360TM 1-1520-237-23-12SWASHPLATE LUBE 5471.8H

A299 Mar 17 201612TM 1-1520-237-23-12SWASHPLATE LUBE Mar 17 2015M

A320 5578.2360TM 1-2840-248-23ENGINE INSPECTION &CLEANING

5218.2H

A400 5578.2720TM 1-1520-237-PMIPMI-1 4858.2H

A401 5938.2720TM 1-1520-237-PMIPMI-2 5218.2H

A408 5938.2720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-2, AREA 5 AND 6)

5218.2H

A410 5578.2720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-1, AREA 1 THRU 4)

4858.2H

A415 5580.2720H-60-10-AMAM-11MAIN GEARBOX OIL SAMPLE-PART # 073, 074, 076

4860.2H

A440 5578.2720TM 1-1520-237-23-12CLEAN TAIL WHEEL LOCKPIN 4858.2H

A470 56371500TM 1-1520-237-23-12REPLACE NUMBER TWOCROSSFEED VALVE

4137H

A471 6529.42160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

4369.4H

A472 6529.42160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

4369.4H

A473 6529.42160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

4369.4H

A476 9858.25000TM 1-1520-237-23-12REPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

4858.2H

A477 10218.25000TM 1-1520-237-23-12REPLACEMENT OF STABILATORACTUATOR BOLTS

5218.2H

A480 9858.25000TM 1-1520-237-23-12REPLACE PIVOT BOLT 70400-08159-101,102,103,104

4858.2H

A485 9858.25000TM 1-1520-237-23-12REPLACE BELLCRANK BOLT70400-08159-105,106,107,108

4858.2H

A501 Nov 21 20156TM 1-1520-237-23-12MAIN ROTOR BLADE PRESSURECHECK

May 21 2015M

A502 Dec 3 20156TM 1-1520-237-23-12INSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

Jun 3 2015M

A530 Feb 11 201612DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

Feb 11 2015M

A532 Apr 22 201612TM 1-1500-204-23-4COMPASS SWING / RMI Apr 22 2015M

A533 Jun 8 201612TM 1-1520-237-23-12PITOT STATIC SYSTEMINSPECTION

Jun 8 2015M

A538 Sep 9 201612TM 1-1520-237-23-12FAT/OAT GAUGEINSPECTION/TEST

Sep 9 2015M

A541 Oct 30 201512TM 1-1520-237-23, C4REPLACE DIGITAL CLOCKBATTERY

Oct 30 2014M






7. FREQUENCY 4.




INSP

A553 Mar 27 201612AR 95-1AIRCRAFT WEIGHINGINVENTORY (365-1)

Mar 27 2015M

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

Jul 20 2015M

A621 Jan 7 201624AR 95-1AIRCRAFT WEIGHING CLASS 2 Jan 7 2014M

A625 Jul 20 202060TM 11-6140-203-23&PREPLACEMENT OF SLABBATTERY (SLAB)

Jul 20 2015M

A630 Jul 1 2022114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

Jan 1 2013M

A633 Feb 1 2018114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

Aug 1 2008M

A638 Feb 1 2018114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

Aug 1 2008M

A640 Jul 1 2022114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

Jan 1 2013M

A642 Apr 25 202072TB 9-1300-385CARGO HOOK CARTRIDGEREPLACEMENT, DODIC MJ21

Apr 25 2014M

A648 Jan 1 2020180TM 1-1520-237-23REPLACE T/R SPRING CAPSULEASSY

Jan 1 2005M

A660 Apr 1 202072TB 9-1300-385REPLACE THRUSTEREMERGENCY RELEASE CARGOHOOK, MJ20

Apr 1 2014M

A665 Jun 9 201848H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

Jun 9 2014M

A670 Dec 18 201748TM 1-1520-237-23-1CABIN TUB INSPECTION Dec 18 2013M

A673 May 19 201848TM 1-1520-237-23-12FUEL CELL CORROSIONINSPECTION

May 19 2014M

A675 May 2 201748TM 1-1520-237-23-12FLIGHT CONTROL ROD INSP May 2 2013M

A695 6052.2720H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

5332.2H

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

Apr 17 2014M

A755 13858.29000H-60-10-ASAM-11PC LINK TO SWASHPLATEBOLTS REPLACEMENT

4858.2H

E135 Dec 26 20156TM 11-5821-333-12AN/ARC-201(V) SINCGARSRADIO HUB BATT REPL

Jun 26 2015M

E300 Nov 23 201530AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

Oct 24 2015D

E300 5681.1120AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

5561.1H

E320 Oct 14 2016360AWR 1516 FOR ELTEMERGENCY LOCATORTRANSMITTER G-SWITCH (EBC-406HM)

Oct 20 2015D






7. FREQUENCY 4.




INSP

E325 Jul 15 201760AWR 1516R2 FOR ELTREPLACEMENT OF ELTBATTERY PN GS-46

Jul 15 2012M




01-Dec-2015

T700-GE-700ENGINE ASSY, TURBINE

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

GEE307130

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

01-Oct-2015 8423935 INSTALLATION OF T700-GE700

6000 87 90 0.9798.5254869 845

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

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

01-Dec-2015

T700-GE-700ENGINE ASSY, TURBINE

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

GEE207736

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

12-Jun-2014 7823014 ENG REPLACED, NEWMAX PWR CHECK,AIRSPEED 119 KIAS(IVHMS)

5000 96 91 1100292212 849

01-Oct-2015 8423935 INSTALLATION OF T700-GE700

6000 94 90 199.5252440 846


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

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: 1/1202-Dec-2015

84239351520010350266 00HELICOPTER, UTILITY

156001095713502C12D

34243424UNK393570219-05001-042TAIL CONE FITTING CCCC COND COND

162001231183103A01

59733889C001-0003670250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001231183103A01 LEFT

45002699C001-0218970250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001421089003B01 TAIL

3450449822670250-13101-044SHOCK ABSORBER (TAIL) CCCC COND COND

165001285302405A01Z RED

13454862A1060368770106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z YELLOW

5944498R106-0120770106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z BLUE


165001285302405A01Z BLACK


531501537465205A02H BLUE LAG

04369B9411262470103-08108-041SOLID BLADE PIN CCCC COND COND

531501537465205A02H RED LAG


531501537465205A02H BLUE LEAD


531501537465205A02H BLACK LEAD


531501537465205A02H RED LEAD


531501537465205A02H YELLOW LAG


531501537465205A02H YELLOW LEAD


531501537465205A02H BLACK LAG


161501106191805A03A

48034498A1070025570104-08000-046SWASHPLATE ASSY CCCC COND COND

161501078571806A11 2

30814498A258-0009470351-08080-043ACCESSORY MODULE CCCC COND COND

161501383899206A11 1

4784498A258-0694370351-08080-045ACCESSORY 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

33315472A2650112970351-08100-076MAIN TRANSMISSIONMODULE

CCCC COND COND

161501353382506E 1

2776449841534170351-08001-049INPUT MODULE CCCC COND COND

161501353382506E 2

42124498A2640020470351-08001-049INPUT MODULE CCCC COND COND

168001074515206F

44164498A005-0212370357-06300-042INTERMEDIATE GEARBOX CCCC COND COND

161501376508906G01

42184498A006-0131270358-06600-046TAIL ROTOR GEARBOXASSY

CCCC COND COND

161501524780506H04 1

6745333C8450193770361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501524780506H04 2

05218C8451008970361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501081277506H06

00A271-0067070361-03001-045SHAFT ASSY, T/R DRV SEC1

CCCC COND COND

161501158951706H08 SEC II

04498WG10897-00183

70361-03009-047SHAFT ASSY, T/R DRV SEC2

CCCC COND COND

161501158952206H09 FWD

04369WG30024-00425

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

CCCC COND COND

161501158952206H09 CENTER

04369WG30024-00746

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

CCCC COND COND

161501158952206H09 AFT

04864WG30049-00366

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

CCCC COND COND

161501083295306H11


CCCC COND COND

161501158578806H12


CCCC COND COND

432001207722807A01 1

524738239089ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01 #2

1714351K0908ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01

4857485820892270652-02300-050PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

481001102247307B05A

04858117803213850-3-1VALVE, SOLENIOD CCCC COND COND

481001102247307B05A

04858142713213850-3-1VALVE, SOLENIOD CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






165001084309607B11

82241408441170A70651-03201-102ACCUMULATOR CCCC COND COND

168001084225608B20 CP

38713778123470450-01043-111PANEL INDICATOR (PDU) CCCC COND COND

168001342049608B20 PILOT

03318337070450-01043-124PANEL INDICATOR (PDU) CCCC COND COND

611501114969609A01 1

68244983210E28B302-8-DMGENERATOR CCCC COND COND

611501114969609A01 2

492449835-A241828B302-8-DMGENERATOR CCCC COND COND

161501260074911C21

05332TMD04643749170400-02300-046MIXER ASSEMBLY CCCC COND COND

156001136211711D17

00UNK3935#170209-22103-050SERVO BEAM RAILING CCCC COND COND

156001136211711D17


156001136211711D17


156001136211711D17


168001261204411D25 UPPER

59943281186DL2155M20STABILATOR ACTUATOR CCCC COND COND

168001261204411D25 LOWER

59643281397DL2155M20STABILATOR ACTUATOR CCCC COND COND

599601316274311D26 1

23764498237970902-02001-048STABILATOR AMPLIFIER CCCC COND COND

599601316274311D26

32655473298670902-02001-048STABILATOR AMPLIFIER CCCC COND COND

299501169529115A04 01

182034677584-0467163290-100ENGINE SEQUENCINGUNIT

CCCC COND COND

599601415867319D01A

04372671AA822-0787-001AMPLIFIER, RADIOFREQUENCY

CCCC COND COND

NSN PENDING19E04B

11155612678P320A002-03SIGNAL DATACONVERTER

CCCC COND COND

661001490516852A

116555316123211825050-1-001AUTOMAT 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 COMPONENTS5/1202-Dec-2015

00

156001081924402C15J21038

B496-00516 0103870209-06051-043TAIL PYLON FITTING RCRC20000

161501450483405A01A9598

015152-01096 0449870103-08112-047HUB, M/R ROTOR ASSY RCRC5100

161501374720305A01I BLACK5966

338964017 2352521870102-08200-056MAIN ROTOR SPINDLEASSY

RCRC3100

161501442692605A01I RED10797

A001-01303 2421521870102-08200-069MAIN ROTOR SPINDLEASSY

RCRC8000

161501442692605A01I YELLOW12858


RCRC8000

161501442692605A01I BLUE12016


RCRC8000

161501074515105A01L15948

1515201844 2550449870351-08186-043MAIN ROTOR SHAFTEXTENDER

RCRC14000

161501127738805A01T13000

5395501 4498449870107-08400-046BIFILAR, M/R ROTORASSY

RCRC13000

161501106190305A02 BLUE11807

A007-09695 3011521870150-09100-043MAIN ROTOR BLADEASSY

RCRC9600

161501106190305A02 RED11372

A00704620 3446521870150-09100-043MAIN ROTOR BLADEASSY

RCRC9600

161501106190305A02 BLACK12099


RCRC9600

161501106190305A02 YELLOW13239


RCRC9600

161501113818805B02 BLU / BLK13225

A00901798 1993521870101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501113818805B02 RED/YELLO11338

A00902055 3880521870101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501083681206G01B13425

33339-7 75150070102-11101-042O/B RETENTION PLATE(T/R)

RCRC12000

156001129125607A24 ROLL17498

C112-01684 991449870410-02500-049SAS ACTUATOR RCRC13000

156001129125607A24 PITCH17858


156001129125607A24 YAW18218


165001305695411C2515136

C300-04314 224436070410-06520-046SERVO ASSY, TAILROTOR

RCRC11000

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

EDITION MAY 67 IS OBSOLETE

AIRCRAFT COMPONENT HISTORICALRECORD

DA FORM 2408-16-E, OCT 91









Report Date:


00

165001143122611D01 FWD28073

B303-12198 8254498274000-1031MAIN ROTOR PRIMARYSERVO

RCRC24400

165001143122611D01 LAT28483

B30311210B 7324815274000-1031MAIN ROTOR PRIMARYSERVO

RCRC24400

165001143122611D01 AFT25688

B30307861B 2896418470410-02820-054MAIN ROTOR PRIMARYSERVO

RCRC24400

156001158968511D0414535

C346-02876 2963449870400-08102-045AFT BELLCRANK RCRC13000

156001164416111D0521498

A391-01970 0449870400-08112-045AFT TIE ROD SUPTFITTING

RCRC17000

168001164416011D066698

MM00400 0449870400-08111-042AFT TIE ROD ASSY RCRC2200

156001286887011D07 AFT9258

39002391 0485870400-08117-049AFT BELLCRANK SPTASSY

RCRC4400

304001287243811D0815858

1515202692 0485870400-08151-061LATERAL SWASHPLATELINK

RCRC11000

161501158965811D097735

A28900489 2263449870400-08150-045LATERAL SERVOBELLCRANK

RCRC5500

168001158965311D1112535

346-0250 2963449870400-08104-048AFT WALKING BEAM RCRC11000

156001289269711D1318498

34402204 0449870400-08115-046LEFT TIE ROD RCRC14000

156001296948611D147380

288-0802-178 618449870400-08114-051RIGHT TIE ROD ASSY RCRC3500

168001158965211D1519858

1033 0485870400-08101-046FORWARD BELLCRANK RCRC15000

156001221261911D169491

B367-03750 607449870400-08162-042FWD BELLCRANK SPTASSY

RCRC5600

SIGNIFICANT HISTORICAL EVENTS7.













Report Date:


00





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 8423935 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 8 of 12

02-Dec-2015

999999

COND

156001095713502C12D

34243424TAIL CONE FITTING UNK393570219-05001-042 CCCC

20000 21038

156001081924402C15J

01038TAIL PYLON FITTING B496-0051670209-06051-043 RCRC

999999

COND

162001231183103A01

59733889FWD FIXED GEARSHOCK

C001-0003670250-12051-045 CCCC

999999

COND

1620012311831 LEFT03A01


C001-0218970250-12051-045 CCCC

999999

COND

1620014210890 TAIL03B01

34504498SHOCK ABSORBER(TAIL)

22670250-13101-044 CCCC

5100 9598

161501450483405A01A

04498HUB, M/R ROTOR ASSY 015152-0109670103-08112-047 RCRC

3100 5966

1615013747203 BLACK05A01I

23525218MAIN ROTOR SPINDLEASSY

33896401770102-08200-056 RCRC

8000 10797

1615014426926 RED05A01I


A001-0130370102-08200-069 RCRC

8000 12858

1615014426926 YELLOW05A01I


A001-0570270102-08200-069 RCRC

8000 12016

1615014426926 BLUE05A01I


A001-0888670102-08200-069 RCRC

14000 15948

161501074515105A01L

25504498MAIN ROTOR SHAFTEXTENDER

151520184470351-08186-043 RCRC

13000 13000

161501127738805A01T

44984498BIFILAR, M/R ROTORASSY

539550170107-08400-046 RCRC

999999

COND

1650012853024 RED05A01Z

13454862DAMPER ASSY, M/R A1060368770106-08100-046 CCCC

999999

COND

1650012853024 YELLOW05A01Z

5944498DAMPER ASSY, M/R R106-0120770106-08100-046 CCCC

999999

COND

1650012853024 BLUE05A01Z


999999

COND

1650012853024 BLACK05A01Z


9600 11807

1615011061903 BLUE05A02

30115218MAIN ROTOR BLADEASSY

A007-0969570150-09100-043 RCRC

9600 11372

1615011061903 RED05A02


A0070462070150-09100-043 RCRC

9600 12099

1615011061903 BLACK05A02


A0071047070150-09100-043 RCRC

9600 13239

1615011061903 YELLOW05A02


A0071408770150-09100-043 RCRC

999999

COND

5315015374652 BLUE LAG05A02H

04369SOLID BLADE PIN B9411262470103-08108-041 CCCC

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

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


HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 9 of 12

02-Dec-2015

999999

COND

5315015374652 RED LAG05A02H


999999

COND

5315015374652 BLUE LEAD05A02H


999999

COND

5315015374652 BLACK LEAD05A02H


999999

COND

5315015374652 RED LEAD05A02H


999999

COND

5315015374652 YELLOW LAG05A02H


999999

COND

5315015374652 YELLOW LEAD05A02H


999999

COND

5315015374652 BLACK LAG05A02H


999999

COND

161501106191805A03A

48034498SWASHPLATE ASSY A1070025570104-08000-046 CCCC

10000 13225

1615011138188 BLU / BLK05B02

19935218TAIL ROTOR BLADEASSY

A0090179870101-31000-043 RCRC

10000 11338

1615011138188 RED/YELLO05B02

38805218TAIL ROTOR BLADEASSY

A0090205570101-31000-043 RCRC

999999

COND

1615010785718 206A11

30814498ACCESSORY MODULE A258-0009470351-08080-043 CCCC

999999

COND

1615013838992 106A11

4784498ACCESSORY MODULE A258-0694370351-08080-045 CCCC

999999

COND

161501503311506A

33315472MAIN TRANSMISSIONMODULE

A2650112970351-08100-076 CCCC

999999

COND

1615013533825 106E

27764498INPUT MODULE 41534170351-08001-049 CCCC

999999

COND

1615013533825 206E

42124498INPUT MODULE A2640020470351-08001-049 CCCC

999999

COND

168001074515206F

44164498INTERMEDIATEGEARBOX

A005-0212370357-06300-042 CCCC

999999

COND

161501376508906G01

42184498TAIL ROTOR GEARBOXASSY

A006-0131270358-06600-046 CCCC

12000 13425

161501083681206G01B

751500O/B RETENTION PLATE(T/R)

33339-770102-11101-042 RCRC

999999

COND

1615015247805 106H04

6745333DRIVESHAFT ASSYENGINE

C8450193770361-08014-041 CCCC

999999

COND

1615015247805 206H04

05218DRIVESHAFT ASSYENGINE

C8451008970361-08014-041 CCCC

999999

COND

161501081277506H06

00SHAFT ASSY, T/R DRVSEC 1

A271-0067070361-03001-045 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 10 of 12

02-Dec-2015

999999

COND

1615011589517 SEC II06H08


WG10897-0018370361-03009-047 CCCC

999999

COND

1615011589522 FWD06H09

04369SHAFT ASSY, T/R SEC3,4,5

WG30024-0042570361-05001-051 CCCC

999999

COND

1615011589522 CENTER06H09


WG30024-0074670361-05001-051 CCCC

999999

COND

1615011589522 AFT06H09


WG30049-0036670361-05001-051 CCCC

999999

COND

161501083295306H11


A273-0187270361-05002-045 CCCC

999999

COND

161501158578806H12


A274-0062970361-06002-047 CCCC

2520 7018

414101329342806H23

26594498FAN AXIAL 5840296SB70361-03005-107 03

999999

COND

4320012077228 107A01

524738PUMP MODULE ASSY,HYDRAUL

239089ABR53023-06 CCCC

999999

COND

4320012077228 #207A01


K0908ABR53023-06 CCCC

999999

COND

432001207722807A01


20892270652-02300-050 CCCC

13000 17498

1560011291256 ROLL07A24

9914498SAS ACTUATOR C112-0168470410-02500-049 RCRC

13000 17858

1560011291256 PITCH07A24


13000 18218

1560011291256 YAW07A24


999999

COND

481001102247307B05A

04858VALVE, SOLENIOD 117803213850-3-1 CCCC

999999

COND

481001102247307B05A

04858VALVE, SOLENIOD 142713213850-3-1 CCCC

999999

COND

165001084309607B11

8224140ACCUMULATOR 8441170A70651-03201-102 CCCC

999999

COND

1680010842256 CP08B20

38713778PANEL INDICATOR (PDU) 123470450-01043-111 CCCC

999999

COND

1680013420496 PILOT08B20

03318PANEL INDICATOR (PDU) 337070450-01043-124 CCCC

999999

COND

6115011149696 109A01

6824498GENERATOR 3210E28B302-8-DM CCCC

999999

COND

6115011149696 209A01

4924498GENERATOR 35-A241828B302-8-DM CCCC

999999

COND

161501260074911C21

05332MIXER ASSEMBLY TMD04643749170400-02300-046 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 11 of 12

02-Dec-2015

2160 6296

161501141753211C23

04136TAIL ROTOR PITCHCHANGE SHAFT

2330434070400-06100-042 00

11000 15136

165001305695411C25

2244360SERVO ASSY, TAILROTOR

C300-0431470410-06520-046 RCRC

24400 28073

1650011431226 FWD11D01

8254498MAIN ROTOR PRIMARYSERVO

B303-12198274000-1031 RCRC

24400 28483

1650011431226 LAT11D01


B30311210B274000-1031 RCRC

24400 25688

1650011431226 AFT11D01


B30307861B70410-02820-054 RCRC

13000 14535

156001158968511D04

29634498AFT BELLCRANK C346-0287670400-08102-045 RCRC

17000 21498

156001164416111D05

04498AFT TIE ROD SUPTFITTING

A391-0197070400-08112-045 RCRC

2200 6698

168001164416011D06

04498AFT TIE ROD ASSY MM0040070400-08111-042 RCRC

4400 9258

1560012868870 AFT11D07

04858AFT BELLCRANK SPTASSY

3900239170400-08117-049 RCRC

11000 15858

304001287243811D08

04858LATERAL SWASHPLATELINK

151520269270400-08151-061 RCRC

5500 7735

161501158965811D09

22634498LATERAL SERVOBELLCRANK

A2890048970400-08150-045 RCRC

11000 12535

168001158965311D11

29634498AFT WALKING BEAM 346-025070400-08104-048 RCRC

14000 18498

156001289269711D13

04498LEFT TIE ROD 3440220470400-08115-046 RCRC

3500 7380

156001296948611D14

6184498RIGHT TIE ROD ASSY 288-0802-17870400-08114-051 RCRC

15000 19858

168001158965211D15

04858FORWARD BELLCRANK 103370400-08101-046 RCRC

5600 9491

156001221261911D16

6074498FWD BELLCRANK SPTASSY

B367-0375070400-08162-042 RCRC

99999 COND

156001136211711D17

00SERVO BEAM RAILING UNK3935#170209-22103-050 CCCC

99999 COND

156001136211711D17


99999 COND

156001136211711D17


99999 COND

156001136211711D17


999999

COND

1680012612044 UPPER11D25

5994328STABILATOR ACTUATOR 1186DL2155M20 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 12 of 12

02-Dec-2015

999999

COND

1680012612044 LOWER11D25

5964328STABILATOR ACTUATOR 1397DL2155M20 CCCC

999999

COND

5996013162743 111D26

23764498STABILATOR AMPLIFIER 237970902-02001-048 CCCC

999999

COND

599601316274311D26

32655473STABILATOR AMPLIFIER 298670902-02001-048 CCCC

999999

COND

2995011695291 0115A04

18203467ENGINE SEQUENCINGUNIT

7584-0467163290-100 CCCC

999999

COND

599601415867319D01A

04372AMPLIFIER, RADIOFREQUENCY

671AA822-0787-001 CCCC

999999

COND

NSN PENDING19E04B

1115561SIGNAL DATACONVERTER

2678P320A002-03 CCCC

999999

COND

661001490516852A

11655531AUTOMAT FLT CONTCOMPUTER

6123211825050-1-001 CCCC

7. SIGNIFICANT HISTORICAL DATA




HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 C001-00036 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

02-Dec-2015

9000 9000

NSN PENDING R/H03A01A

76557655PISTON MAIN L/GEARSTR

C001-0036-15335-0170250-12065-102 RCRC


