Report Date: 20-Jun-2016 1/23 - GSA Auctions · mwo:uh-60-94-asam-08 prioritymnt level 12-apr-1994 m o qc000000 ... ks. 67401 (xd8508) all h-60 aircraft, initial and recurring inspection

PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN

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

ACCUMULATOR 80234554724A1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Report Date: 1/2320-Jun-2016

08-Dec-2003 DM

DT66160513-Jan-2014

0.5AECOMACCUMULATOR OVERHAUL1-1650-376MWO:

Priority Mnt Level

01-Mar-2004 DR

0RECAPPEDDMWR 1-1650-376-1MWO:

Priority Mnt Level

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

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

PIDMWODATE HRS



PUMP MODULE ASSY, HYDRAUL 80234557600290ABR1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


27-Oct-2007 DR

JO57442012-Dec-2007

54CCADMU8551

RECAPPEDDMWR 1-4320-271MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 8023455A001-013761. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


08-Mar-1994 OM

QC00000013-Feb-1995

1CCAD (GP9820)ALL H-60 AIRCRAFT, THIS IS AREVISION TO UH-60-94-ASAM-07

UH-60-94-ASAM-08MWO:

Priority Mnt Level

12-Apr-1994 OM

QC00000013-Feb-1995

2CCAD (GP9820)ALL UH-60 ARMY AIRCRAFT, THIS ISA REVISION TO (UH-60-94-ASAM-03),ONE TIME REFURBISHMENT OFMAIN ROTOR SPINDLE, ANDREPLACEMENT OF CERTAIN MAINROTOR THRUST BEARINGS


Priority Mnt Level

07-Dec-1998 OM

QC00000014-Dec-1998

1AASF LINCOLN,NE (XF3938)

ALL H-60 SERIES AIRCRAFT, ONETIME INSPECTION OF THE MAINROTOR SPINDLE BEARINGASSEMBLY - P/N 70102-08100-044/056, FOR THE EXISTENCE OFSLEEVE BEARING - P/N SB5203-202


Priority Mnt Level

11-Jul-2000 OT

QC00000013-Jul-2000

1AASF #2 SALINA,KS. 67401(XD8508)

ALL H-60 AIRCRAFT, INITIAL ANDRECURRING INSPECTION OF MAINROTOR SPINDLE LUGS

UH-60-00-01MWO:

Priority Mnt Level

05-Mar-2001 FT

QC00000010-Apr-2001

2MOAVCRAD(MP4604)

ALL H-60 AIRCRAFT, REVISION TOUH-60-00-01 INSPECTION OF MAINROTOR SPINDLE

UH-60-01-05MWO:

Priority Mnt Level

26-Mar-2002 OM

QC00000009-Apr-2002


ALL H-60 SERIES AIRCRAFT,REMOVAL OF CHICAGO RAWHIDEM/R SPINDLE THRUST BEARINGSWITH SERIAL NUMBERS C325-00001THROUGH C325-02407


Priority Mnt Level

05-Sep-2012 FM

BB50010703-Apr-2013

0.3D CO 6/101STGSAB

ALL H-60 SERIES AIRCRAFT, MAINROTOR SPINDLE SUB-COMPONENTTRACKING REQUIREMENTS

H-60-12-AMAM-16MWO:

Priority Mnt Level

27-Feb-2013 OU

BB50010703-Apr-2013

0.3D CO 6/101STGSAB

Complied with one-time inspection forsuspect Anti-Flap Bracket Assemblies.

H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS





08-Mar-1994 OM

QC00000013-Feb-1995



Priority Mnt Level

12-Apr-1994 OM

QC00000013-Feb-1995



Priority Mnt Level

07-Dec-1998 OM

QC00000014-Dec-1998




Priority Mnt Level

11-Jul-2000 OT

QC00000013-Jul-2000



UH-60-00-01MWO:

Priority Mnt Level

05-Mar-2001 FT

QC00000010-Apr-2001

2MOAVCRAD(MP4604)


UH-60-01-05MWO:

Priority Mnt Level

26-Mar-2002 OM

QC00000009-Apr-2002




Priority Mnt Level

05-Sep-2012 FM

BB50010703-Apr-2013

0.3D CO 6/101STGSAB


H-60-12-AMAM-16MWO:

Priority Mnt Level

27-Feb-2013 OU

BB50010703-Apr-2013

0.3D CO 6/101STGSAB


H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS





08-Mar-1994 OM

QC00000013-Feb-1995



Priority Mnt Level

12-Apr-1994 OM

QC00000013-Feb-1995



Priority Mnt Level

07-Dec-1998 OM

QC00000014-Dec-1998




Priority Mnt Level

11-Jul-2000 OT

QC00000013-Jul-2000



UH-60-00-01MWO:

Priority Mnt Level

05-Mar-2001 FT

QC00000010-Apr-2001

4MOAVCRAD(MP4604)


UH-60-01-05MWO:

Priority Mnt Level

26-Mar-2002 OM

QC00000009-Apr-2002




Priority Mnt Level

05-Sep-2012 FM

BB50010703-Apr-2013

0.3D CO 6/101STGSAB


H-60-12-AMAM-16MWO:

Priority Mnt Level

27-Feb-2013 OU

BB50010703-Apr-2013

0.4D CO 6/101STGSAB


H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



INTERMEDIATE GEARBOX 8023455A005010921. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


20-Apr-2003 DM

AB242218-Jan-2011

1CCADINTERMEDIATE GEAR BOXASSEMBLY P/N 70357-06300-042(NSN 1615-01-074-5152)

1-1615-288MWO:

Priority Mnt Level

21-Mar-2013 MM

BB50010722-Mar-2013

0.4D CO 6/101STGSAB

Perform one-time inspection of suspectcomponents for residual PMB materialand/or Oxide Flakes. ALL H-60 SERIESAIRCRAFT, PLASTIC MEDIA BLAST(PMB) AND OXIDE FLAKE RESIDUE,H-60-13-ASAM-04

H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR GEARBOX ASSY 8023455A006-045071. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 FT

BB50010702-Jul-2013

0.3D C0 3-10 GSABPLASTIC BLAST (PMB) AND OXIDEFLAKE RESIDUE

H-60-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR BLADE ASSY 8023455A007019371. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


04-May-2015 FM

RJ52090919-Jun-2015

1AASF#3NYARNG

PERFORM A ONE-TIME VOIDCHECK/INSPECTION (COIN TAP) FORSUSPECT MAIN ROTOR BLADEDEBONDING: COMPLIED WITH.

H-60-15-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS





28-Feb-1998 DU

LM674918-Jul-2011

1CCAD/W0MUAAINCREASE IN FATIGUE LIFE FORTHE MAIN ROTOR BLADE CUFFS,P/N 70150-09109-041 AND 70150-09109-043

UH-60-97-ASAM-11 TB 1-1MWO:

Priority Mnt Level

12-Aug-2002 OT

LM674918-Jul-2011

1CCAD/W0MUAAALL H-60 SERIES AIRCRAFT,REVISION TO UH-60-02-11, ONE-TIMEINSPECTION OF MAIN ROTORBLADE CUFF ASSEMBLY

UH-60-02-12MWO:

Priority Mnt Level

07-Jan-2003 DU

LM674918-Jul-2011

1CCAD/W0MUAAONE TIME INSPETION OF M/R BLADECUFF ASSY.

UH-60-03-12MWO:

Priority Mnt Level

15-Sep-2005 DR

LM674918-Jul-2011

130CCAD/W0MUAARECAP REQUIREMENTS FOR UH-60MAIN ROTOR BLADE P/N: 70150-09100-043 NSN: 1615-01-106-1903

DMWR 1-1615-281 C1MWO:

Priority Mnt Level

15-Apr-2010 OT

LM674918-Jul-2011

3CCAD/W0MUAAALL H-60A/K/L SERIES AIRCRAFT,DEPOT REPAIRED LEGACY MAINROTOR BLADES

H-60-10-SOF-01MWO:

Priority Mnt Level

04-May-2015 FM

RJ52090919-Jun-2015

1AASF#3NYARNG


H-60-15-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS





15-Sep-2005 DO

MF203428-Jun-2013

130CCAD/W0MUAARECAP REQUIREMENTS FOR THEUH-60 MAIN ROTOR BLADE P/N:70150-09100-043 NSN: 1615-01-106-1903

DMWR 1-1615-281 C1MWO:

Priority Mnt Level

09-Apr-2012 OT

MF203428-Jun-2013

1CCAD/W0MUAACHANGE TO DEPOT REPAIREDLEGACY MAIN ROTOR BLADESCOMPLIANCE DATE

H-60-12-SOF-05MWO:

Priority Mnt Level

04-May-2015 FM

RJ52090919-Jun-2015

1AASF#3NYARNG


H-60-15-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS





04-May-2015 FM

RJ52090919-Jun-2015

1AASF#3NYARNG


H-60-15-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR BLADE ASSY 8023455A009056511. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


14-Nov-2001 OM

DT66160513-Jan-2014

0.5AECOMINITIAL AND RECURRINGINSPECTION OF THE TAIL ROTORFAIRING ASSEMBLY, ALL H-60AIRCRAFT.

1-1520-237-20-239 (UH-60-MWO:

Priority Mnt Level

14-Nov-2001 OM

RS100511-Jun-2013

1CCAD / W0MUAAINITIAL AND RECURRINGINSPECTION OF THE TAIL ROTORFAIRING ASSEMBLY

UH-60-O2-ASAM-01 TB1-1MWO:

Priority Mnt Level

15-Sep-2005 DR

DT66160513-Jan-2014

0.5AECOMRECAPPED1-1615-281MWO:

Priority Mnt Level

15-Sep-2005 DR

RS100522-Jun-2013

151CCAD / W0MUAARECAPPEDDMWR 1-1615-287 C1MWO:

Priority Mnt Level

24-Jan-2013 FN

RB86798020-Dec-2013

8AECOMAIRWORTHINESS RELEASE (AWR)FOR UH/HH-60A/L/M HELICOPTERSEQUIPPED WITH THE NEW DESIGNDE-ICE CONNECTOR (AWR 1692)

AWR 1692 R5MWO:

Priority Mnt Level



PIDMWODATE HRS





14-Nov-2001 OM

RS100520-Sep-2013



Priority Mnt Level

15-Sep-2005 DR

RS100520-Sep-2013


Priority Mnt Level

24-Jan-2013 FN

RB86798020-Dec-2013


AWR 1692 R5MWO:

Priority Mnt Level



PIDMWODATE HRS



INPUT MODULE 8023455A264015331. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


02-Aug-2000 OT

QC00000003-Aug-2000


ALL H-60 SERIES AIRCRAFT,REMOVAL OF INPUT MODULE GEARBOX ASSEMBLIESWITHPOTENTIALLY CRACKED BEVELGEARS

UH-60-00-02MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN TRANSMISSION MODULE 8023455A265-015591. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


29-Apr-2009 DR

AB242203-May-2011

1CCADRECAPITALIZATION REQUIREMENTSDMWR 1-1615-371,C1MWO:

Priority Mnt Level

05-Oct-2009 OM

AB242203-May-2011

1CCADREDESIGNED PLANETARY GEARCARRIER RETIREMENT LIFE

UH-60-10-AMAM-02MWO:

Priority Mnt Level

21-Mar-2013 OM

BB50010722-Mar-2013

0.3D CO 6/101STGSAB

PLASTIC MEDIA BLAST (PMB) ANDOXIDE FLAKE RESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



LATERAL SERVO BELLCRANK 8023455A289004731. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


07-Jan-1997 OM

QC00000012-Feb-1997

1.2AASF #1TOPEKA, KS.(GP9820)

ALL H-60 AIRCRAFT WITH THELATERAL BELLCRANK ASSEMBLY,P/N 70400-08150-045,MANUFACTURED BY PURDYMACHINE COMPANY (CAGE CODE15152)


Priority Mnt Level

05-Jan-2001 OT

QC00000005-Jan-2001

1AASF #2 SALINA,KS (XS9537)

H-60 SERIES AIRCRAFT, REMOVALOF LATERAL SERVO BELLCRANKASSEMBLY MANUFACTURED BY THEPURDY MACHINE COMPANY, CAGECODE 15152

UH-60-01-03MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR SERVO ASSY 8023455B300-010411. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


18-Oct-2010 MM

18-Oct-20101AAFAH-60-11-ASAM-02 one-time inspection

of TR Servo for Cotter Pin installation.H-60-11-ASAM-02MWO:

Priority Mnt Level



PIDMWODATE HRS



FAN AXIAL 8023455B512-0926SB1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


03-Dec-2001 FR

MU855118-Oct-2007

22CCADRECAPDMWR 1-4140-228MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 8023455D001-014121. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 FM

BB50010703-Apr-2013

0.3D CO 6/101STGSAB


H-60-12-AMAM-16MWO:

Priority Mnt Level

27-Feb-2013 OU

BB50010703-Apr-2013

0.3D CO 6//101STGSAB


H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



ENGINE ASSY, TURBINE 8023455GE-E-2075351. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Oct-2008 OM

TC02154323-Sep-2008

1HAATSALL H-60 SERIES AIRCRAFT, ONETIME VISUAL INSPECTION OF BLUE,YELLOW, AND GREEN CABLEASSEMBLIES FOR SUSPECT ENGINEHARNESSES.

H-60-08-ASAM-14MWO:

Priority Mnt Level

12-Jan-2009 OM

TC02154305-Feb-2009

0.1HAATST701C GAS GENERATOR (GG)ROTOR ASSEMBLIES


Priority Mnt Level

01-Oct-2009 FT

GG60669201-Oct-2009

0.5AASF#1JACKSON,MS

ALL H-60A SERIES AIRCRAFT,HAMILTON SUNSTRAND HYDROMECHANICAL UNITS,

H-60-10-ASAM-01MWO:

Priority Mnt Level

12-Sep-2012 FM

PL54424611-Sep-2012

0.3AASF#1 FTIG,PAH-60A SERIES AIRCRAFT, ENGINEANTI-ICE/START BLEED VALVE

H-60-12-ASAM-10MWO:

Priority Mnt Level

30-Jul-2014 FM

AT56275412-Aug-2014

0.1ASSF-1 FTIGANNVILLE,PA17003

ALL H-60 (EXCEPT MH-60K/M) ANDAH-64 SERIES AIRCRAFT, HYDRO-MECHANICAL UNIT QUICKDISCONNECT PINS

H-60-14-ASAM-08MWO:

Priority Mnt Level



PIDMWODATE HRS



ENGINE ASSY, TURBINE 8023455GEE3061991. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


31-Dec-1986 DM

MB254123-Jun-2009

20W0MUAAMOD OF PTO BEVEL GEAR SHAFTMWO 1-2840-248-50-27MWO:

Priority Mnt Level

19-Dec-1988 DN

MB254123-Jun-2009

1W0MUAASELF-SEAL ADAPTER ASSY.MWO 55-2840-248-50-28MWO:

Priority Mnt Level

31-Jul-1989 OM

MB254123-Jun-2009

33W0MUAAMODIFICATION OF GG ROTORASSEMBLY T700/701 REWORK T700ENGINES

55-2840-248-50-32MWO:

Priority Mnt Level

01-Jul-1992 DM

MB254123-Jun-2009

1W0MUAAINSTALLATION OF PTO DRIVE ASSYMWO 55-2840-248-50-29MWO:

Priority Mnt Level

30-Jun-1994 DM

MB254123-Jun-2009

1W0MUAAONETIME INSPECT/CONVERSION OFFORMS AND RECORDS T700/701/701C ENGINES

TB 1-2840-248-20-2MWO:

Priority Mnt Level

15-Dec-1998 OU

MB254123-Jun-2009

1W0MUAANEW LIFE LIMITS ON G.G. ROTORAND COMPONENTS

1-2840-248-20-22/UH-60-99MWO:

Priority Mnt Level

21-Oct-2008 OM

MB254123-Jun-2009

1W0MUAAALL H-60 SERIES AIRCRAFT, ONETIME VISUAL INSPECTION OF BLUE,YELLOW, AND GREEN CABLEASSEMBLIES FOR SUSPECT ENGINEHARNESSES.

H-60-08-ASAM-14MWO:

Priority Mnt Level

01-Oct-2009 TT

MD66356631-Mar-2010

1WPJN99H-60-10-ASAM-01: HAMILTON-SUNDSTRAND HYDRO-MECHANICALUNITS FOR SUSPECT PN:4046T52G06,4046T52G09,4046T52G11

H-60-10-AMAM-01MWO:

Priority Mnt Level

12-Sep-2012 FM

PL54424611-Sep-2012

0.3AASF#1 FTIG, PAH-60A SERIES AIRCRAFT, ENGINEANTI-ICE/START BLEED VALVE

H-60-12-ASAM-10MWO:

Priority Mnt Level

30-Jul-2014 FM

AT56275412-Aug-2014

0.1AASF-1ANNVILLE, PA17003

ALL H-60 (EXCEPT MH-60K/M) ANDAH-64 SERIES AIRCRAFT, HYDRO-MECHANICAL UNIT QUICKDISCONNECT PINS

H-60-14-ASAM-08MWO:

Priority Mnt Level



PIDMWODATE HRS



PUMP MODULE ASSY, HYDRAUL 8023455K3233ABR1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


29-Jul-2005 DR

SS090703-Dec-2011

54CCAD, CORPUSCHRISTI TX

RECAPPED DMWR 1-4320-271MWO:

Priority Mnt Level



PIDMWODATE HRS



AUXILIARY POWER UNIT 8023455SP-E0511511. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


06-Nov-2003 DR

QC00000006-Jun-2006

8UNKNOWN(LATE ENTRY)

INLET BARRIER FILTER SYSTEM1-1520-237-50-APU IBFMWO:

Priority Mnt Level



NUMBERLOCATIONPIDENTRYORGANIZATION

8.7.DATE

6.REMARKS

4. 5.

UH-60A 8023455HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL

Report Date: Page 1 of 4123-Jun-2016

SIKORSKY ACFTA/C MAIN ROTOR HEAD RIGGED IAW SA DWG70400-00003 REV B SYS CTRLS HAVE BIASEDIAW: A) LATERAL CTRL SERVO INPUT RODP/N 70400-02258-046 SHORTENED 1/4 TURN; B)RET CTRL SERVO INPUT ROD P/N 70400-02258-045 LENGTHENED 5/8 TURN; C) FRWRD CTRLSERVO INPUT ROD P/N 70400-02258-047SHORTENED 5/8 TURN. NOTE: A/C RIGGING ISBIASED RIGGING PIN HOLES ARETEMPORARILY LOST AT THE ABOVE POINTS(NO PID)

21-Oct-1981 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-81-27 OUTPUT DRIVE SHAFTSINSP C/W (NO PID)

02-Nov-1981 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-81-30 INSP OF DE SWIRL DUCTCLAMPS C/W (NO PID)

10-Dec-1981 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-82-06 ONE-TIME INSPECTION OFPILOTS AND COPILOTS SEAT RUBBING BARC/W (NO PID)

04-May-1982 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-82-11 (TB 55-1520-237-20-32) ONE-TIME INSPECTION OF M/R SERVO SCREW C/W(NO PID)

18-Aug-1982 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-82-13 (TB 55-1520-237-20-30) ONE-TIME INSPECTION OF M/R SERVO INPUT LINKBEARINGS C/W (NO PID)

18-Aug-1982 2

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-82-17 (TB 55-1520-237-20-31) NAS-625HF BOLTS ON THE T/R SERVO REPLACEDC/W (NO PID)

16-Sep-1982 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-82-16 (TB 55-1520-237-20-34) ONE-TIME INSPECTION OF MIXER LIMITERBEARING AND MIXER LIMITER ROLLER C/W(NO PID)

22-Sep-1982 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVTB 55-1520-237-20-35) ONE-TIME INSPECTIONOF YAW TRIM AND ROLL SERVOS C/W (NOPID)

22-Oct-1982 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-82-22 (TB 55-1520-237-20-37) ONE-TIME INSP OF UPPER CARGO DOOR TRACKSC/W (NO PID)

28-Dec-1982 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVTB 55-1520-237-20-28 N/A THIS ACFT (NO PID) 29-Mar-1983 1

FT. BRAGG N.C. 28307-5000


FT. BRAGG N.C. 28307-5000


FT. BRAGG N.C. 28307-5000

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


8.7.DATE

6.REMARKS

4. 5.



B TRP 1/17 CAVTB 55-1520-237-20-40 ONE TIME INSP OF FLTCONTROLS C/W (NO PID)

30-Mar-1983 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVTB 55-1520-237-30-01 ONE-TIME INSP OF INLETDUCTS C/W (NO PID)

18-Apr-1983 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVUH-60A-83-10 (TB 55-1520-237-20-44)WASHERSCHANGED ON COLLECTIVE BIAS TUBE C/W(NO PID)

25-Oct-1983 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVUH-60A-83-09 (TB 55-1520-237-20-43)INSPECTION OF STAB AMP C/W (NO PID)

25-Oct-1983 2

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVMIM UH-60A-MEA-83-16 REPLACEMENT OFANTIFLAP PIN C/WFT C/W (NO PID)

11-Jan-1984 1

FT. BRAGG N.C. 28307-5000

SIKORSKY AIRCRAFTTB 55-1520-237-50-1 ONE TIME INSPECTION OFM/R SHAFT C/W (NO PID)

30-Jan-1984 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVACFT SUBJECTED TO SALT WATERENVIRONMENT IN GRENADA, W.I. 26 OCT 85 -22 NOV 83 (NO PID)

09-Feb-1984 1

FT. BRAGG N.C. 28307-5000

OCM SEC TSARCOMOCM/ACE PERFORMED AT 0496 A/C HOURS(NO PID)

21-Feb-1984 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-83-12 (TB 55-1520-237-20-46) ONE-TIME INSP OF T/R SERVO C/W (NO PID)

22-Feb-1984 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-84-02 (TB 55-1520-237-20-48) ONE-TIME INSP OF L/H RELAY PANEL WIRES C/W(NO PID)

30-Mar-1984 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-84-03 (TB 55-1520-237-20-49) ONE-TIME INSP OF TAIL PYLON, FOUND CRACKS INSTA 160, C/W (NO PID)

19-Apr-1984 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-84-08 (TB 55-1520-237-20-50) ONE-TIME INSP OF CARGO HOOKS SQUIB C/W (NOPID)

04-Jun-1984 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-84-11 (TB 55-1520-237-20-56) INSPOF STATIONARY SWASHPLATE LINK C/W (NOPID)

10-Jul-1984 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-84-07 (TB 55-1520-237-20-53) INSPOF ENG OUTPUT SHAFTS FOR 06 BOLTS C/W(NO PID)

10-Jul-1984 2

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-84-04 (TB 55-1520-237-50-02) ONE-TIME INSP OF STABILATOR AMPS C/W (NOPID)

10-Jul-1984 3

FT. BRAGG N.C. 28307-5000



8.7.DATE

6.REMARKS

4. 5.



B TRP 1/17 CAVSOF UH-60A-84-06 (TB 55-1520-237-20-52) ONE-TIME INSP OF T/R G.B.OR AMPS C/W (NO PID)

10-Jul-1984 4

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-84-12 (TB 55-1520-237-20-55) INSPM/R SPINDLE (NO PID)

31-Jul-1984 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-84-10 (TB 55-1520-237-20-54) INSPTAIL PYLON RADIUS BLOCK (NO PID)

30-Aug-1984 1

FT. BRAGG N.C. 28307-5000

OCM SEC AVSCOMOCM/ACE PERFORMED AT 624 A/C HRS (NOPID)

06-Nov-1984 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF MSG UH-60A-84-16 CK OF ENGINEOPERATING HIS C/W (NO PID)

19-Dec-1984 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF MSG UH-60A-84-13 (TB 55-1520-237-20-57)INSP/ REPLACE T.R. TURNBUCKLE C/W (NOPID)

02-Jan-1985 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF MSG UH-60A-84-14 (TB 55-1520-237-20-58)INSP OF T.R. CABLES C/W (NO PID)

02-Jan-1985 2

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF MSG UH-60A-84-17 (TB 55-1520-237-20-59)INSP OF XMSN DOWEL PIN C/W (NO PID)

02-Jan-1985 3

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF MSG UH-60A-85-02 REMOVE TAPE FROMROTER TACH C/W (NO PID)

26-Feb-1985 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF MSG UH-60A-85-06 (TB 55-1520-237-20-61)INSP OF PRIMARY SERVOS C/W (NO PID)

12-Mar-1985 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF MSG UH-60A-85-07 INSP OF FLIGHTCONTOLS C/W (NO PID)

06-Apr-1985 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF MSG UH-60A-85-14 (TB 55-1520-237-20-63)C/W (NO PID)

10-Jul-1985 1

FT. BRAGG N.C. 28307-5000


10-Jul-1985 2

FT. BRAGG N.C. 28307-5000


10-Jul-1985 3

FT. BRAGG N.C. 28307-5000


10-Jul-1985 4

FT. BRAGG N.C. 28307-5000



8.7.DATE

6.REMARKS

4. 5.



B TRP 1/17 CAVSOF MSG UH-60A-85-23 (TB 55-1520-237-20-71)ONE- TIME INSP OF T/R D/S BRNGS C/W (NOPID)

26-Jul-1985 1

FT. BRAGG N.C. 28307-5000

AVSCOM OCMSECOCM/ACE PERFORMED AT 997 HOURS (NOPID)

01-Aug-1985 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF MSG UH-60A-85-24 (TB 55-1520-237-20-72)SUPPLEMENT TO T/R D/S BRNGS C/W (NO PID)

07-Aug-1985 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF MSG UH-60A-85-25 (TB 55-1520-237-20-73)RETORQUE OF M/R SPINDLE HORN BOLTSC/W (NO PID)

01-Nov-1985 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSTRUCT ASSY LOWER FUSELAGE STA 449.0B.L. 45, SKIN DAMAGE REPAIRED IAW TM 55-1500-204-25/1 (NO PID)

07-Feb-1986 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-86-02 (TB 55-1520-237-20-74) T/RFLEX COUPLING BOLTS RETORQUE C/W (NOPID)

05-Mar-1986 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-86-07 (TB 55-1520-237-20-75)UNGROUNDNG REQUIREMENTS C/W (NO PID)

08-May-1986 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-86-06 (MWO 55-1520-237-55-2)A.F.C.S. PANEL MOD N.A. THIS ACFT (NO PID)

08-May-1986 2

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-86-13 REMOVAL OF AN310-8NUTS C/W (NO PID)

06-Aug-1986 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-86-10 (TB 55-1520-237-20-76)STARING OF DIR. CONTROL LEVER BRINGSC/W (NO PID)

08-Aug-1986 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-86-12 (TB 55-1520-237-20-78) YAW& CALL BOOST SERVO S/N CHANGE OUT C/W(NO PID)

08-Aug-1986 2

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-86-17 (TB 55-1520-237-20-82) INSPOF XMSN OIL COOLER SPLINES N/A TO THISACFT (NO PID)

25-Oct-1986 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-86-19 (TB 55-1520-237-20-83) INSPOF EYEBOLT PN 70209-02136-102 N/A TO THISACFT (NO PID)

07-Nov-1986 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-86-20 (TB 55-1520-237-20-84) INSPOF 1ST THREE DRIVESHAFT SPLINES &REMOVAL OF EQUIPMT FROM UNDER CREWSEATS C/W NO CORROSION ON FITTINGNOTED (NO PID)

13-Nov-1986 1

FT. BRAGG N.C. 28307-5000

B TRP 1/17 CAVSOF UH-60A-86-21 (TB 55-1520-237-20-85) INSPOF ARA CREW SEATS N/A TO THIS AIRCRAFT.NORTON SEATS INSTALLED (NO PID)

10-Dec-1986 1

FT. BRAGG N.C. 28307-5000



8.7.DATE

6.REMARKS

4. 5.



AVSCOM OCMSECOCM/ACE PERFORMED AT 787 A/C HOURS(NO PID)

20-Feb-1987 1

FT. BRAGG N.C. 28307-5000

1/17 CAVSOF UH-60A-87-03 ONE-TIME AND RECURRINGINSPECTION ON FIRST THREE TAIL ROTORDRIVE SHAFT SPLINE CPLG (NO PID)

16-Mar-1987 1

FT. BRAGG N.C. 28307-5000

1/17 CAVSOF UH-60A-87-04 REVISION TO INSPECTIONON AIRFRAM EYEBOLTS LOGGED ON DAFOUR 2408-18 UNTIL NEW BOLTS AREINSTALLED (NO PID)

06-Apr-1987 1

FT. BRAGG N.C. 28307-5000

1/17 CAVSOF UH-60A-87-05 STABILATOROPERATIONAL PROCEDURES ACFTRESTRICTED TO 80 KIAS BELOW 3000 FEETAGL (NO PID)

13-Apr-1987 1

FT. BRAGG N.C. 28307-5000

1/17 CAVSOF UH-60A-87-07 ONE TIME AND RECURRINGINSP OF TWO LONGITUDINAL LINK ASSYSAND ONE LATERAL CLEVIS ASSY FORCRACKED BEARING INNER RACE COUPLERS873.2 ACFT HOURS, ONE CRACK FOUND ONAFT LINK ASSY REPLC DUE 973.2 ACFTHOURS (NO PID)

20-May-1987 1

FT. BRAGG N.C. 28307-5000

82ND AVNSOF UH-60A-87-08 ONE TIME INSP OFMIDSECTION BELLCRANKS C/W AT 873.2ACFT HOURS (NO PID)

08-Jul-1987 1

FT. BRAGG N.C. 28307-5000

82ND AVNSOF GEN 87-02 ONE TIME INSP OFHISTORICAL RECORDS C/W (NO PID)

10-Jul-1987 1

FT. BRAGG N.C. 28307-5000

82ND AVNSOF UH 60-87-10 ONE TIME INSP OF INPUTFLANGE ASSY C/W (NO PID)

15-Oct-1987 1

FT. BRAGG N.C. 28307-5000

82ND AVNSOF UH 60-87-12 ONE TIME INSP OF POWERTURBINE MODULES C/W AT 873 A/C HOURS(NO PID)

07-Dec-1987 1

FT. BRAGG N.C. 28307-5000

AVSCOM OMSECOCM/ACE PERFORMED AT 873.0 ACFT HOURS(NO PID)

20-Jan-1988 1

FT. BRAGG N.C. 28307-5000

I CO 159TH AVNMWO TB 55-1520-237-20-86 APPLIED (NO PID) 22-Jan-1988 1

FT. BRAGG N.C. 28307-5000

82ND AVIATIONSOF UH-60-87-09 C/W MWO 55-1520-239-50-46INSTALL BY LSSI FT. BRAGG N.C. (NO PID)

22-Jan-1988 2

FT. BRAGG N.C. 28307-5000

82ND AVIATIONSOF UH-60A-88-01 INSP OF CERTAIN TAILROTOR BLADE SERIAL NUMBERS NOTAPPLICABLE THIS ACFT (NO PID)

17-Feb-1988 1

FT. BRAGG N.C. 28307-5000

82ND AVIATIONSOF UH-60A-88-02 ONE-TIME INSP OF T/R G/BOUTPUT GEAR COMPLIED WITH. (NO PID)

29-Mar-1988 1

FT. BRAGG N.C. 28307-5000



8.7.DATE

6.REMARKS

4. 5.



ASF 157SOF UH-60A-88-03 EXTENSION OF RC TIMEFOR M/R SHFT C/W AT 893.3 ACFT HRS (NOPID)

13-May-1988 1

FORT RUCKER, AL36362

ASF 157SOF UH-60A-88-04 REVISION OF UH-60-88-02C/W AT 893.3 ACFT HRS (NO PID)

13-May-1988 2


ASF 157SOF UH-60A-88-05 INITIATION OF APU MOATC/W AT 913.0 ACFT HRS (NO PID)

15-Jun-1988 1


ASF 157SOF UH-60A-88-06 OVERHAUL LIFE FOR THEXMSN OIL COOLER BLOWER C/W AT 928.5ACFT HRS (NO PID)

11-Jul-1988 1


ASF 157SOF UH-60A-88-07 REVISION TO SOF UH-60A-88-05 C/W AT 935.0 ACFT HRS (NO PID)

18-Jul-1988 1


ASF 157SOF UH-60A-88-08 REVISION TO SOF UH-60A-88-06 C/W AT 946.7 ACFT HRS (NO PID)

08-Aug-1988 1


ASF 157SOF UH-60A-88-09 ONE-TIME INSP OF ARACREW SEATS C/W AT 946.7 ACFT HRS (NOPID)

08-Aug-1988 2


6/159SOF GEN 88-02 INSP FOR INSTALLATION OFCORRECT PORTABLE FIRE EXTINGUISHERSC/W AT 988.7 ACFT HRS (NO PID)

23-Sep-1988 1


ASF 157SOF GEN 88-03 REVISION TO SOF GEN 88-02INSP FOR CORRECT PORTABLE FIREEXTINGUISHERS C/W AT 993.4 ACFT HOURS(NO PID)

11-Oct-1988 1


ASF 157SOF UH-60-83-11 IMMEDIATE RESTRICTION OFRAPPELLNG OPERATIONS C/W AT 993.4 ACFTHOURS (NO PID)

27-Oct-1988 1


ASF 157SOF UH-60-83-13 ONE-TIME INSP OF M/RBLADE PINS C/W 993.0 ACFT HOURS HOURS(NO PID)

18-Nov-1988 1


ASF 157SOF UH-60-89-01 ONE-TIME INSP OF ALL T-700ENGINES FOR SUSPECT GAS GEN STATORSHROUDS C/W 993.4 ACFT HOURS (NO PID)

15-Feb-1989 1


ASF 157SOF UH-60-89-02 CORRECTION OF SOF UH-60-89-01 C/W AT 993.4 ACFT HOURS (NO PID)

21-Feb-1989 1


AVSCOM OCMSECOCM/ACE PERFORMED AT 993.0 ACFT HOURS(NO PID)

21-Feb-1989 2


ASF 157SOF UH-60-89-03 ONE-TIME INSP OF ALL M/RSPINDLE RETAINING NUTS C/W AT 993.0 ACFTHOURS (NO PID)

03-Apr-1989 1




8.7.DATE

6.REMARKS

4. 5.



ASF 157SOF UH-60-89-04 REVISION TO SOF UH-60-89-03 C/W AT 993.0 ACFT HOURS (NO PID)

03-Apr-1989 2


ASF 157SOF UH-60-89-05 ONE-TIME INSP OF WIRESTRIKE PROTECTION SYSTEM C/W AT 993.4ACFT HOURS (NO PID)

16-Jun-1989 1


ASF 157SOF UH-60-89-06 ONE-TIME INSP OF L/H & R/HRELAY PANELS C/W AT 993.4 ACFT HOURS(NO PID)

18-Jul-1989 1


ASF 157SOF UH-60-89-07 REVISION TO SOF UH-60-89-06 C/W AT 993.4 ACFT HOURS (NO PID)

07-Aug-1989 1


ASF 157SOF UH-60-89-08 ONE-TIME INSP OF FUELBOOST PUMP HOSE ATTACHMENT C/W AT993.4 ACFT HOURS (NO PID)

14-Aug-1989 1


ASF 157SOF UH-60-89-09 CORRECTION OFRETIREMENT LIFE COMPONENT SCHEDULEC/W AT 993.4 ACFT HOURS (NO PID)

17-Aug-1989 1


ASF 157TB 55-1520-237-20-104 NEWOVERHAUL/RETIREMENT LIFE SCHEDULEFOR H-60 RETIREMENT LIFE COMPONENTSC/W AT 993.4 ACFT HOURS (NO PID)

23-Aug-1989 1


ASF 157SOF UH-60-89-10 ONE-TIME INSP OF T700-GE-700 ENG GEN ROTOR AND STATOR SHROUDHISTORICAL RECORDS C/W AT 993.4 ACFTHOURS (NO PID)

20-Sep-1989 1


ASF 157SOF UH-60-89-11 ONE-TIME INSPECTION OFOIL COOLER FAN C/W AT 994 ACFT HOURS(NO PID)

13-Nov-1989 1


ASF 157SOF UH-60-89-12 ONE-TIME INSPECTION OFOIL COOLER AXIAL FAN C/W AT 994 ACFTHOURS (NO PID)

27-Nov-1989 1


ASF 157SOF UH-60-89-13 ACFT RESTRICTED AGAINSTUSING FITTING ASSY P/N 70700-20433-045 FORRAPPELING, PARACHUTING, ANDTRANSPORTABILITY TIEDOWN OPNS (NO PID)

08-Dec-1989 1


ASF 157SOF UH-60-90-01 ONE-TIME AND RECURRINGINSP OF M/R BLD EXP PINS C/W AT 1072.8ACFT HOURS (NO PID)

13-Apr-1990 1


ASF 157TB 55-1520-237-20-111 ONE-TIME INSP OFUPPER PRESS PLATE AND SPINDLE TO HUBATTACHMENT BOLTS C/W AT 1106.3 ACFTHRS (NO PID)

02-Aug-1990 1


ASF 157TB 55-1520-237-20-117 ONE-TIME INSP OFPITCH CNTRL HORNS C/W AT 1106.3 ACFTHOURS (NO PID)

02-Aug-1990 2


ASF 157TB 55-1520-237-20-113 INSPECTION FORDEFECTIVE ROSEMOUNT ICE RATE METERSC/W AT 1106.3 ACFT HOURS (NO PID)

02-Aug-1990 3




8.7.DATE

6.REMARKS

4. 5.



ASF 157SOF UH-60-90-02 ONE-TIME AND RECURRINGINSPECTION OF T/R P/C BEAM RETAININGNUT AND WASHER C/W AT 1106.3 ACFTHOURS (NO PID)

16-Aug-1990 1


ASF 157R/H OUTBOARD SIDE OF PYLON STABILATORMOUNT IS DAMAGED BEYOND LIMITS IAW TM55-1520-237-23-2. AUTHORIZATION TO REPAIRDAMAGED AREA WAS GIVEN TO ASF 157 BYMICHAEL J. MAGER, AVSCOM LOGISTICSASSISTANCE COORDINATOR ON 15 AUG 90(NO PID)

20-Aug-1990 1


ASF 157ASAM UH-60-91-01 ONE-TIME REPLACEMENTAND 30 HR INSP OF T/R P/C BEAM RETAININGNUT WASHER C/W AT 1191 ACFT HOURS (NOPID)

09-Jan-1991 1


ASF 157ASAM UH-60-91-02 N/A FOR THIS ACFT. (NOPID)

09-Jan-1991 2


AVSCOM OCMSEC, STLOUIS, MO

OCM/ACE COMPLETED AT 1197 ACFT HOURS(NO PID)

16-Jan-1991 1


HHC, 6TH BN, 159THAVN REG

ASAM UH-60-91-05 INSP OF M/R SPINDLE S/N'SC/W AT 1247 ACFT HOURS (NO PID)

26-Feb-1991 1


ASF 157ASAM UH-60-91-03 EXTENDED TBO HRS FORDESERT SHIELD OPNS N/A FOR THISAIRCRAFT (NO PID)

11-Apr-1991 1


ASF 157ASAM UH-60-91-06 ONE-TIME INSP OF CAFGOHOOK INTERNAL WIRE BUNDLE ROUTING C/WAT 1275.7 A/C HRS (NO PID)

11-Apr-1991 2


ASF 157ASAM UH-60-91-07 ADVANCE NOTIFICATIONOF MANUAL CHANGE FOR MAINTRANSMISSION MODULE C/W AT 1275.7 ACFTHOURS (NO PID)

11-Apr-1991 3


ASF 157ASAM UH-60-91-08 ONE-TIME INSP OF FIREEXTINGUISHR SYSTEM C/W 1275.7 ACFTHOURS (NO PID)

11-Apr-1991 4


ASF 157ASAM UH-60-91-09 CHANGE TO INSPPROCEDURES FOR M/R SPINDLEELASTOMERIC BEARINGS C/W 1275.7 ACFTHOURS (NO PID)

16-May-1991 1


ASF 157ASAM UH-60-91-10 ONE-TIME INSP ANDREPLACEMENT OF MAIN L/G BRAKE ASSYPISTON INSULATORS C/W 1314.4 ACFTHOURS (NO PID)

16-Jul-1991 1


ASF 157ASAM UH-60-91-04 N/A FOR THIS ACFT (NOPID)

13-Aug-1991 1




8.7.DATE

6.REMARKS

4. 5.



ASF 157ASAM UH-60-92-01 INSP FOR THREE 3UNSERVICEABLE SPINDLES C/W 1404 ACFTHOURS (NO PID)

10-Jan-1992 1


ASF 157PERIODIC INSP #3 COMPLETED AT 1404 ACFTHOURS. PERIODIC INSP #4 DUE AT 1904 ACFTHOURS. (NO PID)

03-Mar-1992 1


ASF 157OMC/ACE COMPLETED AT 1407 ACFT HOURSBY AVSCOM OMSEC, ST. LOUIS, MO (NO PID)

11-Mar-1992 1


ASF 157TB 1-1520-237-20-128 DISCONNECTION OF THEPTICH BIAS ACTUATOR C/W AT 1415.7 ACFTHOURS (NO PID)

28-Apr-1992 1


ASF 157ASAM-UH-60-92-02 ONE-TIME INSP ON ALLEVEN S/N ACFT FOR ENG OUTPUT SHAFTBOLT TORQUE & VIB CHECK AT 1416 ACFTHOURS. N/A FOR THIS ACFT (NO PID)

21-May-1992 1


ASF 157ASAM-UH-60-92-03 UH-60 T700 GAS GENTURBINE BLADE FAILURES/ENGINECLEANING PROCEDURES C/W AT 1427 ACFTHOURS (NO PID)

15-Jun-1992 1


ASF 157ASAM-UH-60-92-04 N/A FOR THIS ACFT. (NOPID)

27-Jul-1992 1


ASF 157ASAM-UH-60-92-06 ONE-TIME INSPECTIONFOR PROPER HARDWARE ON TR PEDALADJUSTER ASSEMBLY C/W AT 1482 ACFTHOURS (NO PID)

28-Sep-1992 1


ASF 157ASAM-UH-60-92-05 INSPECTION ANDREPLACEMENT OF M/R BLADE EXPANDABLEPINS C/W AT 1482 ACFT HOURS (NO PID)

29-Sep-1992 1


ASF 157ASAM-UH-60-93-01 ONE-TIME OPERATIONALCHECK OF MAIN MODULE AND GEARBOXCHIP DETECTOR SYSTEMS C/W AT 1497.4ACFT HRS (NO PID)

17-Nov-1992 1


ASF 157ASAM-UH-60-93-02 GAS GEN TURBINE ROTORBLADE FAILURES, ENGING CLEANING ANDSINGLE ENGINE FLIGHT PLANNING C/W AT1497.1 ACFT HRS (NO PID)

17-Nov-1992 2


ASF 157ASAM-UH-60-93-03 INSP AND REPLACEMENTOF M/R BLADE EXP PINS (REVISION) C/W AT1507.2 ACFT HRS (NO PID)

18-Nov-1992 1


ASF 157ASAM-GEN0-93-01 PROHIBIT USE OF BRAYCO599 CORROSION PREVENTIVE COMPOUNDC/W AT 1525 ACFT HRS (NO PID)

04-Dec-1992 1


ASF 157ASAM-UH-60-93-04 REVISION TO ASAM UH-60-92-06 ONE-TIME INSPECTION FOR PROPERHARDWARE ON THE PEDAL ADJUSTER ASSYC/W AT 1525 ACFT HOURS (NO PID)

07-Dec-1992 1




8.7.DATE

6.REMARKS

4. 5.



ASF 157ASAM-UH-60-93-05 ONE-TIME INSP FOR T/RDRIVE SHAFT VISCOUS BEARING CLEANINGAND LUB INSTRUCTIONS C/W (NO PID)

17-Dec-1992 1


ASF 157ASAM-UH-60-93-06 ONE-TIME INSP TOREMOVE SUSPECT T/R PITCH BEAMS C/W AT1525 ACFT HOURS (NO PID)

18-Dec-1992 1


ASF 157ASAM-UH-60-93-07 REVISION OF CORROSIONLIMITS FOR T/R G/B C/W (NO PID)

22-Dec-1992 1


ASF 157ASAM-UH-60-93-08 ALL UH-60A, EH-60-60LHELICOPTERS BUILT PRIOR TO S/N 91-26345,TO BIAS T/R RIGGING THREE DEGREES C/W1529 ACFT HOURS (NO PID)

12-Jan-1993 1


AVSCOM OCMSEC, ST.LOUIS, MO

OCM/ACE COMPLETED AT 1529 ACFT HOURS(NO PID)

14-Jan-1993 1


ASF 157ASAM UH-60-93-09 ONE-TIME INSP TOCOMPLY WITH SYS MWO'S C/W AT 1566.0ACFT HOURS (NO PID)

14-Apr-1993 1


ASF 157ASAM UH-60-93-10 N/A FOR THIS ACFT (NOPID)

14-Apr-1993 2


ASF 157ASAM UH-60-93-11 INSP/REPLACE ARA CREWRESTRAINT SYSTEMS C/W AT 1566.0 ACFTHOURS (NO PID)

14-Apr-1993 3


ASF 157ASAM UH-60-93-12 ABRUPT CHANGE IN M/RTRACK/ VIBRATIONS C/W 1603.9 ACFT HOURS(NO PID)

30-Apr-1993 1



02-Jun-1993 1



03-Jun-1993 1



12-Jul-1993 1


ASF 157ASAM UH-60-93-16 ONE-TIME INSP OF THEHYD PUMP KNURLED BLEED/RELIEF VALVEC/W AT 1665 ACFT HOURS (NO PID)

13-Aug-1993 1


ASF 157ASAM UH-60-94-01 MASTER WARNING PANELREWORK FOR NVG COMPATIBILITY C/W AT1683.9 ACFT HOURS (NO PID)

19-Nov-1993 1


ASF 157ASAM UH-60-94-02 RETURN FOR EXCHANGEOF CERTAIN (ARA) MANUFACTUREDBUCKLE/CROTCH STRAP ASSEMBLIES (P/N4495-28) IN ALL H-60 SERIES ACFT C/W AT1705.0 ACFT HOURS (NO PID)

26-Jan-1994 1




8.7.DATE

6.REMARKS

4. 5.



ASF 157ASAM UH-60-94-03 ONE-TIMEREFURBISHMENT OF M/R SPINDLES ANDREPLACEMENT OF CERTAIN M/R THRUSTBEARING C/W 1705.0 ACFT HOURS (NO PID)

01-Feb-1994 1


ASF 157ASAM UH-60-94-04 ONE-TIME INSP TOREMOVE SUSPECT T/R PITCH BEAMS C/W AT1705.0 ACFT HOURS (NO PID)

03-Feb-1994 1


ATCOM OCM SECACE/AACE PERFORMED AT 1711.7 ACFT HRSBY ACE TEAM MEMBER B (NO PID)

18-Feb-1994 1


ASF 157ASAM UH-60-94-05 ONE-TIME REMOVAL OFT/R GEARBOX WITH OUTPUT SHAFT P/N 70358-06620-101 C/W AT 1711.7 ACFT HOURS (NOPID)

23-Feb-1994 1


ASF 157ASAM UH-60-94-06 COCKPITSTANDARDIZATION OF PILOT/COPILOTRESTRAINT RELEASE SYSTEMS C/W AT1711.7 ACFT HOURS (NO PID)

23-Feb-1994 2


ASF 157ASAM UH-60-94-07 CHANGE TOOVERHAUL/RETIREMENT TABLE C/W AT1711.7 ACFT HOURS (NO PID)

17-Mar-1994 1


ASF 157ASAM UH-60-94-08 CHANGE TO ASAM UH-60-94-07 C/W AT 1711.7 ACFT HOURS. (NO PID)

17-Mar-1994 2


CCADACFT COMPLETEDREFURBISHMENT/STANDARDIZATION PROG04 AUG 95 BY CCAD AT 1711.7 ACFT HOURSIAW ATCOM SOW DTD 05 AUG 93 WHICHINCLUDED MWO 1-1520-237- 55/7 AND PMS-2.(NO PID)

04-Apr-1995 1

CORPUS CHRISTI, TX

CCADNEXT PMS-2 DUE AT 2211.7 ACFT HOURS. (NOPID)

04-Apr-1995 2

CORPUS CHRISTI, TX

CCADACFT EXTERIOR PAINTED WITH LOWREFLECTIVE POLY- URETHANE ACFT GREEN,MIL-C-46168 IAW TM 55-1500- 345-23 DTD 12,AND ECP #0245. (NO PID)

04-Apr-1995 3

CORPUS CHRISTI, TX

CCADACFT SIX-MONTHS FILE WILL BE RETAINEDAT CCAD, IAW TDS NO. AGEN-X0363, CH 1,DTD 13 JAN 84. (NO PID)

04-Apr-1995 4

CORPUS CHRISTI, TX

CCADGEN-92-ASAM-07, USE OF DISCREPANT LOTSOF SYNTECH GREASE, P/N 3913-G1, NSN 9150-00-505-8497, SUBJECT GREAST NOT INST. (NOPID)

04-Apr-1995 5

CORPUS CHRISTI, TX

CCADTB 1-1520-237-20155, (UH-60-94-ASAM-09),REMOVAL OF CERTAIN PRIMARY SERVOASSEMBLIES, C/W (NO PID)

04-Apr-1995 6

CORPUS CHRISTI, TX

CCADTB 1-2835-214-20-1, ONE-TIME INSPECTION OFFORMS AND RECORDS FOR UH-60 APU UNITS,C/W (NO PID)

04-Apr-1995 7

CORPUS CHRISTI, TX

CCADUH-60-95-ASAM-04 (TB 1-1520-237-20-160)REDUCTION OF TORQUE OF SELF-RETAININGPIVOT BOLTS, C/W (NO PID)

04-Apr-1995 8

CORPUS CHRISTI, TX



8.7.DATE

6.REMARKS

4. 5.



CCADUH-60-95-ASAM-04 (TB 1-1520-237-20-162)REDUCTION OF TORQUE OF SELF-RETAININGPIVOT BOLTS, C/W (NO PID)

04-Apr-1995 9

CORPUS CHRISTI, TX

CCADUH-60-95-ASAM-06 (TB 1-1520-237-20-163)CHANGE IN RETIREMENT LIFE FOR SERVOBEAM RAILS. (NO PID)

04-Apr-1995 10

CORPUS CHRISTI, TX

AASF #1UH-60-95-ASAM-06 (TB 1-1520-237-20-168) ONE-TIME AND RECURRING INSPECTION FORCRACKED MAIN TRANS- MISSION BEAMS,UPPER DECK SKIN CRACKS AND FRAMECRACKS. C/W 1725.7 ACFT HOURS. (GP9820)

13-Jul-1995 1

TOPEKA, KANSAS

AASF #1UH-60-95-ASAM-07, INSP ALL GUNNER/TROOPSEATS UPPER ATTENUATION WIRES &ATTENUATOR ROLLER ASSY, C/W AT1738L.2ACFT HOURS (GP9820)

17-Aug-1995 1

TOPEKA, KANSAS

AASF #1UH-60-96-SOF-01 CHANGE IN RET. LIFE OFFORWARD BELLCRANK SUP. P/N -048 MANUF.BY HMW AND REMOVAL OF SPECIFIED SNFOR. BELLCRANKS SUP. ASSY C/W AT 1752ACFT HOURS (MT0000)

08-Nov-1995 1

TOPEKA, KANSAS

AASF #1UH-60-96-SOF-02 (TB 1-1520-237-20-173) ONE-TIME INSPECTION FOR SUSPECT TAIL ROTORINBOARD RETENTIN PLATES, C/W AT 1751.8A/C HOURS (GP9820)

28-Nov-1995 1

TOPEKA, KANSAS

AASF #1UH-60-95-ASAM-08 ONE TIME INSP OF GGROTORS WITH USED BLADES C/W AT 1751.8HOURS (MT0000)

29-Nov-1995 1

TOPEKA, KANSAS

AASF #1UH-60-96-ASAM-03 CERTAIN M/R BLADECUFFS HAVE REDUCED RET. LIFE C/W AT1751.8 HOURS (MT0000)

05-Dec-1995 1

TOPEKA, KANSAS

AASF #1UH-60-96-ASAM-02 (TB 1-1520-237-20-171) ONE-TIME INSPECTION FOR SUSPECT MAINROTOR SHAFT NUT BOLTS C/W AT 1751.8ACFT HOURS (GP9820)

26-Dec-1995 1

TOPEKA, KANSAS

AASF #1UH-60-96-ASAM-04 (TB 1-1520-237-20-176)REMOVAL OFSPECIFIC SERIAL NUMBEREDAFT BELLCRANK SUPT ASSYS C/W AT 1757.8ACFT HOURS (GP9820)

11-Jan-1996 1

TOPEKA, KANSAS

AASF #1UH-60-96-ASAM-03 C/W ON UH-60-96-ASAM-02(MT0000)

17-Jan-1996 1

TOPEKA, KANSAS

AASF #1UH-60-96-ASAM-04 (TB 1-1520-237-20-176) TOREVISE OPERATIONAL LOAD LIMITS ON FASTROPE INSERT/EXTRACTION SYSTEMS C/W1758.7 ACFT HOURS (GP9820)

31-Jan-1996 1

TOPEKA, KANSAS

AASF #1UH-60-96-ASAM-05 CHANGE CERTAIN SERIALNUMBERS FOR BELLCRANK SUPPORT ASSYFROM 500 TO 1800 HOURS TBO C/W AT 1798.8ACFT HOURS (MT0000)

18-Jul-1996 1

TOPEKA, KANSAS

AASF #1UH-60-96-ASAM-07 REPLACE CERTAIN SN#SPINDLE ASSYS WITHIN REGUIREMENTS OFASAM C/W AT 1804.3 ACFT HRS (MT0000)

05-Sep-1996 1

TOPEKA, KANSAS



8.7.DATE

6.REMARKS

4. 5.



AASF #1UH-60-96-ASAM-08 SERIAL NUMBERVERIFICATION OF CERTAIN PART NO.INBOARD T/R RET. PLATE C/W AT 1804.3 ACFTHOURS (MT0000)

06-Oct-1996 1

TOPEKA, KANSAS

AASF #1UH-60-96-ASAM-10 (TB 1-1520-237-20-182)ESTABLISH REQUIREMENTS FORREPLACEMENT OF THE TEFLON SLEEVEBEARING IN THE SPHERICAL ELASTOMERICBEARING ASSY AT EVERY 500 HOURS PMS-2INSP C/W AT 1804.3 ACFT HRS (GP9820)

10-Oct-1996 1

TOPEKA, KANSAS

AASF #1UH-60-96-ASAM-11 (TB 1-1520-237-20-183)MAINT. MANDATORY INCREASE IN FATIGUELIFE OF CERTAIN M/R BLADE CUFFS C/W AT1806.6 ACFT HRS (GP9820)

10-Oct-1996 2

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-02 (TB 1-1520-237-20-184) ONETIME INSP TAIL ROTOR DRIVE FLEXCOUPLINGS C/W AT 1813.0ACFT HOURS(GP9820)

11-Dec-1996 1

TOPEKA, KANSAS

AASF #1UH-60-96-ASAM-09 (TB 1-1520-237-20-180)VISUALLY INSP ALL STABILATOR ACTUATORCLEVISES BY NEXT PMS 2 C/W AT 1806.6ACFT HRS (GP9820)

18-Dec-1996 1

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-04 CERTAIN M/R CUFF TBOTIME TO 2400 HRS C/W AT 1825.9 ACFT HRS(GP9820)

03-Jan-1997 1

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-01 SOF REMOVAL OFCERTAIN REWORKED M/R SWASHPLATEASSYS C/W AT 1825.9 ACFT HRS (GP9820)

03-Jan-1997 2

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-01 (TB 1-1520-237-20-181) INSPOF M/R HUB ASSYS FOR PROPER EDGEBREAK C/W AT 1833.5 (GP9820)

07-Jan-1997 1

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-01 (TB 1-1520-237-20-181)INSPECTION OF MAIN ROTOR HUB ASSYSFOR PROPER EDGE BREAK, C/W 1833.5 ACFTHOURS. (GP9820)

07-Feb-1997 1

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-05 (TB 1-1520-237-23-3) ONE-TIME INSP OF VISCOUS DAMPER BRGSUPPORT ASSYS, C/W 1833.6 A/C HOURS(GP9820)

08-Feb-1997 1

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-06 (TB 1-1520-237-20-189) INSPLATERAL BELLCRANK ASSY FOR CERTAINSN# REDUCED RETIREMENT LIFE, C/W 1833.6A/C HOURS (GP9820)

12-Feb-1997 1

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-07 (TB 1-1520-237-20-188)REMOVE FROM SERVICE ALL T/R SERVO CYLASSY WITH CERTAIN SN#, C/W 1833.6 ACFTHOURS (GP9820)

13-Feb-1997 1

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-08 (TB 1-1520-237-20-187)CERTAIN CONNECTING LINK ASSYS MUST BEREMOVED FROM SERVICE C/W 1833.6 A/CHOURS (GP9820)

13-Feb-1997 2

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-09 (TB 1-1520-237-20-190) INSPALL M/R SHAFT EXTENSION ASSYS C/W AT1833.6 ACFT HRS (GP9820)

18-Feb-1997 1

TOPEKA, KANSAS



8.7.DATE

6.REMARKS

4. 5.



AASF #1UH-60-97-ASAM-10 FATIGUE LIFE CHANGE OFCERTAIN MAIN SUPPORT BRIDGES C/W AT1833.6 ACFT HRS (GP9820)

20-Feb-1997 1

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-11 (TB 1-1520-237-20-192)INCREASE IN FATIGUE LIFE FOR THE MAINROTOR BLADE CUFFS, C/W 1840.1 ACFTHOURS. (GP9820)

11-Mar-1997 1

TOPEKA, KANSAS

AASF #1HIRSS "B" KIT INSTALLED BY PROJ OLRDYNCORP AT TOPEKA, KS. AT 1849.2 ACFTHRS (GP9820)

09-May-1997 1

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-13 (TB 1-1520-237-20-194) ONETIME INSP OF M/R SPINDLE SPHERICALELASTROMIC BEARING C/W AT 1859.7 ACFTHRS (GP9820)

10-Jul-1997 1

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-14 (TB 1-1520-237-20-195) INSPALL ACFT FOR BELLCRANK SUPPORTS FORCERTAIN P/N AND REMOVE, C/W 1886.2 ACFTHOURS (GP9820)

02-Sep-1997 1

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-15 (TB 1-1520-237-20-196) INSPALL ACFT FOR CERTAIN BRG ROD END P/NAND REMOVE C/W AT 1886.2 ACFT HRS(GP9820)

02-Sep-1997 2

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-17 (TB 1-1520-237-20-199) INSPALL ACFT WITH THE INTERNAL RESCUEHOIST BRACKET ASSY, C/W 1886.2 ACFTHOURS (GP9820)

03-Sep-1997 1

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-18 (TB 1-1520-237-20-201) INSPSWASHPLATE ASSY SN# TO REMOVESUSPECT ASSY C/W AT 1888.1 ACFT HOURS(MT0000)

11-Sep-1997 1

TOPEKA, KANSAS

AASF #1UH-60-97-ASAM-19 (TB 1-1520-237-20-99) INSPHUDS CIRCUIT CARD ASSY C/W AT 1891.5 A/CHOURS (MT0000)

03-Oct-1997 1

TOPEKA, KANSAS

AASF #1UH-60-98-ASAM-01 (TB 1-1520-237-20-202)REVISE TBO FOR M/R SHAFT EXT C/W AT1891.5 A/C HOURS (MT0000)

03-Oct-1997 2

TOPEKA, KANSAS

AASF #1UH-60-98-ASAM-16 (TB 1-1520-237-20-198) ONE-TIME INSPECTION FOR CAGE CODE ONCLEVIS CONNECTOR C/W AT 1892.9 ACFTHOURS (MT0000)

21-Oct-1997 1

TOPEKA, KANSAS

AASF #1UH-60-98-ASAM-02 (TB 1-1520-237-20-197) INSPALL ACFT FOR PUSH ROD CAGE CODE 6S522C/W AT 1892.9 AC HOURS (MT0000)

24-Oct-1997 1

TOPEKA, KANSAS

AASF #1UH-60-98-ASAM-03 VERIFY MANUFACTURESCAGE CODE ON THE SWASHPLATE LINK PN70400-08110-54 (MT4634)

30-Oct-1997 1

TOPEKA, KS.

AASF #2ONE TIME INSP FOR REWORKED PRIMARY,YAW & COLLECTIVE BOOST, & T/R SERVOS(XD8508)

14-Apr-1998 1

SALINA, KS. 67401

AASF #2UH-60-98-ASAM-07 (TB 1-1520-237-20-206) ONETIME INSPECTION OF LEFT TIE ROD P/N 70400-08115-043 FORCAGE CODE 3R021 C/W(XD8508)

30-Sep-1998 1

SALINA, KS. 67401



8.7.DATE

6.REMARKS

4. 5.



AASF #2UH-60-99-ASAM-03 TB 1-2840-248-20-22 ALLUH-60A AND EH-60A SERIES HELICOPTERSONE TIME INSPECTION OF ALL T700-GE-700ENGINES RECORDS C/W (XS9537)

24-Nov-1998 1

SALINA, KS

AASF #2UH-60-99-ASAM-06 VISUALLY INSPECT PITCHHORNS FOR CERTAIN SERIAL NUMBERS ANDREDUCE RETIREMENT LIFE TO 2500 HOURS.(XD8508)

29-Dec-1998 1

SALINA, KS. 67401

ARMY AVIATIONSUPPORT FACILITY #2

RECURRING INSPECTION OF MAIN ROTORHUB ASSYS FOR PROPER EDGE BREAK, C/W1994.9 ACFT HRS (XD8508)

30-Mar-1999 1

SALINA, KANSAS 67401

AASF #2UH-60-99-ASAM-07 TB 1-1520-237-20-212 INSPOF M/R HUB ASSY C/W (XS9537)

08-Apr-1999 1

SALINA, KS

AASF #2UH-60-99-ASAM-08 (TB 1-1520-237-20-211) ALLH-60 ACFT REVISED RETIREMENT LIFE OFBELLCRANK SUPPORT ASSY P/N 70400-08162-042/043/045 MANUFACTURED BY AIRINDUSTRIES CAGE 8L513 C/W 2009.6 (XS9537)

11-Jun-1999 1

SALINA, KANSAS

AASF #2JACE.CPC PERFORMED AT 2037 ACFT HRS ATBY TEAM MEMBER N AMCOM OLR/MWOBRANCH KILLEEN TX (DS5651)

15-Jul-1999 1

SALINA, KS. 67401

AASF #2UH-60-99-ASAM-09 (TB1-1520-237-20-214) ONETIME INSPECTION OF THE MAIN ROTORBLADE EXPANDABLE PINS P/N 70103-08107-101/102/103 (XD8508)

29-Jul-1999 1

SALINA, KS. 67401

AASF #2UH-60-99-ASAM-10 (TB1-1520-237-20-213)INSPECTION AND PREVENTIVE MAINTENANCEON THE NUMBER TWO CROSSFEEDBREAKAWAY VALVE, P/N 70307-03006-103(XD8508)

06-Aug-1999 1

SALINA, KS. 67401

AASF #2UH-60-99-ASAM-11 (TB1-2840-248-20-23) ONETIME INSPECTION OF T700-GE-700/701/701CENGINES (XD8508)

06-Aug-1999 2

SALINA, KS. 67401

AASF #2UH-60-99-ASAM-12 TB 1-2840-229- ALL UH-60A,EH-60A AND UH-60Q ACFT INSPECTIONINTERVAL CHANGE FOR HAMILTONSTANDARD HYDRO MECHANICAL UNITS HMUC/W 2059.4 ACFT HRS. #1 ENG S/N GEE207568HMU S/N DA93537 #2 ENG S/N GEE207996 HMUS/N J7949 (XS9537)

19-Aug-1999 1

SALINA, KS

AASF #2UH-60-00-ASAM-01 (TB 1-1520-237-20-215)REVISION OF UH-60-99-ASAM-07 RECURRINGINSPECTION OF M/R HUB ASSY FOR PROPEREDGE BREAK C/W AT 2096.1 ACFT HRS(XD8508)

22-Nov-1999 1

SALINA, KS. 67401

AASF #2UH-60-00-ASAM-02 (TB 1-1520-237-20-216) ALLH-60'SONE TIME INSPECTION OF CYCLICSTICK WIRE BUNDLES FOR CLEARANCE ANDCHAFFING. (XD8508)

15-Dec-1999 1

SALINA, KS. 67401

AASF #2UH-60-00-ASAM-03/TB 1-1520-237-20-217 INSP& REMOVAL OF SUSPECT PRIMARY SERVOASSY C/W 2106.0 ACFT HRS (XS9537)

06-Jan-2000 1

SALINA, KS



8.7.DATE

6.REMARKS

4. 5.




UH-60-99-ASAM-10 (TB1-1520-237-20-213) #2CROSSFEED BREAKAWAY VALVE REPLACEDAT 2109.8 ACFT. HRS 11 JAN 2000 (XD8508)

11-Jan-2000 1

SALINA, KS. 67401

AASF #2INSPECT TAIL LANDING GEAR STRUT I/A/WUH-60-00-ASAM-04 COMPLETED 03 MAR 002111.2 ACFT HRS (XD8508)

03-Mar-2000 1

SALINA, KS. 67401

AASF #2UH-60-00-ASAM-05 (TB 1-1520-237-20-219) INSPFIRE EXTINGUISHER WIRING FOR CORRECTMARKING AND ROUTING C/W AT 2153.9 ACFTHRS. (XD8508)

23-May-2000 1

SALINA, KS

AASF #2UH-60-00-ASAM-06 (CHG 1 TP TB 1-1520-237-20-219) INSP FIRE EXTINGUISHER WIRING FORCORRECT MARKING AND ROUTING C/W AT2194.4 ACFT HRS. (XD8508)

27-Jun-2000 1

SALINA, KS

AASF #2UH-60-00-01 TB 1-1520-237-20-221 H-60AIRCRAFT INITIAL AND RECURRINGINSPECTION OF MAIN ROTOR SPINDLE LUGSC/W 2202.7 ACFT HRSP (XS9537)

13-Jul-2000 1

SALINA, KS

AASF #2UH-60-00-02 (TB 1-1520-237-20-222) INSP INPUTMODULE RECORDS C/W AT 2201.9 ACFT HRS(XD8508)

03-Aug-2000 1

SALINA, KS. 67401

AASF #2UH-60-00-ASAM-07 TB 1-1520-237-20-224, ONETIME INSPECTION OF WIRE HARNESSESCONNECTING THE NO. 1 AND NO. 2 JUNCTIONBOXES THAT HAVE BEEN REFURBISHED C/W(XS9537)

21-Sep-2000 1

SALINA, KS. 67401

AMCOM OLR/MWOBRANCH

ACE/CPCE PERFORMED AT 2211 ACFT HRSBY TEAM MEMBER K/W AMCOM OLR/MWOBRANCH KILLEEN, TX (JP2527)

16-Oct-2000 1

SALINA, KS

AASF #2TB 1-1520-237-20-167 INSP AND REPAIR OFSTATION 635 FRAME ASSY FOR TAIL WHEELSTRUT INSTALLATION CLEARANCE C/W AT2211.0 ACFT HRS. (XS9537)

18-Oct-2000 1

SALINA, KANSAS

AASF #2UH-60-01-01 (TB 1-1520-237-20-225) INITIALAND RECURRING INSP OF MAIN LANDINGGEAR DRAG BEAM ASSY AND DECREASETORQUE ON THE JACKPAD NUT C/W AT2215.1ACFT HRS (XD8508)

08-Nov-2000 1

SALINA, KS 67401

AASF #2PMS-2 COMPLETED AT 2211.0 ACFT HRS NEXTPMS-2 WILL BE DUE AT 2219.0 ACFT HRS(XS9537)

30-Nov-2000 1

SALINA, KANSAS

AASF #2UH-60-01-03 TB 1-1520-237-20-229 INSPECTIONAND REMOVAL OF LATERAL SERVOBELLCRANK ASSEMBLY MANUFACTURED BYTHE PURDY MACHINE COMPANY CAGE CODE15152 C/W AT 2209.3 ACFT HRS. (XS9537)

05-Jan-2001 1

SALINA,KS 67401

AASF #2UH-60-01-04 TB 1-1520-237-20-228 INSPECTFOR INSTALLATION OF FUEL MONITORINGSYSTEM C/W AT 2223.2 ACFT HRS. (XS9537)

05-Jan-2001 2

SALINA, KS



8.7.DATE

6.REMARKS

4. 5.



AASF #2UH-60-01-02 TB 1-1520-237-20-225 REVISIONTO UH-60-01-01, INITIAL AND RECURRINGINSPECTION OF MAIN LANDING GEAR DRAGBEAM ASSY AND DECREASE TORQUE ON THEJACKPAD NUT C/W AT 2223.2 ACFT HRS(XD8508)

15-Jan-2001 1

SALINA,KS 67401

AASF #2UH-60-01-05 TB 1-1520-237-20-230 ALL H-60AIRCRAFT REVISION TO UH-60-00-01INSPECTION OF MAIN ROTOR SPINDLE C/WAT 2294.3 ACFT HRS. (XS9537)

23-Mar-2001 1

SALINA, KS

AASF #2UH-60-01-06 TB 1-1520-237-20-231 ALL H-60SERIES AIRCRAFT, INSPECTION OF ALL SASACTUATORS C/W AT 2276.4 ACFT HRS.(XS9537)

27-Mar-2001 1

SALINA, KS

AASF #2UH-60-01-SOF-12 (TB1-1520-237-20-236) INSPEXPANDABLE PIN IAW MSG PRIOR TO NEXTFLT BUT NLT 27 AUG O1. AT 2292.4 ACFT HRS(XD8508)

24-Apr-2001 1

SALINA, KS 67401

AASF #2UH-60-01-08 TB 1-1520-237-20-232 REVISIONTO UH-60-01-07 INSPECTION OF MAIN ROTORFLIGHT CONTROL SELF LOCKING BOLTS C/WAT 2340.0 ACFT HRS. (XS9537)

13-Jun-2001 1

SALINA, KS

AASF #2UH-60-01-09 TB 1-1520-237-20-233 ONE TIMEINSPECTION OF MAIN ROTOR BLADEEXPANDABLE PINS C/W AT 2351.7 ACFT HRS.(XS9537)

13-Jun-2001 2

SALINA, KS 67401

AASF #2UH-60-01-10 TB 1-1520-237-20-234 ONE TIMEINSPECTION OF MAIN ROTOR BLADEEXPANDABLE PINS C/W AT 2362.1 ACFT HRS.(XS9537)

17-Jul-2001 1

SALINA, KS

AASF #2UH-60-01-11 TB 1-1520-237-20-235 DECREASETHE INTERVAL BETWEEN REQUIRED INSP OFM/R HUB ASSY FOR CRACKS IN SPECIFIEDAREAS FROM 200 TO 100 HRS ANDIMPLEMENT A BEFORE 1ST FLT OF DAYVISUAL INSP OF THE VISIBLE AREA OF HUBNEAR THE 11:00 BOLT HOLE AT 2369.4 ACFTHRS (XD8508)

24-Aug-2001 1

SALINA, KS. 67401

AASF #2UH-60-01-12 TB 1-1520-237-20-236 INSPEXPANDABLE PINS IAW MSG PRIOR TO NEXTFLT BUT NLT 27AUG01 CW AT2 2372.6 ACFTHRS (XD8508)

24-Aug-2001 2

SALINA, KS

AASF#2ACE/CPCE PERFORMED AT ACFT HRS. BYTEAM MEMBERS W & TT. AMCOM PROJECTOLR.KILLEEN, TX (JP2527)

27-Sep-2001 1

SALINA, KANSAS

AASF #2UH-60-02-ASAM-01 TB 1-1520-237-20-239 H-60SERIES, INITIAL AND RECURRINGINSPECTION OF THE TAIL ROTOR FAIRINGASSEMBLY C/W AT 2424.5 ACFT HRS (XS9537)

16-Nov-2001 1

SALINA, KS

AASF # 2INSPECT OIL COOLER FAN SHAFT ASSEMBLYFORWARD MOUNT FLANGE IAW UH-60-02-01(TB 1-1520-237-20-240) PRIOR TO NEXTFLIGHT, BUT NLT 30 NOVEMBER 2001,COMPLETED 19 NOV. 01 AT 2426.5 ACFT HRS.(XD8508)

19-Nov-2001 1

SALINA, KS. 67401



8.7.DATE

6.REMARKS

4. 5.



AASF #2UH-60-02-03 TB 1-1520-237-10-241 ALL H-60SERIES AIRCRAFT ONE TIME INSPECTION OFTHE FLIGHT CONTROL SYSTEM, PITCH TRIMASSEMBLY C/W AT 2431.3 ACFT HRS (XS9537)

13-Dec-2001 1

SALINA, KS

AASF # 2UH-60-02-02 (TB1-1520-237-20-237) INSPECTMAIN ROTOR HUB RECORDS AND DATAPLATE FOR REWORK CANDIDATE C/W AT2433 ACFT HRS (XD8508)

15-Dec-2001 1

SALINA, KS. 67401

AASF #2UH-60-02-04 (TB1-1520-237-20-242) COMPLIEDWITH AT 2460.3 ACFT HRS (XD8508)

29-Jan-2002 1

SALINA, KS. 67401

AASF #2INSP ENGINE CONTROL QUADRANT POWERCONTROL LEVER (PCL) WIRING UH-60-02-ASAM-03 TB 1-1520-237-20-245 C/W AT 2505.1ACFT HRS. (XS9537)

13-Feb-2002 1

SALINA, KS

AASF #2INSPECT THE CONTROL ROD JAMNUTS IAWUH-60-02-ASAM-02 TB 1-1520-237-20-246 C/WAT 2476.7 ACFT HRS (XS9537)

13-Feb-2002 2

SALINA, KS

AASF #2INSPECT EXPANDABLE PINS IAW UH-60-02-05TB 1-1520-237-20-243 C/W AT 2476.6 ACFTHRS. (XS9537)

14-Feb-2002 1

SALINA, KS

AASF #2UH-60-02-ASAM-04 (TB1-1520-237-20-244)RESTRAINT SYSTEM INSPECTION CW AT2490.5 ACFT HRS (XD8508)

29-Mar-2002 1

SALINA, KS 67401

AASF #2UH-60-02-ASAM-05 (TB1-1520-237-20-251)INSPECTION OF M/R SPINDLE ASSY'S CWAT 2497.0 ACFT HRS APR 9 02 (XD8508)

09-Apr-2002 1

SALINA, KS. 67401

AASF #2UH-60-02-ASAM-06 TB 1-1520-237-20-252INSPECT SWAGE PINS/COLLARS ON BOOSTSERVO ASSEMBLIES C/W AT 2499.5 ACFTHRS. (XS9537)

19-Apr-2002 1

SALINA, KS

AASF #2UH-60-02-07 MAIN MODULE PLANETARYCARRIER ASSEMBLYC/W AT 2505.1 ACFTHRS. (XS9537)

02-May-2002 1

SALINA, KS

AASF #2MAIN MODULE PLANETARY CARRIERASSEMBLY UH-60A, EH-60A,UH-60Q UH-60-02-08 TB 1-1520-237-20-255 C/W AT 2505.1 ACFTHRS (XS9537)

07-May-2002 1

SALINA, KS

AASF #2MAIN MODULE PLANETARY CARRIERASSEMBLY UH-60A, EH-60A,UH-60Q UH-60-02-09 TB 1-1520-237-20-258 C/W AT 2505.1 ACFTHRS (XS9537)

23-May-2002 1

SALINA, KS

C CO 1/108TH AVNUH-60-SOF-02-10 MAIN MODULE PANETARYCARRIER ASSY.(RAF) COMPLETED AT 2514ACFT HRS (KJ1803)

09-Jun-2002 1

TOPEKA,KS

AASF #2UH-60 SERIES AIRCRAFT INSPECT AN/ARC-220 WIRING FOR CHAFING UH-60-02-ASAM-08TB 1-1520-237-20-256 C/W AT 2520.8 ACFTHRS. (XS9537)

14-Jun-2002 1

SALINA, KS

AASF #2H-60 SERIES AIRCRAFT TAIL ROTORQUADRANT HARDWARE INSTALLATION UH-60-02-ASAM-09 TB 1-1520-237-20-257 C/W AT2523.1 ACFT HRS (XS9537)

15-Jun-2002 1

SALINA, KS



8.7.DATE

6.REMARKS

4. 5.



AASF #2UH-60-02-11 TB 1-1520-237- ONE TIMEINSPECTION OF MAIN ROTOR BLADE CUFFASSEMBLY C/W AT 2574.9 ACFT HRS (XS9537)

12-Aug-2002 1

SALINA,KS

AASF #2UH-60-02-12 TB 1-1520-237- REVISION TO UH-60-02-11 ONE TIME INSPECTION OF MAINROTOR BLADE CUFF ASSEMBLY C/W AT2574.9 ACFT HRS (XS9537)

13-Aug-2002 1

SALINA, KS

DYNCORPACE/CPCE PERFORMED AT 2619 ACFT. HRS.BY TEAM MEMBERS K & W. AMCOM PROJECTOLR. KILLEEN, TX. (JP2527)

24-Sep-2002 1

KILLEEN, TX.

AASF #2INSPECT AN/ARC-220 WIRING FOR CHAFING,UH-60-02-ASAM-11 TB 1-1520-237-20-261 C/WAT 2618.6 ACFT HRS (XD8508)

27-Sep-2002 1

SALINA, KS.

PROJECT OLRINSTALLATION OF THE 90 DEGREEBACKSHELL I/A/W UH-60-02-ASAM-11COMPLETED (JC1523)

20-Nov-2002 1

KILLEEN, TX

AASF #2UH-60-03-01 COMPLY WITH REQUIREMENT OFNDI ON MAIN MOD PLANETARY CARRIER C/WAT 2628.6 ACFT HRS (XD8508)

10-Dec-2002 1

SALINA, KS. 67401

AASF # 2UH-60-03-ASAM-01 BELLCRANK SUPPORTASSY RETIREMENT LIFE C/W AT 2683.6 ACFTHRS (JD8508)

16-Dec-2002 1

SALINA, KS. 67401

AASF # 2UH-60-03-ASAM-02 TAIL ROTOR SERVORETIREMENT LIFE AT 2685.0 ACFT HRS(JD8508)

20-Jan-2003 1

SALINA, KS. 67401

AASF #2UH-60-03-02 COMPLIED WITH ON MAIN ROTORBLADE CUFF BLLTS. INSPECT FORCORRORSION AND CRACKS. (XD8508)

23-Jan-2003 1

SALINA, KS. 67401

AASF # 2UH-60-03-03 PLANETARY CARRIERRETIREMENT LIFE C/W AT 2685.0 ACFT HRS(JD8508)

21-Feb-2003 1

SALINA, KS. 67401

AASF # 2UH-60-03-ASAM-03 PERFORMANCE PLANNINGDURING DESERT OPS N/A (JD8508)

21-Feb-2003 2

SALINA, KS. 67401

AASF #2PMS-2 COMPLETED AT 2685.0ACFT HRS NEXTPMS-2 WILL BE DUE AT 3185.0 ACFT HRS(XD8508)

22-May-2003 1

SALINA, KS.

AASF # 2UH-60-03-04 PLANETARY CARRIERRETIREMENT LIFE C/W AT 2687.3 ACFT HRS(JD8508)

04-Jun-2003 1

SALINA, KS. 67401

DYNCORPACE/CPCE PERFORMED AT 2757 ACFT HRSBY TEAM MEMBERS K & I AMCOM PROJECTOLR KILLEEN, TX. (JL7296)

04-Sep-2003 1

KILLEEN, TX.

AASF # 2UH-60-04-01 FWD BELLCRANK SUPPORTINSTALLATION HARDWARE C/W AT 2843.3ACFT HRS (JD8508)

08-Oct-2003 1

SALINA, KS. 67401

AASF #2UH-60-04-ASAM-01 ALL UH-60A/L, GLARESHIELD LIGHTING CIRCUIT BREAKERREPLACEMENT C/W AT 2873.9 ACFT HRS.(XS9537)

29-Jan-2004 1

SALINA,KS


UH-60-04-ASAM-02, LOOSE NUTS ON TAILROTOR DIVE SHAFT, N/A BY ACFT HRS ANDS/N (XD8508)

01-Apr-2004 1

SALINA, KS 67401



8.7.DATE

6.REMARKS

4. 5.



AASF #2UH-60-04-ASAM-03 ALL H-60 SERIESAIRCRAFT, FUEL SYSTEM INTEGRITYCHECKS, COMPLETED AT ACFT HRS (XS9537)

08-Apr-2004 1

SALINA, KS

AASF # 2UH-60-04-02 DISABLING OF COCPIT AIRBAGSYSTEM AT 2901.5 ACFT HRS (JD8508)

16-Jun-2004 1

SALINA, KS. 67401

AASF # 2UH-60-04-03 CRASHWORTHY EXTERNAL FUELSYSTEM NA THIS ACFT AT 2904.2 ACFT HRS(JD8508)

30-Jun-2004 1

SALINA, KS. 67401

DYNCORP OLRACE/CPCE PERFORMED AT 2907 ACFT HRSBY TEAM MEMBERS K&W AMCOM PROJECTOLR (JP2527)

07-Jul-2004 1

KILLEEN, TX.

AASF # 2UH-60-04-04 MAIN ROTOR HUBSUBASSEMBLY REWORK C/W AT 3024.0 ACFTHRS. (JD8508)

17-Aug-2004 1

SALINA, KS. 67401

AASF # 2UH-60-04-ASAM-04 FUEL SYSTEM INTEGRITYCHECK REVISED AT 3024.0 ACFT HRS(JD8508)

18-Aug-2004 1

SALINA, KS. 67401

AASF # 2UH-60-04-ASAM-05 RESTRAINT SYSTEMINSPECTION C/W AT 2950.9 ACFT HRS(JD8508)

28-Sep-2004 1

SALINA, KS. 67401

AASF # 2UH-60-05-ASAM-01 REVISED FUEL SYSTEMINTEGRITY CHECK 3024.0 ACFT HRS (JD8508)

07-Jan-2005 1

SALINA, KS. 67401

AASF # 2UH-60-05-ASAM-02 BLUE FORCE TRACKERN/A THIS ACFT AT 2986.7 ACFT HRS (JD8508)

03-Mar-2005 1

SALINA, KS. 67401

AASF # 2UH-60-05-01 REACTIVATION OF COCKPITAIRBAG NA THIS ACFT AT 2986.7 ACFT HRS.(JD8508)

17-Mar-2005 1

SALINA, KS. 67401

AASF # 2UH-60-05-ASAM-03 AIRCREW RESTRAINTSYSTEM COMPATIBILITY C/W AT 2991.4 ACFTHRS (JD8508)

07-Apr-2005 1

SALINA, KS. 67401

AASF # 2UH-60-05-ASAM-04TAIL LANDING GEAR YOKEASSY N/A BY P/N AT 2991.4 ACFT HRS(JD8508)

12-Apr-2005 1

SALINA, KS. 67401

AASF # 2UH-60-05-ASAM-06 TROOP SEAT RESTRAINTBUCKLE C/W AT 2994.8 ACFT HRS (JD8508)

03-May-2005 1

SALINA, KS. 67401

AASF # 2UH-60-05-ASAM-05 TIE ROD ASSY C/W AT2994.8 ACFT HRS (JD8508)

03-May-2005 2

SALINA, KS. 67401

DYNCORP OLRACE/CPCE PERFORMED AT 3004 ACFT HRSBY TEAM MEMBERS K&W AMCOM PROJECTOLR (JP2527)

20-May-2005 1

KILLEEN, TX.

AASF #2UH-60-05-ASAM-08 TIE ROD REINSPECTIONC/W AT 3006.6 ACFT HRS (JD8508)

07-Jun-2005 1

SALINA KS 67401

AASF #2AIRCRAFT PLACED ON ESM 06/21/2005 ACFTHRS 3013.4 PMI # 2 DUE AT 3034.4 ACFT HRS(BM7522)

21-Jun-2005 1

SALINA KS 67401

AASF # 2UH-60-05-ASAM-07 AIR INTRUSION OFHYDRAULIC SYSTEM C/W AT 3018.5 ACFT HRS(JD8508)

28-Jun-2005 1

SALINA, KS. 67401



8.7.DATE

6.REMARKS

4. 5.



AASF # 2UH-60-05-ASAM-09 CRASHWORTHYEXTERNAL FUEL SYSTEM (CEFS)INSTALLATION BOLTS, (JD8508)

03-Aug-2005 1

SALINA, KS. 67401

AASF #2C/W REQUIREMENTS OF UH-60-05-ASAM-10N/A BY S/N (JD8508)

21-Aug-2005 1

SALINA, KS. 67401

AASF #2C/W REQUIREMENTS OF UH-60-05-ASAM-11AT ACFT HRS (JD8508)

29-Sep-2005 1

SALINA, KS. 67401

AASF #2PMI-2 COMPLETED AT 3024.0 ACFT HRS, PMI-1DUE AT 3374 ACFT HRS. (JD8508)

06-Oct-2005 1

SALINA, KS. 67401

AASF #2UH-60-06-ASAM-01 TAIL LNDING GEAR SHOCKSTRUT. COMPLIED WITH AT XXXX.X ACFTHRS

14-Dec-2005 1

SALINA, KANSAS

JM884376

AASF #2AWR 548, UHH-60A AIRCRAFT EQUIPPEDWITH RT-1518C/ARC-164 HAVE QUICK II (HQII)UHF/AM RADIO. SUCCESSFUL COMPLETIONOF EMCTEST AND DAILY INSPECTION, ANDINCLUDES TEMPORARY OR PERMANENTCHANGES IN CONFIGURATION

02-Feb-2006 1

SALINA, KS. 67401

JD508508

36TH CAB 1-108TH AVNCO.D

UH-60-06-ASAM-03 COMPLIED WITH 14-Jun-2006 1

FT. HOOD, TEXAS

JR759141


UH-60-06-ASAM-04 COMPLIED WITH 24-Jun-2006 1

FT. HOOD, TEXAS

JR759141

36 CAB 1-108TH AVNCO.D

UH-60-06-SOF-02 COMPLIED WITH (N/A THISACFT).

25-Jun-2006 1

FT. HOOD, TEXAS

JR759141

AASF IDARNGUH-60-07-ASAM-01, WHITE ENGINE CABLEHARNESS REROUTING C/W.

10-Jan-2007 1

BOISE, ID

BJ117531

AASF IDARNGUH-60-07-ASAM-02, REVISION TO UH-60-07-ASAM-01 C/W.

10-Jan-2007 2

BOISE, ID

BJ117531

AASF IDARNGUH-60-07-ASAM-04, AUTOROTATION RPMVERIFICATION C/W.

11-Jan-2007 1

BOISE, ID

BJ117531

AASF IDARNGUH-60-07-ASAM-03, YAW AND COLLECTIVEBOOST SERVOS ROLL PIN C/W.

17-Jan-2007 1

BOISE, ID

BJ117531

AASF IDARNGUH-60-07-ASAM-05, ARC-220/KY-100 START-UPPROCEDURES C/W.

24-Jan-2007 1

BOISE, ID

BJ117531

AASF IDARNGUH-60-07-ASAM-06, INTERNAL RESCUE HOISTCABLE (GUARD) DEFLECTOR C/W, N/A THISACFT.

09-Feb-2007 1

BOISE, ID

BJ117531

AASF IDARNGUH-60-07-ASAM-07, INSTALLATION OF STATICBONDING JUMPERS ON CEFS ACFT C/W. N/ATHIS ACFT.

15-May-2007 1

BOISE, ID

BJ117531

AASF IDARNGUH-60-07-AMAM-01, COMMON MISSILEWARNING SYSTEM (CMWS) C/W.

24-May-2007 1

BOISE, ID

BJ117531



8.7.DATE

6.REMARKS

4. 5.




UH-60-06-ASAM-05 COMPLIED WITH AT 3134.8ACFT HRS.

04-Aug-2007 1

FT. HOOD, TEXAS

JR759141

AAS F# 2UH-60-07-ASAM-10 ,MAIN FUEL MANIFOLDCHAFING,COMPLIED WITH

27-Aug-2007 1

W.TRENTON N.J.

FD986611

AASF-ID#1 INPUT MODULE S/N A264-00863 11:00 BOLTHOLE REPAIRED IAW MEC# F64282 DATED 29-JUN-2007

19-Sep-2007 1

GOWEN FIELD BOISEIDAHO

RH982367

AASF-ID# 2 INPUT MODULE S/N: A264--1533 12:00BOLT HOLE REPAIRED IAW MEC# F64289DATED 29-JUN-2007

19-Sep-2007 2


RH982367

AASF-IDTEMP REPAIR INSTALLED ON L/H CARGODOOR TRACK. TRACK DUE REPLACEMENT ATNEXT SCHEDULED PMI IAW MEC # 64605DATED 12-JUL-2007

19-Sep-2007 3

GOWEN FIELD, BOISEIDAHO

RH982367

AASF-IDT/R D/S SUPPORTS AT STA'S 531 AND 591 DUEREPLACEMENT AT NEXT PMI(3384.0 ACFT.HRS) IAW MEC# 64655 DATED 13-JUL-2007

19-Sep-2007 4


RH982367

AASF-IDACE/CPCE PERFORMED AT 3200.0 ACFT HRS.BY TEAM MEMBER X

19-Sep-2007 5


RH982367

AASF-IDCOMPLETED ACFT. RIG AT 3200.0 ACFT. HRS.T/R BIAS SET: RED-4.496, BLUE-4.996,YELLOW-4.489, BLACK-5.022

19-Sep-2007 6


RH982367

D CO 1-150 AIRASSUALT

H-60-08-AMAM-01 COMPLIED WITH 23 OCT2007 @ 3233.9 ACFT HRS

26-Oct-2007 1

WEST TRENTON NJ

RS581167

D CO 1-150 ASSAULT(LATE ENTRY) AIRCRAFT TRANSFERRED TO ACO 1-150 ASSAULT @ 3233.9 ACFT HRS.

08-Nov-2007 1

WEST TRENTON NJ

RS581167

NJARNG AASF#2UH-60-08-ASAM-01 TROOP/GUNNERS SEATUPPER ENERGY ATTENUATING WIRES,COMPLIED WITH 24 OCT 07 @ 3233.9 ACFTHRS.

26-Nov-2007 1

WEST TRENTON NJO8628

RS581167

AASF#2H-60-08-ASAM-03 COMPLIED WITH 28NOV2007ACFT HRS:3235.3

29-Nov-2007 1

W.TRENTON N.J.

FD986611

NJARNG AASF#2H-60-08-AMAM-02 COMPLIED WITH . T/ROUTBOARD RETENTION PLATE SERIAL # NOTIN SUSPECT GROUP

30-Nov-2007 1

WEST TRENTON NJ08628

RS581167

NJARNG AASF#2H-60-08-AMAM-02 TAIL ROTOR OUTBOARDRETENTION PLATE SHIMS, COMPLIED WITH .T/R OUTBOARD RETENTION PLATE SERIAL #NOT IN SUSPECT GROUP

30-Nov-2007 2

WEST TRENTON NJ08628

RS581167

AASF#2UH-60-08 ASAM-04 PILOTS LOWER SEAT RAILCHAFING ELECTRICAL HARNESS. C/W

05-Dec-2007 1

W.TRENTON N.J.

FD986611

AASF# 2H-60-08-ASAM-05 T/R SPRING CAPSULE ASSYCOMPLIED WITH 12 DEC 2007

12-Dec-2007 1

WEST TRENTON N.J.

FD986611



8.7.DATE

6.REMARKS

4. 5.



AASF # 2H-60-08-SOF-01,MAIN ROTOR BLADEEXPANDABLE PIN INSPECTIONCHANGE,COMPLIED WITH

29-Jan-2008 1

W. TRENTON N.J.

FD986611

AASF # 2H-60-08-AMAM-04,COCKPIT DOORJETTISONABLE WINDOWS,COMPLIED WITH

29-Jan-2008 2

W. TRENTON N.J.

FD986611

FORT HOOD PROJECTOLR

H-60-08-ASAM-06 COMPLIED WITH 03-Mar-2008 1

FT. SILL OK 73503

GL501680

FT HOOD OLRH-60-08-AMAM-07 INSPECTION CRITERIACOMPLIED WITH SYSTEM NOT INSTALLED ONACFT

25-Mar-2008 1

FT. SILL

RL590558

AASF # 2AIRCRAFT TRANSFERED TO A. CO 1-150THAASB, WV75A0 TRENTON, N.J. 08628 AT3317.2 AIRCRAFT HOURS ON 29APR2008FROM A.CO 2/104

02-May-2008 1

WEST TRENTON, NJ08628-1302

FD986611

AASF # 2H-60-08-AMAM-08,FLIGHT CONTROL RIGGINGUPDATE,COMPLIED WITH

10-Jun-2008 1


FD986611

DS2ACE COMPLETED AT 3340 A/C HRS. BY ACETEAM MEMBER BB/G. AMCOM MWO/OLRBRANCH.

14-Aug-2008 1


JG389608

AASF # 2H-60-08-ASAM-11( FLIGHT CONTROLINSPECTION) COMPLIED WITH

08-Sep-2008 1


GB548643

AMCOM OLR (DS2)AWR 1494 DATED 9 MAY 08 INSTALLATION OFCMWS FIFTH SENSOR IS IN EFFECT

24-Sep-2008 1


JK887338

AASF # 2AUTHORIZED REPLACEMENT OF MAIN ROTORBLADE EXPANDABLE PINS NSN 5315-01-329-0707 FOR SOLID BLADE PINS NSN 5315-01-537-4652 BY ISAQ 127 DATED 24 OCT 06COMPLETED AT 3366.3 ACFT HOURS

25-Sep-2008 1


FD986611

AASF#2COMPLIED WITH H-60-08-ASAM-13 25-Sep-2008 2


JS889951

DOL (LSI)H-60-09-SOF-01 (H.M.U. INSPECTION)COMPLIED WITH

21-Oct-2008 1

FT DRUM, NY 13602

SD726739

DOL(LSI)MEC F83808; AUTHORIZATION TO DRAIN ANDFLUSH MAIN MODULE SN:A265-01080,PERFORM SERVICEABILITY CHECK AND DOBASELINE OIL SAMPLE, FLY ACFT FOR 10HRSAND REINSPECT MAIN MODULE FOR DEBRISIN DECTECTOR SCREEN. IF DEBRIS FOUNDCONTACT AMCOM LAR ADN AMRDEC-MEDFOR FURTHER INSTRUCTIONS. AS PERENGINEER: NICHOLAS W. HURTA DATED 31OCT 08 3369 ACFT HRS

03-Nov-2008 1

FT DRUM, NY 13602

SD726739

DOL (LSI)H-60-08-ASAM-10(ELECTRICAL WIRE CHAFFISSUE INSPECTION) COMPLIED WITH @ 3369ACFT HRS

04-Nov-2008 1

FT DRUM, NY 13601

SD726739



8.7.DATE

6.REMARKS

4. 5.



DOL (LSI)H-60-08-ASAM-12(PARKER AEROSPACE AIRTURBINE STARTER (ATS) INSPECTION)COMPLIED WITH @ 3369 ACFT HRS

05-Nov-2008 1

FT DRUM, NY 13601

SD726739

DOL (LSI)H-60-08-ASAM-13( FIRE EXTINGUISHING TUBEUNION RING INSPECTION) COMPLIED WITH @3369 ACFT HRS

05-Nov-2008 2

FT DRUM, NY 13601

SD726739

DOL (LSI)H-60-08-ASAM-14(SUSPECT ENGINE HARNESSINSPECTION) COMPLIED WITH @ 3369 ACFTHRS

05-Nov-2008 3

FT DRUM, NY 13601

SD726739

DOL(LSI)H-60-09-SOF-02 AN/ALQ-144 INFRA-REDCOUNTERMEASURES SYSTEM (IRCMS)COMPLIED WITH @ 3369 ACFT HRS

10-Nov-2008 1

FT DRUM,NY 13601

SD726739

DOL AVIMH-60-09-SOF-03 POSSIBLE RETIREMENT LIFEOVER-FLIGHT COMPLIED WITH @ 3369 ACFTHRS.

06-Dec-2008 1

FT DRUM NY 13602

SD726739

DOL AVIMTR RIG COMPLETED AT 3369 ACFT HRS ASFOLLOWS: RED INITIAL 4.794 BIAS 5.142 DIFF.348, BLUE INITIAL 3.937 BIAS 4.280 DIFF .343,YELLOW INITIAL 4.730 BIAS 5.071 DIFF .341,BLACK INITIAL 4.004 BIAS 4.351 DIFF .347 TRCABLE TENSION L/H 165 R/H 165 @ 22 DEG.CELCIUS.

06-Dec-2008 2

FT DRUM NY 13602

GW604262

DOL AVIMTR DS SUPPORTS WERE REPLACED AT3369ACFT HRS AS PER MEC # F84663 DATED 20NOV 08 AT STA. 470.0, RUN OUT .021,STA.531.0 RUN OUT .032, & STA.592.0 RUNOUT .031 MAX. ALLOWED .060 AT ALL STA.

06-Dec-2008 3

FT DRUM NY 13602

GW604262

DOL AVIMUH-60-07-ASAM-08 HAMILTON-SUNDSTRANDHMU COMPLIED WITH AT 3369 ACFT HRS.

15-Dec-2008 1

FT DRUM NY 13602

GW604262

DOL AVIMH-60-08-ASAM-02 POWER AVAILABLECONTROL CABLE COMPLIED WITH AT 3369ACFT HRS.

15-Dec-2008 2

FT DRUM NY 13602

GW604262

DOL AVIMH-60-08-AMAM-05 GOODRICH INTERNALRESCUE HOISTS COMPLIED WITH NA THISACFT AT 3369 ACFT HRS.

15-Dec-2008 3

FT DRUM NY 13602

GW604262

DOL AVIMH-60-.08-AMAM-06 COMMON MISSILEWARNING SYSTEM COMPLIED WITH AT 3369ACFT HR

15-Dec-2008 4

FT DRUM NY 13602

GW604262

DOL AVIMPMI-1 COMPLETED AT 3369.4 ACFT HRS NEXTDUE PMI-2 AT 3729.4 ACFT HRS

15-Dec-2008 5

FT DRUM NY 13602

GW604262

DOL AVIMH-60-09-ASAM-01 GG ROTORS ASSY C/W AT3373.5 ACFT HRS.

13-Jan-2009 1

FT DRUM NY 13602

GW604262

D.CO 1/150TH AHBH-60-09-ASAM-04 RESCUE HOIST MARK 44MOD 0 CARTRIDGE ACTIVATION DEVICECOMPLIED WITH

05-Mar-2009 1

FT. SILL, OK

FD986611

D.CO 1/150TH AHBH-60-09-ASAM-05 UPDATE TO LIFE LIMITCHANGE FOR TAIL ROTOR QUADRANTSPRING CAPSULES COMPLIED WITH

05-Mar-2009 2

FT. SILL, OK

FD986611

AASFH60-09-ASAM-07 FIRE EXTINGUISHER WIRING(BREAK AWAY THREAD) COMPLIED WITH .

06-Apr-2009 1

FT. LEONARD WOOD,MO

DB707781



8.7.DATE

6.REMARKS

4. 5.



AAFAH60-09-ASAM-07 FIRE EXTINGUISHER WIRING(BREAKAWAY THREAD) COMPLIED WITH

06-Apr-2009 2

SPRINGFIELD, MO 65803

DB707781

FAASF#2AIRCRAFT TRANSFERRED TO C. CO. 1-106THAVN REGT, WYDECO FORT LEONARD WOOD,MO.

14-Apr-2009 1

FT. LEONARD WOOD,MO 65101

DB889823

AASFH-60-09-ASAM-08 ENGINE COWLING WEIGHTRESTICTION,COMPLIED WITH 3475 A/C HRS.

13-May-2009 2

FT. LEONARD WOOD,MO

DB707781

AAFAH60-09-ASAM-08 ENGINE COWLING WEIGHTRESTRICTION COMPLIED WITH

13-May-2009 3

SPRINGFIELD, MO 65803

DB707781

SAAFAH-60-09-ASAM-09 FIRE EXTINGUISHER WIRING(BREAKAWAY THREAD) C/W @ 3481.5 ACFTHRS

19-May-2009 1

SPRINGFIELD, MO

JM962206

MO-AVCRADH-60-09-ASAM-11 CARGO DOOR WINDOWJETTISON HANDLE COMPLIED WITH @3541.2A/C HRS.

29-Jun-2009 1

FT. LEONARD WOOD,MO

DB707781

AASFH-60-09-AMAM-04 CO-PILOT SEATINTEREFENCE WITH A2C2S, COMPLIED WITH

25-Aug-2009 1

FT. LEONARD WOOD,MO

DB707781

MO-AVCRADH-60-09-AMAM-05 (N/A) PUBS CHANGE. 26-Aug-2009 1

SPRINGFIELD, MO.

RW626133

AASFH-60-09-AMAM-06 CARGO HOOK CARTRIDGEACTUATED DEVICE (CAD) LIFE REDUCTION

27-Aug-2009 1

FT. LEONARD WOOD,MO

DB707781

AASFH-60-09-AMAM-06 CARGO HOOK CARTRIDGEACTUATED DEVICE (CAD) LIFE REDUCTIONCOMPLIED WITH

27-Aug-2009 2

FT. LEONARD WOOD,MO

DB707781

MOAVCRADH-60-09-AMAM-07 HALON HAND-HELD FIREEXTINGUSHERS,COMPLIED WITH

21-Sep-2009 2

FT. LEONARD WOOD,MO

DB707781

FT HOOD AFMAACE PERFORMED AT 3570 AIRCRAFT HOURSAT SPRINGFIELD, MO BY TEAM MEMBERS K &Q.

28-Sep-2009 1

FT. LEONARD WOOD,MO

WS244328

SAAFAH-60-10-ASAM-03 FIRE BOTTLE DISCHARGELINES AND NOZZLES, COMPLIED WITH AT A/CHRS 3651.1 HRS.

13-Nov-2009 1

FT. LEONARD WOOD,MO

DB707781

SAAFAAFT BELLCRACK SPT ASSY,P/N 70400-08117-051,NSN 1560-01-374-7157,S/N E38000031.RECIEVED MEC # F100456,DATED 4 NOV2009,FOR AN 67.0 HOUR EXTENSION TOALIGN REPLACEMENT WITH THE NEXT PMI 2AT 3730.0 A/C HRS.

16-Nov-2009 1

FT. LEONARD WOOD,MO

DB707781

MO-AVCRADH-60-10-ASAM-04 SAS LINKS. ENTRIES MADEAS REQUIRED ON DA FORM 2408-13-1 IAWPARA 7.1 OF THE ASAM. THIS COMPLETESTHE FIRST REQUIREMENTS OF THE ASAM ASSTATED IN PARA 7.5

18-Nov-2009 1

SGF., MO.

RW626133



8.7.DATE

6.REMARKS

4. 5.



SAAFAH-60-10-AMAM-04 ASN-128B/C DOPPLERGLOBAL POSITIONING SYSTEM GPSNAVIGATION SET COMPLIED WITH

23-Nov-2009 1

FT. LEONARD WOOD,MO

DB707781

AAFAH-60-AMAM-05INTERGRATED MATERIALMANAGEMENT CENTER (IMMC) LEGITMATECODE FILE (LCF) CHANGE 60BREQUIREMENTS,COMPLIED WITH AT 3694.3A/C HRS.

08-Dec-2009 1

FT. LEONARD WOOD,MO

DB707781

AAFAH-60-10-ASAM-04, RELPACED PITCH LINK(P/N70410-02334-045,S/N SA607114) REPLACEDYAW LINK (P/N 70410-02334-045,S/NN108100471.

07-Jan-2010 1

FT. LEONARD WOOD,MO

DB707781

URS MOAVCRADH-60-10-AMAM-06 N/A THIS ACFT 10-Feb-2010 1

SPRINGFIELD MO

MM413003

URS MOAVCRADH-60-10-AMAM-11 OIL SAMPLING SCHEDULECHANGES C/W

08-Mar-2010 1

SPRINGFIELD MO

MM413003

FT HOOD AFMAACE PERFORMED AT 3729 AIRCRAFT HOURSAT SPRINGFIELD, MO BY TEAM MEMBERS K &Q.

22-Apr-2010 1

FT. LEONARD WOOD,MO

WS244328

MOAVCRADH-60-06-ASAM-02 C/W @ 3729 ACFT HOURS(LATE ENTRY)

11-May-2010 1

SPRINGFIELD MO

MM413003

MOAVCRADH-60-10-ASAM-01 C/W @ 3729 ACFT HOURS 17-May-2010 1

SPRINGFIELD MO

MM413003

MOAVCRADH-60-10-AMAM-12 CW @ 3729 ACFT HRS 17-May-2010 2

SPRINGFIELD MO

MM413003

MOAVCRADH-60-10-ASAM-07 C/W @ 3729 ACFT HRS 17-May-2010 3

SPRINGFIELD MO

MM413003

AAFAH-60-10-ASAM-08 AUXILIARY POWER UNIT(APU) AND APU FIREWALL, COMPLIED WITH.

01-Jun-2010 1

FT. LEONARD WOOD,MO

DB707781

AAFAH-60-10-SOF-02 SPINDLE LUG (NDI) ANDRETIREMENT LIFE CHANGES,COMPLIEDWITH.

21-Jun-2010 1

FT. LEONARD WOOD,MO

DB707781

AAFAH-60-10-AMAM-16 COMMON MISSILEWARNING SYSTEM GUARDED DISPENSESWITCH, COMPLIED WITH

28-Jun-2010 1

FT. LEONARD WOOD,MO

DB707781

AAFAH-60-ASAM-11 COMMON COPONENTRETIREMENT CHANGE TIMES UPDATED,COMPLIED WITH.

09-Aug-2010 1

FT. LEONARD WOOD,MO

DB707781

AAFAH-60-ASAM-11 COMMON COPONENTRETIREMENT CHANGE TIMES UPDATED,COMPLIED WITH.

09-Aug-2010 2

FT. LEONARD WOOD,MO

DB707781

AAFAH-60-10-ASAM-12 T700 SERIES ENGINESCOMMON COMPONENT RETIREMENT CHANGETIMES, COMPLIED WITH.

23-Aug-2010 1

FT. LEONARD WOOD,MO

DB707781



8.7.DATE

6.REMARKS

4. 5.



AAFAH-60-10-ASAM-15 IMPROVED EXTERNALSTORES SUPPORT SYSTEM (ESSS) FUELSYSTEM VENTELBOW, COMPLIED WITH.

25-Aug-2010 1

FT. LEONARD WOOD,MO

DB707781

AAFAH-60-10-ASAM-16 RESCUE HOIST CABLE CUTHARNESS CONNECTOR,COMPLIED WITH.

09-Sep-2010 1

FT. LEONARD WOOD,MO

DB707781

AAFAH-60-11-AMAM-03 (OIL COOLER FAN AXIALBEARING)C/W AT 3969.5 ACFT HRS

26-Oct-2010 1

FT. LEONARD WOOD,MO

DB707781

AAFAH-60-11-ASAM-04 (AN/ARN-153 TACANRECEIVER BEARING ERROR)C/W AT 3984.1ACFT HRS,N/A THIS ACFT

03-Dec-2010 1

FT. LEONARD WOOD,MO

DB707781

AAFAH-60-11-AMAM-04 (CODE FILE CHANGE 61REQUIREMENTS) C/W AT 3994.8 ACFT HRS.

09-Dec-2010 1

FT. LEONARD WOOD,MO

DB707781

FAASF#2COMPLIED WITH H-60-ASAM-06 28-Dec-2010 1


FAASF#2COMPLIED WITH THE REQUIREMENTS OF H-60-11-AMAM-06 (MEDEVAC CAROUSEL) AS NOTINSTALLED

07-Feb-2011 1


BH787046

AAFAH-60-11-ASAM-08 (LOS)(IFF) AND (IVHMS)CONNECTOR SAFETY WIRE , COMPLIED WITH.

09-Feb-2011 1

FT. LEONARD WOOD,MO

DB707781

FAASF#2H-60-11 ASAM-09 COMPLIED WITH AS N/A 07-Apr-2011 2


FAASF@2COMPLIED WITH THE REQUIREMENTS OF H-60-AMAM-09

22-Apr-2011 1


BH787046

FAASF#2COMPLIED WITH THE REQUIREMENTS OF H-60-AMAM-11

22-Apr-2011 2


BH787046

FAASF#2OMPLIED WITH THE REQUIREMENTS OF H-60-11-AMAM-13 AS NOT APPLICABLE

07-Jun-2011 1


FT HOOD AFMAACE COMPLETED AT 4082 AIRCRAFT HOURSAT FT LEONARD WOOD, MO BY TEAMMEMBERS W & Q.

23-Jun-2011 1


WS244328

AASF#2COMPLIED WITH THE REQUIREMENTS OF H-60-11 ASAM-13

29-Jun-2011 1


AASF#2COMPLIED WITH THE REQUIREMENTS OH H-60-11-SOF-01

08-Jul-2011 1




8.7.DATE

6.REMARKS

4. 5.



AASF#2COMPLIED WITH THE REQUIREMENTS OF H-60-11-ASAM-14

18-Jul-2011 1


AASF#2COMPLIED WITH THE REQUIREMENTS OH H-60-11-AMAM-15

13-Sep-2011 1


AASF#2COMPLETED ULLSA(E) LCF CHANGE 62 29-Sep-2011 1


BH787046

AASF#2COMPLIED WITH THE REQUIREMENTS OF H-60-11-AMAM-20

04-Oct-2011 1


AASF#2COMPLIED WITH THE REQUIREMENTS OF H-60-12-SOF-01

11-Oct-2011 1


BH787046

AASF#2COMPLIED WITH THE REQUIREMENTS OF H-60-12-SOF-02

11-Oct-2011 2


BH787046

FAASF#2REMOVED IBF CONTROL HEAD 22-Nov-2011 1


FAASF#2REMOVED MANUAL CHAFF DISPENCERCONTROL HEAD.

22-Nov-2011 2


AASF#2COMPLED WITH THE REQUIRMENTS OF H-60-12-ASAM-02

06-Dec-2011 1


BH787046

MO-TASMGMEC# F137731 A (REPAIR OF R/H 34.5 BEAM)COMPLETED AT 4086.3 ACFT HOURS

10-Jan-2012 1

FT. LEONARD WOOD,MO

SC625917

AASF#2COMPLIED WITH THE REQUIREMENTS OF H-60-11-AMAM-20

25-Jan-2012 1


AASF # 1ACFT TRANSFERRED TO A CO, 1-185TH AHB,WTQGA0, JACKSON MS

16-Feb-2012 1

JACKSON, MS 39209-3436

AB198454

AASF # 1H-60-12-AMAM-06, INTERCOMMUNICATIONSYSTEM (ICS) CABLE ROUTING ANDCLAMPING, DOES NOT APPLY TO UH-60A

21-Feb-2012 1


AB198454

AASF #1H-60-12-ASAM-06, FUEL SYSTEM BREAKAWAYVALVE & FIRE SYSTEM DIRECTIONAL VALVE,INSP OK/PASS

21-Feb-2012 2


AB198454

AASF # 1H-60-12-SOF-04, BREEZE EASTERN EXTERNALRESCUE HOIST OPERATIONS, COMPLIEDWITH. EXTERNAL HOIST NOT INSTALLED ONTHIS AIRFRAME, SOF IS COMPLETE.

21-Feb-2012 3


AB198454



8.7.DATE

6.REMARKS

4. 5.



AASF # 1**LATE ENTRY** H-60-11-AMAM-17, TAILROTOR INBOARD/OUTBOARD RETENTIONPLATE SHIMS, PREVIOUSLY COMPLIED WITHON 25JAN12 AT FT LEONARDWOOD MO.INSPECTION PASSES.

07-Mar-2012 1


AB198454

AASF # 1H-60-12-AMAM-07, MAIN ROTOR BLADEWATER INTRUSION INSPECTION, DOES NOTAPPLY TO THIS AIRCRAFT. (H-60M ONLY)

08-Mar-2012 1


AB198454

FT. HOOD AFMAMWO 1-1520-237-30-3 AUTO RELIGHT APPLIEDTO ACFT @ 4125 HRS BY FT. HOOD AFMA

07-May-2012 1

BOISE, IDAHO

DB082704

A CO 1-168 GSABMWO 1-1520-237-20-3, T700-701D ENGINE MODAPLIED TO ACFT @ 4125 ACFT HRS.

09-May-2012 1

FT. HOOD, TX

BJ117531

A CO 1-168 AVNACFT TRANSFERRED TO A CO 1-168 AVN AT4125.0 ACFT HRS.

09-May-2012 2

BOISE, IDAHO

BJ117531

1108TH TASMGA-MWO 1-1520-237-SATCOM WITH CHANGE 6APPLIED TO ACFT @ 4145.0 ACFT HRS

16-Jun-2012 1

BAF

DH575013

D CO. 1-168 GSABCOMPLIED WITH THE REQUIREMENTS OF H-60-12-AMAM-12

14-Jul-2012 1

BAGRAM, AFG

RN021857

D CO TF TALON**LATE ENTRY** H-60-12-AMAM-03(TRANSPONDER AND CMWS INSTALLATION)PREVIOUSLY COMPLIED WITH ON 31 OCT 11AT FT LEONARDWOOD MO. CMWS MWO NOTINSTALLED

22-Jul-2012 1

BAGRAM, AFG

CM173024

D. CO 1-168TH GSABCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-08

23-Jul-2012 1

BAGRAM, AFG

RN021857

D CO. 1-168TH GSABCOMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-09 @ 4307.0 ACFT HOURS

29-Jul-2012 1

BAGRAM, AFG

RN021857

D CO 3-82 GSABCOMPLIED WITH [email protected] HRS

31-Jul-2012 1

BAGRAM, AFG

JH469582

D CO 3-82 GSABCOMPLIED WITH REQUIREMENTS [email protected] ACFT HR

01-Aug-2012 1

BAGRAM, AFG

JH469582

D CO. 1-168TH GSABCOMPLIED WITH REQUIREMENTS OF [email protected] HRS

04-Aug-2012 1

BAGRAM, AFG

JH469582

D CO 1-168TH GSABMEC # F151496 EXTENTION OF UP TO 120DAYS ON THE 48TH MONTH A670 CABIN TUBINSPECTION.

16-Aug-2012 1

BAGRAM, AFG

RN021857

D CO 1-168TH GSABMEC #F151231 PRIMARY SERVO BEAM P/N70219-02134-048, -50, -52 REQUIREEXTENTION TO NEXT PMI-2

16-Aug-2012 2

BAGRAM, AFG

RN021857

D CO. 1-168TH GSABH-60-12-ASAM-09 (BREEZE EASTERN) NOTREQUIRED EQUIPMENT NOT INSTALLED

23-Aug-2012 1

BAGRAM, AFG

RN021857

D CO. 1-168TH GSABCOMPLIED WHITH REQUIREMENTS OF H-60-12-AMAM-15

31-Aug-2012 1

BAGRAM, AFG

RN021857

B CO 96TH ASB**LATE ENTRY** COMPLIED WITH THEREQUIREMENTS OF H-60-12-SOF-03 @ 4425.6ACFT HRS

02-Sep-2012 1

BAF

CB830490



8.7.DATE

6.REMARKS

4. 5.



B CO 96TH ASB**LATE ENTRY** COMPLIED WITH THEREQUIREMENTS OF H-60-12-SOF-05 @ 4425.6ACFT HRS

03-Sep-2012 1

BAF

CB830490

B CO 96TH ASBMEC# F151231 ADDENDUM TO SERVO BEAMFITTINGS (PN:70219-02134-048, 70219-02134-050, 70219-02134-052) ORIGINAL DISPOSITIONHAD A MIX UP AS TO WHICH PMI INSPECITIONTHE AIRCRAFT WAS IN. 390 HR TIMEEXTENSION REMAINS IN PLACE W/ ORGINALMEC @ (4802.6 ACFT HRS). FITTINGS REQUIREREPLACEMENT AT RESET OR NEXT PMI-1,WHICHEVER OCCURS FIRST.

04-Sep-2012 1

BAF

CB830490

D CO 6-101 GSABCOMPLIED WITH H-60-12-ASAM-01 (TR BEVELGEAR NDI) @ 4425.6 ACFT HOURS

06-Sep-2012 1

BAGRAM, AFG

RN021857

B CO 96TH ASBCOMPLIED WITH THE REQUIREMENTS OF H-60-12-ASAM-11 @ 4425.6 ACFT HRS (NOTAFFECTED THIS AIRCRAFT)

10-Sep-2012 1

BAF

CB830490

B CO 96TH ASBCOMPLIED WITH THE REQUIREMENTS OF H-60-12-ASAM-10 @ 4425.6 ACFT HRS (NOTAFFECTED THIS AIRCRAFT)

10-Sep-2012 2

BAF

CB830490

B CO 96TH ASBCOMPLIED WITH THE REQUIREMENTS OF H-60-12-AMAM-16 @ 4425.6 ACFT HRS

10-Sep-2012 3

BAF

CB830490

B CO 96TH ASBCOMPLIED WITH THE REQUIREMENTS OF H-60-12-AMAM-17 (DOES NOT APPLY TO ACFT -H60M ONLY)

19-Sep-2012 1

BAF

CB830490

B CO 96TH ASBCOMPLIED WITH THE REQUIREMENTS OF H-60-12-AMAM-18 (DOES NOT APPLY TO ACFT -H60M ONLY)

19-Sep-2012 2

BAF

CB830490

B CO 96TH ASBM/R RIG COMPLETED IAWTM 1-1520-BLACKHAWK@ 4425.6 ACFT HRSRED BLADEPOSITIONSARE AS FOLLOWS:LOW COLL ANG90RT 8.5 180FWD-0.4270LFT -10.0 0AFT -0.7TOTAL -2.6 AVG -0.650RED 90RT 8.5 BLUE8.5BLACK 8.4 YELLOW 8.5HIG COLL ANG90RT 20.4 180FWD 12.4270 LFT 9.8 0AFT 17.4TOTAL 60.0 AVG 15.00FWD CYC ANG 90RT -2.0270LFT 31.2 TOTAL 33.20AFT CYC ANG90RT 25.5 270LFT 4.9 TOTAL 20.60LFT CYCANG 180FWD -8.1 0AFT 6.9 TOTAL15.00RHT CYC ANG 180FWD 6.7 0AFT-8.1TOTAL 14.80SERVO ROD BIAS:FWD: 4 FLATSCLOCKWISEAFT: 4 FLATS COUNTERCLOCKWISELAT: 3 FLATS CLOCKWISE(FACING AFT)

20-Sep-2012 1

BAF

CB830490

B CO 96TH ASBT/R RIG COMPLETED IAW TM-1-1520-BLACKHAWK@ 4425.6 ACFT HRST/R RIG IS ASFOLLOWS:PUSH ROD LENGTH: 12.58T/RSERVO INPUT:INIT 3.51 AFTER 3.50INIT 0AFTER 0.05T/R RIG BFR AFT DIFRED4.820 5.150 .33BLU 4.150 4.490 .34YEL4.690 5.010 .32BLK 4.080 4.420 .34CBLTNS L/H 156 R/H 155TEMP 29C AVG155.5 DIF 1ALLOWABLE DIFFERENCE 3.1

20-Sep-2012 2

BAF

CB830490

B CO 96TH ASBPMI-2 COMPLETED @ 4425.6 ACFT HRS, NEXTPMI-1 DUE @ 4785.6 ACFT HRS

20-Sep-2012 3

BAF

CB830490



8.7.DATE

6.REMARKS

4. 5.



AMCOM TASM-OCONUSA3T EVALUATION COMPLETED AT 4432.4ACFT HRS BY ACE TEAM MEMBERS "F" AND"M"

01-Oct-2012 1

BAGRAM, AFG

TA459908

DCO 6-101 GSABCOMPLIED WITH H-60-13-AMAM-02 07-Nov-2012 1

BAGRAM, AFG

JC246510

D CO 1-168THCOMPLIED WITH H-60-13-AMAM-03(DECU/EDECU TGT BIAS)

28-Nov-2012 1

BAGRAM, AFG

RN021857

D CO 1-168TH GSABCOMPLIED WITH H-60-13-ASAM-01 (ANTICOLLISION POWER SUPPLY)

28-Nov-2012 2

BAGRAM, AFG

RN021857

D CO 1-168THCOMPLIED WITH H-60-13-AMAM-04 (LCF 63CHANGE)

16-Dec-2012 1

BAGRAM, AFG

RN021857

D CO 1-168TH GSABCOMPLIED WITH H-60-13-AMAM-05 (MAILLANDING GEAR WHEEL BRAKE ASSEMBLY)

19-Jan-2013 1

BAGRAM, AFG

RN021857

1109TH TASMG4 SERVO RAIL BEAM REMOVED ANDREPLACED BY CCAD DEPOT FIELD TEAM IAWPROJECT DIR# 13BARJ3-387-00I

26-Feb-2013 1

BAGRAM,AFGHANISTAN 09354

JF986581

1109TH TASMGGUSSET L/H FWD ON THE NO 4 SERVO BEAMREPAIRED IAW MEC F161708

26-Feb-2013 2


JF986581

DYN-CORP INTLCOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-03 (MR SPINDLE ANTI-FLAPASSEMBLY) PASSED

27-Feb-2013 1


JL590345

DYN-CORP INTLMEC GRANTED FOR REPAIR OF R/S BEADEDPANEL BROKEN TANG (F161869).

01-Mar-2013 1


JL590345

DYN-CORP INTLMEC GRANTED FOR REPAIR OF STA 729 SKINWEAR. MEC# F162020

02-Mar-2013 1


JL590345

DYN-CORP INTLMEC GRANTED FOR USE OF CPC(MIL-C-16173E) GRADE 1 AS ALTERNATE TO CPC(MIL-C-16173) IN THE FUEL CELL AREA. MEC #F162022

02-Mar-2013 2


JL590345

DYN-CORP INTLT/R RIG COMPLETED AT 4779.4 ACFT HRS.NUMBERS ARE= INITIAL RED- -1.26, BLK- -1.56,YELL- -1.25, BLU- -1.54, DIM A= RED- 4.75,BLK- 4.12, YELL- 4.82, BLU- 4.00, DIM B= RED-5.10, BLK- 4.45, YELL- 5.13, BLU- 4.38,DIFFERENCE= RED- 0.35, BLK- 0.33, YELL-O.31, BLU- 0.38. FINAL DEG= RED-3.01, BLK-3.01, YELL- 3.00, BLU- 3.00 COMPLETED IAW H-60-13-AMAM-01

12-Mar-2013 1


JL590345

DYN-CORP INTLMAIN ROTOR RIG COMPLETED AT 4779.4ACFT HOURS, IAW H-60-13-AMAM-01.NUMBERS ON FILE WITH DYN-CORP. FWDBIAS=+1 FLAT AFT BIAS=+1 FLAT LATBIAS=+3FLATS

12-Mar-2013 2


JL590345

DYN-CORP INTLT/R CABLE TENSION CHECK COMPLETED AT4779.4 ACFT HRS. NUMBERS ARE L=145,R=145, TEMP=22 CELCIUS

12-Mar-2013 3


JL590345



8.7.DATE

6.REMARKS

4. 5.



DYN-CORP INTLCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-01 (T/R RIG) AMTRACKS UPDATED

12-Mar-2013 4


JL590345

TASM-OPMI 1 AND 2 COMPLETED @ 4779.4 ACFT HRS.NEXT PMI DUE IS PMI [email protected] CFT HRS

16-Mar-2013 1


EW744892

DYNCORP TASM-0COMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-07 ( LDS CABLE CLEARANCE)

25-Mar-2013 1


EW744892

DYNCORP TASM-OCOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-04 (PMB)

25-Mar-2013 2


EW744892

AECOMT/R CABLE TENSION CHECK COMPLETED AT4790.4 ACFT HRS. NUMBERS ARE L=150,R=150, TEMP=22 CELCIUS

31-Mar-2013 1


SS706201

D CO 6/101ST GSABCOMPLIED WITH THE REQUIREMENTS OF H-60-13-ASAM-05 (RESCUE HOIST) @ 4810.4 ACFTHRS

08-Apr-2013 2


BB500107

D CO 6/101ST GSABCOMPLIED WITH THE REQUIREMENTS OF H-60-13-ASAM-06 (PMI CHECK LIST CHG) @ 4918.9ACFT HRS

08-May-2013 1

BAF

BB500107

D C0 3-10 GSABCOMPLIED WITH THE REQUIREMENTS OF H-60-13-SOF-01 (AHRS) @ 5025.6 ACFT HRS

31-May-2013 1

BAF

BB500107

D CO 3-10 GSABCOMPLIED WITH THE REQUIREMENTS OF H-60-13-AMAM-11 (XMSN FILTER BOWLATTACHMENT HWD) @ 5138.3 ACFT HRS.

01-Jul-2013 1

BAF

BB500107

D C0 3-10 GSABREPAIRED RIGHT HAND ENGINE SHEAR DECKSTA. 350 WL 35R I/A/W MEC # F168683 BY1106TH TASMG @ 5138.3 ACFT HRS.

04-Jul-2013 1

BAF

BB500107

D 3/10 GSABT/R TENSION CHECK COMPLETED @ 5138.3ACFT HRS. R/H 169 LBS, L/H 168 LBS @ 29DEGREES CELCIUS

10-Jul-2013 1

BAF

AS587078

D 3/10 GSABT/R RIG CHECK COMPLETED @5138.3 ACFTHRS. INITIAL DEGREE: RED-3.0,BLK-3.0,YEL-3.0,BLU-3.0 FINALDEGREE: RED-2.9,BLK-3.0,YEL-3.1,BLU-3.0 DIM A: RED-4.813,BLK-4.160,YEL- 4.865,BLU-4.133 DIM B:RED5.138,BLK-4.482,YEL-5.210,BLU-4.420DIFFERANCE: RED-.325,BLK-.322,YEL-.345,BLU-.287

10-Jul-2013 2

BAF

AS587078



8.7.DATE

6.REMARKS

4. 5.



D 3/10 GSABM/R RIG CHECK COMPLETED AT 5138.3 ACFTHRS. LOW COLL ANGLE: 90 RT 8.8,180 FWD -2.1,270 LFT -9.8,0 AFT 1.2,TOTAL -1.9 AVG -0.475. HIGH COLL ANGLE: 90 RT 19.5,180 FWD20.8, 270 LFT 11.4, 0 AFT 9.7, TOTAL 61.4, AVG15.35, MIN RANGE 15.825 . FWD CYCLICANGLE: 90 RT -1.9, 270 LFT 31.1, TOTAL 33.0 .AFT CYCLIC ANGLE: 90 RT 25.4, 270 LFT 4.5,TOTAL 20.9 . LEFT CYCLIC ANGLE: 180 FWD -8.5, 0 AFT 6.7, TOTAL 15.3 . RIGHT CYCLICANGLE: 180 FWD 6.3, 0 AFT -7.8, TOTAL 14.1 .PRIMARY SERVO CONTROL ROD BIAS: FWD 1FLAT CLOCKWISE, AFT 1 FLATCOUNTERCLOCKWISE, LAT NOADJUSTMENT.

10-Jul-2013 3

BAF

AS587078

D C0 3-10 GSABPMI-1 COMPLETED @ 5138.3 ACFT HRS NEXTPMI DUE IS PMI-2 @ 5498.3 ACFT HRS

11-Jul-2013 1

BAF

BB500107

D CO 3-10 GSABCOMPLIED WITH THE REQUIREMENTS OF GEN-13-AMAM-04 (AN/APN-209 RADAR ALTIMETERSET COMPONENT TRACKING)

16-Jul-2013 1

BAF

BB500107

AECOMM/R COMPLETE RIG: @ 5143.1 ACFT HOURS.LOW COLL ANGLES: 90 RT: 9.1 , 180 FWD: -1.1, 270 LFT: -10.5 , 0 AFT: 0.1 , TOTAL: -2.4 , AVG:-0.600HIGH COLL ANGLE: 90 RT: 20.7 , 180FWD: 12.2 , 270 LFT: 9.5 , 0 AFT: 18.0 , TOTAL:60.4 , AVG: 15.1COLL ANGLE SPREAD:15.7FWD CYCLIC ANGLE: 90 RT: -2.4 , 270 LFT:30.8 , TOTAL: 33.2AFT CYCLIC ANGLE: 90 RT:25.8 , 270 LFT: 5.7 , TOTAL: 20.1LEFT CYCLICANGLE: 180 FWD: 8.4 , 0 AFT: 6.7 , TOTAL:15.1RIGHT CYCLIC ANGLE: 180 FWD: 6.8 , 0AFT: 7.4 , TOTAL: 14.2PRIMARY SERVOCONTROL ROD BIAS: FWD: -1 FLAT , AFT: +1FLAT , LAT: -3 FLATS

17-Jul-2013 1

BAGRAM AF,AFGHANISTAN

SS706201

AECOMTAIL ROTOR COMPLETE RIG PERFORMED @5143.1 ACFT HOURS. CABLE TENSIONS R: 152L: 154 @ 28C 1ST DEG2ND DEG FINAL DEG. DIM A DIMB DIFF.RED 3.0 2.93.0 4.75 5.10.350BLACK 3.0 3.03.0 4.11 4.42.310YELLOW 3.0 3.13.0 4.88 5.17 .290BLUE3.0 3.0 3.0 4.024.40 .380

18-Jul-2013 1


SS706201



8.7.DATE

6.REMARKS

4. 5.



AECOMTAIL ROTOR COMPLETE RIG PERFORMED @5147.7 ACFT HOURS. CABEL TENSIONS R: 172L: 172 @ 33C 1ST DEG2ND DEG FINAL DEG. DIM ADIM B DIFFRED 3.02.9 3.1 4.812 5.102.290BLACK 3.0 3.03.0 4.119 4.419 .300YELLOW 3.0 3.13.1 4.859 5.179.320BLUE 3.0 3.13.0 4.088 4.408 .320

27-Jul-2013 1


SS706201

AECOMTAIL ROTOR RIG CHECK COMPLETED @5157.3 ACFT HOURS. 1STDEG 2ND DEG FINAL DEG DIM A DIMB DIFFRED 3.2 3.23.2 5.120 5.120 0BLACK3.1 3.1 3.1 4.4404.440 0YELLOW 3.2 3.23.2 5.200 5.200 0BLUE3.2 3.2 3.2 4.4254.425 0

01-Aug-2013 1


SS706201

D C0 3-10 GSABCOMPLIED WITH THE REQUIREMENTS OF H-60-13-AMAM-10 (LCF CHANGE 64REQUIREMENTS) @ 5191.3 ACFT HRS

11-Aug-2013 1

BAF

BB500107

TASM-O/DYNCORPINTERNATIONAL

A3T INSP COMPLETED AT ACFT TIME 5242.9BY TEAM MEMBER "S"

22-Aug-2013 1

BAF

WC643445

D C0 3-10 GSABTHE GENERATION 3 ELECTRONIC CONTROLUNIT (ECU), WITH OPERATIONAL FLIGHTPROGRAM (OFP) 1.54 (INDIA) SOFTWAREINSTALLED [AWR1896 DTD 05 SEP 13]INSTALLED @ 5315.8 ACFT HRS

18-Sep-2013 1

BAGRAM,AFAGHANISTAN

BB500107

D CO 3-10 GSABCOMPLIED WITH THE REQUIREMENTS OF H-60-13-AMAM-15 (CEFS R/H FUEL CELL COVERPLATE) @ 5354.9 ACFT HRS.

28-Sep-2013 1

BAGRAM,AFAGHANISTAN

BB500107

D CO 3-10 GSABH-60-14-SOF-01, BREEZE EASTERN EXTERNALHOIST. COMPLIED WITH THIS ACFT. HOISTNOT INSTALLED

02-Nov-2013 1

BAGRAM, AFGANISTAN

MD563062

A CO 3-126TH AVNCOMPLIED WITH H-60-14-ASAM-02. R/H SIDEPASS CHECK AND RAP TEST IAW ASAM @5481.9 ACFT HRS.

24-Nov-2013 1

BAGRAM, AFGANISTAN

DM702539

A CO 3-126TH AVNCOMPLIED WITH H-60-14-ASAM-02. L/H SIDEPASS CHECK AND RAP TEST IAW ASAM @5481.9 ACFT HRS.

24-Nov-2013 2

BAGRAM, AFGANISTAN

DM702539

AECOMT/R BLADE S/N: A00905651, DE-ICEELECTRICAL CONNECTORS MODIFIED IAWAWR 1692, DATED 24 JAN 13 (R5)

20-Dec-2013 1

BAGRAM, AFGANISTAN

RB867980

AECOMT/R BLADE S/N: A00907293, DE-ICEELECTRICAL CONNECTORS MODIFIED IAWAWR 1692, DATED 24 JAN 13 (R5)

20-Dec-2013 2

BAGRAM, AFGANISTAN

RB867980

AECOMCOMPLIED WITH H-60-14-AMAM-03. LATERALSWASHPLATE LINK VERIFIED "PASS" BYSERIAL NUMBER CHECK

26-Dec-2013 1

BAGRAM, AFGANISTAN

RB867980



8.7.DATE

6.REMARKS

4. 5.



AECOMXMSN HOUSING S/N: A211-01153 ISAPPROVED FOR A TBO EXTENSION OF 41.1HRS @ 5493.1 ACFT HRS, NEW TBOREPLACEMENT IS DUE AT 5812.0 ACFT HRS,IAW MEC # F176774A

26-Dec-2013 2

BAGRAM, AFGANISTAN

RB867980

AECOMMEC F177583 AUTHORIZATION IS GRANTEDTO TEMPORARY REPAIR THE CRACKED RHFORWARD DOOR POST ANGLE, PN 70070-20566-107. STOP DRILL WAS DONE IAW 1-500-323-204-10. OPERATION WITH THE ABOVETEMPORARY REPAIR IS AUTHORIZED FOR APERIOD NOT TO EXCEED 40 ACFT HOURS.LAR RECOMMENDS THAT DOOR POST MWOKIT 50-22 BE INSTALLED ID ACFT IN GOING TOBE INDUCTED INTO RESET.

13-Jan-2014 1


DT661605

AECOMMEC F177091 REPAIRED WAS WAS BY 1107THTASM ON THE PRIMARY SKIN LOACTEDUNDERTHE SHIMMED MANIFOLD STA 288, BL10R & BL 10R, WL 260. PRIMARY SKIN IS 7575T6 .025 FLASH PATCH REPAIR WAS UTILIZEDWITH THE FLUSH PORTION EVEN WITH THEPRIMARY SKIN OF THE HYDRAULIC DECK.

13-Jan-2014 2


DT661605

AECOMMEC F176774 A APPROVAL IS GRANTED TOEXTEND THE TBO ON MAIN TRANSMISSIONHOUSING ASSEMBLY (P/N 70351-08110-045,S/N A211-01153) BY 41.1 HRS. THIS IS A ONETIME AUTHORIZATION.

13-Jan-2014 3

BAGRAM, AFGANISTAN

DT661605

AECOMM/R RIG COMPLETED READS AS FOLLOWS:90RT 180 FWD 270LFT 0 AFT TOTALAVG LOW COLL ANGLE 9.7 -0.3-10.5 -0.9 -2.0 0.500HIGH COLLANGLE 22.0 14.5 9.5 17.563.5 15.88COLL ANGLE SPREAD16.38FW CYCLIC ANGLE 1.6-31.4 33.00AFT CYCLIC26.1 5.121.02LEFT CYCLIC 7.77.4 15.10RT CYCLIC8.7 6.6 `15.33 PRIAMRYSERVO CONTROL ROD BIAS: FWD 4 FLATS-CW AFT 4FLATS CCW LAT 3 FLAT CWBALDEANGLE MEASUREMENTS: BLADE SET1ST 2ND FINALRED.06 3.00 3.013.01BLUE -.1.693.00 3.00 3.02YELLOW.08 3.00 2.982.97BLACK -1.193.00 3.01 2.99DIM A DIM B DIF RED5.340 5.710 .370 BLUE4.700 4.980 .280 LH 153 RH152 TEMP 23YELLOW5.370 4.980 .360 BLACK4.610 4.940 .330

13-Jan-2014 4

BAGRAM, AFGANISTAN

DT661605

AECOMCOMPLIED WITH H-60-14-ASAM-04 MAINROTOR ASSY

14-Jan-2014 1

BAGRAM, AFGANISTAN

DD293466



8.7.DATE

6.REMARKS

4. 5.



AECOMCOMPLIED WITH H-60-14-AMAM-03DISCREPANT CONNECTING LINK

14-Jan-2014 2

BAGRAM, AFGANISTAN

DD293466

AECOM PMI 2 COMPLETED @ 5493.1 ACFT HRS NEXTPHASE DUE AT 5853.1

14-Jan-2014 3

BAGRAM, AFGANISTAN

DD293466

AECOMT/R RIG COMPLTED RED:3.01, BLUE:3.02,YELLOW:2.97, BLACK 2.99. T/R CABLETENSION: 23 DG C, L/H 153, R/H 152. T/RPISTON TRAVEL 3.45.

14-Jan-2014 4

BAGRAM, AFGANISTAN

DT661605

AASF# 1H-60-14-AMAM-08, AN/ASC-15E C/B PANEL,C/W, NOT INSTALLED.

26-Mar-2014 1

OTIS CGAS, MA 02542

KM567930

AASF#1H-60-14-AMAM-12 SPINDLE NUT RETIREMENTLIFE EXTENSION , C/W

01-May-2014 1

OTIS CGAS, MA 02542

MD563062

DRUM AFMALATE ENTRY H-60-14-ASAM-03 (ENGINE INLETBARRIER FILTERBRACKET REMOVAL(CORRECTION) ) PREVIOUSLY COMPLIEDWITH

21-May-2014 1

FT. DRUM, NY 13602

JJ682125

DRUM AFMALATE ENTRY H-60-13-AMAM-06 (CRASHWORTHY EXTERNAL FUEL SYSTEM(CEFS) ) PREVIOUSLY C/W N/A THIS ACFT.

21-May-2014 2

FT. DRUM, NY 13602

JJ682125

DRUM AFMALATE ENTRY H-60-14-AMAM-10 (HONTEKCOATED MAIN ROTOR BLADE REMOVAL )COMPLIED WITH 16 MAY 14, NA THIS ACFT.

21-May-2014 3

FT. DRUM, NY 13602

JJ682125

DRUM AFMA H-60-14-AMAM-05 ( ULLS-A(E) ALCLEGITIMATE CODE FILE (LCF)CHANGE 65)COMPLIED WITH

21-May-2014 4

FT. DRUM, NY 13602

JJ682125

AFMAACFT 8023455 COMPLETED ACE ON 5 JUNE2014 AT 5493.1 ACFT HRS AT FORT DRUMRESET BY TEAM MEMBER 00.

23-Jun-2014 1

FT. DRUM, NY 13602

DM489127

AFMA FT. DRUMCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-14 ( INTEGRATED VEHICLE HEALTHMANAGEMENT SYSTEM (IVHMS) CABLING )THIS DATE IN RESET

25-Jun-2014 1

FT. DRUM, NY 13602

JJ682125

AFMA FT DRUMCOMPLIED WITH H-60-14-ASAM-06 (FLIGHTCONTROL MIXER ASSEMBLY) REPLACEDWITH S/N B995-01908 P/N 70400-02300-048THIS DATE IN RESET AT 5493.1 ACFT HRS

02-Jul-2014 1

FT. DRUM, NY 13602

JJ682125

AFMA FT DRUMCOMPLIED WITH H-60-14-SOF-03(DISCREPANT SELF LOCKING DOUBLEHEXAGON NUTS) THIS DATE IN RESET AT5493.1 ACFT HOURS.

07-Jul-2014 1

FT. DRUM, NY 13602

JJ682125



8.7.DATE

6.REMARKS

4. 5.



AFMAMAIN ROTOR AND T/R COMPLETE RIGCOMPLETED AT 5493.1 ACFT HRS.FWDPRIMARY ROD SHORTENED -1 FLATS,AFTPRIMARY ROD LENGTHENED 1 FLATSANDLAT PRIMARY ROD SHORTENED -2.5FLATS.LEFT TR CABLE TENSION 160RIGHTCABLE TENSION 160 AT 70DEGREESFAHRENHEIT. TR BIASIS RED DIM A5.260 DIM B5.620 DIFF OF.360FINAL ANGLE 3DEG, BLACK DIM A 4.605DIM B 4.910 DIFF OF.305 FINAL ANGLE 3DEG, YELLOW DIM A 5.370DIM B 5.650 DIFFOF .280 FINAL ANGLE 3 DEG,BLUE DIM A4.600 DIM B 4.934 DIFF OF .334FINALANGLE 3 DEG

14-Jul-2014 1

FT. DRUM, NY 13602

DM489127

AFMACOMPLIED WITH H-60-14-AMAM-16 ATTITUDEHEADING REFERENCE UNIT (AHRU) 2410TRACKING

15-Jul-2014 1

FT. DRUM, NY 13602

DM489127

AFMA FT DRUMCOMPLIED WITH REQUIREMENTS OF TB 1-1520-237-30-1 , HH-60L/UH-60A/LAIRCRAFTDESERT OPERATIONS SPECIALINSPECTIONAND CLEANINGREQUIREMENTS IN [email protected] ACFT HRS

25-Jul-2014 1

FT. DRUM, NY 13602

JJ682125

AFMA FT DRUMCOMPLETED 48 MONTH FUEL CELLCORROSION INSP , FLIGHT CONTROLRODINSP , CABIN TUB INSPECTION,ANDREPLACED FUEL CELL O-RINGS INRESET @ 5493.1 ACFT HRS

25-Jul-2014 2

FT. DRUM, NY 13602

JJ682125

AFMA FT DRUMALL PHASE INSPECTIONS FOR PMI -1 AND PMI-2 COMPLETED DURING RESET @ 5493.1 ACFTHRS, NEXT PHASE INSPECTION DUE AT 5853.1ACFT HRS.

25-Jul-2014 3

FT. DRUM, NY 13602

JJ682125

AFMA FT DRUMCOMPLIED WITH H-60-14-ASAM-09 (ENGINEOUTPUT SHAFT) THIS DATE IN RESET AT5497.8 ACFT HRS.

01-Aug-2014 1

FT. DRUM, NY 13602

JJ682125

AFMA FT DRUMMEC F184484 L/H CARGO DOOR VOIDAPPLIED IN RESET AT 5493.1 ACFT HRS.

05-Aug-2014 1

FT. DRUM, NY 13602

JJ682125

AFMA FT DRUMMEC F184606 B,ANGLE BRACKET PN 70211-03002-162, APPLIED IN RESET AT 5493.1 ACFTHRS.

05-Aug-2014 2

FT. DRUM, NY 13602

JJ682125

AASF#3 NYARNGAIRCRAFT TRANSFERRED FROM AASF# 1, MACO A 3/126 AVN UIC: WPNVAO,TO AASF# 3,LATHAM, NYARNG UIC:WUATA0 AT 5501.1ACFT HOURS

19-Aug-2014 1

LATHAM, NY 12110-2299

RJ520909



8.7.DATE

6.REMARKS

4. 5.



AASF#3 NYARNGUPDATED THE FOLLOWING AWRS TO THIERCURRENT REVISON NUMBERS:AWR 980 R10DTD 18APR14(RESCUE HOIST EQUIP.):AWR1037R12 3 JAN 14 (SATCOM RADIO); AWR1127R5 DTD 25 JAN 13 HELIBASKET OPS,AWR 1309R8 14 APR 14(OREGON AERO SEATCUSHIONS); AWR1324R11 18 SEP 12 (CMWS);AWR 1346R21, 24 JAN 14 (IVHMS); AWR1425R17 18 SEP 12 (CMWS P3I); AWR 1444 R714 APR 14,( SINGLE AHRU), AWR 1453R3 08NOV 12 (AIR WARRIOR)); AWR 1494R7 29 JUN12 (CMWS 5TH SENSOR); AWR 1513R7, 21MAY14 (IPAC SOFTWARE); AWR 1516 R7DATED 11 OCT 12 (ELT); AWR 1524R4 14 DEC12 (BAPS); AWR 1529R3 30 OCT 13(AHRU/FOGS); AWR 1566R3 18 MAR 13 (CABLEGUARD); AWR 1590R5 4 APR 14(AN/ARN-147VOR/MOUNT BASE); AWR 1607R5 29 MAR 13(LED CDU & PDU); AWR 1648R3 28 MAR 14(MAGNUS LAPTOP ONBOARD ANDOPERATING); AWR 1682R14 26 FEB 14 (T700-GE-701D ENGINE AUTO RELIGHT); AWR1692R6 19 JUN 14(NEW DESIGN DE-ICECONNECTOR); AWR 1694R4 06 JAN 14 (DUALSTABILATOR CONTROLLER); AWR 1738R1 01FEB 13 (AN/APX-118); AWR 1750R2 29 MAR 13(ANVIS AN/AVS-6); AWR 1753R2 26 JUN 13(DGNS); AWR 1787 R1 28 AUG 13 (AN/ARN-123; AWR 1788R4 18 DEC 12 (AN/ARN-147);AWR 1800R3, 16 JUL 14 (BFT); AWR1823R1DTD 29 MAY 14(HUMS)SOFTWARE BLOCK5,AWR 1858R3 02 APR 14(EAWIS), AWR 187224 JAN 13 (AWIS)

21-Aug-2014 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGCOMPLIED WITH REQUIREMENTS OF H-60-14-SOF-04,( OPERATORS AND CREWMEMBERSCHECKLIST),RJ520909.

31-Aug-2014 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGCOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-10 (MAIN TRANSMISSION PLANETARYCARRIER ASSEMBLY),RJ520909.

03-Sep-2014 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGAWR 1914R2 DATED 14 JAN 14, APPLE IPAD,SUPERSEDED BY AWR 1965 DATED 8 OCT 14,APPLE IPAD OPERATION 60 MODELHELICOPTERS.

24-Oct-2014 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGUPDATED THE FOLLOWING AWRS TO THIERCURRENT REVISION NUMBERS: AWR 1127R6DTD 12 SEP 14 (HELIBASKET), AWR 1324R12DTD 18 SEP 14 (CMWS,ICMD), AWR 1425 R18(P31 ICMD) DATED 18 SEP 14, AWR 1466R6DTD 27 AUG 13(GARMAN GPS), AWR 1494 R8DATED 26 SEP 14 5TH SENSOR (CMWS), AWR1516 R8 DATED 15 SEP 14 (ELT), AWR 1682R152 SEP 14 (T700-GE-701D ENGINE AUTORELIGHT)AWR 1753 R3 (ASN-128D) 5 SEP 14,RJ520909

24-Oct-2014 2

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGCOMPLIED WITH REQUIREMENTS OF H-60-15-AMAM-02,(IVHMS WIRING MANAGEMENT).

05-Nov-2014 1

LATHAM, NY 12110-2299

RJ520909



8.7.DATE

6.REMARKS

4. 5.



AASF#3 NYARNGCOMPLIED WITH H-60-15-SOF-01, OILCOOLER FAN AXIAL BEARING.

06-Nov-2014 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-19,(ULLS-A(E) LCF CHANGE 66REQUIREMENTS).

07-Nov-2014 1

LATHAM, NY 12110-2299

RJ520909

AASF #3 NYARNGCOMPLIED WITH H-60-15-AMAM-05, AHRSEMERGENCY PROCEDURES

16-Dec-2014 1

LATHAM, NY 12110-2299

CG543558

AASF#3 NYARNGCOMPLIED WITH H-60-15-ASAM-01,LEDCAUTION ADVISORY PANEL,N/A THISACFT,RJ520909

22-Dec-2014 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGUPDATED THE FOLLOWING AWRS TO THIERCURRENT REVISION NUMBERS: AWR1054R14, DTD 17 NOV 14, (BAMBI BUCKET);AWR 1308R10, DTD 18APR13, (GOODRICHRESCUE HOIST); AWR 1346R22, DTD 15DEC14,(IVHMS); AWR 1453R4, DTD 08NOV14,(AIRWARRIOR BLOCK 1); AWR 1513R8, 1DEC14 (IPAC SOFTWARE); AWR 1524R5 16JAN 15 (BAPS); AWR 1529R4, DTD 22JAN15,(DUAL AHRS/FOGS); AWR 1682R17, DTD 9JAN15, (701D ENG IN UH60A); AWR 1753 R4(ASN-128D) 17 DEC 14, AWR 1788R5 23 DEC 14(AN/ARN-147);AWR1823R2 DTD 1 DEC 14SOFTWARE BLOCK 5, AWR 1872 24 JAN 13(AWIS),RJ520909.

06-Feb-2015 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGCOMPLIED WITH REQUIREMENTS OF H-60-15-AMAM-06, (IDENTIFICATION OF AVIATIONSURVIVABILITY EQUIPMENT).RJ520909

08-Mar-2015 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGSUPERSEDED THE FOLLOWING AWR 1648R3DATED 09 MAR 12 (NCS MAGNUS ACFTLAPTOP OPERATION), AND APPLIED AWR1913, 25 OCT 13 (ELECTRONICNOTEBOOK),REPLACED NCS MAGNUS ACFTLAPTOP WITH MSD-V3 LAPTOP, RJ520909

09-Apr-2015 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGUPDATED THE FOLLOWING AWRS TO THIERCURRENT REVISION NUMBERS: AWR1054R15, DTD 6 APR 15, (BAMBI BUCKET),AWR1566R4, DTD 13 MAR15, (RESCUE HOISTCABLE GUARD); AWR 1607R6 1 APR 15 (LEDCDU & PDU);AWR 1750R3 ANVIS AN/AVS-6SERIES NVG'S DATED 31 MAR 15, AWR 1753R5 (ASN-128D) 30 JAN 15,AWR 1913, 25 OCT 13(ELECTRONIC NOTEBOOK). RJ520909

09-Apr-2015 2

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGCOMPLIED WITH H-60-15-ASAM-03,TROOP/GUNNER SEAT ENERGYATTENUATORS,RJ520909.

30-Apr-2015 1

LATHAM, NY 12110-2299

RJ520909

L-3ACE COMPLETED AT 5579.0 A/C HRS. BY ACETEAM MEMBERS B/G. AFMA, RASME, AMCOM.

05-May-2015 1

LATHAM, NY 12110-2299

JG389608

AASF#3 NYARNGCOMPLIED WITH H-60-15-AMAM-10, "AV-DECGASKET INSPECTION, WAS NOT INSTALLED.

12-May-2015 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGAPPLIED THE FOLLOWING AWR 1407R3 28MAY 14, (FLAT PANEL DISPLAY), RJ520909

04-Jun-2015 1

LATHAM, NY 12110-2299

RJ520909



8.7.DATE

6.REMARKS

4. 5.



AASF#3 NYARNGUPDATED THE FOLLOWING AWRS TO THIERCURRENT REVISION NUMBERS: AWR1054R16, DTD 7 MAY 15, (BAMBI BUCKET);AWR 1308R11, DTD 24APR15, (GOODRICHRESCUE HOIST);AWR 1309R9 15 APR15(OREGON AERO SEAT CUSHIONS), AWR1682R18, DTD 15 APR15, (701D ENG IN UH60A);AWR 1858R4 15 MAY 15(EAWIS),RJ520909

04-Jun-2015 2

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGCOMPLIED WITH H-60-15-AMAM-11, MODE-STRANSPONDER ADDRESS REVIEW, M-SADDRESS 53405445

12-Jun-2015 1

LATHAM, NY 12110-2299

GJ727193

AASF#3 NYARNGCOMPLIED WITH REQUIREMENTS OF H-60-15-AMAM-14, ULLS-A(E) LCF CHANGE 67,RJ520909.

02-Jul-2015 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGCOMPLIED WITH H-60-15-SOF-02, FRIESRELEASE CABLE, N/A THIS ACFT.

28-Sep-2015 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGAPPLIED/INSTALLED THE FOLLOWING AWR:AWR 1348R11 30 APR 14 (12 STATION ICSINST). RJ520909

06-Oct-2015 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGUPDATED THE FOLLOWING AWRS TO THIERCURRENT REVISION NUMBERS: AWR 1324R13DTD 25 SEP 15 (CMWS,ICMD), AWR 1425 R19(P31 ICMD) DATED 25 SEP 15, AWR 1453R5,DTD 15JUN15, (AIRWARRIOR BLOCK 1); AWR1494 R9 DATED 30 SEP 15 5TH SENSOR(CMWS), AWR 1566R5 30 SEP 15 (HOISTCABLE GUARD);AWR 1607R7 15 JUN 15 (LEDCDU & PDU AWR 1682R20, DTD 2 SEP 15,(701D ENG IN UH60A),AWR 1787 R2 11 AUG 15(AN/ARN-123, AWR 1965R1 DATED 16 SEP 15,APPLE IPAD.RJ520909

06-Oct-2015 2

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGCOMPLIED WITH H-60-15-AMAM-18, N/A THISACFT, MEDEVAC CAROUSEL NOTINSTALLED/ASSIGNED.RJ520909

28-Oct-2015 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGCOMPLIED WITH H-60-16-AMAM-01, EIBFFRAMES, N/A THIS ACFT, B-KIT NOTINSTALLED.

05-Nov-2015 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGCOMPLIED WITH H-60-16-ASAM-01, INBOARDRETENTION PLATE TORQUECHECKS.RJ520909

17-Nov-2015 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGCOMPLIED WITH H-60-16-AMAM-03,“PERSONNEL LOCATOR SET REMOVAL, N/ATHIS ACFT

30-Nov-2015 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGCOMPLIED WITH H-60-16-AMAM-04, T-CLIPINSTALLATION, N/A THIS ACFT.

12-Jan-2016 1

LATHAM, NY 12110-2299

RJ520909

AASF#3 NYARNGCOMPLIED WITH H-60-16-ASAM-02,DEFECTIVE FUEL HOSES, N/A THIS ACFT.

12-Jan-2016 2

LATHAM, NY 12110-2299

RJ520909



8.7.DATE

6.REMARKS

4. 5.



AASF#3 NYARNGUPDATED THE FOLLOWING AWRS TO THIERCURRENT REVISION NUMBERS: AWR 1127R7DTD 21 JAN 16 (HELIBASKET), AWR1513R9DATED 20 NOV 15 (IPAC, AWR 1524R6 20 JAN16 (BAPS); AWR 1607R8, 14 OCT 15 LED(CDU/PDU), AWR 1682R21, DTD 30 OCT 15,(AUTO-RELIGHT TDI), AWR1692R7 16 OCT15(NEW DEICE CONNECTOR), AWR1694R5DATED 31 JAN 15 DUAL STAB CONTROLLER,AWR 1800R4 DATED 5 JAN 16, (EDM, BFT),AWR1823R3 16 OCT 15 (HUMS)SOFTWAREBLOCK 5,AWR 1858R4 15 MAY 15(EAWIS),AWR 1872R1 15 DEC 14 (AWIS), AWR 1913R1, 6NOV 15 (ELECTRONIC NOTEBOOK),RJ520909

01-Feb-2016 1

LATHAM, NY 12110-2299

RJ520909

SCIENCE ANDENGINEERINGSERVICES LLC

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

20-Jun-2016 1

HUNTSVILLE

JM866540


H-60-16-AMAM-09, ULLS-A(E) COMPONENTSDUPLICATION, BY 6 JUL 16

20-Jun-2016 2

HUNTSVILLE

JM866540


EFFECTIVE THIS DATE, ACFT TRANSFEREDTO SES FOR INDUCTION TO B.E.S.T.PROGRAM

21-Jun-2016 1

HUNTSVILLE

JM866540


H-60-16-ASAM-05, MAIN ROTOR BLADEDEBONDING, NOT COMPLIED WITH

21-Jun-2016 2

HUNTSVILLE

JM866540


DATE AC HRS SHAFT VERTICAL REASON FOR VIB CHECKLONGITUDINALLATERAL

IPS READINGS4.

8023455HELICOPTER, UTILITYUH-60A3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Report Date: 23-Jun-2016 1/4

100 HR REG04-May-1995 #1 ENG OUT 0.2001711.7

100 HR REG04-May-1995 #2 ENG OUT 0.2001711.7

100 HR REG04-May-1995 AXIAL FAN 0.20.501711.7

REMOVAL & REINSTALLATION06-Jun-1995 #1 ENG OUT 0.2001711.9

MWO 1-1520-237-50-7301-Aug-1995 #1 ENG OUT 0.32001782.5

MWO 1-1520-237-50-7301-Aug-1995 #2 ENG OUT 0.45001782.5

CHANGE #1 INPUT MODULE02-Apr-1998 #1 ENG OUT 0.29001898.5

100 HR REQ09-Jan-2000 #1 ENG OUT 0.35002109.8

100 HR REQ09-Jan-2000 #2 ENG OUT 0.33002109.8

100 HR REQ09-Jan-2000 AXIAL FAN 0.110.3602109.8

100 HR REQ/PMS-208-Dec-2000 #1 ENG OUT 0.4002217.4

100 HR REQ/PMS-208-Dec-2000 #2 ENG OUT 0.79002217.4

100 HR REQ/PMS-208-Dec-2000 AXIAL FAN 0.140.2102217.4

100 HR REG03-May-2001 #1 ENG OUT 0.22002308.5

100 HR REQ03-May-2001 #2 ENG OUT 0.01002308.5

100 HR REQ03-May-2001 AXIAL FAN 0.120.3902308.5

100 HR REQ09-Sep-2001 #1 ENG OUT 0.26002408.2

100 HR REQ09-Sep-2001 #2 ENG OUT 0.06002408.2

100 HR REQ09-Sep-2001 AXIAL FAN 0.180.5902408.2

100 HR REG09-May-2002 #1 ENG OUT 0.25002505.1

100 HR REG09-May-2002 #2 ENG OUT 0.06002505.1


100 HR REG18-Sep-2002 #1 ENG OUT 0.25002611

100 HR REG18-Sep-2002 #2 ENG OUT 0.22002611

100 HR18-Sep-2002 AXIAL FAN 0.270.5402611

PMS-229-May-2003 #1 ENG OUT 0.39002685

PMS-229-May-2003 #2 ENG OUT 0.08002685

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.



PMS-229-May-2003 AXIAL FAN 0.190.4402685

100 HR REG25-Nov-2003 #1 ENG OUT 0.33002782.2

100 HR REG25-Nov-2003 #2 ENG OUT 0.41002782.2

100 HR REG26-Nov-2003 AXIAL FAN 0.140.4702782.2

100 HR REG21-May-2004 #1 ENG OUT 0.11002884.5

100 HR REG21-May-2004 #2 ENG OUT 0.37002884.5


100 HR REG09-Jan-2005 #1 ENGINE 0.3002978.3

100 HR REG09-Jan-2005 #2 ENGINE 0.38002978.3

100 HR REG09-Jan-2005 FAN AXIAL 0.150.4702978.3

100 HR REG09-Jan-2005 TAIL ROTOR 0.09002978.3

COMPLETION OF PMS-221-Sep-2005 AXIAL FAN 0.170.403024

COMPLETION OF PMS-221-Sep-2005 #2 ENGINE 0.18003024

100 HR REG22-Sep-2005 TAIL ROTOR 0.05003024

COMPLETION OF PMS-229-Sep-2005 #1 ENGINE 0.06003024

ENGINE INSTALLATION17-Jan-2006 #2 ENGINE 0.05003050.7

120 HOUR INSP08-Feb-2008 TAIL ROTOR 0.06003259.6

12O HOUR INSP08-Feb-2008 #1 ENG H/S 0.15003259.6

120 HOUR INSP08-Feb-2008 #2 ENG H/S 0.38003259.6

120 HOUR INSP08-Feb-2008 OIL COOLER 0.28003259.6

DCS INSTALLATION22-Dec-2008 #1 DCS 0.38003369.4

DCS INSTALLATION22-Dec-2008 #2 DCS 0.38003369.4

PMI 122-Dec-2008 OIL COOLER 00.2503369.4

PMI 1, TAIL ROTOR REBUILD.29-Dec-2008 TAIL ROTOR 0.15003369.4

PMI 109-Jan-2009 #1 ENG 0.38003373.4

PMI I09-Jan-2009 #2 ENG 0.38003373.4

PMI 109-Jan-2009 OIL COOLER 00.2503373.4




IPS READINGS4.



REMOVED AND REINSTALLED ENGINE09-Dec-2010 #1 0.42003990.5

120HR/PMI 1+228-Mar-2013 #1 HSS 0.32004783.4

120HR/PMI1 +228-Mar-2013 #2 HSS 0.11004783.2

120HR/ PMI 1+228-Mar-2013 OILCOOLER 0.050.0404783.4

120HR/ PMI 1+228-Mar-2013 TAIL ROTOR 0.07004783.4

120 HR03-May-2013 #1 ENG 0.13004898.1

120 HR03-May-2013 #2 ENG 0.24004898.1

120 HR03-May-2013 OIL COOLER 0.130.0904898.1

120 HR03-May-2013 T/R 0.13004898.1

120 HR30-May-2013 #1 ENG 0.24005019.2

120 HR30-May-2013 #2 ENG 0.19005019.2

120 HR30-May-2013 OIL COOLER 0.190.1405019.2

120 HR30-May-2013 T/R 0.07005019.2

PRE-PMI 127-Jun-2013 #1 ENG 0.47005133.9

PRE-PMI-127-Jun-2013 #2 ENG 0.24005133.9

PRE-PMI-127-Jun-2013 OIL COOLER 0.430.3905133.9

PRE-PMI-127-Jun-2013 T/R 0.17005133.9

POST PMI-114-Jul-2013 #1 ENG 0.15005138.3

POST PMI-114-Jul-2013 # 2 ENG 0.03005138.3

POST PMI-114-Jul-2013 OIL COOLER 0.50.4905138.3

POST PMI-114-Jul-2013 T/R 0.03005138.3

120 HR27-Aug-2013 #1 ENG 0.11005261.3

120 HR27-Aug-2013 #2 ENG 0.18005261.3

120 HR27-Aug-2013 OIL COOLER 0.320.1705261.3

120 HR27-Aug-2013 T/R 0.05005261.3

120 HR VIBE08-Oct-2013 #1 ENG 0.08005377.9

120 HR VIBE08-Oct-2013 #2 ENG 0.05005377.9




IPS READINGS4.



120 HR VIBES08-Oct-2013 OILCOOLER 0.350.1505377.9

120 HR VIBES08-Oct-2013 T/R 0.11005377.9

PREPHASE29-Nov-2013 T/R 0.14005493.1

PREPHASE29-Nov-2013 #1 ENG 0.56005493.1

PREPHASE29-Nov-2013 # 2 ENG 0.43005493.1

PREPHASE29-Nov-2013 OIL COOLER 00.4305493.1

PRE PHASE29-Nov-2013 OIL COOLER 0.56005493.1

POST RESET/120 HR25-Jul-2014 #1 HSS 0.15005493.1

POST RESET/120 HR25-Jul-2014 #2 HSS 0.108005493.1

POST RESET/120 HR25-Jul-2014 OIL COOLER 0.160.0305493.1

POST RESET/ 120 HR25-Jul-2014 T/R 0.08005493.1

ENGINE CHANGE04-Dec-2015 #1 HSS 0.32005734.1








CHECKED DURING ENGINE CHANGE08-Dec-2015 OIL COOLER 0.030.0405734.1

CHECKED DURING ENGINE CHANGE08-Dec-2015 T/R 0.11005734.1

6. Remarks



h

CONDITION ITEMS

kjifdcba g.

RMVL HR

RMVL HRSWUC HRS)COMPO/H

NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE

SINCEPREVSER NO.ANDNOMENCLATURE DUE

REPLACE

INST HRSTIMEINST HRSNO.COMPONENTPNCOMP REP.O/H ORNOMEN6.

3. PART NUMBER ORMODEL

2. NSN 4. SERIAL NUMBER 5. WUC1. NOMENCLATURE


80234551520010350266 00HELICOPTER, UTILITY

156001095713502C12D

00UNK345570219-05001-042TAIL CONE FITTING CCCC COND COND

162001231183103A01 R/S

6514779BEM 021270250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001231183103A01 L/S

04779BEM119170250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001421089003B01 R/S

8595493BMC71470250-13101-044SHOCK ABSORBER (TAIL) CCCC COND COND

165001285302405A01Z YELLOW

33004779A106-0254270106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z BLUE


165001285302405A01Z BLACK


165001285302405A01Z RED

12355417A1061102970106-08100-046DAMPER ASSY, M/R CCCC COND COND

531501537465205A02H YELLOW/LEAD

03366B9410485970103-08108-041SOLID BLADE PIN CCCC COND COND

531501537465205A02H YELLOW/LAG


531501537465205A02H BLACK/LEAD


531501537465205A02H RED/LEAD


531501537465205A02H BLUE/LEAD


531501537465205A02H BLUE/LAG


531501537465205A02H RED/LAG


531501537465205A02H BLACK/LAG


161501199764605A03A

03200015152-187670104-08000-050SWASHPLATE ASSY CCCC COND COND

161501078571806A11 #1

19081899A258-0086670351-08080-043ACCESSORY MODULE CCCC COND COND

161501078571806A11

24491712A2580024870351-08080-043ACCESSORY MODULE CCCC COND COND

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

DA FORM 2408-16-E, OCT 91 AIRCRAFT COMPONENT HISTORICAL RECORD

h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






161501503311506A

42914426A265-0155970351-08100-076MAIN TRANSMISSIONMODULE

CCCC COND COND

161501230621806E 1

3113477943327170351-08001-046INPUT MODULE CCCC COND COND

161501230621806E

15621712A2640153370351-08001-046INPUT MODULE CCCC COND COND

168001074515206F

35264082A0050109270357-06300-042INTERMEDIATE GEARBOX CCCC COND COND

161501376508906G01

05138A006-0450770358-06600-046TAIL ROTOR GEARBOXASSY

CCCC COND COND

161501524780506H04 2

03369C845-0249970361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501524780506H04

1973729C845-0351770361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501081277506H06

6681712A2710110770361-03001-045SHAFT ASSY, T/R DRV SEC1

CCCC COND COND

161501158951706H08

03729WG30040-00211

70361-03009-047DRIVESHAFT ASSY SECT II CCCC COND COND

161501082650006H09

6681712A2720361070361-05001-045SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501158952206H09

6681712A272-0356570361-05001-051SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501158952206H09

04779WG300240085970361-05001-051SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

NSN PENDING06H11


CCCC COND COND

161501277910606H12


CCCC COND COND

432001207722807A01 #1

47233607600290ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01 BACK UP

12664779K3233ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01

12024426K5656ABR70652-02300-050PUMP MODULE,HYDRAULIC

CCCC COND COND

481001102247307B05A

04645213513213850-3-1VALVE, SOLENIOD CCCC COND COND

481001102247307B05A 1

05619237803213850-3-1VALVE, SOLENIOD CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






165001222431607B11

125854934724A3197170-5ACCUMULATOR CCCC COND COND

168001342049608B20

027993804100-601561-000PANEL INDICATOR (PDU) CCCC COND COND

168001342049608B20

12484307467570450-01043-124PANEL INDICATOR (PDU) CCCC COND COND

168001566036608F01

04082113330279-0302IVHMU (CBM MONITORSYSTEM)

CCCC COND COND

611501114969609A01

027991268E28B302-8-DMGENERATOR CCCC COND COND

611501114969609A01

676412874A168928B302-8-DMGENERATOR CCCC COND COND

168001310225911C21

05493B9950190870400-02300-048MIXER ASSEMBLY CCCC COND COND

156001411515111D17

04779F3380913470209-22103-065SERVO BEAM FITTING CCCC COND COND

156001411515611D17


156001411515011D17


156001411514811D17


168001261204411D25

140154931795DL2155M20STABILATOR ACTUATOR CCCC COND COND

168001261204411D25

66354932604DL2155M20STABILATOR ACTUATOR CCCC COND COND

599601547345211D26

0478146281011445-1STABILATOR AMPLIFIER(DUAL)

CCCC COND COND

299501496368615A04

0477922304504587ENGINE SEQUENCINGUNIT

CCCC COND COND

599601415867319D01A

267850512318AA822-0787-001AMPLIFIER, RADIOFREQUENCY

CCCC COND COND

599601188333219D01F

04779915BB622-6545-003AMPLIFIER, RADIOFREQUENC

CCCC COND COND

582101413423619D

96950512540AA822-0788-001HFRECEIVER/TRANSMITTER

CCCC COND COND

NSN PENDING19E04B

20954932943P320A002-03SIGNAL DATACONVERTER

CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






589501245909019E05A

24356191743ASM-C-967292RECEIVER-TRANSMITTERRADAR

CCCC COND COND

584101245909319E05C

5005506278FFA3060591INDICATOR HEIGHT CCCC COND COND

660501503528419E06A

0549310742765100-20ATTITUDE HEADINGREFERENCE UNIT

CCCC COND COND

581001376138019H

0550179860N616736-1TSEC/KY-100 PROCESSOR CCCC COND COND

661001490516852A

048333429979825050-1-001AUTOMAT FLT CONTCOMPUTER

CCCC COND COND

589501395744776A03

231255011026AA3214085COMPARATOR/PROCESSOR

CCCC COND COND

589501395744776A03

231255011026AAA3214085COMPARATOR/PROCESSOR

CCCC COND COND

SIGNIFICANT HISTORICAL EVENTS7.




kjigfdcbaRMVL HR RMVL HRS

NOMEN HRS)COMPO/HO/HLOCATIONNSNWUC

he (ACFTLIFESINCEPRESER NO.ANDAND

INST HRSP/N DUEREPLACE

INST HRSTIMENO.COMPONENTNOMENCLATURE

NOMEN REP.O/H OCOMP6.

4. SERIAL NUMBER3. PART NUMBER OR MODEL2. NSN 5. WUC1. NOMENCLATUR

Report Date:

TIME CHANGE COMPONENTS5/1224-Jun-2016

00

156001081924402C15J MT00121712

UNK3455 0171270209-06051-043TAIL PYLON FITTING RCRC20000

161501450483405A01A9519

1515201209 360477970103-08112-047HUB, M/R ROTOR ASSY RCRC5100

161501442692605A01I BLUE8611

A001-01376 0221170102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501442692605A01I BLACK8611


RCRC6400

161501442692605A01I YELLOW8611


RCRC6400

161501442692605A01I RED10826

D001-01412 0442670102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501074515105A01L10208

E28600132 6477268570351-08186-043MAIN ROTOR SHAFTEXTENDER

RCRC14000

161501127738805A01T13000

01515200545 3849384970107-08400-046BIFILAR, M/R ROTORASSY

RCRC13000

161501106190305A02 YELLOW10575

A00701937 3309428470150-09100-043MAIN ROTOR BLADEASSY

RCRC9600

161501106190305A02 RED10416


RCRC9600

161501106190305A02 BLACK10158


RCRC9600

161501106190305A0212809


RCRC9600

161501113818805B0212735

A00905651 2758549370101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501113818805B0212703

A00907293 2790549370101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501083681206G01B11599

A25700245 2113171270102-11101-042O/B RETENTION PLATE(T/R)

RCRC12000

414101329342806H236249

B512-0926SB 4297550670361-03005-107FAN AXIAL 177712520

156001129125607A24 YAW15196B11210455 3065526170410-02500-049SAS ACTUATOR RCRC

13000

156001129125607A2415425B11211843 3088551370410-02500-049SAS ACTUATOR RCRC

13000

156001129125607A2417429C11204505 1064549370410-02500-049SAS ACTUATOR RCRC

13000

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

EDITION MAY 67 IS OBSOLETE

AIRCRAFT COMPONENT HISTORICALRECORD

DA FORM 2408-16-E, OCT 91









Report Date:


00

161501141753211C235889

B233-02098 2000372970400-06100-042TAIL ROTOR PITCHCHANGE SHAFT

022160

165001305695411C2513037B30001041 451225492227000-17TAIL ROTOR SERVO

ASSYRCRC

15000

165001143122611D0129893

B30316230 05493274000-1031MAIN ROTOR PRIMARYSERVO

RCRC24400

165001143122611D0123380B303-00533 6281526170410-02820-054MAIN ROTOR PRIMARY

SERVORCRC

24400

165001143122611D0118774B303-X01004 8788316270410-02820-054MAIN ROTOR PRIMARY

SERVORCRC

24400

156001158968511D0413930C34502700 3849477970400-08102-045AFT BELLCRANK RCRC

13000

156001164416111D0518712

A39101788 0171270400-08112-045AFT TIE ROD SUPTFITTING

RCRC17000

168001164416011D065929

MM1049 0372970400-08111-042AFT TIE ROD ASSY RCRC2200

156001286887011D078129

390-02392 0372970400-08117-049AFT BELLCRANK SPTASSY

RCRC4400

304001287243811D0816138

1515203738 0513870400-08151-061LATERAL SWASHPLATELINK

RCRC11000

161501158965811D096944A28900473 268171270400-08150-045LATERAL SERVO

BELLCRANKRCRC

5500

168001158965311D1111782C34600411 3300408270400-08104-048AFT WALKING BEAM RCRC

11000

156001083295411D1315444C34400499 268171270400-08115-043LEFT TIE ROD RCRC

14000

156001329789211D1424085D36600762 601468670400-08165-043RIGHT TIE ROD ASSY RCRC

20000

168001158965211D1519779

1720 0477970400-08101-046FORWARD BELLCRANK RCRC15000

156001221261911D168762

B367-04729 0316270400-08162-042FWD BELLCRANK SPTASSY

RCRC5600













Report Date:


00

SIGNIFICANT HISTORICAL EVENTS7.





ji kgfdcbaRMVL HRSRMVL HRSCOMPO/HNOMENWUC

HRS)O/HLOCATIONNSN

AND he SINCELIFE (ACFT

PREVSER NO. OAND

NOMENCLATURE PN TIMEINST HRS DUEREPLACE

INST HRSNO.COMPONENTNOMEN REP.O/H ORCOMP6.

1520010350266HELICOPTER,UTILITY

UH-60A 8023455 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 8 of 12

24-Jun-2016

COND COND

156001095713502C12D

00TAIL CONE FITTING UNK345570219-05001-042 CCCC

20000 21712

1560010819244 MT00102C15J

01712TAIL PYLON FITTING UNK345570209-06051-043 RCRC

COND COND

1620012311831 R/S03A01

6514779FWD FIXED GEARSHOCK

BEM 021270250-12051-045 CCCC

COND COND

1620012311831 L/S03A01


BEM119170250-12051-045 CCCC

COND COND

1620014210890 R/S03B01

8595493SHOCK ABSORBER(TAIL)

BMC71470250-13101-044 CCCC

5100 9519

161501450483405A01A

3604779HUB, M/R ROTOR ASSY 151520120970103-08112-047 RCRC

6400 8611

1615014426926 BLUE05A01I

02211MAIN ROTOR SPINDLEASSY

A001-0137670102-08200-069 RCRC

6400 8611

1615014426926 BLACK05A01I


A001-0138270102-08200-069 RCRC

6400 8611

1615014426926 YELLOW05A01I


A001-0159270102-08200-069 RCRC

6400 10826

1615014426926 RED05A01I


D001-0141270102-08200-069 RCRC

14000 10208

161501074515105A01L

64772685MAIN ROTOR SHAFTEXTENDER

E2860013270351-08186-043 RCRC

13000 13000

161501127738805A01T

38493849BIFILAR, M/R ROTORASSY

0151520054570107-08400-046 RCRC

COND COND

1650012853024 YELLOW05A01Z

33004779DAMPER ASSY, M/R A106-0254270106-08100-046 CCCC

COND COND

1650012853024 BLUE05A01Z


COND COND

1650012853024 BLACK05A01Z


COND COND

1650012853024 RED05A01Z

12355417DAMPER ASSY, M/R A1061102970106-08100-046 CCCC

9600 10575

1615011061903 YELLOW05A02

33094284MAIN ROTOR BLADEASSY

A0070193770150-09100-043 RCRC

9600 10416

1615011061903 RED05A02


A0070744570150-09100-043 RCRC

9600 10158

1615011061903 BLACK05A02


A0070958270150-09100-043 RCRC

9600 12809

161501106190305A02


A0071431570150-09100-043 RCRC

COND COND

5315015374652 YELLOW/LEAD05A02H

03366SOLID BLADE PIN B9410485970103-08108-041 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

24-Jun-2016

COND COND

5315015374652 YELLOW/LAG05A02H


COND COND

5315015374652 BLACK/LEAD05A02H


COND COND

5315015374652 RED/LEAD05A02H


COND COND

5315015374652 BLUE/LEAD05A02H


COND COND

5315015374652 BLUE/LAG05A02H


COND COND

5315015374652 RED/LAG05A02H


COND COND

5315015374652 BLACK/LAG05A02H


COND COND

161501199764605A03A

03200SWASHPLATE ASSY 015152-187670104-08000-050 CCCC

10000 12735

161501113818805B02

27585493TAIL ROTOR BLADEASSY

A0090565170101-31000-043 RCRC

10000 12703

161501113818805B02

27905493TAIL ROTOR BLADEASSY

A0090729370101-31000-043 RCRC

COND COND

1615010785718 #106A11

19081899ACCESSORY MODULE A258-0086670351-08080-043 CCCC

COND COND

161501078571806A11

24491712ACCESSORY MODULE A2580024870351-08080-043 CCCC

COND COND

161501503311506A

42914426MAIN TRANSMISSIONMODULE

A265-0155970351-08100-076 CCCC

COND COND

1615012306218 106E

31134779INPUT MODULE 43327170351-08001-046 CCCC

COND COND

161501230621806E

15621712INPUT MODULE A2640153370351-08001-046 CCCC

COND COND

168001074515206F

35264082INTERMEDIATEGEARBOX

A0050109270357-06300-042 CCCC

COND COND

161501376508906G01

05138TAIL ROTOR GEARBOXASSY

A006-0450770358-06600-046 CCCC

12000 11599

161501083681206G01B

21131712O/B RETENTION PLATE(T/R)

A2570024570102-11101-042 RCRC

COND COND

1615015247805 206H04

03369DRIVESHAFT ASSYENGINE

C845-0249970361-08014-041 CCCC

COND COND

161501524780506H04

1973729DRIVESHAFT ASSYENGINE

C845-0351770361-08014-041 CCCC

COND COND

161501081277506H06

6681712SHAFT ASSY, T/R DRVSEC 1

A2710110770361-03001-045 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 10 of 12

24-Jun-2016

COND COND

161501158951706H08

03729DRIVESHAFT ASSY SECTII

WG30040-0021170361-03009-047 CCCC

COND COND

161501082650006H09

6681712SHAFT ASSY, T/R SEC3,4,5

A2720361070361-05001-045 CCCC

COND COND

161501158952206H09


A272-0356570361-05001-051 CCCC

COND COND

161501158952206H09


WG300240085970361-05001-051 CCCC

COND COND

NSN PENDING06H11


A2730100570361-05001-044 CCCC

COND COND

161501277910606H12


A2740118770361-06002-044 CCCC

2520 6249

414101329342806H23

42975506FAN AXIAL B512-0926SB70361-03005-107 17771

COND COND

4320012077228 #107A01

4723360PUMP MODULE ASSY,HYDRAUL

7600290ABR53023-06 CCCC

COND COND

4320012077228 BACK UP07A01

12664779PUMP MODULE ASSY,HYDRAUL

K3233ABR53023-06 CCCC

COND COND

432001207722807A01

12024426PUMP MODULE,HYDRAULIC

K5656ABR70652-02300-050 CCCC

13000 151961560011291256 YAW07A24

30655261SAS ACTUATOR B1121045570410-02500-049 RCRC

13000 15425156001129125607A24

30885513SAS ACTUATOR B1121184370410-02500-049 RCRC

13000 17429156001129125607A24

10645493SAS ACTUATOR C1120450570410-02500-049 RCRC

COND COND

481001102247307B05A

04645VALVE, SOLENIOD 213513213850-3-1 CCCC

COND COND

4810011022473 107B05A

05619VALVE, SOLENIOD 237803213850-3-1 CCCC

COND COND

165001222431607B11

12585493ACCUMULATOR 4724A3197170-5 CCCC

COND COND

168001342049608B20

02799PANEL INDICATOR (PDU) 3804100-601561-000 CCCC

COND COND

168001342049608B20

12484307PANEL INDICATOR (PDU) 467570450-01043-124 CCCC

COND COND

168001566036608F01

04082IVHMU (CBM MONITORSYSTEM)

113330279-0302 CCCC

COND COND

611501114969609A01

02799GENERATOR 1268E28B302-8-DM CCCC

COND COND

611501114969609A01

6764128GENERATOR 74A168928B302-8-DM CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 11 of 12

24-Jun-2016

COND COND

168001310225911C21

05493MIXER ASSEMBLY B9950190870400-02300-048 CCCC

2160 5889

161501141753211C23

20003729TAIL ROTOR PITCHCHANGE SHAFT

B233-0209870400-06100-042 02

15000 13037165001305695411C25

45122549TAIL ROTOR SERVOASSY

B300010412227000-17 RCRC

24400 29893

165001143122611D01

05493MAIN ROTOR PRIMARYSERVO

B30316230274000-1031 RCRC

24400 23380165001143122611D01


B303-0053370410-02820-054 RCRC

24400 18774165001143122611D01


B303-X0100470410-02820-054 RCRC

13000 113930156001158968511D04

38494779AFT BELLCRANK C3450270070400-08102-045 RCRC

17000 18712

156001164416111D05

01712AFT TIE ROD SUPTFITTING

A3910178870400-08112-045 RCRC

2200 5929

168001164416011D06

03729AFT TIE ROD ASSY MM104970400-08111-042 RCRC

4400 8129

156001286887011D07

03729AFT BELLCRANK SPTASSY

390-0239270400-08117-049 RCRC

11000 16138

304001287243811D08

05138LATERAL SWASHPLATELINK

151520373870400-08151-061 RCRC

5500 6944161501158965811D09

2681712LATERAL SERVOBELLCRANK

A2890047370400-08150-045 RCRC

11000 117782168001158965311D11

33004082AFT WALKING BEAM C3460041170400-08104-048 RCRC

14000 15444156001083295411D13

2681712LEFT TIE ROD C3440049970400-08115-043 RCRC

20000 24085156001329789211D14

6014686RIGHT TIE ROD ASSY D3660076270400-08165-043 RCRC

15000 19779

168001158965211D15

04779FORWARD BELLCRANK 172070400-08101-046 RCRC

5600 8762

156001221261911D16

03162FWD BELLCRANK SPTASSY

B367-0472970400-08162-042 RCRC

COND COND

156001411515111D17

04779SERVO BEAM FITTING F3380913470209-22103-065 CCCC

COND COND

156001411515611D17


COND COND

156001411515011D17


COND COND

156001411514811D17





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 12 of 12

24-Jun-2016

COND COND

168001261204411D25

14015493STABILATOR ACTUATOR 1795DL2155M20 CCCC

COND COND

168001261204411D25

6635493STABILATOR ACTUATOR 2604DL2155M20 CCCC

COND COND

599601547345211D26

04781STABILATOR AMPLIFIER(DUAL)

46281011445-1 CCCC

COND COND

299501496368615A04

04779ENGINE SEQUENCINGUNIT

22304504587 CCCC

COND COND

599601415867319D01A

26785051AMPLIFIER, RADIOFREQUENCY

2318AA822-0787-001 CCCC

COND COND

599601188333219D01F

04779AMPLIFIER, RADIOFREQUENC

915BB622-6545-003 CCCC

COND COND

582101413423619D

9695051HFRECEIVER/TRANSMITTE

2540AA822-0788-001 CCCC

COND COND

NSN PENDING19E04B

2095493SIGNAL DATACONVERTER

2943P320A002-03 CCCC

COND COND

589501245909019E05A

2435619RECEIVER-TRANSMITTER RADAR

1743ASM-C-967292 CCCC

COND COND

584101245909319E05C

5005506INDICATOR HEIGHT 278FFA3060591 CCCC

COND COND

660501503528419E06A

05493ATTITUDE HEADINGREFERENCE UNIT

10742765100-20 CCCC

COND COND

581001376138019H

05501TSEC/KY-100PROCESSOR

79860N616736-1 CCCC

COND COND

661001490516852A

04833AUTOMAT FLT CONTCOMPUTER

3429979825050-1-001 CCCC

COND COND

589501395744776A03

23125501COMPARATOR/PROCESSOR

1026AA3214085 CCCC

COND COND

589501395744776A03

23125501COMPARATOR/PROCESSOR

1026AAA3214085 CCCC

7. SIGNIFICANT HISTORICAL DATA



23-Jun-2016

T700-GE-700ENGINE ASSY, TURBINE

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

GEE306199

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

04-Dec-2015 8023455 REINSTALLED T700'S6000 101 102 0.999922651 852


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

23-Jun-2016

T700-GE-700ENGINE ASSY, TURBINE

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

GE-E-207535

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

04-Dec-2015 8023455 REINSTALLED T700ENGINES

6000 101 102 0.99972640 841


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


HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM 0212 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

24-Jun-2016

9000 13128

1650011250907 R/S03A01A

00PISTON, MAIN L/GEARSTR

BEM021270250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM 0212 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

24-Jun-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM1191 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

24-Jun-2016

9000 13779

165001125090703A01A

00PISTON, MAIN L/GEARSTR

BEM250570250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM1191 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

24-Jun-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615014426926MAIN ROTORSPINDLE ASSY

70102-08200-069 A001-01376 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

24-Jun-2016

COND COND

3110011589607 BLUE05A01I02C

02215THRUST BEARING C325-04288SB7002-048 CCCC

COND COND

161501161437305A01I02

8172215SPHERICAL BEARINGASSY

B32426366SB7001-048 CCCC

13000 15685

531001126944405A01I04

10441518M/R SPINDLE NUT 35590-130670102-08105-102 RCRC

6400 8611

5306014606020 BLUE05A01I06

00TIE ROD (M/R SPINDLE) B504-0149238023-10372-101 RCRC

20000 22211

1615012149140 BLUE05A01I07

00HORN ASSEMBLY A24111346A70102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

24-Jun-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

24-Jun-2016

COND COND

3110011589607 BLACK05A01I02C

02215THRUST BEARING B325-38812SB7002-048 CCCC

COND COND

1615011614373 BLACK05A01I02

03282ELASTOMERIC BEARING B32439599SB7001-048 CCCC

13000 16729

5310011269444 BLACK05A01I04

01518M/R SPINDLE NUT C479-0847270102-08105-102 RCRC

6400 8611

5306014606020 BLACK05A01I06


20000 22211

1615012149140 BLACK05A01I07

00HORN ASSEMBLY A241-1163670102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

24-Jun-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

24-Jun-2016

COND COND

311001158960705A01I02C

03282THRUST BEARING C32504293SB7002-48 CCCC

COND COND

161501161437305A01I02

03282ELASTOMERIC BEARING B32439753SB7001-048 CCCC

13000 16729

5310011269444 YELLOW05A01I04

01518M/R SPINDLE NUT 03714HAD70102-08105-102 RCRC

6400 8611

5306014606020 YELLOW05A01I06


20000 22211

1615012149140 YELLOW05A01I07






HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

24-Jun-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 D001-01412 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

24-Jun-2016

COND COND

3110011589607 RED05A01I02C

00THRUST BEARING B325-43587SB7002-048 CCCC

COND COND

1615011614373 RED05A01I02

6970SPHERICAL BEARINGASSY

LK4244SB7001-048 CCCC

13000 17426

5310011269444 RED05A01I04

00M/R SPINDLE NUT C4791572870102-08105-102 RCRC

6400 10826

5306014606020 RED05A01I06

00TIE ROD (M/R SPINDLE) C5040688338023-10372-101 RCRC

20000 24426

1615012149140 RED05A01I07






HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 D001-01412 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

24-Jun-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70150-09100-043 A00701937 05A024. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

24-Jun-2016

COND COND

156001447977405A02E

03507M/R BLADE TIP CAP B8491027770150-09207-041 CCCC

5000 9284

161501099234105A02I

03309M/R BLADE CUFF G2370144570150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

24-Jun-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

24-Jun-2016

COND COND

1560014479774 RED05A02E

8533468M/R BLADE TIP CAP A8490946870150-09207-041 CCCC

5000 6162

1615010992341 RED05A02I

31223468M/R BLADE CUFF A2370494970150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

24-Jun-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

24-Jun-2016

COND COND

156001447977405A02E


5000 9346

1615010992341 BLACK05A02I

11474935M/R BLADE CUFF G2370113470150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

24-Jun-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

24-Jun-2016

COND COND

1560014479774 BLUE05A02E


5000 7951

161501099234105A02I

21861928M/R BLADE CUFF E2370015070150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

24-Jun-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615011997646SWASHPLATE ASSY 70104-08000-050 015152-1876 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

24-Jun-2016

COND COND

161501087160205A03A01

15791579STATIONARYSWASHPLATE

01515270104-08010-044 CCCC

11000 14200

161501357508905A03A02

00ROTATINGSWASHPLATE ASSEMBL

015152-187670104-08001-045 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615011997646SWASHPLATE ASSY 70104-08000-050 015152-1876 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

24-Jun-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70351-08100-076 A265-01559 06A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

24-Jun-2016

17000 17812

161501078571106A08

36144291SWASHPLATE GUIDE B425-0043170351-08227-041 RCRC

3000 5812

161501110149106A13

16144291MAIN GEARBOXHOUSING ASSY

A2110115370351-08110-045 RCRC

6875 11301

304001415838806A18

04291MAIN ROTOR SHAFT E253-0472070351-08131-048 RCRC

12000 15427

161501497725706A19

9994291PLANETARY CARRIERASSY

F240-0003170351-08175-046 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70351-08100-076 A265-01559 06A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

24-Jun-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615013765089TAIL ROTORGEARBOX ASSY

70358-06600-046 A006-04507 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

24-Jun-2016

12000 17138

161501074515306G01C

00I/B RETENTION PLATET/R

K2591200270358-06612-042 RCRC

5000 10138

304001292161706G01D

00GEARSHAFT, BEVEL G3200091170358-06620-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615013765089TAIL ROTORGEARBOX ASSY

70358-06600-046 A006-04507 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

24-Jun-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



4141013293428FAN AXIAL 70361-03005-107 B512-0926SB 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

24-Jun-2016

2520 6249

311001127300506H23A

17764296BALL BRNG ANN (OILCOOLER FWD)

3617210SFFC3 RCRC

2520 6249

311001127300506H23A

17764296BALL BRNG ANN (OILCOOLER FWD)

3749210SFFC3 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



4141013293428FAN AXIAL 70361-03005-107 B512-0926SB 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

24-Jun-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70400-06100-042 B233-02098 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

24-Jun-2016

2160 5889

311001113828811C23A

02000BRNG T/R PITCH CHGSHAFT

B84006185SB1162-102 RCRC

COND COND

534001094578911C23C

20902090CLEVIS, ROD END B2330209809092010

70400-06702-041 CCCC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70400-06100-042 B233-02098 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

24-Jun-2016





8023455HELICOPTER, 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 5829.610TM 1-1520-237-PMDPERFORM M/R SPINDLE LUGS,M/R CUFF, TIP CAPSINSPECTION

5819.6H

A022 29 Jun 201614TM 1-1520-237-23-914 DAY FLYABLE STORAGEENGINE RUN UP

15 Jun 2016D

A045 5859.640H-60-11-AMAM-03REQUIRE DOWNLOAD ANDTRANSMIT OF IVHMS FULL RAWDATA

5819.6H

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

10 Jun 2016D

A100 21 Jul 201630DA PAM 738-751#1 ENGINE HISTORY RECORDERREADING DUE

21 Jun 2016D

A101 21 Jul 201630DA PAM 738-751#2 ENGINE HISTORY RECORDERREADING DUE

21 Jun 2016D

A103 17 Jun 201630TM 1-1500-344-23AIRCRAFT WASH DUE 18 May 2016D

A110 5855.640TM 1-1520-237-PMSPMS 40 HOUR INSPECTION 5815.6H

A115 08 Jul 201630TM 1-1520-237-23-12LUBE REQUIRMENTS 08 Jun 2016D

A115 5859.640TM 1-1520-237-23-12LUBE REQUIRMENTS 5819.6H

A116 6015.2360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

5655.2H

A116 05 Aug 201612H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

05 Aug 2015M

A117 6015.2360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 5655.2H

A117 05 Aug 201612H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 05 Aug 2015M

A140 5861.4120AWR 1346R16, IVHMSIN ACF

DOWNLOAD AND REVIEW IVHMSDATA

5741.4H

A160 07 Aug 201690TM 1-1520-237-23-1290 DAY CORROSIONINSPECTION

09 May 2016D

A177 09 Aug 201690AR 95-190 DAY REVIEW/UPDATE OF 365-4 ENTRIES

11 May 2016D

A210 5852.6120TM 1-1520-237-23-12120 HOUR INSPECTIONREQUIREMENTS

5732.6H

A211 6015.2360H-60-10-AMAM-11APU OIL SAMPLE 5655.2H

A211 26 Jul 201612H-60-10-AMAM-11APU OIL SAMPLE 26 Jul 2015M

A213 5852.6120TM 1-2840-248-23ENGINE COMPRESSORCLEANING

5732.6H

A214 5853.1120TM 1-1520-237-23-12CLEAN TAIL WHEEL ADAPTER 5733.1H

A222 12 Feb 2017360TM 1-1680-377-13&PAMSS SURVIVAL KITINSPECTION

18 Feb 2016D

For use of this form, see DA PAM 738-751; the proponent agency is DCSLOGDA FORM 2408-18, NOV 91, MAY BE USED

DA FORM 2408-18 E, OCT 97 EQUIPMENT INSPECTION LIST

A = APU OPERATING HOURS P = APU STARTS F = HOT SECTION FACTORSFREQUENCY LEGEND: H = ACFT HRS D = DAYS M = MONTHS Y = YEARS R = ROUNDS C = CYCLES S = ENG1 STARTS Z = ENG2 STARTS



7. FREQUENCY 4.




INSP

A230 02 Jul 2016120MWO 1-1520-237-50-77INSPECT BATTERYCOMPARTMENT FORCORROSION (SLAB)

04 Mar 2016D

A295 5853.1360TM 1-1520-237-23-12STABILATOR ACTUATOR ASSYLUBE

5493.1H

A296 5853.1360TM 1-1520-237-23-12STABILATOR INSPECTION 5493.1H

A298 6171.1360TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 5811.1H

A298 09 May 201712TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 09 May 2016M

A299 6017.2360TM 1-1520-237-23-12SWASHPLATE LUBE 5657.2H

A299 18 Aug 201612TM 1-1520-237-23-12SWASHPLATE LUBE 18 Aug 2015M

A320 5853.1360TM 1-2840-248-23ENGINE INSPECTION &CLEANING

5493.1H

A400 5853.1720TM 1-1520-237-PMIPMI-1 5133.1H

A401 6213.1720TM 1-1520-237-PMIPMI-2 5493.1H

A408 6213.1720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-2, AREA 5 AND 6)

5493.1H

A410 5853.1720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-1, AREA 1 THRU 4)

5133.1H

A415 6213.1720H-60-10-AMAM-11MAIN GEARBOX OIL SAMPLE-PART # 073, 074, 076

5493.1H

A440 6213.1720TM 1-1520-237-23-12CLEAN TAIL WHEEL LOCKPIN 5493.1H

A470 6639.41500TM 1-1520-237-23-12REPLACE NUMBER TWOCROSSFEED VALVE

5139.4H

A471 6585.62160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

4425.6H

A472 6585.62160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

4425.6H

A473 6585.62160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

4425.6H

A476 6719.15000TM 1-1520-237-23-12REPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

1719.1H

A477 80245000TM 1-1520-237-23-12REPLACEMENT OF STABILATORACTUATOR BOLTS

3024H

A480 9779.45000TM 1-1520-237-23-12REPLACE PIVOT BOLT 70400-08159-101,102,103,104

4779.4H

A485 9779.45000TM 1-1520-237-23-12REPLACE BELLCRANK BOLT70400-08159-105,106,107,108

4779.4H

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

23 Jan 2016M

A501 04 Aug 20166TM 1-1520-237-23-12MAIN ROTOR BLADE PRESSURECHECK

04 Feb 2016M






7. FREQUENCY 4.




INSP

A502 25 Jul 20166TM 1-1520-237-23-12INSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

25 Jan 2016M

A530 23 Jun 201612DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

23 Jun 2015M

A532 30 Jul 201612TM 1-1500-204-23-4COMPASS SWING / RMI 30 Jul 2015M

A533 25 Jul 201612TM 1-1520-237-23-12PITOT STATIC SYSTEMINSPECTION

25 Jul 2015M

A534 31 Oct 201724TM 1-1500-204-23-1FIRST AID KIT INSPECTION 31 Oct 2015M

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

23 Jun 2015M

A541 29 May 201712TM 1-1520-237-23, C4REPLACE DIGITAL CLOCKBATTERY

29 May 2016M

A550 05 Jun 201712AWR1346R16IVHUMS BATTERYREPLACEMENT

05 Jun 2016M

A553 28 Jul 201612AR 95-1AIRCRAFT WEIGHINGINVENTORY (365-1)

28 Jul 2015M

A580 09 Jul 201624TM 11-6140-203-23&PRETURN SLAB TO AVIM FORCAPACITY CHECK (VEREY 24MONTH)

09 Jul 2014M

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

A625 25 Jun 201860TM 11-6140-203-23&PREPLACEMENT OF SLABBATTERY (SLAB)

25 Jun 2013M

A630 27 Nov 2019114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

27 May 2010M

A633 27 Nov 2019114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

27 May 2010M

A638 27 Nov 2019114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

27 May 2010M

A640 27 Nov 2019114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

27 May 2010M

A648 03 Sep 2023180TM 1-1520-237-23REPLACE T/R SPRING CAPSULEASSY

03 Sep 2008M

A660 01 Feb 202272TB 9-1300-385REPLACE THRUSTEREMERGENCY RELEASE CARGOHOOK, MJ20

01 Feb 2016M

A665 03 Jun 201848H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

03 Jun 2014M

A670 25 Jun 201848TM 1-1520-237-23-1CABIN TUB INSPECTION 25 Jun 2014M

A673 25 Jun 201848TM 1-1520-237-23-12FUEL CELL CORROSIONINSPECTION

25 Jun 2014M

A675 15 Jul 201848TM 1-1520-237-23-12FLIGHT CONTROL ROD INSP 15 Jul 2014M

A695 6213.1720H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

5493.1H






7. FREQUENCY 4.




INSP

A695 10 Jun 201848H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

10 Jun 2014M

A755 12819.29000H-60-10-ASAM-11PC LINK TO SWASHPLATEBOLTS REPLACEMENT

3819.2H

E015 21 Oct 2016180MWO 1-1520-237-50-92ASN 128D DOPPLER GPSBATTERY REPLACEMENT

24 Apr 2016D

E040 05 Jul 201690TM 11-5841-294-12APR-39 RADAR/LASERWARNING OPNL CHECK, 5841-01-236-8951

06 Apr 2016D

E050 30 Jun 201630TM 11-5821-357-12PARC-220 RADIO SET BATTERYINSPECTION OR REPLACE

31 May 2016D

E108 04 Jul 201630TM 11-5810-262-23KY-58 PMCS/OPNL CHECK(STANDBY)

04 Jun 2016D

E125 18 Jul 201690TM 11-5810-262-23KY-58 PMCS/OPNL CHECK 19 Apr 2016D

E135 17 Dec 20166TM 11-5821-333-12AN/ARC-201(V) SINCGARSRADIO HUB BATT REPL

17 Jun 2016M

E145 17 Dec 20166TM 11-5821-333-12AN/ARC-201 A(V) SINCGARS HUBBATT REPL

17 Jun 2016M

E155 24 Oct 2016180TM 11-5810-262-23KY-58 BATTERY REPLACEMENT 27 Apr 2016D

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

10 Jun 2016D

E300 5939.6120AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

5819.6H

E320 15 Jul 2016360AWR 1516 FOR ELTEMERGENCY LOCATORTRANSMITTER G-SWITCH (EBC-406HM)

21 Jul 2015D

E325 15 May 201860AWR 1516R2 FOR ELTREPLACEMENT OF ELTBATTERY PN GS-46

15 May 2013M

E330 16 May 20176AWR1346R16UNDER WATER ACOUSTICBEACON BATTERYREPLACEMENT

16 May 2011Y

E351 25 Jul 20166TM 11-5895-1841-13PREPLACE APX-118TRANSPONDER BATTERY

25 Jan 2016M




PIDMWODATE HRS



ACCUMULATOR 80234554724A1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


08-Dec-2003 DM

DT66160513-Jan-2014

0.5AECOMACCUMULATOR OVERHAUL1-1650-376MWO:

Priority Mnt Level

01-Mar-2004 DR

0RECAPPEDDMWR 1-1650-376-1MWO:

Priority Mnt Level



365

360

5493.1

8023455 953 0

e. ACFT HRS INSTALLEDc. TIME SINCE NEW OR OVERHAULc. SERIAL NUMBER

UH-60A SP-E051151 Days

b. MAKE OR TYPE d. ACFT HRS LAST OIL CHANGEb. SERIAL NUMBER

HELICOPTER, UTILITY AUXILIARY POWER UNIT Hrs

a. NOMENCLATURE AND TYPEa. NOMENCLATUREFREQUENCY

COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b

SAMPLE DATE PIDSAMPLELAST OILEND ITEM

RESULTSDATE RESULTS RECEIVED7. 8.6. REASON FORHOURS5.4.

COMPONENTCHANGE

JW74915210-Jun-2010NORMALROUTINE12.0387374327-May-2010

JC49048307-Jun-2012NORMALROUTINE397.0387412806-Jun-2012

JC49048302-Oct-2012NORMALROUTINE696.04427442730-Sep-2012

BB50010702-Feb-2013NORMALROUTINE1048.0387477902-Feb-2013

TV37483028-Mar-2013NORMALROUTINE1050.0701478124-Mar-2013

BB50010728-Jun-2013NORMALROUTINE1407.0783513828-Jun-2013

DF79966501-Dec-2013NORMALROUTINE1762.0701549328-Nov-2013

MD56306215-May-2014NORMALROUTINE1770.48815493.112-May-2014

RJ52090911-Aug-2015NORMALROUTINE917.05655.205-Aug-2015

9. REMARKS:

For use of this form, see DA PAMs 738-751; the proponent agency is DCSLOGDA FORM 2408-20, DEC 91, MAY BE USED

OIL ANALYSIS LOGDA FORM 2408-20, OCT 1997


8023455116305-302AUXILIARY POWER UNITSP-E051151

701

701

4089

4089

0

0

0

0

5=

TOTAL COMPONENT COUNTS

COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-

READING AT INSTALLATION OF

MODULE/RECORDER3

READING AT REMOVAL OF

7. HISTORY RECORDER S/N

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE

OPERATING HOURSTEMP/TEMP INDEXLCF - 2LCF - 1

HISTORICAL COUNTS ON COMPONENT/MODULE

7. HISTORY RECORDER S/N6.

5. NHA - Serial Number4. P/N3. NOMENCLATURE2. Serial Number1. MODEL

**Note - APU Information LCF1 = NUMBER OF OVERHAULS LCF2 = STARTS SINCEOVERHAUL TTI = STARTS SINCE NEW OPH = ONLY FOR APU's WITH HOUR METERINSTALLED - ENTER TIME ON METER

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

HISTORY RECORDER, COMPONENT, MODULE RECORDDA FORM 2408-16-1-E, OCT91

OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-

12.HISTORY COUNTS AT LAST DEPOTREPL

11.

O/H OR

10.

SERIAL NUMBER9.PART NUMBERNOMENCLATURE

8.

ReportDate:

Major Nomenclature Major Part NumberMajor Wuc Major Serial Number

24-Jun-2016 2/2

15B 116305-302 AUXILIARY POWER UNIT SP-E051151

0000

0000V42C70444502902WHEEL,COMPRESSOR

6000

6000

0000

0000V04-HE5554503991WHEEL, TURBINE

6000

6000


REVERSE OF DA FORM 2408-16-1 E, OCT 91

PIDMWODATE HRS



AUXILIARY POWER UNIT 8023455SP-E0511511. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


06-Nov-2003 DR

QC00000006-Jun-2006

8UNKNOWN(LATE ENTRY)

INLET BARRIER FILTER SYSTEM1-1520-237-50-APU IBFMWO:

Priority Mnt Level



PIDMWODATE HRS



8023455UH-60AHELICOPTER, UTILITY

3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE


FR08-Jul-2013

D CO 3-10 GSAB 801-Aug-2013

SSG BILLIG,BRADLEY K

CONFIGURATION WORK ORDER.INSTRUCTIONS FOR REMOVAL OFTHE #1 (CO-PILOTS) AHRU ANDINSTALLATION OF NAVIGATIONALSYSTEMS: CN-1314 (VG), TRU-2A/A(RG) ON H-60A/L AIRCRAFT

CWO 1-1520-237-20-2MWO:

Mnt LevelPriority

DR21-Jun-2004

PROJECT OLR,DYNCORP,FTCKY

6702-Feb-2006

1SG DEGAND,JOHN L

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

1-1520-237-50-84MWO:

Mnt LevelPriority

DR01-Nov-2006

B CO 96TH ASB 903-Sep-2012

SPC BURKS,CALVIN L

MODIFICATION FOR THE DAULINSTALLATION OF ATTITUDEHEADING REFERENCE UNITS (AHRU)

1-1520-237-50-94MWO:

Mnt LevelPriority

FR23-Jun-2008

FT. HOOD AFMA 14007-May-2012

CIV BRAMLEY,DANIEL R

INSTALLATION OF AUTO RELIGHT &TRANSIENT DROOP IMPROVEMENTFOR T700-GE-701D ENGINES ON UH-60A/HH-60A AIRCRAFT

MWO 1-1520-237-30-3MWO:

Mnt LevelPriority

DM18-Feb-2008

A CO 1-168 3009-May-2012

SSG JOHNSON,BRIAN D

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

1-1520-237-20-3MWO:

Mnt LevelPriority

DM08-Feb-2005


36110-Jan-2006

1SG DEGAND,JOHN L

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

Mnt LevelPriority

DM08-Feb-2005


32010-Jan-2006

1SG DEGAND,JOHN L

INSTALLATION OF BLUE FORCETRACKER REVISION 2

1-1520-237-50-BFT2MWO:

Mnt LevelPriority

DR04-Apr-2006

1108TH TASMG 2015-Jun-2012

SGT HENNIG,DEREK

MODIFICATION OF UH-60A/LHELICOPTERS TO INSTALL THEAN/PRC-117F SATCOM RADIO,MOUNTING FRAME AND ELECTRICALINTERFACE

*1-1520-237-SATCOMMWO:

Mnt LevelPriority


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

PIDMWODATE HRS






FR20-Jan-2011

1108TH TASM7G 2015-Jun-2012

SGT HENNIG,DEREK

MODIFICATION OF UH-60A/LHELICOPTERS TO INSTALL THEAN/PRC-117F SATCOM RADIO,MOUNTING FRAME AND ELECRTICALINTERFACE

1- 1520 -237- SATCOMMWO:

Mnt LevelPriority

DR20-Jan-2011

1108TH T7ASMG 2015-Jun-2012

SGT HENNIG,DEREK

MODIFICATION OF UH-60A/LHELICOPTERS TO INSTALL THEAN/PRC-177F SATCOM RADIO,MOUNTING FRAME AND ELECTRICALINTERFACE.

1- 1520- 237-SATCOMMWO:

Mnt LevelPriority

DR19-Jun-2009

1108TH TASMG 2015-Jun-2012

SGT HENNIG,DEREK

MODIFICATION OF UH6A/LHELICOPTERS TO INSTALL THEAN/PRC-117F SATCOM RADIO,MOUNTING FRAME AND ELECTRICALINTERFACE

A MWO 1-1520-237-SATCOMMWO:

Mnt LevelPriority

DN22-Feb-2010

1108TH TASMG 2015-Jun-2012

SGT HENNIG,DEREK


MWO 1-1520-237-SATCOMMWO:

Mnt LevelPriority

CR20-Jul-2009

1108TH TASMG 2015-Jun-2012

SGT HENNIG,DEREK

A-MWO 1-1520-237-SATCOMINSTALLATION OF AN/PRC-117FSATCOM RADIO

A-MWO 1-1520-237-SATCOM

MWO:

Mnt LevelPriority

DN04-Apr-2006

1108TH TASMG 2015-Jun-2012

SGT HENNIG,DEREK


A-MWO 1-1520-237-SATCOMMWO:

Mnt LevelPriority

FR20-Jan-2011

1108TH TASMG 2016-Jun-2012

SGT HENNIG,DEREK

MODIFICATON OF UH-60A/LHELICOPTERS TO INSTALL THEAN/PRC-117F SATCOM RADIO,MOUNTING FRAME AND ELECTRICALINTERFACE. 1037 (R8)

A-MWO 1-1520-237-SATCOMW/ CHG 5

MWO:

Mnt LevelPriority



PIDMWODATE HRS






DR22-Feb-2010

1108TH TASMG 2016-Jun-2012

SGT HENNIG,DEREK


A-MWO 1-1520-237-SATCOMW/CH4

MWO:

Mnt LevelPriority

FR20-Dec-2011

1108TH TASMG 2016-Jun-2012

SGT HENNIG,DEREK

A-MWO 1-1520-237-SATCOM W/CHG5DATED 20 JAN 2011 MODIFICATION OFUH-60A/L HELICOPTERS TO INSTALLTHE AN/PRC-117F SATIM RADIO ,MOUNTING FRAME AND ELECTRICALINTERFACE.

A-MWO 1-1520-237-SATCOMW/CHG5

MWO:

Mnt LevelPriority

DR22-Feb-2010

1108TH TASMG 2016-Jun-2012

SGT HENNIG,DEREK

MODIFICATION OF UH-60A/LHELICOPTERS TO INSTALL THEAN/PRC-117F SATCOM RADIO,MOUNTING FRAME AND ELECTRICALINTERFACE.

AMWO 1-1520-237-SATCOMMWO:

Mnt LevelPriority

CR10-Feb-2005

1108TH TASMG 2016-Jun-2012

SGT HENNIG,DEREK

INSTALL AN/PRC-117F SATCOMRADIO,MOUNTITNG FRAME &ELECTRICAL INTERFACE

1-1520-237-SATCOMMWO:

Mnt LevelPriority

DN22-Feb-2010

1108TH TASMG 2016-Jun-2012

SGT HENNIG,DEREK

MODIFICATION OF UH-60A/LHELICOPTERS TO INSTALL THEAN/PRC 117F SATCOM RADIO,MOUNTING FRAME, AND ELECTRICALINTERFACE

1-1520-237-SATCOM CH4MWO:

Mnt LevelPriority

CR24-Aug-2009

FT HOOD AFMA,KILLEEN, TX76542

91216-May-2011

W, TINSTALLATION OF IVHMS(INTEGRATED VEHICLE HEALTHMONITORING SYSTEM)

01-1520-237-50-100MWO:

Mnt LevelPriority

DR31-Dec-2007


9016-May-2011

W, TINSTALLATION OF DOPPLER GPSNAVIGATION SYSTEM SETPREPLANNED PRODUCTIMPROVEMENT (DGNS P3I) ON THEUH-60A/L HELICOPTER.

1-1520-237-50-92 (DGNS P3I)MWO:

Mnt LevelPriority



PIDMWODATE HRS






DR13-Oct-2009


25016-May-2011

W, TMODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE AN/AAR-57 IMPROVED COUNTERMEASUREDISPENSER SYSTEM (ICDM) COMMONMISSILE WARNING SYSTEM (CMWS)MODERNIZATION (P3I) ON UH-60A/LAIRCRAFT

1-1520-237-50-97 (P3I)MWO:

Mnt LevelPriority

DM07-Jan-2008

AMCOM/OLRDEFENSESUPPORTSERVICE (DS2)

7619-Sep-2008

CIV KING, JAMESH

INSTALLATION OF CMWS FIFTHSENSOR

1-1520-237-50-99MWO:

Mnt LevelPriority

FR25-Feb-2011


SPC BURKS,CALVIN L

AIRWORTHINESS RELEASE (AWR)FOR UH/HH-60A/L HELICOPTERSEQUIPPED WITH THE DUALSTABILATOR CONTROLLER

AWR 1694MWO:

Mnt LevelPriority

DR25-Jan-2007


SPC BURKS,CALVIN L

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

1-1520-237-20-94MWO:

Mnt LevelPriority

DN02-Jun-2006

MO-AVCRAD 4021-May-2009

INSTALLATION OF RESCUE HOISTCABLE GUARD DEFLECTOR

1-1520-237-50-MEDMWO:

Mnt LevelPriority

DR28-Feb-2005


9422-Feb-2006

1SG DEGAND,JOHN L

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

1-1520-237-50-85MWO:

Mnt LevelPriority

DR21-Apr-2006

DYNCORP,PROJECT OLR.(JS1134)

900029-Jun-2006

SGT REYES,JORGE B

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

1-1520-237-50-CMWSMWO:

Mnt LevelPriority



PIDMWODATE HRS






DR03-Dec-2005

DYNCORP,PROJECT OLR(JS1134)

3829-Jun-2006

SGT REYES,JORGE B

INSTALLATION OF ELECTRONIC DATAMANAGEMENT (EDM) SYSTEM FORBLUE FORCE TRACKING

1-1520-237-50-EDMMWO:

Mnt LevelPriority

DN06-Nov-2003

PROJECT OLRDYNCORPFTCKY

3529-Jun-2006

SSG JOHNSON,BRIAN D

INSTALLATION OF AUXILIARY POWERUNIT (APU) INLET BARRIER FILTER(IBF) SYSTEM FOR T-62T-40-1

1-1520-237-50-APU-IBFMWO:

Mnt LevelPriority

DN23-Apr-2004

PROJECT OLRDYNCORPFTCKY

1029-Jun-2006

SSG JOHNSON,BRIAN D

INSTALLATION OF BALLISTICPROTECTION SYSTEM

1-1520-237-50-BPSMWO:

Mnt LevelPriority




ECDH0745

80234556035T00G01ENGINE ASSY, TURBINEGE-E-207535

320

5601

2458

28546

1156

11728

247

2968

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE





T700-GE-700




OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


24-Jun-2016 2/12

04A 6035T00G01 ENGINE ASSY, TURBINE GE-E-207535

41922601597072421

3821906133891113GEC0076576035T02G01COLD SECTIONMODULE

COND

COND

419228546117282968

0000GGM93R306064T55G01COMBUSTION LINER

COND

COND

41922601597072421

40732125084512018MRS074316055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

419228546117282968

1786000AMDA38925043T24G14STAGE 1 NOZZLEASSY

COND

COND

41922601597072421

44631512887892623GEL0077436064T98G01POWER TURBINEMODULE

COND

COND

419228546117282968

3655000GED00073616035T01G01ACCESSORY MODULE

COND

COND

419228546117282968

1739000FIAL15966034T62P16PARTICLESEPARATOR BLOWER

COND

COND

557828546117282968

5055000UDA968225074T79G07FUEL CONTROL

COND

COND

515328546117282968

3684000APM893RS4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

546828546117282968

4227000CAO009464046T29G09ELECTRICALCONTROL UNIT

COND

COND

547128351112902907

64028171810572ECDH07454046T26G03HISTORY RECORDER

COND

COND


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


24-Jun-2016 3/12

04A 6035T00G01 ENGINE ASSY, TURBINE GE-E-207535

419228546117282968

2511000UDC051504046T25G01COOLER, OIL

COND

COND

419228546117282968

1612000G65985066T38G04ANTI-ICE VALVE

COND

COND




ECDH0745

GE-E-2075356035T02G01COLD SECTION MODULEGEC007657

640

5230

2817

11592

1810

5410

572

1660

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


24-Jun-2016 5/12

04A01 6035T02G01 COLD SECTION MODULE GEC007657

3817902933821110

3550473976861628AGRA27095044T27G02POWER TAKEOFFDRIVE

COND

COND

3817902933821110

3817902933821110GLB004046035T77G10COMPRESSORROTOR ASSEMBLY

COND

COND

3817902933821110

0000NCE1053Y6035T88P07GAS GENERATORTURBINE SHAFT

10227

11000

3817902933821110

0000BJWF42365036T95P01INNER BALANCEPISTON SE

COND

COND

3817902933821110

2552045896131MMTF21186035T79P04COMPRESSORDISCHARGE SEAL

COND

COND

3817902933821110

248049182802977GATN11036035T83P01COMPRESSOR REARSHAFT

1747

5000

3817902933821110

0000VAEM91555044T07P01NO 3 LABYRINTHSEAL

COND

COND

3817902933821110

754025130284617565ASV201435035T57P02VORTEX SPOILER

COND

COND

3817902933821110

22791614659981125GAT8628G5043T04P02TIE ROD,COMPRESSOR

6948

10000

3817902933821110

31442178851412202GAT9284J5066T79P01RING, SPACERCOMPRESSOR

6083

10000

3817902933821110

0000GLHTJ1TF6055T59P01COMPRESSORIMPELLER

4227

5000


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


24-Jun-2016 6/12


3817902933821110

44462895094822729GGA060366039T56G04OUTPUT SHAFT ASSY

COND

COND

3817902933821110

0000GLHT0G66032T26G09STAGE 1 BLISK

4227

5000

3817902933821110

0000GLHTHW836032T27P08STAGE 2 BLISK

6227

7000

3817902933821110

0000GLHTHMLW6038T08P04STAGE 3 & 4 BLISK

6227

7000

3817902933821110

0000GLHTHPWF6038T09P04STAGE 5 BLISK

6227

7000

3817902933821110

30663478271641915BARB14006043T45P01NO 3 BALL BEARING

COND

COND

3817902933821110

86934892281460FCAD03526064T15P03NO 4 ROLLERBEARING

COND

COND




ECDH0745

GEC0076576039T56G04OUTPUT SHAFT ASSYGGA06036

640

5859

2817

31513

1810

11510

572

3279

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


24-Jun-2016 8/12

04A01G 6039T56G04 OUTPUT SHAFT ASSY GGA06036

44462895094822729

2801525573971648BARA19065034T07P03NO 1 BALL BEARING

COND

COND

44462895094822729

2762913155041432MDAA03625035T71P01NO 2 ROLLERBEARING

COND

COND




ECDH0745

GE-E-2075356055T20G05MTCHD ROTOR/STATORASSY

MRS07431

640

5482

2817

23781

1810

10472

572

2565

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


24-Jun-2016 10/12

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRS07431

40732125084512018

0000GATHH6LK6064T85P02STAGE 1 TURBINEDISK

4231

5000

40732125084512018

40732125084512018GGA076656039T57G24G/G STATOR ASSY

COND

COND

40732125084512018

0000GATHGD0N6064T86P01STAGE 2 TURBINEDISK

4231

5000

40732125084512018

1554227073523903BCM065006039T53P04STAGE 1 FWDCOOLING PLATE

1677

4000

40732125084512018

0000GFF5CT7N6064T82P01STAGE 1 REARCOOLING PLATE

4231

5000

40732125084512018

0000PAMEN6576064T83P01STG 2 FWD COOLINGPLATE

4231

5000

40732125084512018

0000GFF5D2J66064T84P02STAGE 2 REARCOOLING PLATE

4231

5000

40732125084512018

40732125084512018GGA074316039T54G13G/G ROTORASSEMBLY

COND

COND




ECDH0745

GE-E-2075356064T98G01POWER TURBINE MODULEGEL007743

640

5872

2817

17659

1810

10810

572

3170

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


24-Jun-2016 12/12

04A03 6064T98G01 POWER TURBINE MODULE GEL007743

44631512887892623

44631512887892623GGA075075043T75G07POWER TURBINEROTOR

COND

COND

44631512887892623

47424501040164GATHC3G86038T32P01STAGE 3 TURBINEDISK

3757

5000

44631512887892623

47424501040164GATHCCEL6038T34P05STAGE 4 TURBINEDISK

3757

5000

44631512887892623

221931181958841GATN H2445125T92G01REPOWER TURBINESHAFT

2012

5000

44631512887892623

552198764236FCAF51475034T27P02NO 5 ROLLERBEARING

COND

COND

44631512887892623

89528381461554MDA485PV6064T37P01NO 6 BALL BEARING

COND

COND




ECD03237

80234556035T00G01ENGINE ASSY, TURBINEGEE306199

2288

3966

18224

7139

6347

8913

1110

2429

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE





T700-GE-700




OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


24-Jun-2016 2/12

04A 6035T00G01 ENGINE ASSY, TURBINE GEE306199

3966713989132429

25711932564851782GEC0070016035T02G01COLD SECTIONMODULE

COND

COND

3375713989132429

976000GGM8WKWNA6064T55G01COMBUSTION LINER

COND

COND

3894713989132429

3185901975031995MRS098456055T20G01MTCHDROTOR/STATOR ASSY

COND

COND

3375713989132429

4368000AMDA01355043T24G04STAGE 1 NOZZLEASSY

COND

COND

3382713989132429

387013919110982522GEL0060986064T98G01POWER TURBINEMODULE

COND

COND

3382713989132429

4240000GED0071006035T01G01ACCESSORY MODULE

COND

COND

3375713989132429

717000SUSJ29166034T62P11PARTICLESEPARATOR BLOWER

893

1000

3966713989132429

1046000133498395074T79G07FUEL CONTROL

COND

COND

3382713989132429

3163000APM194RT4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

3966713989132429

4528000ECD008354046T29G13ELECTRICALCONTROL UNIT

COND

COND

3375604774452169

1697171324879850ECD032374046T26G03HISTORY RECORDER

COND

COND


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


24-Jun-2016 3/12

04A 6035T00G01 ENGINE ASSY, TURBINE GEE306199

3382713989132429

2472000UDC086204046T25G06COOLER, OIL

COND

COND

3375713989132429

0000COMH107874046T28G14ANTI-ICE VALVE

COND

COND




ECD03237

GEE3061996035T02G01COLD SECTION MODULEGEC007001

2288

2571

18224

19325

6347

6485

1110

1782

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


24-Jun-2016 5/12


25291906264031748

2747839251861487ACH397915044T27G02POWER TAKEOFFDRIVE

COND

COND

25291906264031748

25291906264041748GLB209596035T77G14COMPRESSORROTOR ASSEMBLY

COND

COND

25291906264031748

0000NCE304BF6035T88P02GAS GENERATORTURBINE SHAFT

13246

11000

25291906264031748

0000WESN93055056T91P01INNER BALANCEPISTON SEAL

COND

COND

25291906264031748

0000MMTF72416035T79P02COMPRESSORDISCHARGE SE

COND

COND

25291906264031748

0000GAT598176035T83P01COMPRESSOR REARSHAFT

4535

5000

25291906264031748

0000VAEAC5385044T07P01NO 3 LABYRINTHSEAL

COND

COND

25291906264031748

3195988644851565CWAE21845035T57P02VORTEX SPOILER

COND

COND

25291906264031748

38705157079893229GATP90765043T04P02TIE ROD,COMPRESSOR

8376

10000

25291906264031748

2770687552801753GATR67644045T08P01RING, SPACERCOMPRESSOR

9476

10000

25291906264031748

0000GLHTK2RP6055T59P01COMPRESSORIMPELLER

7246

5000


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


24-Jun-2016 6/12


25291906264031748

378913737112222686GGA004936039T56G02OUTPUT SHAFTASSEMBLY

COND

COND

25291906264031748

0000GLHTJMT76032T26G09STAGE 1 BLISK

7246

5000

25291906264031748

0000GLHTJFH36032T27P08STAGE 2 BLISK

9246

7000

25291906264031748

0000GLHTJ69R6038T08P03STAGE 3 & 4 BLISK

9246

7000

25291906264031748

0000GLHTJGE36038T09P04STAGE 5 BLISK

9246

7000

25291906264031748

4775416189401992MDAM16696038T48P02NO 3 BALL BEARING

COND

COND

25291906264031748

2281325586664972MDA613YW6064T14P01NO 4 ROLLERBEARING

COND

COND


11/9/201212:00:00 AM

1 09 NOV 12 - COLD SECTION MODULE INSPECTED, TESTED, AND FOUNDSERVICEABLE ON 06 NOV 12 IAW DMWR1-2840-248 & CHANGES. MT5543,CCAD, CORPUS CHRISTI, TX.

MT5543 CCAD CORPUS CHRISTI, TX



ECD03237

GEC0070016039T56G02OUTPUT SHAFT ASSEMBLYGGA00493

2288

3831

18224

14000

6347

11304

1110

2720

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


24-Jun-2016 8/12

04A01G 6039T56G02 OUTPUT SHAFT ASSEMBLY GGA00493

39151906264031748

013727112222686FCAL70976064T34P02NO 1 BALL BEARING

COND

COND

39151906264031748

117813727112222686MABF85595035T69P01NO 2 ROLLERBEARING

COND

COND




ECD03237

GEE3061996055T20G01MTCHD ROTOR/STATORASSY

MRS09845

2288

3185

18224

9019

6347

7503

1110

1995

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


24-Jun-2016 10/12

04A02B 6055T20G01 MTCHD ROTOR/STATOR ASSY MRS09845

3185901975031995

0000GATHJ6N96064T85P02STAGE 1 TURBINEDISK

7288

5000

3185901975031995

3185901975031995GGA069996068T48G02STATOR GGASSEMBLY

COND

COND

3185901975031995

2390444079541166GAT8261U6064T86P01STAGE 2 TURBINEDISK

4898

5000

3185901975031995

67657823101627GFF5A2206064T81P01STAGE 1 FWDCOOLING PLATE

6612

5000

3185901975031995

16691458155861204GFFR8JY36064T82P01STAGE 1 REARCOOLING PLATE

5619

5000

3185901975031995

189841199979591PAMR22626064T83P01STG 2 FWD COOLINGPLATE

5390

5000

3185901975031995

93323822430643BCM268446064T84P02STAGE 2 REARCOOLING PLATE

6355

5000

3185901975031995

318523822430643GGA098456039T54G13G/G ROTORASSEMBLY

COND

COND




ECD03237

GEE3061996064T98G01POWER TURBINE MODULEGEL006098

2288

3870

18224

13919

6347

11098

1110

2522

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


24-Jun-2016 12/12

04A03 6064T98G01 POWER TURBINE MODULE GEL006098

387013919110982522

387013919110982522GGA079565043T75G07POWER TURBINEROTOR

COND

COND

387013919110982522

0000GATHM8AH6038T32P02STAGE 3 TURBINEDISK

7288

5000

387013919110982522

30171767564201736GATNV7446038T34P05STAGE 4 TURBINEDISK

4271

5000

387013919110982522

2839296938421241GATRN2945125T92G01REPOWER TURBINESHAFT

4449

5000

387013919110982522

0000TMKAE7AW5034T27P01NO 5 ROLLERBEARING

COND

COND

387013919110982522

3105736462271763MABW59756064T36P01NO 6 BALL BEARING

COND

COND



PIDMWODATE HRS



ENGINE ASSY, TURBINE 8023455GE-E-2075351. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


22-Sep-2008 OM

TC02154323-Sep-2008

1HAATSALL H-60 AND H-64 SERIESAIRCRAFT, SUSPECT ENGINEHARNESSES

H-60-08-ASAM-14MWO:

Priority Mnt Level

12-Jan-2009 OM

TC02154305-Feb-2009

0.1HAATST701C GAS GENERATOR (GG)ROTOR ASSEMBLIES


Priority Mnt Level

01-Oct-2009 OM

GG60669201-Oct-2009

0.5AASF#1JACKSON,MS

ALL H-60A SERIES AIRCRAFT,HAMILTON-SUNDSTRAND HYDRO-MECHANICAL UNITS

H-60-10-ASAM-01MWO:

Priority Mnt Level

05-Sep-2012 FU

PL54424611-Sep-2012

0.3AASF#1 FTIG,PAENGINE ANTI-ICE / START BLEEDVALVE (AISBV) PART NUMBER.

H-60-12-ASAM-10MWO:

Priority Mnt Level

30-Jul-2014 FM

AT56275412-Aug-2014

0.1ASSF-1 FTIGANNVILLE,PA17003

HYDRO-MECHANICAL UNIT (HMU)QUICK DISCONNECT PINS,PERFORM ONE-TIME INSPECTIONFOR PRESENCE OF THE SPRINGCLIPS ON THE HMU AND ARM TOTHE VARIABLE GEOMETRY ANTI-ICESTART BLEED VALVE ACTUATINGSHAFT QUICK DISCONNECT PINS.

H-60-14-ASAM-08MWO:

Priority Mnt Level



PIDMWODATE HRS



ENGINE ASSY, TURBINE 8023455GEE3061991. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


31-Dec-1986 DM

MB254123-Jun-2009

20W0MUAAMOD OF PTO BEVEL GEAR SHAFTMWO 1-2840-248-50-27MWO:

Priority Mnt Level

19-Dec-1988 DN

MB254123-Jun-2009

1W0MUAASELF-SEAL ADAPTER ASSY.MWO 55-2840-248-50-28MWO:

Priority Mnt Level

31-Jul-1989 OM

MB254123-Jun-2009

33W0MUAAMODIFICATION OF GG ROTORASSEMBLY T700/701 REWORK T700ENGINES

55-2840-248-50-32MWO:

Priority Mnt Level

01-Jul-1992 DM

MB254123-Jun-2009

1W0MUAAINSTALLATION OF PTO DRIVE ASSYMWO 55-2840-248-50-29MWO:

Priority Mnt Level

30-Jun-1994 DM

MB254123-Jun-2009

1W0MUAAONETIME INSPECT/CONVERSION OFFORMS AND RECORDS T700/701/701C ENGINES

TB 1-2840-248-20-2MWO:

Priority Mnt Level

15-Dec-1998 OU

MB254123-Jun-2009

1W0MUAANEW LIFE LIMITS ON G.G. ROTORAND COMPONENTS

1-2840-248-20-22/UH-60-99MWO:

Priority Mnt Level

22-Sep-2008 OM

MB254123-Jun-2009

1W0MUAAALL H-60 AND H-64 SERIESAIRCRAFT, SUSPECT ENGINEHARNESSES

H-60-08-ASAM-14MWO:

Priority Mnt Level

01-Oct-2009 TT

MD66356631-Mar-2010

1WPJN99H-60-10-ASAM-01: HAMILTON-SUNDSTRAND HYDRO-MECHANICALUNITS FOR SUSPECT PN:4046T52G06,4046T52G09,4046T52G11

H-60-10-AMAM-01MWO:

Priority Mnt Level

05-Sep-2012 FU

PL54424611-Sep-2012

0.3AASF#1 FTIG, PAENGINE ANTI-ICE / START BLEEDVALVE (AISBV) PART NUMBER.

H-60-12-ASAM-10MWO:

Priority Mnt Level

30-Jul-2014 FM

AT56275412-Aug-2014

0.1AASF-1ANNVILLE, PA17003

HYDRO-MECHANICAL UNIT (HMU)QUICK DISCONNECT PINS,PERFORM ONE-TIME INSPECTIONFOR PRESENCE OF THE SPRINGCLIPS ON THE HMU AND ARM TOTHE VARIABLE GEOMETRY ANTI-ICESTART BLEED VALVE ACTUATINGSHAFT QUICK DISCONNECT PINS.

H-60-14-ASAM-08MWO:

Priority Mnt Level



T/T I HIST RCDR SNSERIAL NO. OP HRSLCF-2LCF-1POSHOURSAIRCRAFT AIRCRAFT ENGINE SERIAL NO. 13.12.11. 14.10.9.8.7.6.

(256)123-3456HUNTSVILLEK08DD23. UIC 5. TELEPHONE NUMBER4. LOCATION

16136 SESI

2. Organization

CSGLD-1052

REQUIREMENT CONTROL SYMBOL(Julian)1. PERIOD ENDING DATE


1GE-E-306353 CAO0133557592364213456327956117822971

2GE-E-306443 CAO0151948772574114851323756117822971

1GEE306778 CAO0069179133729522055330062997923307

2GEE307870 ECD0006246941266711817276162997923307

1GEE307962 ECD00980513511917856667923323

2GEE307426 ECD01537470242414456667923323

1GE-E-207878 ECD0336441252618811716284655238023432

2GE-E-307570 ECDH0497240497096544156155238023432

1GEE306199 ECD032372730186347167123858168023455

2GE-E-207535 ECDH07457092835184039158168023455

1GE-E-306531 CAO0106273371177310192332452678223704

2GE-E-207409 ECD0055858152402217718315752678223704


ENGINE COMPONENT OPERATING HOURS RECORDDA FORM 2408-19-3 E, DEC 1991

Workers

Highlight

360

360

5493.6

8023455 5271.1 4082


UH-60A A00501092 Days


HELICOPTER, UTILITY INTERMEDIATE GEARBOX Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

CF70899521-Oct-2011ABNORMALROUTINE4082.03526408217-Oct-2011

BB50010712-Nov-2011NORMALSPECIAL0.03526408203-Nov-2011

RN02185707-Jun-2012ABNORMALROUTINE46.03572412806-Jun-2012

JC49048312-Jun-2012NORMALLAB REQUES49.03575413110-Jun-2012

JC49048302-Oct-2012NORMALROUTINE345.03871442730-Sep-2012


BB50010724-Mar-2013ABNORMALROUTINE699.04225478124-Mar-2013

BB50010701-Apr-2013NORMALSPECIAL702.04228478430-Mar-2013

BB50010728-Jun-2013NORMALROUTINE1056.04582513828-Jun-2013


MD56306215-May-2014NORMALROUTINE1419.74937.15493.113-May-2014

MD56306230-Jul-2014NORMALROUTINE1420.24937.65493.628-Jul-2014

RJ52090911-Aug-2015ABNORMALROUTINE161.65099.25655.205-Aug-2015

EXCEEDS TREND LIMITS, DRAIN/FLUSH RESAMPLE AFTER 30 MIN GROUND RUN.

9. REMARKS:



PIDMWODATE HRS



INPUT MODULE 8023455A264015331. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


02-Aug-2000 OT

QC00000003-Aug-2000


ALL H-60 SERIES AIRCRAFT,REMOVAL OF INPUT MODULE GEARBOX ASSEMBLIESWITHPOTENTIALLY CRACKED BEVELGEARS

UH-60-00-02MWO:

Priority Mnt Level



PIDMWODATE HRS



INTERMEDIATE GEARBOX 8023455A005010921. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


20-Apr-2003 DM

AB242218-Jan-2011

1CCADINTERMEDIATE GEAR BOXASSEMBLY P/N 70357-06300-042(NSN 1615-01-074-5152)

1-1615-288MWO:

Priority Mnt Level

21-Mar-2013 FM

BB50010722-Mar-2013

0.4D CO 6/101STGSAB

ONE-TIME INSPECTION OF SUSPECTSERIAL NUMBERED COMPONENTSFOR PLASTIC MEDIA BLAST (PMB)AND OXIDE FLAKE RESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



LATERAL SERVO BELLCRANK 8023455A289004731. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


07-Jan-1997 OM

QC00000012-Feb-1997

1.2AASF #1TOPEKA, KS.(GP9820)

ALL H-60 AIRCRAFT WITH THELATERAL BELLCRANK ASSEMBLY,P/N 70400-08150-045,MANUFACTURED BY PURDYMACHINE COMPANY (CAGE CODE15152)


Priority Mnt Level

05-Jan-2001 OT

QC00000005-Jan-2001

1AASF #2 SALINA,KS (XS9537)

H-60 SERIES AIRCRAFT, REMOVALOF LATERAL SERVO BELLCRANKASSEMBLY MANUFACTURED BY THEPURDY MACHINE COMPANY, CAGECODE 15152

UH-60-01-03MWO:

Priority Mnt Level



PIDMWODATE HRS





13-May-2015 FM

RJ52090919-Jun-2015

1AASF#3NYARNG

H-60-15-ASAM-04, MAINTENANCEMANDATORY, MAIAN ROTOR BLADEDEBONDING

H-60-15-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS





28-Feb-1998 DU

LM674918-Jul-2011

1CCAD/W0MUAAINCREASE IN FATIGUE LIFE FORTHE MAIN ROTOR BLADE CUFFS,P/N 70150-09109-041 AND 70150-09109-043


Priority Mnt Level

12-Aug-2002 OT

LM674918-Jul-2011

1CCAD/W0MUAAALL H-60 SERIES AIRCRAFT,REVISION TO UH-60-02-11, ONE-TIMEINSPECTION OF MAIN ROTORBLADE CUFF ASSEMBLY

UH-60-02-12MWO:

Priority Mnt Level

07-Jan-2003 DM

LM674918-Jul-2011

1CCAD/W0MUAAONE TIME INSPECTION OF M/RBLADE CUFF ASSY.

UH-60-03-12MWO:

Priority Mnt Level

15-Sep-2005 DT

LM674918-Jul-2011

130CCAD/W0MUAARECAP REQUIREMENTS FOR THEUH-60 MAIN ROTOR BLADE P/N;70150-09100-043, NSN: 1615-01-106-1903

DMWR 1-1615-281 C1MWO:

Priority Mnt Level

15-Apr-2010 OT

LM674918-Jul-2011

3CCAD/W0MUAAALL H-60A/K/L SERIES AIRCRAFT,DEPOT REPAIRED LEGACY MAINROTOR BLADES

H-60-10-SOF-01MWO:

Priority Mnt Level

13-May-2015 FM

RJ52090919-Jun-2015

1AASF#3NYARNG


H-60-15-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS





15-Sep-2005 DO

MF203428-Jun-2013

130CCAD/W0MUAARECAP REQUIREMENTS FOR THEUH-60 MAIN ROTOR BLADE P/N:70150-09100-043 NSN: 1615-01-106-1903

DMWR 1-1615-281 C1MWO:

Priority Mnt Level

09-Apr-2012 OT

MF203428-Jun-2013

1CCAD/W0MUAACHANGE TO DEPOT REPAIREDLEGACY MAIN ROTOR BLADESCOMPLIANCE DATE

H-60-12-SOF-05MWO:

Priority Mnt Level

13-May-2015 FM

RJ52090919-Jun-2015

1AASF#3NYARNG


H-60-15-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS





09-Apr-2012 OT

10-Apr-20120.1COAASFCHANGE TO DEPOT REPAIRED

LEGACY MAIN ROTOR BLADESCOMPLIANCE DATE

H-60-12-SOF-05MWO:

Priority Mnt Level

13-May-2015 FM

RJ52090919-Jun-2015

1AASF#3NYARNG


H-60-15-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS





08-Mar-1994 OM

QC00000013-Feb-1995



Priority Mnt Level

12-Apr-1994 OM

QC00000013-Feb-1995



Priority Mnt Level

07-Dec-1998 OM

QC00000014-Dec-1998




Priority Mnt Level

11-Jul-2000 OT

QC00000013-Jul-2000



UH-60-00-01MWO:

Priority Mnt Level

05-Mar-2001 FT

QC00000010-Apr-2001

2MOAVCRAD(MP4604)


UH-60-01-05MWO:

Priority Mnt Level

26-Mar-2002 OM

QC00000009-Apr-2002




Priority Mnt Level

05-Sep-2012 FM

BB50010703-Apr-2013

0.3D CO 6/101STGSAB


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

BB50010703-Apr-2013

0.3D CO 6/101STGSAB

PERFORM ONE-TIME INSPECTIONFOR SUSPECT MAIN ROTORSPINDLE ANTI-FLAP BRACKETASSEMBLIES

H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS





08-Mar-1994 OM

QC00000013-Feb-1995



Priority Mnt Level

12-Apr-1994 OM

QC00000013-Feb-1995



Priority Mnt Level

07-Dec-1998 OM

QC00000014-Dec-1998




Priority Mnt Level

11-Jul-2000 OT

QC00000013-Jul-2000



UH-60-00-01MWO:

Priority Mnt Level

05-Mar-2001 FT

QC00000010-Apr-2001

2MOAVCRAD(MP4604)


UH-60-01-05MWO:

Priority Mnt Level

26-Mar-2002 OM

QC00000009-Apr-2002




Priority Mnt Level

05-Sep-2012 FM

BB50010703-Apr-2013

0.3D CO 6/101STGSAB


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

BB50010703-Apr-2013

0.3D CO 6/101STGSAB


H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS





08-Mar-1994 OM

QC00000013-Feb-1995



Priority Mnt Level

12-Apr-1994 OM

QC00000013-Feb-1995



Priority Mnt Level

07-Dec-1998 OM

QC00000014-Dec-1998




Priority Mnt Level

11-Jul-2000 OT

QC00000013-Jul-2000



UH-60-00-01MWO:

Priority Mnt Level

05-Mar-2001 FT

QC00000010-Apr-2001

4MOAVCRAD(MP4604)


UH-60-01-05MWO:

Priority Mnt Level

26-Mar-2002 OM

QC00000009-Apr-2002




Priority Mnt Level

05-Sep-2012 FM

BB50010703-Apr-2013

0.3D CO 6/101STGSAB


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

BB50010703-Apr-2013

0.4D CO 6/101STGSAB


H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 8023455D001-014121. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 FM

BB50010703-Apr-2013

0.3D CO 6/101STGSAB


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

BB50010703-Apr-2013

0.3D CO 6//101STGSAB


H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN TRANSMISSION MODULE 8023455A265-015591. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


29-Apr-2009 DR

AB242203-May-2011

1CCADRECAPITALIZATION REQUIREMENTSDMWR 1-1615-371,C1MWO:

Priority Mnt Level

05-Oct-2009 OM

AB242203-May-2011

1CCADREDESIGNED PLANETARY GEARCARRIER RETIREMENT LIFE

UH-60-10-AMAM-02MWO:

Priority Mnt Level

21-Mar-2013 FM

BB50010722-Mar-2013

0.3D CO 6/101STGSAB

ONE-TIME INSPECTION OF SUSPECTSERIAL NUMBERED COMPONENTSFOR PLASTIC MEDIA BLAST (PMB)AND OXIDE FLAKE RESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level



0

720

4966.9

8023455 5692.1 4426


UH-60A A265-01559 Days


HELICOPTER, UTILITY MAIN TRANSMISSION MODULE Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

JC49048302-Oct-2012NORMALBASELINE1.04292442730-Sep-2012


TV37483028-Mar-2013NORMALROUTINE355.04646478124-Mar-2013

BB50010701-Apr-2013NORMALSPECIAL358.04649478430-Mar-2013

BB50010704-Apr-2013NORMALSPECIAL371.04662479703-Apr-2013

BB50010720-May-2013ABNORMALSPECIAL541.04832496719-May-2013

BB50010722-May-2013NORMALSPECIAL6.04838497322-May-2013

BB50010728-Jun-2013ABNORMALROUTINE171.05003513828-Jun-2013

BB50010721-Jul-2013NORMALSPECIAL172.05004513914-Jul-2013

BB50010711-Aug-2013NORMALSPECIAL217.05074520909-Aug-2013


MD56306215-May-2014NORMALROUTINE534.55358.15493.113-May-2014


09 AUG 13 MAIN MOD FILTER BOTTON POPPED

9. REMARKS:



PIDMWODATE HRS



PUMP MODULE ASSY, HYDRAUL 80234557600290ABR1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


27-Oct-2007 DR

JO57442012-Dec-2007

54CCADMU8551

RECAPPEDDMWR 1-4320-271MWO:

Priority Mnt Level



PIDMWODATE HRS



PUMP MODULE ASSY, HYDRAUL 8023455K3233ABR1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


29-Jul-2005 DR

SS090703-Dec-2011

54CCAD, CORPUSCHRISTI TX

RECAPPED DMWR 1-4320-271MWO:

Priority Mnt Level



SECTION I COCKPITSES BEST

4. EQUIPMENT CHECKLIST

8023455 UH-60A

3. AREA NAME 2. MODEL 1. SERIAL NUMBER


1RECEIVER RADIO - R-1496A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER

QTY REQ:NOMENCLATURITEM NO

1DISPLACEMENT GYRO - CN-1314/A (9000C)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GYRO, DIRECTIONAL - CN-998/ASN-43

Unt

UUUUUUnt

Unt

Un

Unt

Un0

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SIGNAL DATA CONVERTER - CV-3338A/ASN-128B

Unt

UUUUUUnt

Unt

Un

Unt

Un0

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U

Unt

UUUUUUnt

Unt

Un

Unt

Un0

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER - R-2139/ARN-123(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING - MT-4834/ARN-123(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMMAND INSTR SYS PROCESSOR - 70600-01038-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING RACK - 70600-01038-102

Unt

UUUUUUnt

Unt

Un

Unt

Un1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT FOR TSEC/KY-58 - 5290279-502

Unt

UUUUUUnt

Unt

Un

Unt

Un1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM ANTENNA - AS-4171/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SAS AMPLIFIER - 70901-02908-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY - 70600-01047-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2RATE GYRO - TRU-2A/A

Unt

UUUUUUnt

Unt

Un

Unt

Un1

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1AMPILIFIER IMPEDANCE - AM-4859A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

AIRCRAFT INVENTORY RECORDDA FORM 2408-17 E, NOV 91



8023455 UH-60A



1VHF/AM ANTENNA FILTER - 70600-01012-102

Unt

UUUUUUnt

Unt

Un

Unt

Un1

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2VHF/FM ANTENNA FILTER - 70600-01011-103

Unt

UUUUUUnt

Unt

Un

Unt

Un2

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER RADAR - RT-1193/ASN-128

Unt

UUUUUUnt

Unt

Un

Unt

Un1

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2ANTENNA - AS-3831/APN-209(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un2

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GLIDE SLOPE ANTENNA - 70600-01043-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM, VHF-AM SENSE ANTENNA - 70600-01019-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2FIRST AID KIT - 6545-00-919-6650

Unt

UUUUUUnt

Unt

Un

Unt

Un2

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRE EXTINGUISHER - FR23-4-11848

Unt

UUUUUUnt

Unt

Un

Unt

Un1

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BAROMETERIC ALTIMETER - AAU-31/A-1

Unt

UUUUUUnt

Unt

Un

Unt

Un1

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BAROMETERIC ALTIMETER - AAU-32/A

Unt

UUUUUUnt

Unt

Un

Unt

Un1

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CREW SEAT - D3801-2

Unt

UUUUUUnt

Unt

Un

Unt

Un2

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF-AM RADIO SET - RT-1518/ARC-164(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

31

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2INTERPHONE CONTROL - C6533/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un2

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER - RT-1115D/APN-209

Unt

UUUUUUnt

Unt

Un

Unt

Un1

33

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1INDICATOR ALTIMETER - ID-1917C/APN-209

Unt

UUUUUUnt

Unt

Un

Unt

Un1

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8023455 UH-60A



1CONTROL RADIO SET - C-7392/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

35

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CONTROL - C-10604(V)6/ARN-184

Unt

UUUUUUnt

Unt

Un

Unt

Un0

36

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPARATOR SIGNAL DATA - CM482/ARC-186(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

38

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2MOUNTREVERSIBLE ARC-186/ARC-201 - 4290268-501

Unt

UUUUUUnt

Unt

Un

Unt

Un2

40

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPUTER DISPLAY UNIT - CP-1252C/ASN-128B

Unt

UUUUUUnt

Unt

Un

Unt

Un1

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CIVIL NAVIGATION CONTROL - C-10048/ARN-123(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

43

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS SET CONTROLLER - C-8021E/ASN-75

Unt

UUUUUUnt

Unt

Un

Unt

Un0

44

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADIO RETRANSMISSION PANEL -70550-01008-042

Unt

UUUUUUnt

Unt

Un

Unt

Un0

45

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MAGNETIC COMPASS - MS17983-4

Unt

UUUUUUnt

Unt

Un

Unt

Un1

46

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2OUTSIDE AIR TEMP INDICATOR - MS28028-1

Unt

UUUUUUnt

Unt

Un

Unt

Un2

47

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOR WING PANEL - 70500-01152-093

Unt

UUUUUUnt

Unt

Un

Unt

Un1

48

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOR WING PANEL - 70500-01152-094

Unt

UUUUUUnt

Unt

Un

Unt

Un1

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MISC. SWITCH PANEL - 70450-01090-044

Unt

UUUUUUnt

Unt

Un

Unt

Un1

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1STABILATOR/FLT CONT PANEL - 70902-01070-048

Unt

UUUUUUnt

Unt

Un

Unt

Un1

51

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2AHRU MOUNTING PLATE FOGS

Unt

UUUUUUnt

Unt

Un

Unt

Un1

60

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8023455 UH-60A



1MOUNTING BASE APX-118

Unt

UUUUUUnt

Unt

Un

Unt

Un1

61

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1765200-20 FOGS CONTROL UNIT (AHRU)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

62

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2ATTITUDE & HEADING REFERENCE UNIT, CN-1716/A (FOGS)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

63

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY 70600-01213-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

64

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER




5/5Report Date: 23-Jun-2016AREA NAMEMODELSERIAL NUMBER

SECTION I COCKPITSES BEST8023455 UH-60A

NAME OR PIDNUMBER DATE

db c

DATE NUMBER RANKRANK NAME OR PID

CHECK CHECK

ba ad

5. VERIFICATION

c

JM8665401 CIV 21-Jun-2016

b. LOCATION/REMARKSCHECK NO.

6. LOCATION OR REMARKS

a. ITEM NUMBER

Nomenclature

GYRO, DIRECTIONAL - CN-998/ASN-43

1 ACFT ARIVED TO BEST IN THIS CONFIGURATION3

SIGNAL DATA CONVERTER -CV-3338A/ASN-128B


MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U


RATE GYRO - TRU-2A/A1 ACFT ARIVED TO BEST IN THIS CONFIGURATION14

CONTROL - C-10604(V)6/ARN-184


COMPARATOR SIGNAL DATA -CM482/ARC-186(V)


COMPASS SET CONTROLLER- C-8021E/ASN-75


RADIO RETRANSMISSIONPANEL -70550-01008-042


AHRU MOUNTING PLATEFOGS


ATTITUDE & HEADINGREFERENCE UNIT, CN-1716/A(FOGS)


REVERSE OF DA FORM 2408-17 E, NOV 91

SECTION II CABINSES BEST


8023455 UH-60A



1CARGO HOOK, FE-7590-145 70800-02503-111

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MARKER BEACON ANTENNA - 70600-02011-103

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-105

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRST AID KIT - 6545-00919-6650

Unt

UUUUUUnt

Unt

Un

Unt

Un1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2FIRE EXTINGUISHER - FR23-4-11848

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRASH AXE - 56D6221

Unt

UUUUUUnt

Unt

Un

Unt

Un0

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HAND SET - H-250/U

Unt

UUUUUUnt

Unt

Un

Unt

Un1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SLAB BATTERY -D8565/11-1

Unt

UUUUUUnt

Unt

Un

Unt

Un1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3INTERPHONE CONTROL - C6533/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un3

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ADAPTER FUEL DRAIN - 70307-03018-102

Unt

UUUUUUnt

Unt

Un

Unt

Un1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4LOCK ASSY BLADE TIEDOWN - 70700-20369-041

Unt

UUUUUUnt

Unt

Un

Unt

Un4

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2PLUG ASSY INTAKE - HIRSS SUPP - 70700-20515-041/042

Unt

UUUUUUnt

Unt

Un

Unt

Un2

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2PLUG ASSY EXHAUST - HIRSS - 70700-20515-043

Unt

UUUUUUnt

Unt

Un

Unt

Un0

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PLUG ASSY APU EXHAUST - 70700-20509-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8023455 UH-60A



1COVER ASSY OIL COOLER - 70700-20511-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BLADE FOLD SET - 70700-20412-011

Unt

UUUUUUnt

Unt

Un

Unt

Un1

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER PITOT TUBE - 70700-20460-041

Unt

UUUUUUnt

Unt

Un

Unt

Un2

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


7TROOP SEATS - 70500-02151-045

Unt

UUUUUUnt

Unt

Un

Unt

Un7

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3TROOP SEATS - 70500-02151-047

Unt

UUUUUUnt

Unt

Un

Unt

Un3

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


10RESTRAINT SYSTEM - 70500-02153-103

Unt

UUUUUUnt

Unt

Un

Unt

Un10

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GUNNER SEAT - 70500-02152-047

Unt

UUUUUUnt

Unt

Un

Unt

Un1

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GUNNER SEAT - 70500-02152-048

Unt

UUUUUUnt

Unt

Un

Unt

Un1

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2RESTRAINT SYSTEM - 70500-02156-102

Unt

UUUUUUnt

Unt

Un

Unt

Un2

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ICS WALK-AROUND CORD - 70602-02016-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PORTABLE INSP. FLOOD LIGHT - 15-0366-1

Unt

UUUUUUnt

Unt

Un

Unt

Un1

29

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HYD. PUMP HANDLE - 15400-50126

Unt

UUUUUUnt

Unt

Un

Unt

Un1

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRING KEY - 70550-03101-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

31

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2EQUIPMENT LOGBOOK - MIL-D-43064

Unt

UUUUUUnt

Unt

Un

Unt

Un1

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1WEIGHT AND BALANCE HANDBOOK - TM 55-1500-342-23

Unt

UUUUUUnt

Unt

Un

Unt

Un1

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8023455 UH-60A



1ELECTRONIC SEQUENCE UNIT - 163290-100-E

Unt

UUUUUUnt

Unt

Un

Unt

Un1

52

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION II CABINSES BEST8023455 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

JM8665401 CIV 21-Jun-2016



a. ITEM NUMBER

Nomenclature

FIRE EXTINGUISHER - FR23-4-11848


CRASH AXE - 56D62211 ACFT ARIVED TO BEST IN THIS CONFIGURATION7

PLUG ASSY EXHAUST - HIRSS- 70700-20515-043


COVER ASSY OIL COOLER -70700-20511-041


ICS WALK-AROUND CORD -70602-02016-041


EQUIPMENT LOGBOOK - MIL-D-43064



SECTION III TRANSITION SECTIONSES BEST


8023455 UH-60A



1ANTENNA LOOP - AS-2108A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2IFF ANTENNA - 70600-02010-103

Unt

UUUUUUnt

Unt

Un

Unt

Un2

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF/AM ANTENNA - 70600-03002-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PUMP FUEL SAMPLER - 82829/4P156-3

Unt

UUUUUUnt

Unt

Un

Unt

Un0

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPENSATOR MAGNETIC FLUX - CN-405/ASN

Unt

UUUUUUnt

Unt

Un

Unt

Un1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS TRANSMITTER - T-611/ASN-43

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS ANTENNA - 22433-40

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF AMPLIFIER - AM-7531/URC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA. GPS (BFT) S67-1575-863

Unt

UUUUUUnt

Unt

Un

Unt

Un1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA, L-BAND (BFT) S65-8282-301

Unt

UUUUUUnt

Unt

Un

Unt

Un1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT, IFM AMPLIFIER-MT-6592/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un1

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3933/ARN-149(V)1, ANTENNA, LOOP

Unt

UUUUUUnt

Unt

Un

Unt

Un0

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP COMMANDER ANTENNA (CMWS ONLY)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IVHMU (CBM MONITOR SYSTEM)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

55

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION III TRANSITION SECTIONSES BEST8023455 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

JM8665401 CIV 21-Jun-2016



a. ITEM NUMBER

Nomenclature

PUMP FUEL SAMPLER -82829/4P156-3


HF AMPLIFIER - AM-7531/URC1 ACFT ARIVED TO BEST IN THIS CONFIGURATION8

AS-3933/ARN-149(V)1,ANTENNA, LOOP


IVHMU (CBM MONITORSYSTEM)



SECTION IV TAIL CONESES BEST


8023455 UH-60A



2VOR/LOC ANTENNA - 70600-05002-101

Unt

UUUUUUnt

Unt

Un

Unt

Un2

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IFM AMPLIFIER - AM-7189A/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF ANTENNA - 4700516-30

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION IV TAIL CONESES BEST8023455 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

JM8665401 CIV 21-Jun-2016



a. ITEM NUMBER

Nomenclature

IFM AMPLIFIER - AM-7189A/ARC



SECTION V TAIL ROTOR PYLONSES BEST


8023455 UH-60A



1CU-2457/ARC(405-11-1), VHF-FM #1 COUPLER ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM10-267, VHF-FM #2 (LEADING EDGE) ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM10-3230, VHF-FM TROOP COMMANDER ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un0

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION V TAIL ROTOR PYLONSES BEST8023455 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

JM8665401 CIV 21-Jun-2016



a. ITEM NUMBER

Nomenclature

FM10-3230, VHF-FM TROOPCOMMANDER ANTENNA



PIDMWODATE HRS





14-Nov-2001 OM

DT66160513-Jan-2014

0.5AECOMINITIAL AND RECURRINGINSPECTION OF THE TAIL ROTORFAIRING ASSEMBLY, ALL H-60AIRCRAFT.

1-1520-237-20-239 (UH-60-MWO:

Priority Mnt Level

14-Nov-2001 OM

RS100511-Jun-2013


UH-60-O2-ASAM-01 TB1-1MWO:

Priority Mnt Level

15-Sep-2005 DR

DT66160513-Jan-2014

0.5AECOMRECAPPED1-1615-281MWO:

Priority Mnt Level

15-Sep-2005 DR

RS100522-Jun-2013


Priority Mnt Level

24-Jan-2013 FN

RB86798020-Dec-2013


AWR 1692 R5MWO:

Priority Mnt Level



PIDMWODATE HRS





14-Nov-2001 OM

RS100520-Sep-2013



Priority Mnt Level

15-Sep-2005 DR

RS100520-Sep-2013


Priority Mnt Level

24-Jan-2013 FN

RB86798020-Dec-2013


AWR 1692 R5MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR GEARBOX ASSY 8023455A006-045071. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 FT

BB50010702-Jul-2013

0.3D C0 3-10 GSABPLASTIC BLAST (PMB) AND OXIDEFLAKE RESIDUE

H-60-ASAM-04MWO:

Priority Mnt Level



360

360

5493.6

8023455 689.1 5138


UH-60A A006-04507 Days


HELICOPTER, UTILITY TAIL ROTOR GEARBOX ASSY Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

BB50010714-Jul-2013ABNORMALBASELINE5138.0513813-Jul-2013

BB50010717-Jul-2013ABNORMALSPECIAL0.05514315-Jul-2013

BB50010717-Jul-2013ABNORMALSPECIAL5143.055208.618-Jul-2013

BB50010721-Jul-2013NORMALSPECIAL2.07514521-Jul-2013


MD56306215-May-2014ABNORMALROUTINE358.4355.15394.113-May-2014


RJ52090911-Aug-2015NORMALROUTINE161.6517.25655.205-Aug-2015

21 JUL 13 EXCESSIVE RUBBING WEAR, TEST RESULTS INDICTAE NO CHANGE IN OIL CONDITION DFR THEN RESAMPLE AT THE END OF THE NEXT FLIGHTDAY/CYCLE

9. REMARKS:



UNIT UNIQUE INVENTORY ITEMSSES BEST


8023455 UH-60A



1BFT PALLET ASSEMBLY (040537-001)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

66

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





UNIT UNIQUE INVENTORY ITEMSSES BEST8023455 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

JM8665401 CIV 21-Jun-2016



a. ITEM NUMBER

Nomenclature

BFT PALLET ASSEMBLY(040537-001)



Documents

Report Date: 20-Jun-2016 1/23 - GSA Auctions · mwo:uh-60-94-asam-08 prioritymnt level 12-apr-1994 m o qc000000 ... ks. 67401 (xd8508) all h-60 aircraft, initial and recurring inspection