UH-60A HELICOPTER, UTILITY 8023495 - GSA Auctions€¦ · aircraft acceptance insp. c/w i/a/w tm...

NUMBERLOCATIONPIDENTRYORGANIZATION

8.7.DATE

6.REMARKS

4. 5.

UH-60A 8023495HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL

Report Date: of 4419-Feb-2016

UNKNOWNAIRCRAFT M/R HEAD RIGGED I/A/W SADWG70400-00003 REV. B SYSTEM CONTROLS HAVEBEEN BIASED I/A A. LATERAL CONTROLSERVO INPUT ROD P/N 70400-02258046 HASBEEN SHORTENED 1/8 TURN. B. AFTCONTROL SERVO INPUT ROD P/N 70400-02258-045 HAS BEEN LENGTHENED 1/2 TURN. C.FWD CONTROL SERVO INPUT ROD P/N 70400-02258-047 HAS BEEN SHORTENED 1/2 TURN.NOTE; WHEN ACFT RIGGING IS BIASEDRIGGING PIN HOLES ARE TEMPORARILYLOST AT THE ABOVE POINTS. (QC000000) (NOPID)

04-Feb-1982 1

UNKNOWN

HI000000

HHT 2ND SQDN 17THCAVALRY

AIRCRAFT ACCEPTANCE INSP. C/W I/A/W TM55-1500-238-25. ACFT ACCEPTED AT THISSTATION WITH 21.4 AIRFRAME HRS. F. LOUISSSG. (QC000000) (NO PID)

08-Mar-1982 1

FT CAMPBELL KY 42223

HI000000


SOF MSG UH-60-82-01; 10 HR INSP. OF ENGINEOUTPUT SHAFTS P/N 70361-08004-042 NSN2835-01-093-4763.TWX DOES NOT APPLY TOTHE SHAFT INSTALLED ON THIS AIRCRAFTWHICH HAS P/N 70361-08004-043 SHAFTSINST. (QC000000) (NO PID)

15-Mar-1982 1

FT CAMPBELLKY 42223

HI000000


SOF MSG UH060-82-05; INSTALLATION OF UH-60A ACFT ENGINE EXAUST DESWIRL DUCT.P/N 70070-30011-108 NSN 15160-01-100-8243.TWX DOES NOT APPLY TO THIS SERIES ACFTSIGNED F. LOUIS. (QC000000) (NO PID)

15-Mar-1982 2


HI000000


SOF MSG UH-60-82-06; ONE TIME INSP. OFPILOT/CO-PILOT SEATS RUBBING BAR C/W.(QC000000) (NO PID)

03-May-1982 1


HI000000


SOF MSG UH-60-82-07; ONE TIME INSP. FORUH-60A AIRCRAFT MAIN TRANSMISSIONBEAM FASTENER HARDWARE. TB 55-1520-237-20-28. TWX DOES NOT APPLY TO THISSERIES ACFT. (QC000000) (NO PID)

06-Jul-1982 1


HI000000


SOF MSG UH-60-82-09; ONE TIME INSP. FORUH-60A ACFT GIMBAL, ENG. MOUNTELASTOMERIC P/N 70361-08001-102. TB 55-1520-237-20-29. TWX DOES NOT APPLY TOTHIS SERIES ACFT. (QC000000) (NO PID)

06-Jul-1982 2


HI000000


SOF MSG UH-60-82-08; RECURRING INSP. FORUH-60A ACFT SHAFT ASSY. ENG OUTPUTINITIATED ON 9 JULY 82 ACFT HRS. 76.2SIGNED F. LOUIS. (QC000000) (NO PID)

09-Jul-1982 1


HI000000


SOF MSG UH-60-82-10; M/R BLADE TIP CAPSCHANGED TO RETIREMENT LIFE COMPONENTC/W. (QC000000) (NO PID)

12-Jul-1982 1


HI000000


SOF MSG UH-60-82-11; ONE TIME INSP. FORUH-60A ACFT M/R SERVO SCREWS COMP.(QC000000) (NO PID)

05-Aug-1982 1


HI000000


SOF MSG UH-60-82-13; ONE TIME INSP. FORUH-60A ACFT M/R SERVO INPUT LINKBEARINGS C/W SIGNED F. LOUIS. (QC000000)(NO PID)

16-Aug-1982 1


HI000000

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.




SOF MSG UH-60-82-14; ONE TIME INSP. FORT/R SERVO C/W SIGNED F. LOUIS. (QC000000)(NO PID)

07-Sep-1982 1


HI000000


SOF MSG UH-60-82-15; DAILY INSP. FORPRIMARY SERVO INPUT ROD INITIALREQUIREMENT C/W SIGNED F. LOUIS.(QC000000) (NO PID)

07-Sep-1982 2


HI000000


SOF MSG UH-60-82-17; ONE TIME INSP. FORT/R SERVO C/W SIGNED F. LOUIS (QC000000)(NO PID)

10-Sep-1982 1


HI000000


SOF MSG UH-60-82-16; ONE TIME INSP. FORFLIGHT CONTROLS MIXER LIMITER BEARINGS& ROLLERS C/W SIGNED F. LOUIS (QC000000)(NO PID)

27-Sep-1982 1


HI000000


(DAMO LETTER) ONE TIME INSP. OFDIRECTIONAL CONTROL LEVER BEARINGS.C/W SIGNED J. BANK. (QC000000) (NO PID)

10-Mar-1983 1


HI000000


SOF MSG UH-60-83-04 ONE TIME INSP. OF ENGAIR INLET C/W SIGNED J. BANK (QC000000)(NO PID)

22-Apr-1983 1


HI000000

BHMOD DYNALECTRONCORP

MOD W1001 UPDATE OF CREW DOORWINDOW DOUBLER SEALANT COMPLETED.SIGNED P. BARKLEY. (QC000000) (NO PID)

10-Aug-1983 1


HI000000


MOD W1002 UPDATE OF CREW DOORWINDOW SCREW WASHER SEALCOMPLETED. SIGNED P. BARKLEY.(QC000000) (NO PID)

10-Aug-1983 2


HI000000


MOD W1007 UPDATE OF CHINESE HAT FWDTO DECK COMP. SIGNED P. BARKLEY.(QC000000) (NO PID)

10-Aug-1983 3


HI000000


MOD W1009 UPDATE OF SEALANT TO FUELLINE SWIVLES COMPLETED. SIGNED P.BARKLEY. (QC000000) (NO PID)

10-Aug-1983 4


HI000000


MOD W1012 UPDATE OF LEFT AND RIGHTGUNNERS WINDOWS COMPLETED. SIGNED P.BARKLEY (QC000000) (NO PID)

10-Aug-1983 5


HI000000


MOD W1013 UPDATE OF LEFT AND RIGHTGUNNERS WINDOWS FWD AIR FRAME SEALCOMPLETED. SIGNED P. BARKLEY (QC000000)(NO PID)

10-Aug-1983 6


HI000000


MOD W1016 UPDATE OF SEAL THICKNESS TOCARGO DOOR LEADING EDGE COMPLETED.SIGNED P. BARKLEY (QC000000) (NO PID)

10-Aug-1983 7


HI000000


MOD W1021 UPDATE OF WASHERS ONELECTRICAL STAND OFFS TOP DECKCOMPLETED. SIGNED P. BARKLEY.(QC000000) (NO PID)

10-Aug-1983 8


HI000000


MOD W1022 UPDATE OF SEALANT TO UPPERDECK MATING SURFACES COMPLETED.SIGNED P. BARKLEY (QC000000) (NO PID)

10-Aug-1983 9


HI000000



8.7.DATE

6.REMARKS

4. 5.




MOD W1023 UPDATE OF SEALANT TOOVERHEAD INSIDE CABIN COMPLETED.SIGNED P. BARKLEY (QC000000) (NO PID)

10-Aug-1983 10


HI000000


MOD W1024 UPDATE OF DRAIN HOLES INLOWER TUB CARGO HOOK AREACOMPLETED. SIGNED P. BARKLEY.(QC000000) (NO PID)

10-Aug-1983 11


HI000000


MOD W1025 UPDATE OF DRAIN HOLES INGLIDES SLOPE REAR ATTACHMENTCOMPLETED. SIGNED P. BARKLEY.(QC000000) (NO PID)

10-Aug-1983 12


HI000000


MOD W1026 UPDATE OF TUBES AT XMSNAREA AROUND T/R CABLES COMPLETED.SIGNED P. BARKLEY. (QC000000) (NO PID)

10-Aug-1983 13


HI000000


MOD W1027 UPDATE OF DRAIN HOLES IN TUBNOSE AREA COMPLETED. SIGNED P.BARKLEY. (QC000000) (NO PID)

10-Aug-1983 14


HI000000


MOD W1028 UPDATE OF SECOND DRAIN LINETO NOSE DOOR COMPLETED. SIGNED P.BARKLEY. (QC000000) (NO PID)

10-Aug-1983 15


HI000000


MOD W1029 UPDATE OF CAPS TO XMSNBARREL NUTS COMPLETED. SIGNED P.BARKLEY. (QC000000) (NO PID)

10-Aug-1983 16


HI000000

ACE TEAMOCM/ACE PERFORMED AT 266 A/C HRS. AT FTCOMPBELL KY. BY ACE TEAM MEMBER LOUISDAILY TSARCOM OCM SEC. ST. LOUIS MO.(QC000000) (NO PID)

16-Aug-1983 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-83-09; ONE TIMEINSPECTION OF STABILATOR AMPLIFIERS BYS/N'S C/W. (QC000000) (NO PID)

11-Oct-1983 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-83-10; ONE TIMEINSPECTION AND REPLACEMENT OFCOLLECTIVE BIAS TUBE ROD END WASHERC/W SIGNED J. BACUS (QC000000) (NO PID)

18-Oct-1983 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-83-12; ONE TIMEINSPECTION OF T/R SERVO FOR BENT VALVESTEM C/W SIGNED J. BACUS. (QC000000) (NOPID)

08-Nov-1983 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-161430Z ONE TIMEINSPECTION OF WIRE HARNESS ROUTINGBETWEEN NO. 1 AND NO. 2 JUNCTION BOXFOR CAHFFING C/W. (QC000000) (NO PID)

19-Mar-1984 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-84-03 ONE TIMEINSPECTION OF T/R PYLON COVER HINGEC/W SIGNED UNKNOWN (QC000000) (NO PID)

06-Apr-1984 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-84-01 ONE TIMEINSPCETION OF M/R SHAFT EXTENDER BY S/NNONE ON ACFT C/W 19 JAN 84 SIGNEDUNKNOWN (QC000000) (NO PID)

24-Apr-1984 1


HI000000



8.7.DATE

6.REMARKS

4. 5.



HHT 2/17TH CAVALRYSOF MSG UH-60A-84-04 ONE TIMEINSPECTION OF STABILATOR AMP'S BY S/NNONE ON ACFT C/W 17JAN 84 SIGNEDUNKNOWN (QC000000) (NO PID)

24-Apr-1984 2


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-84-06 ONE TIMEINSPECTION OF T/R G/B AND INTERMEDIATEG/B OIL LEVEL SIGHT GAUGE C/W SIGNEDUNKNOWN (QC000000) (NO PID)

24-Apr-1984 3


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-84-07 ONE TIMEINSPECTION OF ENGINE OUTPUT SHAFT FORP/N MS 9724-08 BOLTS AND RETORQUE ONALL NUTS AND BOLTS ON SHAFT ASSY #1AND #2 SHAFTS HAVE P/N 08 BOLTS C/WSIGNED J. BACHUS. (QC000000) (NO PID)

14-May-1984 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-84-08 ONE TIMEINSPECTION OF CARGO HOOK SQUIB P/N FE7590-65 FOR EXPIRATION DATE C/W SIGNEDJ. BACHUS. (QC000000) (NO PID)

29-May-1984 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-84-11 ONE TIMEINSPECTION OF LONG/LATERAL LINKS FORBEARING CRACKS C/W SIGNED J. BACHUS.(QC000000) (NO PID)

10-Jul-1984 1

FT. CAMPBELL KY42223

HI000000

ACE TEAMOCM/ACE PERFORMED AT 415 A/C HRS. AT FTCAMPBELL KY BY ACE TEAM MEMBER IAVSCOM OCM SEC. ST LOUIS MO. (QC000000)(NO PID)

18-Jul-1984 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-84-12 ONE TIMEINSPECTION OF M/R SPINDLE BOLTS C/WSIGNED J. BACHUS. (QC000000) (NO PID)

01-Aug-1984 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-84-10 ONE TIME INPECTIONOF TAIL CONE CANTED HINGE BULKHEADRADIUS BLOCKS P/N 70219-05001-108/110-111C/W SIGNED SANTAFERRARA. (QC000000) (NOPID)

27-Aug-1984 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-84-13 ONE TIMEINSPECTION AND REPL. OF T/R CONTROLCABLE BRASS TURNBUCKES MS21251 C/WSIGNED SANTAFERRARA. (QC000000) (NOPID)

07-Nov-1984 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-84-13 ONE TIMEINSPECTION OF T/R CONTROL CABLES C/WSIGNED SANTAFERRARA. (QC000000) (NOPID)

07-Nov-1984 2


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-85-01 ONE TIMEINDPECTION OF STABILATOR AMPLIFIERSWITH NON-LOCKING POTENTIOMETERS C/WINSP. OK NOT SIGNED. (QC000000) (NO PID)

13-Feb-1985 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-85-02 REMOVAL OF REDTAPE ON TACHOMETER TM 55-1520-237-10CHG COMPLETED 1 MAR 85 NOT SIGNED(QC000000) (NO PID)

01-Mar-1985 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-85-03 ONE TIME INSP. OFSTABILATOR AMPLIFIERS P353, P580 NOTINCLUDED IN MESSAGE C/W NOT SIGNED.(QC000000) (NO PID)

01-Mar-1985 2


HI000000



8.7.DATE

6.REMARKS

4. 5.



HHT 2/17TH CAVALRYSOF MSG UH-60A-85-06 ONE TIME INSP. OFPRIMARY SERVOS AND THE OUTPUT RODS,MWO 55-1520-237-13 APPLIED, INSP OK NOTSIGNED (QC000000) (NO PID)

25-Mar-1985 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-85-07 ONE TIME INSP. OFTHE FLT. CONTROL SYSTEM COMPLETED 6APR 85 NO FAULTS NOTED NOT SIGNED.(QC0000000) (NO PID)

06-Apr-1985 1


HI000000

HHT 2/17TH CAVALRYSOF MSG DTG 17200Z APR 85 PP ONE TIMEINSP. OF BUSHING SLEEVE NSN 3120-01-127-8616 FOR SLIPPAGE FROM SUPPORT ASSY1560-01-096-5353 INSP. OK NOT SIGNED(QC000000) (NO PID)

18-Apr-1985 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-85-10 ONE TIME INSP. INUH60A ACFT AS PER TWX INSTRUCTIONSCOMPLETED 2 MAY 85 NOT SIGNED(QC000000) (NO PID)

02-May-1985 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-85-11 ONE TIME SERIALNUMBER CHECK ON M/R SPINDLE & LINERSFOR REPORTING PURPOSE. C/W NOT SIGNED(QC0000000 (NO PID)

02-May-1985 2


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-85-13 CHECK HISTORICALRECORDS FOR SPINDLE REPLACEMENTALSO PREPARE AIRCRAFT FOR MODIFIEDFLYABLE STORAGE. SPINDLE WASREPLACED FOR CORRODED SNAP RING, C/WNOT SIGNED (QC000000) (NO PID)

21-May-1985 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-85-14 CHECKS RECORDSFOR M/R SHAFT AND MAIN MODULE DATAC/W. NOT SIGNED. (QC000000) (NO PID)

04-Jun-1985 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-85-15 CHECK RECORDSFOR M/R HUB DATA C/W NOT SIGNED.(QC000000) (NO PID)

04-Jun-1985 2


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-85-16 UPDATE OF SOF-15C/W NOT SIGNED (QC000000) (NO PID)

04-Jun-1985 3


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-85-17 OUTPUT VIBRATIONCK COMPLETED 25 JUNE 85 #1 ENG .3 IPS TQ34 ACFT HRS 567.7 #2 ENG. .4 IPS TQ 33 NOTSIGNED. (QC000000) (NO PID)

25-Jun-1985 1


HI000000

ACE TEAMOCM/ACE PERFORMED AT 568 A/C HRS. AT FTCAMPBELL KY. BY ACE TEAM MEMBER KAVSCOM OCM SEC. ST. LOUIS MO. NOTSIGNED (QC000000) (NO PID)

08-Jul-1985 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-85-18 REQUIREMENTS FORUNGROUNDING UH-60A BLACKHAWKS C/WNOT SIGNED (QC000000) (NO PID)

13-Jul-1985 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-85-23 ONE TIME INSP. OFT/R DRIVE SHAFT BEARINGS P/N SB1138-101C/W SIGNED MICHEL MARK. (QC000000) (NOPID)

05-Aug-1985 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-85-24 SUPPLEMENT TO ONETIME INSP. T/R DRIVE SHAFT BEARINGS P/NSB1138-101 C/W SIGNED MICHAEL MARK(QC000000) (NO PID)

05-Aug-1985 2


HI000000



8.7.DATE

6.REMARKS

4. 5.



HHT 2/17TH CAVALRYINSTALLATION OF CMA-734 OMEGA/VLFNAVIGATION SET WAS TEMPORARYINSTALLED FOR APPROXIMATELY 150 DAYSINSTRUCTIONS FOR INSTALLATION AREHISTORICAL RECORDS. NOT SIGNED(QC000000) (NO PID)

30-Oct-1985 1


HI000000

HHT 2/17TH CAVALRYINSTALLATION OF ARC-174 (HF) AND KY 75PROVISIONS WAS COMPLETED, WIRINGDIAGRAM IN HISTORICAL RECORD NOTSIGNED (QC000000) (NO PID)

30-Oct-1985 2


HI000000

HHT 2/17TH CAVALRYTB 55-1520-237-20-27 WAS COMPLETEDAPPROXIMATLY 4 NOV 85 (TORQUESTABLIZATION FOR M/R PITCH HORNATTACHMENT BOLTS) NOT SIGNED(QC000000) (NO PID)

11-Dec-1985 1


HI000000

HHT 2/17TH CAVALRYFROM 31 OCT 85 THRU 8 DEC 85, ACFT WASDEPLOYED AT SALT WATER OPERATIONSACFT WAS WASHED AND ENGINES FLUSHEDEVERY 3 DAYS. NOT SIGNED (QC000000) (NOPID)

11-Dec-1985 2


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-86-01 COMPLETEDAPPROXIMATLY 15 APR 86 #13 #4 MRCBEARINGS WERE REPLACED. SOF UH-60-85-02 WAS ALSO COMPLETED AT THIS TIME. NOTSIGNED (QC000000) (NO PID)

15-Apr-1986 1


HI000000

HHT 2/17TH CAVALRYINSTALLATION ON CMA-734 OMEGA/VLFNAVIGATION SET WAS REMOVED TO INCLUDEALL WIRING: SEE WRITE UP ON 2408-15 30OCT 85. NOT SIGNED (QC000000) (NO PID)

23-Apr-1986 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-86-07 C/W 30 APR 86 NOFAULTS NOTED NOT SIGNED (QC000000) (NOPID)

01-May-1986 1


HI000000

ACE TEAMOCM/ACE PERFORMED AT 777 A/C HRS. AT FTCAMPBELL KY BY ACE TEAM MEMBER W.FAVSCOM OCM SEC. ST LOUIS MO. (QC000000)(NO PID)

10-Jun-1986 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-86-06 DOES NOT PERTAINTO THIS ACFT SIGNED A APPLING. (QC000000)(NO PID)

29-Sep-1986 1


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-86-10 ONE TIME STAKINGBEARING IN YAW LEVER ASSY COMPLIEDWITH 9 JULY 86 SIGNED M.D. SSG. (QC000000)(NO PID)

29-Sep-1986 2


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-86-12 S/N OF YAW &COLLECTIVE SERVO ASSY COMPLIED WITH 3JULY 86 SIGNED M DOTS. (QC000000) (NO PID)

29-Sep-1986 3


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-86-13 TIE-DOWN RING NUTREPLACEMENT COMPLIED WITH 29 AUG 86SIGNED M DOTS (QC000000) (NO PID)

29-Sep-1986 4


HI000000

HHT 2/17TH CAVALRYSOF MSG UH-60A-86-18 INSP. ANDREPLACEMENT OF STAB ACTUATOR SIGNEDA APPLING. (QC000000) (NO PID)

29-Sep-1986 5


HI000000

174TH AVN COSOF MSG UH-60A-86-16 BLACKHAWK ACFTLEVER ASSY P/N 70400-02623-09 COMPLETED30 ACT 86 NOT SIGNED. (QC000000) (NO PID)

14-Oct-1986 1

HAAF GA 31409

HI000000



8.7.DATE

6.REMARKS

4. 5.



174TH AVN COSOF MSG UH-60A-86-17 CONTRACTOR INSPON XMSN OIL COOLER FAN SPLINES & T/RDRIVESHAFT COMP. 24 OCT 86 NOT SIGNED(QC000000) (NO PID)

22-Oct-1986 1

HAAF GA 31409

HI000000

174TH AVN COSOF MSG UH-60A-86-19 REPETITIVE INSP OFEYE BOLT P/N 70209-02136-102 COMPLETED 5NOV 86. NOT SIGNED (QC000000) (NO PID)

31-Oct-1986 1

HAAF GA 31409

HI000000

174TH AVN COSOF MSG UH-60A-86-20 FIELD INSP. OF THEFIRST 3 T/R DRIVE SHAFT SPLINESCOUPLINGS AND REMOVAL OF MATERIALUNDER CREW SEATS COMPLETED AT 7 NOV86 799.2 ACFT HRS. NOT SIGNED (QC000000)(NO PID)

07-Nov-1986 1

HAAF GA 31409

HI000000

174TH AVN COSOF MSG UH-60A-86-21 ONE TIME INPS OFCREW SEATS FOR "ARA" MFG. COMPLETED 1DEC 86 805.2 ACFT HRS. SIGNED K.H.(QC000000) (NO PID)

04-Dec-1986 1

HAAF GA 31409

HI000000

174TH AVN COSOF MSG UH-60A-87-03 ONE TIME &RECURRING INSP OF FIRST THREE T/R DRIVESHAFT SPLINE COUPLINGS COMP. 14 MAR 87SIGNED B STEWART. (QC000000) (NO PID)

14-Mar-1987 1

HAAF GA 31409

HI000000

174TH AVN COSOF MSG UH-60A-87-04 REVISION T INSP. OFEYE BOLT P/N 70209-02136-102 COMPLETED25 MARCH 87 NOT SIGNED (QC000000) (NOPID)

25-Mar-1987 1

HAAF GA 31409

HI000000

174TH AVN COSOF MSG UH-60A-87-06 ONE TIME ANDRECURRING INSP OF OIL COOLER SLPINESCOMP. 14 MAY 87 SIGNED ROBERT MACKE(QC000000) (NO PID)

15-May-1987 1

HAAF GA 31409

HI000000

174TH AVN COSOF MSG UH-60A-87-07 ONE TIME ANDRECURRING INSP OF LAT/LONG LINK ASSYCOMP. 15 MAY 87 NOT SIGNED (QC000000)(NO PID)

15-May-1987 2

HAAF GA 31409

HI000000

174TH AVN COSOF MSG UH-60A-87-04 REVISION TO INSP OFEYEBOLTS P/N 70209-02136-102 COMPLETED26 MAR 87 NOT SIGNED. (QC000000) (NO PID)

27-May-1987 1

HAAF GA 31409

HI000000

174TH AVN COSOF MSG UH-60A-87-01 ONE TIME INSP &VALIDATION OF CORRECT TORQUE OF T-700ENG. FUEL DIFFERENTIAL PSI INDICATOR.COMPLETED 23 FEB 87. NOT SIGNED(QC000000) (NO PID)

27-May-1987 2

HAAF GA 31409

HI000000

174TH AVN COSOF MSG UH-60A-87-02 REVISION TOMESSAGE ON T-700 ENGINE FUELDIFFERENTIAL PSI INDICATOR COMPLETED24 FEB 87. NOT SIGNED (QC000000) (NO PID)

27-May-1987 3

HAAF GA 31409

HI000000

174TH AVN COSOF MSG UH-60A-87-05 STABILATOROPERATIONAL PROCEDURES COMPLETED 13APR 87 NOT SIGNED (QC000000) (NO PID)

27-May-1987 4

HAAF GA 31409

HI000000

ASF 157SOF MSG GEN 87-02 ONE TIME INSP FORLOCAL PURCHASED ACFT TIME CHANGECOMPONENTS/PARTS C/W 924.2 ACFT HRS.SIGNED J. JONES WG11. (QC000000) (NO PID)

13-Jul-1987 1

FT RUCKER AL 36362

HI000000



8.7.DATE

6.REMARKS

4. 5.



ASF 157SOF MSG UH-60A-87-08 ONE TIME INPS OFMIDSECTION BELLCRANK ASSY C/W AT 924.9ACFT HRS SIGNED C. YOHN WG11 (QC000000)(NO PID)

15-Jul-1987 1

FT RUCKER AL 36362

HI000000

ACFT INSP MAINT DIVSOF MSG UH-60A-87-10 ONE TIME INSP OFINPUT FLAN COMPLETED BY ACFT HRS 936.8SIGNED G.S TI. (QC000000) (NO PID)

14-Oct-1987 1

FORT B. GA

HI000000

ASF 157TB 55-1520-237-20-86 ELECTRICALLYDISCONNECTION OF PBA C/W AT 949 ACFTHRS SIGNED J. YORK WG11 (QC000000) (NOPID)

02-Nov-1987 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-87-11 ONE TIME INSP OFUPPER & LOWER ROLLER SUPPORT ASSY.C/W AT 949 ACFT HRS. SIGNED R. MICHAELSWG11 (QC000000) (NO PID)

05-Nov-1987 1

FT RUCKER AL 36362

HI000000

ASF 157MIM MSG UH-60A-87-02 TB 55-1520-237-20-93ONE TIME AND RECURRING INSP. OF ENGINECOWLING C/W AT 956 ACFT HRS SIGNED J.YORK WG11 (QC000000) (NO PID)

15-Nov-1987 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-87-12 ONE TIME INSP OFENG POWER TURBINE MODULES FORCERTAIN SERIAL NUMBERS C/W AT 959.8ACFT HRS SIGNED C. YOHN WG11 (QC000000)(NO PID)

03-Dec-1987 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60-87-09 UH-60/EH-60 SERIESACFT CYCLE STABILATOR SLEW SWITCHAND MWO 55-1520-235-50-46 C/W AT 964.9ACFT HRS SIGNED J. YORK WG11 (QC000000)(NO PID)

17-Dec-1987 1

FT RUCKER AL 36362

HI000000

ACE TEAMOCM/ACE PERFORMED AT 971 A/C HRS. AT FTCAMPBELL KY BY ACE TEAM MEMBER WAVSCOM OCM SEC. ST LOUIS NO. SIGNED F.SCHOEDER. (QC000000) (NO PID)

22-Jan-1988 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-88-01 ONE TIME INSP FORCERTAIN S/N T/R BLD C/W 976.7 ACFT. HRS.SIGNED C. YOHN WG11 (QC000000) (NO PID)

16-Feb-1988 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-88-02 ONE TIME INSP OF T/RG/B OUTPUT SHAFT C/W AT 976.7 ACFT HRS.SIGNED C. YOHN WG11 (QC000000) (NO PID)

29-Mar-1988 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-88-04 REVISION TO SOF UH-60-88-02 C/W AT 979 ACFT HRS SIGNED C.YOHN WG11 (QC000000) (NO PID)

12-May-1988 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-88-03 EXTENTION OF RCTIME FOR M/R SHAFT N/C/W DUE TO P/N 70351-08131-044 SHAFT INST. IN MODULE AT 979ACFT HRS. SIGNED C. YOHN WG11(QC000000) (NO PID)

13-May-1988 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-88-04 REVISION TO SOF UH-60-88-02 C/W AT 979 ACFT HRS SIGNED C.YOHN WG11. (NO PID)

13-May-1988 2

FT RUCKER AL 36362

ASF 157SOF MSG UH-60A-88-05 INITIATION OF APUMOAT C/W AT 982 ACFT HRS. SIGNED J. YORKWG11 (QC000000) (NO PID)

15-Jun-1988 1

FT RUCKER AL 36362

HI000000



8.7.DATE

6.REMARKS

4. 5.



6TH BN/159 REG,SOF MSG UH-60A-88-06 OVERHAUL LIFE FORXMSN OIL COOLER BLOWER C/W AT 982 ACFTHRS SIGNED J. YORK WG11 (QC000000) (NOPID)

11-Jul-1988 1

FT RUCKER AL 36362

HI000000

6TH BN/159 REGSOF MSG UH-60A-88-07 REVISION TO SOF UH-60-88-05 C/W AT 986.5 ACFT HRS SIGNED J.YORK WG121 (QC000000) (NO PID)

18-Jul-1988 1

FT RUCKER AL 36362

HI000000

6TH BN/159SOF MSG UH-60A-88-08 REVISION TO SOF UH-60-88-06 C/W AT 986.5 ACFT HRS SIGNED R.SMITH SSG (QC000000) (NO PID)

08-Aug-1988 1

FT RUCKER AL 36362

HI000000

6TH BN/159 REGSOF MSG UH-60A-88-09 ONE TIME INSP OFARA CREW SEATS FOR LOOSE CLEVISSCREWS C/W 986.5 ACFT HRS. SIGNED R.SMITH SSG (QC000000) (NO PID)

08-Aug-1988 2

FT RUCKER AL 36362

HI000000

6TH BN/159 REGSOF MSG UH-60A-88-09 ONE TIME INSP OFARA CREW SEATS FOR LOOSE CLEVISSCREWS C/W 986.5 ACFT HRS. SIGNED R.SMITH SSG. (NO PID)

08-Aug-1988 3

FT RUCKER AL 36362

R/C USARMAVCENINST TWO SHIMS P/N 70361-03013-105BETWEEN OUTER BEARING HOUSING P.N70361-05061-102 AND DRIVE SHAFT BRACKETP.N 70219-03006-011 AT FUSELAGE STATION471 TO CORRECT T/R D/S SHIMMINGPROBLEM, A/C HRS 987.9 INSP. SIGNED C.WALSH. (QC000000) (NO PID)

13-Sep-1988 1

FT RUCKER AL 36362

HI000000

R/C USARMAVCENTB 55-1520-237-20-101 (UH-60-88-10) INSP.TROOP - GUNNER SEAT AND THREE MANMEDEVAC UPPER SUPPORT INSTALLATIONASSEMBLIES C/W INSP. B. MILLS SIGNED C.WALSH. (QC000000) (NO PID)

11-Oct-1988 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-88-11 IMMEDIATERESTRICTIONS OF RAPPELING OPERATIONSC/W AT 992.4 ACFT HRS. SIGNED J. YORKWG11 (QC000000) (NO PID)

27-Oct-1988 1

FT RUCKER AL 36362

HI000000

ASF 157SOF GEN UH-60A-88-02 INSP. FOR INST. OFPORTABLE FIRE EXTINGUISHER C/W AT 992.4ACFT HRS. SIGNED J. YORK WG11 (QC000000)(NO PID)

27-Oct-1988 2

FT RUCKER AL 36362

HI000000

ASF 157SOF GEN UH-60A-88-03 REVISION TO SOF GEN-88-02 INSP FOR CORRECT PORTABLE FIREEXTINGUISHER C/W AT 992.4 ACFT HRS J.YORK WG11 (QC000000) (NO PID)

27-Oct-1988 3

FT RUCKER AL 36362

HI000000

ASF 157PHASE MAINT. INSP. #2 (PMS-2) COMPLETEDAT 987.9 ACFT HRS. BY SIKORSKY SUPPORTSERVICES PHASE #3 DUE AT 1487.9 ACFT HRSC. YOHN WG11. (QC000000) (NO PID)

27-Oct-1988 4

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-88-12 REVISION TO UH-60-88-10 ONE TIME INSP OF TROOP/GUNNER SEATUPPER SUPPORT INST. C/W AT 1001.4 ACFTHRS. SIGNED J. YORK WG11 (QC000000) (NOPID)

09-Nov-1988 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-88-13 ONE TIME INSP. OFM/R BLD PINS C/W AT 1007 ACFT HRS. SIGNEDC. YOHN WG11 (QC000000) (NO PID)

18-Nov-1988 1

FT RUCKER AL 36362

HI000000



8.7.DATE

6.REMARKS

4. 5.



ASF 157SOF MSG UH-60A-89-01 ONE TIME INSP. OFALL T-700 ENGS FOR SUSPECT GAS GENSTATOR SHROUDS C/W AT 1034.1 ACFT HRS.SIGNED C. YOHN WG11 (QC000000) (NO PID)

15-Feb-1989 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-89-02 CORRECTION OF SOFUH-60-89-01 C/W 1034.1 ACFT HRS. SIGNED C.YOHN WG11 (QC000000) (NO PID)

21-Feb-1989 1

FT RUCKER AL 36362

HI000000

ACE TEAMOCM/ACE PERFORMED AT 1034 A/C HRS. ATFT CAMPBELL KY BY ACE TEAM MEMBER NAVSCOM OCM SEC. ST LOUIS MO. SIGNED D.SCHROEDER. (QC000000) (NO PID)

27-Feb-1989 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-89-03 ONE TIME INSP OFM/R SPINDLE RETAINING NUT C/W AT 1066ACFT HRS. SIGNED C. YOHN WG11 (QC000000)(NO PID)

03-Apr-1989 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-89-04 REVISION TO SOF UH-60-89-03 C/W AT 1066.1 ACFT HRS. SIGNED C.YOHN WG11 (QC000000) (NO PID)

03-Apr-1989 2

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-89-05 ONE TIME INSP. OFWIRE STRIKE PROTECTION SYSTEM C/W AT1279.7 ACFT HRS. SIGNED L MEDLEY WG11(QC000000) (NO PID)

15-Jun-1989 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-89-06 ONE TIME INSP OF L/H& R/H RELAY PANELS C/W AT 1152 ACFT HRS.SIGNED J. JONES WG11 (QC000000) (NO PID)

18-Jul-1989 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-89-07 REVISION TO SOF UH-60A-89-06 C/W AT 1162.2 ACFT HRS. SIGNED L.MEDLEY WG11 (QC000000) (NO PID)

07-Aug-1989 1

FT RUCKER AL 36362

HI000000

ASF 157MSG UH-60A-89-08 ONE TIME INSP. OF FUELBOOST PUMP HOSE ATTACHMENT C/WSIGNED L. MEDLEY WG11 (QC000000) (NO PID)

14-Aug-1989 1

FT RUCKER AL 36362

HI000000

ASF 157MSG UH-60A-89-09 CORRECTION OFRETIREMENT LIFE COMPONENT SCHEDULEC/W AT 1162.2 ACFT HRS. SIGNED C. YOHNWG11 (QC000000) (NO PID)

17-Aug-1989 1

FT RUCKER AL 36362

HI000000

ASF 157TB 55-1520-237-20-104 NEWOVERHAUL/RETIREMENT LIFE SCHEDULEFOR UH-60 RETIREMENT LIFE COMPONENTSC/W AT 1172.2 ACFT HRS. SIGNED C. YOHNWG11 (QC000000) (NO PID)

24-Aug-1989 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-89-10 ONE TIME INSP. OFT700 ENG GAS GEN ROTOR AND STATORHISTORICAL RECORDS C/W 1186.8 ACFT HRSSIGNED C. YOHN WG11 (QC000000) (NO PID)

26-Sep-1989 1

FT RUCKER AL 36362

HI000000

AVSCOM OCM SECT, STLOUIS MO,

OCM/ACE PERFOMED AT 1208 ACFT HRS.SIGNED D. SCHROEDER. (QC000000) (NO PID)

09-Nov-1989 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-89-11 ONE TIME INSP. OFOIL COOLER AXIAL FAN C/W 1207.6 ACFTHRS SIGNED C. YOHN WG11 (QC000000) (NOPID)

13-Nov-1989 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-89-12 ONE TIME INSP OF OILCOOLER AXIAL FAN C/W 1207.6 ACFT HRSSIGNED C. YOHN WG11 (QC000000) (NO PID)

27-Nov-1989 1

FT RUCKER AL 36362

HI000000



8.7.DATE

6.REMARKS

4. 5.



ASF 157SOF MSG UH-60A-89-13 ACFT RESTRICTEDAGAINST USING FITTING ASSY P/N 70700-20433-045 FOR RAPPELLING, PARACHUTING,AND TRANSPORTABILITY TIEDOWNOPERATIONS C/W AT 1242.6 ACFT HRS.SIGNED C. YOHN WG11 (QC000000) (NO PID)

08-Dec-1989 1

FT RUCKER AL 36362

HI000000

ASF 157SOF MSG UH-60A-09-01 ONE TIME ANDRECURRING INSP OF M/R BLD EXP PINS C/WAT 1317.1 ACFT HRS. SIGNED C. YOHN WG11(QC000000) (NO PID)

13-Apr-1990 1

FT RUCKER AL 36362

HI000000

ASF 157TB 55-1520-237-20-111 ONE TIME INSP OFUPPER PRESSURE PLATE AND SPINDLE TOHUB ATTACHMENT BOLTS C/W AT 1347.8ACFT HRS. SIGNED C. YOHN WG11 (QC000000)(NO PID)

01-Aug-1990 1

FT RUCKER AL 36362

HI000000

ASF 157TB 55-1520-237-20-117 ONE TIME INSP OFPITCH CONTROL HORNS C/W AT 1347.8 ACFTHRS. SIGNED C, YOHN WG11 (QC000000) (NOPID)

01-Aug-1990 2

FT RUCKER AL 36362

HI000000

ASF 157TB 55-1520-237-20-113 INSP FOR DEFECTIVEROSEMOUNT ICE RATE METERS C/W AT1347.8 ACFT. HRS. SIGNED C. YOHN WG11(QC000000) (NO PID)

01-Aug-1990 3

FT RUCKER AL 36362

HI000000

ASF 157SOF UH-60-90-02 ONE TIME AND RECURRINGINSP OF T/R P/C BEAM RETAINING NUT ANDWASHER C/W AT 1350.1 ACFT HRS SIGNED R.MICHAELS. (QC000000) (NO PID)

16-Aug-1990 1

FT RUCKER AL 36362

HI000000


OCM/ACE PERFORMED AT 1482 ACFT HRS.SIGNED D. EASLEY. (QC000000) (NO PID)

16-Jan-1991 1

FT RUCKER AL 36362

HI000000

ACFT INSP MAIN DIV,ASAM UH-60-91-05 ONE TIME INSP FOR 4UNSERVICABLE M/R SPINDLES C/W AT 1487.6ACFT HRS. NOT SIGNED (QC000000) (NO PID)

28-Feb-1991 1

FT BENNING GA

HI000000

ACFT INSP MAIN DIV,PERIODIC INSP #3 COMPLETED AT 1487.6ACFT HRS PERIODIC INSP #4 AT 1987.6 HRSNOT SIGNED (QC000000) (NO PID)

07-Mar-1991 1

FT BENNING GA

HI000000

ASF 157ASAM UH-60-91-01 ONE TIME REPLACEMENTAND 30 HR INSP. OF T/R P/C BEAM RETAININGNUT WASHER C/W AT 1504.2 ACFT HRS.SIGNED C. YOHN WG11 (QC000000) (NO PID)

11-Apr-1991 1

FT RUCKER AL 36362

HI000000

ASF 157ASAM UH-60-91-02 RECURRING EROSIONINSP. OF M/R BLDS N/A FOR THIS ACFTSIGNED C. YOHN WG11 (QC000000) (NO PID)

11-Apr-1991 2

FT RUCKER AL 36362

HI000000

ASF 157ASAM UH-60-91-03 EXTENDED TBO HRS FORDESERT SHEILD OPERATIONS N/A FOR THISACFT. SIGNED C. YOHN WG11 (QC000000) (NOPID)

11-Apr-1991 3

FT RUCKER AL 36362

HI000000

ASF 157ASAM UH-60-91-06 ONE TIME INSP. IF CARGOHOOK INTERNAL WIRE BUNDLE ROUTING C/WAT 1504.2 ACFT HRS C. YOHN WG11(QC000000) (NO PID)

11-Apr-1991 4

FT RUCKER AL 36362

HI000000



8.7.DATE

6.REMARKS

4. 5.



ASF 157ASAM UH-60-91-07 ADVANCE NOTIFICATIONOF MANUAL CHANGE FOR MAIN XMSNMODULE C/W AT 1504.2 ACFT HRS C. YOHNWG11 (QC000000) (NO PID)

11-Apr-1991 5

FT RUCKER AL 36362

HI000000

ASF 157ASAM UH-60-91-08 ONE TIME INPS OF FIREEXTENGUISHING SYSTEM C/W AT 1504.2 ACFTHRS SIGNED C. YOHN WG11 (QC000000) (NOPID)

11-Apr-1991 6

FT RUCKER AL 36362

HI000000

ASF 157ASAM UH-60-91-09 CHANGE TO INSPPROCEDURES FOR M/R SPINDLEELASTROMERIC BEARINGS C/W AT 1541.8ACFT HRS. C. YOHN WG11 (QC000000) (NOPID)

08-Aug-1991 1

FT RUCKER AL 36362

HI000000

ASF 157ASAM UH-60-91-10 ONE TIME INPS ANDREPLACEMENT FOR M/L/G BRAKE ASSYPISTON INSULATORS C/W 1544.7 ACFT HRS.C. YOHN WG11 (QC000000) (NO PID)

08-Aug-1991 2

FT RUCKER AL 36362

HI000000

ASF 157ASAM UH-60-91-04 N/A FOR THIS ACFTSIGNED C. YOHN WG11 (QC000000) (NO PID)

13-Aug-1991 1

FT RUCKER AL 36362

HI000000

ASF 157ASAM UH-60-92-01 INSP. FOR THREEUNSERVICABLE SPINDLES C/W AT 1578 ACFTHRS. C. YOHN WG11 (QC000000) (NO PID)

10-Jan-1992 1

FT RUCKER AL 36362

HI000000

ASF 157ASAM UH-60-92-03 UH-60 T700 GAS GENTURBINE BLADE FAILERS/ENGINE CLEANINGPROCEDURES C/W AT 1981 ACFT HRS.SIGNED C. YOHN WG11 (QC000000) (NO PID)

15-Jun-1992 1

FT RUCKER AL 36362

HI000000

ASF 157ASAM UH-60-92-04 N/A THIS ACFT. SIGNED C.YOHN (QC000000) (NO PID)

27-Jul-1992 1

FT RUCKER AL 36362

HI000000

ASF 157ASAM UH-60-92-06 ONE TIME INSPECTIONFOR PROPER HARDWARE ON T/R PEDALADJUSTER ASSY C/W AT 1979 ACFT HRSSIGNED C. YOHN WG11 (QC000000) (NO PID)

28-Sep-1992 1

FT RUCKER AL 36362

HI000000

ASF 157,ASAM UH-60-92-05 INSPECTION ANDREPLACEMENT OF M/R BLADE EXPANDABLEPINS C/W AT 1979 ACFT HRS. SIGNED C. YOHNWG11 (QC000000) (NO PID)

29-Sep-1992 1

FT RUCKER AL 36362

HI000000

ASF 157,ASAM UH-60-93-01 ONE TIME OPERATIONALCHECK OF MAIN XMSN AND G/B CHIPDETECTOR SYSTEMS C/W AT 1979 ACFT HRS.SIGNED C. YOHN WG11. (QC000000) (NO PID)

01-Dec-1992 1

FT RUCKER AL 36362

HI000000

ASF 157,ASAM UH-60-93-02 T700 ENG GAS TURBINEROTOR FAILURES/ENG CLEANING ANDSINGLE ENG OPERATION PLANNING C/W 1979ACFT HRS. SIGNED C. YOHN WG11.(QC000000) (NO PID)

02-Dec-1992 1

FT RUCKER AL 36362

HI000000

ASF 157,ASAM UH-60-93-03 REVISION TO ASAM UH-60-92-05 INSP AND REPLACEMENT OF M/RBLADE EXPANDABLE PINS C/W AT 1979 ACFTHRS. SIGNED C. YOHN WG11. (QC000000) (NOPID)

03-Dec-1992 1

FT RUCKER AL 36362

HI000000

ASF 157,ASAM GEN-93-01 PROHIBIT USE OF BRACO599 CORROSION PREVENTATIVE COMPOUNDC/W AT 1979 ACFT HRS. SIGNED C. YOHNWG11. (QC000000) (NO PID)

04-Dec-1992 1

FT RUCKER AL 36362

HI000000



8.7.DATE

6.REMARKS

4. 5.



ASF 157,ASAM UH-60-93-04 REVISION TO ASAM UH-60-92-06 ONE TIME INSP FOR PROPERHARDWARE ON THE T/R PEDAL ADJUSTERASSY C/W AT 1979 ACFT HRS. SIGNED C.YOHN. (QC000000) (NO PID)

09-Dec-1992 1

FT RUCKER AL 36362

HI000000

ASF 157,PERIODIC INSP #4 COMPLETED AT 1997 ACFTHRS. PERIODIC INSP #4 DUE AT 2479 ACFTHRS. SIGNED C. YOHN WG11. (QC000000) (NOPID)

09-Dec-1992 2

FT RUCKER AL 36362

HI000000

ASF 157,ASAM UH-60-93-05 ONE TIME INSP FOR T/RDRIVE SHAFT VISCOUS DAMPER BEARINGSC/W AT 1979.1 ACFT HRS. SIGNED C. YOHNWG11. (QC000000) (NO PID)

22-Dec-1992 1

FT RUCKER AL 36362

HI000000

ASF 157,ASAM UH-60-93-06 ONE TIME INSP TOREMOVE SUSPECT T/R PITCH BEAMS C/W AT1979.1 ACFT HRS. SIGNED C. YOHN WG11.(QC000000) (NO PID)

22-Dec-1992 2

FT RUCKER AL 36362

HI000000

ASF 157,ASAM UH-60-93-07 REVISION TO CORROSIONLIMITS FOR T/R G/B SERVO MOUNTING BOREC/W AT 1981 ACFT HRS. SIGNED C. YOHNWG11. (QC000000) (NO PID)

23-Dec-1992 1

FT RUCKER AL 36362

HI000000

ASF 157,ASAM UH-60-93-08 BIAS T/R RIGGING BY 3DEGREES C/W AT 1989 ACFT HRS. SIGNED C.YOHN WG11. (QC000000) (NO PID)

05-Jan-1993 1

FT RUCKER AL 36362

HI000000

ASF 157,ACM/ACE COMPLETED AT 1900 ACFT HRS BYAVSCOM OCM SEC. ST LOUIS MO. SIGNED C.YOHN WG11. (QC000000) (NO PID)

13-Jan-1993 1

FT RUCKER AL 36362

HI000000

DYNCORP OLR,ASAM UH-60-93-09 ONE TIME INSP TOCOMPLY WITH SYSTEM MWOS C/W AT 2013ACFT HRS. SIGNED R. CLARK. (QC000000) (NOPID)

01-Apr-1993 1

FT HOOD TX.

HI000000

ASF 157,ASAM UH-60-93-10 N/A THIS ACFT. SIGNED C.YOHN WG11. (QC000000) (NO PID)

10-Apr-1993 1

FT RUCKER AL 36362

HI000000

DYNCORP OLR,ASAM UH-60-93-11 ONE TIME INSP ANDREPLACEMENT OF ARA CREW RESTRAINTSYSTEMS C/W AT 2013 ACFT HRS. SIGNED R.CLARK. (QC000000) (NO PID)

12-Apr-1993 1

FT HOOD TX

HI000000

ASF 157,ASAM UH-60-93-12 ABRUPT CHANGE IN M/RTRACK/VIBRATIONS C/W AT 2010.9 ACFT HRS.SIGNED C. YOHN WG11. (QC000000) (NO PID)

14-Apr-1993 1

FT RUCKER AL 36362

HI000000

ASF 157,ASAM UH-60-93-13 N/A THIS ACFT. SIGNED C.YOHN. (QC000000) (NO PID)

02-Jun-1993 1

FT RUCKER AL 36362

HI000000


03-Jun-1993 1

FT RUCKER AL 36362

HI000000


12-Jul-1993 1

FT RUCKER AL 36362

HI000000

ASF 157,ASAM UH-60-93-16 ONE TIME INSP OF THEHYD PUMP KNURLED BLEED RELIEF VALVEC/W AT 2129 ACFT. HRS. SIGNED C. YOHNWG11. (QC000000) (NO PID)

13-Aug-1993 1

FT RUCKER AL 36362

HI000000



8.7.DATE

6.REMARKS

4. 5.



ASF 157,ASAM UH-60-94-01 MASTER WARNING PANELREWORK FOR NVG COMPATABILITY C/W AT2174.7 ACFT. HRS. SIGNED C. YOHN WG11.(QC000000) (NO PID)

19-Nov-1993 1

FT RUCKER AL 36362

HI000000

ASF 157,ASAM UH-60-94-02 RETURN FOR EXCHANGEOF CERTAIN (ARA) MANUFACTUREBUCKLE/CROTCH STRAP ASSY'S P/N 4495-28IN ALL H-60 SERIES ACFT C/W AT 2204.5 ACFTHRS. SIGNED C. YOHN WG11. (QC000000) (NOPID)

26-Jan-1994 1

FT RUCKER AL. 36362

HI000000

ASF 157,ASAM UH-60-94-03 ONE TIMEREFURBISHMENT OF M/R SPINDLES ANDREPLACEMENT OF CERTAIN M/R THRUSTBEARINGS C/W AT 2204.5 ACFT HRS. SIGNEDC. YOHN WG11. (QC000000) (NO PID)

01-Feb-1994 1

FT RUCKER AL. 36362

HI000000

ASF 157,ASAM UH-60-94-04 ONE TIME INSP TOREMOVE SUSPECT T/R PITCH BEAMS C/W AT2204.5 ACFT HRS. SIGNED C. YOHN WG11.(QC000000) (NO PID)

03-Feb-1994 1

FT RUCKER AL. 36362

HI000000


OCM/ACE PERFORMED AT 2210.9 ACFT HRS.BY ACE TEAM MEMBER B. SIGNED C.MAUSER. (QC000000) (NO PID)

18-Feb-1994 1

FT RUCKER AL. 36362

HI000000

ASF 157,ASAM UH-60-94-05 ONE TIME REMOVAL OFT/R GEARBOX WITHOUT SHAFT P/N 70358-06620-101 C/W AT 2210 ACFT HRS SIGNED C.YOHN WG11. (QC000000) (NO PID)

23-Feb-1994 1

FT RUCKER AL. 36362

HI000000

ASF 157,ASAM UH-60-94-06 COCKPITSTANDARDIZATION OF PILOTS/COPILOTSRESTRAINT RELEASE SYSTEMS. C/W AT2210.9 ACFT HRS SIGNED C. YOHN WG11.(QC000000) (NO PID)

23-Feb-1994 2

FT RUCKER AL. 36362

HI000000

ASF 157,ASAM UH-60-94-07 CHANGE TOOVERHAUL/RETIREMENT TABLE C/W AT2212.3 ACFT HRS. SIGNED C YOHN WG11.(QC000000) (NO PID)

17-Mar-1994 1

FT RUCKER AL. 36362

HI000000

ASF 157,ASAM UH-60-94-08 CHANGE TO ASAM UH-60-94-07 C/W AT 2212.3 ACFT HRS. SIGNED CYOHN WG11. (QC000000) (NO PID)

17-Mar-1994 2

FT RUCKER AL. 36362

HI000000

ASF 157,ASAM UH-60-94-09 REMOVAL OF CERTAIN S/NPRIMARY SERVO ASSEMBLIES C/W AT 2218.6ACFT HRS. SIGNED C YOHN (QC000000) (NOPID)

07-Apr-1994 1

FT RUCKER AL. 36362

HI000000

ASF 157,ASAM UH-60-94-10 REVISION TO ASAM UH-60-94-03 ONE TIME REFURBISHMENT OF M/RSPINDLES AND REPLACEMENT OF M/RTHRUST BEARING (ADD -046 THRUSTBEARING) C/W AT 2222.9 ACFT HRS. SIGNEDC. YOHN WG11. (QC000000) (NO PID)

26-Apr-1994 1

FT RUCKER AL. 36362

HI000000

ASF 157,ASAM UH-60-94-11 M/R BLADE DE-ICEHEATER MAT RESISTANCE MEASUREMENTSTEST METHOD C/W AT 2222.9 ACFT HRSSIGNED C. YOHN WG11. (QC000000) (NO PID)

26-Apr-1994 2

FT RUCKER AL. 36362

HI000000

ASF 157,ASAM UH-60-94-12 N/A THIS ACFT SIGNED C.YOHN WG11. (QC00000) (NO PID)

13-Jul-1994 1

FT RUCKER AL. 36362

HI000000



8.7.DATE

6.REMARKS

4. 5.



ASF 157,UH-60-95-ASAM-05 CHANGE IN RETIREMENTLIFE FOR SERVO BEAM RAILS AND PMS-2INSP. OF P/N 70209-22103-050/052/054/056RAILS. C/W AT 2374 ACFT HRS. SIGNED R.MICHAELS. (QC00000) (NO PID)

28-Feb-1995 1

FT RUCKER AL. 36362

HI000000

ASF 157,ACE/AACE INSPECTION COMPLETED AT 2382ACFT HRS. SIGNED R. MICHAELS. (QC00000)(NO PID)

12-Apr-1995 1

FT RUCKER AL. 36362

HI000000

ASF 157,UH-60-95-ASAM-06 ONE TIME INSP. FORCRACKED MAIN XMSN BEAMS, UPPER DECKSKIN CRACKS. C/W AT 2398 ACFT HRS.SIGNED R. MICHAELS (QC000000) (NO PID)

30-Jun-1995 1

FT RUCKER AL. 36362

HI000000

ASF 157,UH-60-95-ASAM-07 CRITERIA FORTROOP/GUNNER SEAT ATTENUATION WIRE,EXPLICIT SHIMMING PROCEDURES FORATTENUATION ROLLERS C/W AT 2424.5 ACFTHRS. SIGNED R. MICHAELS. (QC000000) (NOPID)

12-Aug-1995 1

FT RUCKER AL. 36362

HI000000

ASF 157,ASAM UH-60-95-01 HOISTING AND AERIALRECOVERY OF UH-60/EH-60 ESSS FIXEDPROVISIONED HELICOPTERS C/W AT 2328.2ACFT HRS. SIGNED C. YOHN WG11.(QC000000) (NO PID)

17-Oct-1995 1

FT RUCKER AL. 36362

HI000000

ASF 157,ASAM UH-60-95-02 ALL UH-60 ACFT,REQUIREMENT TO OPERATE THE FUELTANKS SUBMERGED BOOST PUMPS-ON-ATALL TIMES WITH ALL FUELS DURING GROUNDRUN AND FLT OPERATIONS C/W AT 2329.1ACFT HRS SIGNED C. YOHN. (QC000000) (NOPID)

25-Oct-1995 1

FT RUCKER AL. 36362

HI000000

ASF 157,ASAM UH-60-95-03 ALL UH-60 ACFT, SHALLREQUIRE RESHIMMING OF T/R PIVOTBEARINGS PER REVISED PROCEDURES ANDCERTAIN BLADE ASSEMBLIES WILL BEINSPECTED FOR SPECIFIED SERIALNUMBERS WHICH CONTAIN COMPOSITEPIVOT BEARING RETAINERS C/W AT 2329.1ACFT HRS. SIGNED C. YOHN WG11.(QC000000) (NO PID)

01-Nov-1995 1

FT RUCKER AL. 36362

HI000000

ASF 157,ASAM UH-60-95-04 REDUCTION OF TORQUEOF SELF RETAINING PIVOT BOLTS ANDRECURRING INSPECTION AT PMS-2 C/W AT2330 ACFT. HRS. SIGNED R. MICHAELS.(QC000000) (NO PID)

23-Nov-1995 1

FT RUCKER AL. 36362

HI000000

ASF 157,TB 1-2840-248-20-3 ONE TIME INSP ANDCONVERSION OF T700 ENG RECORDS C/W AT2330.9 ACFT HRS SIGNED C. YOHN WG11.(QC000000) (NO PID)

29-Nov-1995 1

FT RUCKER AL. 36362

HI000000

ASF 157,TB 1-2835-214-20-1 ONE TIME INSP OF FORMSAND RECORDS FOR H-60 ACFT APU C/W AT2330.9 ACFT HRS. SIGNED C. YOHN WG11.(QC000000) (NO PID)

29-Nov-1995 2

FT RUCKER AL. 36362

HI000000

ASF 157,UH-60-95-SOF-01 THREE PART INSP.PROCEDURE AND REPL. OF T/R GEARBOXC/W AT 2333 ACFT HRS. SIGNED R. MICHAELS.(QC000000) (NO PID)

09-Dec-1995 1

FT RUCKER AL. 36362

HI000000



8.7.DATE

6.REMARKS

4. 5.



1106TH AVCRAD,UH-60-95-ASAM-08 INSP OF T700-GE-700ENGINES FOR UNDAMPENED GG TURBINEROTOR BLADES C/W AT 2446 ACFT HRS.SIGNED ILLEGIBLE. (QC000000) (NO PID)

02-Jul-1996 1

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-96-ASAM-01 MANDATORYREPLACEMENT OF SPECIFIC FLIGHTCONTROL SYSTEM PIVOT BOLTS ANDATTACHMENT NUTS C/W AT 2446 ACFT HRS.SIGNED ILLEGIBLE. (QC000000) (NO PID)

02-Jul-1996 2

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,SOF UH-60-96-01 INSPECTION OF FORWARDBELLCRANK SUPPORT ASSEMBLY C/W AT2446 ACFT HRS. SIGNED ILLEGIBLE.(QC000000) (NO PID)

02-Jul-1996 3

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-96-ASAM-02 ONE TIME INSP. FORSUSPECT M/R SHAFT BOLTS C/W AT 2446ACFT HRS. SIGNED ILLEGIBLE. (QC000000)(NO PID)

02-Jul-1996 4

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-96-ASAM-03 REVISION TO UH-60-96-ASAM-02 ONE TIME INSP M/R SHAFT NUTBOLTS C/W AT 2446 ACFT HRS SIGNEDILLEGIBLE. (QC000000) (NO PID)

02-Jul-1996 5

FRESNO, CA. 93727

HI000000

1106TH AVCRADSOF UH-60-96-02 ONE TIME INSP. FORSUSPECT BAD T/R INBOARD RETENTIONPLATE. C/W AT 2446 ACFT HRS SIGNEDILLEGIBLE. (QC000000) (NO PID)

02-Jul-1996 6

FRESNO, CA. 93727

HI000000

1106TH AVCRADSOF UH-60-06-03 INSP OF M/R BLADES FORINST. OF CERTAIN S/N M/R CUFFS MFG BYFENN C/W AT 2446 ACFT HRS. SIGNEDILLEGIBLE. (QC000000) (NO PID)

02-Jul-1996 7

FRESNO, CA. 93727

HI000000

1106TH AVCRADSOF UH-60-96-04 INSP OF AFT BELLCRANKASSY FOR SPECIFIC SERIAL NUMBER C/W AT2446 ACFT. HRS SIGNED ILLEGIBLE.(QC000000) (NO PID)

02-Jul-1996 8

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-96-ASAM-05 INCREASE LIFE OF FWDSUPPORT ASSY P/N 70400-08116-048 C/W AT2446 ACFT HRS SIGNED V ILLEGIBLE.(QC000000) (NO PID)

23-Jul-1996 1

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-96-ASAM-05 INCREASE LIFE OF FWDSUPPORT ASSY P/N 70400-08116-048 C/W AT2446 ACFT. HRS SIGNED V ILLEGIBLE.(QC000000) (NO PID)

23-Jul-1996 2

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-96-ASAM-07 ONE TIME INSP. OFCERTAIN P/N S/N SPINDLE ASSY. RETAININGRODS C/W AT 2446 ACFT. HRS SIGNEDILLEGIBLE. (QC000000) (NO PID)

27-Sep-1996 1

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-96-ASAM-08 INCREASE FATIGUE LIFEOF AREX MFG T/R I/B RETENTION PLATE C/WAT 2446 ACFT. HRS SIGNED ILLEGIBLE.(QC000000) (NO PID)

27-Sep-1996 2

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-96-ASAM-09 INSP. OF STABILATORACTUATOR CLEVIS FOR EPOXY PRIMER N/L/TNEXT PMS-2 C/W AT 2446 ACFT HRS. SIGNEDILLEGIBLE. (QC000000) (NO PID)

27-Sep-1996 3

FRESNO, CA. 93727

HI000000



8.7.DATE

6.REMARKS

4. 5.



1106TH AVCRADUH-60-96-ASAM-10 INSP. AND REPLACEMENTOF ELASTROMERIC BEARING SLEEVE C/W AT2446 ACFT HRS SIGNED ILLEGIBLE.(QC000000) (NO PID)

27-Sep-1996 4

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-96-ASAM-11 INCREASE FATIGUE LIFEOF FENN MFG M/R BLADE CUFF C/W AT 2446ACFT HRS SIGNED ILLEGIBLE. (QC000000) (NOPID)

27-Sep-1996 5

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-96-ASAM-06 INFORMATIONAL, UH-60AMAIN ROTOR SPINDLE CRACK C/W AT 2446ACFT SIGNED ILLEGIBLE. (QC000000) (NO PID)

27-Sep-1996 6

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-97-ASAM-01 INSP OF MAIN ROTOR HUBASSY'S C/W AT 2446 ACFT HRS. (QC000000)(NO PID)

17-Sep-1997 1

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-97-ASAM-02 ONE TIME INSP OF T/RDRIVE FLEXIBLE COUPLING CONNECTIONSC/W AT 2446 ACFT HRS. (QC000000) (NO PID)

17-Sep-1997 2

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-97-ASAM-03 REPLACEMENT OFUNDAMPED GG ROTOR/STATOR ASSY'S C/WAT 2446 ACFT HRS. (QC000000) (NO PID)

17-Sep-1997 3

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-97-SOF- 01 REMOVAL OF CERTAINREWORKED M/R SWASHPLATE ASSY'S C/WAT 2446 ACFT HRS. (QC000000) (NO PID)

17-Sep-1997 4

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-97-ASAM-04 CHANGE IN RETIREMENTLIFE OF M/R BLADE CUFF. P/N 70150-09109-041 & -043 C/W AT 2446 ACFT HRS. (QC000000)(NO PID)

17-Sep-1997 5

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-97-ASAM-05 ONE TIME INSP OFCERTAIN VISCOUS DAMPER BEARINGSUPPORT ASSY'S C/W AT 2446 ACFT HRS.(QC000000) (NO PID)

17-Sep-1997 6

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-97-ASAM-06 INSP OF LATERALBELLCRANK ASSY'S MFG. BY PURDYMACHINE COMPANY (CAGE CODE 15152) C/WAT 2446 ACFT HRS. (QC000000) (NO PID)

17-Sep-1997 7

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-97-ASAM-07 REPLACEMENT OFSPECIFIC S/N T/R SERVO CYLINDERS C/W AT2446 ACFT HRS. (QC000000) (NO PID)

17-Sep-1997 8

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-97-ASAM-08 INSP OF CONNECTINGLINK ASSY P/N 70400-08155-056 MFG. BYPURDY MACHINE COMPANY C/W AT 2446ACFT HRS. (QC000000) (NO PID)

17-Sep-1997 9

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-97-ASAM-09 INSP OF M/R SHAFT EXTMFG BY FENN MFG COMPANY C/W AT 2446ACFT HRS. (QC000000) (NO PID)

17-Sep-1997 10

FRESNO, CA. 93727

HI000000

1106TH AVCRADUH-60-97-ASAM-10 ESTABLISHMENT OFFATIGUE LIFE FOR MAIN SUPPORT BRIDGEMFG BY AIR INDUSTRIES C/W AT 2446 ACFTHRS. (QC000000) (NO PID)

17-Sep-1997 11

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-97-ASAM-11 INCREASE IN FATIGUELIFE FOR M/R BLADE CUFFS -041 & -043 C/WAT 2446 ACFT HRS. (QC000000) (NO PID)

17-Sep-1997 12

FRESNO, CA. 93727

HI000000



8.7.DATE

6.REMARKS

4. 5.



1106TH AVCRAD,UH-60-97-ASAM-12 INCREASE IN FATIGUELIFE FOR T/R INBOARD RETENTION PLATESC/W AT 2446 ACFT HRS. (QC000000) (NO PID)

17-Sep-1997 13

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-97-ASAM-13 INSP M/R SPINDLEELASTOMERIC BEARING FOR INNER SLEEVEC/W AT 2446 ACFT HRS. (QC000000) (NO PID)

17-Sep-1997 14

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-97-ASAM-14 INSP BELLCRANKSUPPORT P/N 70400-08158-101 MFD BYAMERICAN GENERAL C/W AT 2446 ACFT HRS.(QC000000) (NO PID)

17-Sep-1997 15

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-97-ASAM-15 INSP ROD END BEARINGP/N 70101-08002-101 MFD BY ISLANDENGINEERING C/W AT 2446 ACFT HRS.(QC000000) (NO PID)

17-Sep-1997 16

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-97-ASAM-16 INSP SWASHPLATELINKAGE, CLEVIS CONNECTOR P/N 70400-08151-050 C/W AT 2446 ACFT HRS. (QC000000)(NO PID)

17-Sep-1997 17

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-97-ASAM-17 INSP INTERNAL RESCUEHOIST BRACKET N/A THIS ACFT AT 2446 ACFTHRS. (QC000000) (NO PID)

17-Sep-1997 18

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-97-ASAM-18 IDENTIFICATION/REMOVALSPECIFIC SWASHPLATE ASSY'S C/W AT 2446HRS. (QC000000) (NO PID)

17-Sep-1997 19

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-97-ASAM-19 INSP ANVIS POWERSUPPLY N/A AT 2446 ACFT HRS. (QC000000)(NO PID)

17-Sep-1997 20

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-98-ASAM-01 INCREASE IN FATIGUELIFE FOR M/R SHAFT EXTENSIONS MFD BYPURDY CORP C/W AT 2446 ACFT HRS.(QC000000) (NO PID)

17-Oct-1997 1

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-60-98-ASAM-02 INSP PUSHROD P/N 70400-08155-050/051 MFD BY VERSATILE MACHINECO C/W AT 2446 ACFT HRS. (QC000000) (NOPID)

17-Oct-1997 2

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,UH-98-ASAM-03 INSP FOR SWASHPLATE LINKP/N 70400-08110-054 MFD BY 65780 C/W AT2446 ACFT HRS. (QC000000) (NO PID)

13-Jan-1998 1

FRESNO, CA. 93727

HI000000

1106TH AVCRAD,MWO 1-1520-237-55-07 REFURB/PMS2COMPLETED AT 2446.1 ACFT HRS. ACFTRIGGED, THE FOLLOWING ADJUSTMENTSWERE MADE: SHORTENED FWD 1 TURN,LENGTHENED AFT 1 TURN, SHORTENED LAT1 TURN. T/R BIAS COMPLETED: YLW-4.050-4.340=.290/ BLU-4.660-4.980=.320/ RED -4.050-4.380=.330/ BLK -4.640-4.980=.340 NEXT PMS2DUE @ 2946.1 ACFT HRS. (QC000000) (NO PID)

13-Jan-1998 2

FRESNO, CA. 93727

HI000000

AASF COARNG,AIRCRAFT TRANSFERED TO COARNG @2468.0 ACFT HRS. (QC000000) (NO PID)

06-Mar-1998 1

AURORA, CO 80011

HI000000

AASF COARNG,AWR 543 - AUTHORIZATION FORINSTALLATION OF THE EBC-302HM ELT C/W.(QC000000) (NO PID)

12-Mar-1998 1

AURORA, CO 80011

HI000000



8.7.DATE

6.REMARKS

4. 5.



AASF COARNG,UH-60-98-ASAM-04 INSP OF HUCK BOLTS ONCCAD O/H PRIMARY SERVOS, YAW BOOSTSERVOS, COLLECTIVE BOOST SERVOS, ANDT/R SERVOS (ONE TIME) C/W. (QC000000) (NOPID)

18-Mar-1998 1

AURORA, CO 80011

HI000000

AASF, COARNG,UH-60-98-ASAM-05 ONE TIME INSP OFSWASHPLATE LINK P/N 70400-08110-054/-061FOR SUSPECT CAGE CODES DUE N/L/T 10ACFT. HRS. OR 14 DAYS (QC000000) (JN1399)

12-May-1998 1

AURORA, CO 80011

HI000000

COARNG AASF,EMC TEST REQUIRED FOR INSTALLATION OFBENDIX KING RADIO IAW AWR 784 DATED 30JUL 98. COMPLIED WITH 4 AUG 98, TESTEDOK. (QC000000) (CD9117)

04-Aug-1998 1

BUCKLY ANG BASE

HI000000

AASF COARNG,UH-60-98-ASAM-07 ONE TIME INSP OF LEFTTIE ROD FOR CAGE CODE 3R021 C/W.(QC000000) (TS6746)

16-Sep-1998 1

AURORA, CO 80011

HI000000

COARNG, COAASFUH-60-99-ASAM-01 RESTORATION OF FULLSERVICE LIFE ON SWASHPLATE LINK MFG BYTEK C/W. (QC000000) (TS6746)

12-Nov-1998 1

AURORA, CO 80011

HI000000

COARNG, COAASFUH-60-99-ASAM-02 INSP OF ALL EXTERNALRESCUE HOISTS MFG BY BREEZE EASTERNC/W. (QC000000) (TS6746)

12-Nov-1998 2

AURORA, CO 80011

HI000000

COARNG, COAASFUH-60-99-ASAM-03 ONE TIME INSP OF ALLT700-GE-700 ENGINE RECORDS C/W.(QC000000) (TS6746)

23-Nov-1998 1

AURORA, CO 80011

HI000000

COARNG, COAASFUH-60-99-ASAM-05 ONE TIME INSP OF MRSPINDLE BEARING ASSY FOR THEEXISTANCE OF SLEEVE BEARINGS C/W.(QC000000) (TS6746)

24-Dec-1998 1

AURORA, CO 80011

HI000000

COARNG, COAASFUH-60-99-ASAM-06 INSPECTION AND REVISEDRETIREMENT LIFE OF MAIN ROTOR PITCHHORNS, P/N 70102-08111-047 C/W. (QC000000)(TS6746)

05-Jan-1999 1

AURORA, CO 80011

HI000000

COARNG, COAASFUH-60-99-ASAM-07 NDI INSP OF MAIN ROTORHUB ASSY P/N 70103-08112-041. (QC000000)(TS6746)

23-Mar-1999 1

AURORA, CO 80011

HI000000

DYNCORP OLR,AUXILIARY CABIN HEATER INSTALLED THISACFT I/A/W TM 1-1520-237-23. (QC000000)(LM2968)

12-Apr-1999 1

KILLEEN TX

HI000000

DYNCORP OLR,ACE/CPCE PERFORMED AT 2576 ACFT HRSAT KILLEEN AIRPORT FACILITY BY TEAMMEMBER W. (QC00000) (LM2968)

20-Apr-1999 1

KILLEEN TX

HI000000

COARNG, COAASFUH-60-99-ASAM-08 REVISED RETIREMENTLIFE OF BELLCRANK SUPPORT ASSY.(QC000000) (TS6746)

29-Jun-1999 1

AURORA, CO 80011

HI000000

COARNG, COAASFUH-60-99-ASAM-09 ONE-TIME INSP OF THEM/R BLADE EXPANDABLE PIN. (QC000000)(TS6746)

03-Aug-1999 1

AURORA, CO 80011

HI000000

COARNG, COAASFUH-60-99-ASAM-10 INSP AND PM ON THE #2CROSSFEED BREAKAWAY VALVE. (QC000000)(TS6746)

03-Aug-1999 2

AURORA, CO 80011

HI000000

COARNG, COAASFUH-60-00-ASAM-02 CYCLIC STICK WIRINGBUNDLE RELOCATION. (QC000000) (TS6746)

15-Dec-1999 1

AURORA, CO 80011

HI000000



8.7.DATE

6.REMARKS

4. 5.



COARNG, COAASFUH-60-00-ASAM-03 INSP AND REMOVAL OFSUSPECT PRIMARY SERVO ASSEMBLIES.(QC000000) (TS6746)

04-Jan-2000 1

AURORA, CO 80011

HI000000

COARNG, COAASFUH-60-00-ASAM-04 INSP TAIL LANDING GEARSHOCK ASSY FOR MISSING BEARINGRETENTION PIN. (QC000000) (TS6746)

02-Mar-2000 1

AURORA, CO 80011

HI000000

AASF COARNG,BUCKLEY ANG BASE

UH-60-00-ASAM-05 INSP FIRE EXTINGUISHERWIRING FOR PROPER ROUTING ANDLABELING (QC000000) (MS8258)

23-May-2000 1

AURORA CO

HI000000

AASF-COARNG,BUCKLEY ANG BASE,

SOF UH-60-00-01 INITIAL AND RECURRINGINSPECTION OF MAIN ROTOR SPINDLE LUGS.(QC000000) (CK4971)

13-Jul-2000 1

AURORA, CO

HI000000

AASF, COARNG,REVISION TO UH-60-00-ASAM-05, ADDING TAILNUMBERS 91-26318 TO 91-26367. (QC000000)(KR7732)

18-Jul-2000 1

BUCKLEY ANG BASE

HI000000

PROJECT OLR, FORTHOOD TX AASFCOARNG

ACE/CPCE PERFORMED AT 2664 ACFT HRSAT BUCKLEY ANG CO BY ACE TEAM MEMBEREVEL GEARS. (QC000000) (JC9399)

25-Jul-2000 1

BUCKLEY ANG BASE

HI000000

AASF, COARNG,UH-60-00-SOF-02, REMOVAL OF INPUTMODULES WITH POTENTIALLY CRACKEDBEVEL GEARS. (QC000000) (KR7732)

09-Aug-2000 1

BUCKLEY ANG BASE

HI000000

AASF-COARNG,SOF UH-60-01-01, TB 1-1520-237-20-225INSPECT MAIN LANDING GEAR DRAG BEAM(QC000000) (CK4671)

07-Nov-2000 1

AURORA, CO 80011

HI000000

AASF COARNG,UH-60-01-02. EXTENSION OF UH-60-01-01 TO28 FEB 01. (QC000000) (MS8258)

02-Jan-2001 1

BUCKLEY AFB

HI000000

AASF COARNG,INSP. LATERAL SERVO BELLCRANK ASSYI/A/W UH-60-01-03 (TB 1-1520-237-20-229).(QC000000) (MS8258)

05-Jan-2001 1

BUCKLEY AFB

HI000000

AASF COARNG,UH-60-01-04 (TB 1-1520-237-20-228) INSPECTFOR INST OF FUEL MONITORING SYSTEM.(QC000000) (KR7732)

16-Jan-2001 1

BUCKLEY AFB AURORACO

HI000000

AASF COARNG,UH-60-01-05- (TB 1-1520-237-20-230) REVISIONTO UH-60-00-01 INSPECTION OF MAIN ROTORSPINDLE (QC000000) (KR7732)

06-Mar-2001 1

BUCKLEY AFB

HI000000

AASF COARNG,UH-60-01-07 (TB 1-1520-237-20-232) MAINROTOR FLT CONTROL SELF LOCKING BOLTS.(QC000000) (BM2318)

06-Jun-2001 1

BUCKLEY AFB

HI000000

AASF COARNG,UH-60-01-08 (TB 1-1520-237-20-232) MAINROTOR FLT CONTROL SELF LOCKING BOLTS(QC000000) (BM2318)

06-Jun-2001 2

BUCKLEY AFB

HI000000

AASF COARNG,UH-60-01-10 ONE TIME INSPECTION OF M/RBLADE EXPANDABLE PINS (QC000000)(KR7732)

18-Jul-2001 1


HI000000

AASF COARNG,60-01-11 INSPECTION OF M/R HUB ASSEMBLY.(QC000000) (KR7732)

24-Aug-2001 1

BUCKLY AFB AURORACOLO

HI000000



8.7.DATE

6.REMARKS

4. 5.



AASF COARNG,UH-60-01-12 INSPECTION OF M/R BLADEEXPANDABLE PIN. (QC000000) (KR7732)

24-Aug-2001 2

BUCKLEY AFB AURORACOLO

HI000000

PROJECT OLR FT.HOOD, TX 76543,

ACE/CPCE PERFORMED AT 2825 ACFT. HRS.AT BUCKLEY AFB, CO. BY ACE TEAMMEMBER Y. (QC000000) (JC9399)

13-Oct-2001 1

BUCKLEY AFB AURORACOLO

HI000000

AASF COARNG,UH-60-02-ASAM-02 (TB 1-1520-237-20-239)INSP. T/R BLADE FAIRING ASSY. (QC000000)(MS8258)

15-Nov-2001 1

BUCKLEY AFB CO.

HI000000

AASF COARNGUH-60-SOF-02-01 (TB 1-1520-237-20-240) INSP.OIL COOLER FAN SHAFT ASSY. FWD. MOUNTFLANGE. (QC000000) (LK5034)

19-Nov-2001 1

BUCKLEY AFB

HI000000

AASF COARNG,UH-60-02-ASAM-02 MAIN ROTOR HUBSUBASSEMBLY REWORK CONTROL SYSTEMPITCH TRIM ASSEMBLY. (QC000000) (KR7732)

11-Dec-2001 1

BUCKLEY AFB

HI000000

AASF COARNG,UH-60-02-03 ONE TIME INSPECTION OF THEFLIGHT CONTROL SYSTEM PITCH TRIMASSEMBLY. (QC0000000 (KR7732)

12-Dec-2001 1

BUCKLEY AFB

HI000000

AASF COARNG,SOF UH-60-02-04 (TB 1-1520-237-20-242) INSP.APU FUEL LINE GROMMET.(QC000000)(MS8258)

29-Jan-2002 1

BUCKLEY AFB AURORACO.

HI000000

AASF COARNG,SOF UH-60-02-05 (TB 1-1520-237-243) INSP. M/REXPANDABLE PINS & CHG INSP TO 30 HR.(QC000000) (MS8258)

05-Feb-2002 1

AURORA CO

HI000000

AASF COARNG,UH-60-02-ASAM-02 (TM 1-1520-237-20-246)INSP CONTROL ROD JAM NUTS. (QC000000)(MS8258)

08-Feb-2002 1

BUCKLEY AFB AURORACO.

HI000000

AASF COARNG,UH-60-02-ASAM-03 (TB 1-1520-237-20-245)INSP. OF ENGINE PCL QUADRANT DUEBEFORE COMPLETION OF NEXT PMS-2 OR 15FEB 2005. (QC000000) (MS8258)

14-Feb-2002 1


HI000000

COARNG AASFUH-60-02-ASAM-04 (TB 1-1520-237-20-244) INSPALL RESTARAINT SYSTEMS. (QC000000)(BM2318)

26-Mar-2002 1


HI000000

AASF COARNGUH-60-02-ASAM-05 (TB 1-1520-237-20-251)INSPECT M/R SPINDLE ASSEMBLIES.(QC000000) (LK5034)

04-Apr-2002 1

BUCKLEY AFB

HI000000

AASF COARNG,UH-60-02-ASAM-06 (TB 1-1520-237-20-252)INSP. SWAGE PINS/COLLARS ON BOOSTSERVO ASSEMBLIES (QC000000) (LK5034)

19-Apr-2002 1

BUCKLEY AFB

HI000000

COARNG AASF,SOF UH-60-02-07 MAIN MODULE PLANETARYCARRIER ASSY. (QC000000) (BM2318)

03-May-2002 1


HI000000

CO AASF,SOF UH-60-02-08 (TB 1-1520-237-20-255)SUPERCEDE SOF UH-60-02-07 RECORDS CHKOF MAIN MODULES TO DETERMINE TSN.(QC000000) (MS8258)

07-May-2002 1

BUCKLEY AF BASE

HI000000

AASF, COARNGUH-60-02-09 MAIN MODULE PLANETARYCARRIER ASSEMBLY SUPERCEDES UH-60-02-08 (QC000000) (KR7732)

22-May-2002 1

(NO LOCATION)

HI000000



8.7.DATE

6.REMARKS

4. 5.



CO AASF,SOF UH-60-02-10 MAIN MODULE PLANETARYCARRIER ASSEMBLY. (QC000000) (LK5034)

11-Jun-2002 1

BUCKLEY AFB,AURORA, CO

HI000000

AASF COARNG,UH-60-02-ASAM-08 INSPECT AN/ARC-220WIRING FOR CHAFING (QC0000000 (KR7732)

14-Jun-2002 1


HI000000

AASF COARNG,UH-60-02-ASAM-09, TAIL ROTOR QUADRANTHARDWARE INSTALLATION. (QC000000)(KR7732)

15-Jun-2002 1


HI000000

PROJECT OLR,ACE/CPCE PERFORMED AT 2928 ACFT. HRS.AT BUCKLEY AFB, CO. ACE TEAM MEMBER Y.(QC000000) (JC9399)

14-Aug-2002 1

FT HOOD TX 76542

HI000000

AASF COARNGUH-60-02-11 SOF ONE TIME INSP OF EACHUPPER & LOWER M/R BLADE CUFF.(QC000000) (BM2318)

20-Sep-2002 1

BAFB AURORA CO

HI000000

AASF COARNG,UH-60-02-12 SOF REVISION TO UH-60-02-11SOF. (QC000000) (BM2318)

24-Sep-2002 1

BAFB AURORA CO

HI000000

COAASF,UH-60-02-ASAM-11 INSPECT AN/ARC-220WIRING FOR CHAFING REVISION TO 02-ASAM-08. (QC000000) (MC6457)

01-Oct-2002 1

BKF AURORA CO

HI000000

AASF COARNG,UH-60-03-ASAM-02 TAIL ROTOR SERVORETIREMENT LIFE. (QC000000) (MC6457)

10-Dec-2002 1

BUCKLEY AFB

HI000000

AASF COARNG,UH-660-03-ASAM-01 INSP. OF BELLCRANKSUPPORT ASSY. RETIREMENT LIFE.(QC000000) (LK5034)

11-Dec-2002 1

BUCKLEY AFB

HI000000

CO-AASF ARNG,GEN-03-ASAM-01 ARC 201 BATTERY BOX.(QC000000) (BM2318)

30-Dec-2002 1


HI000000

AASF COARNG,UH-60-03-02 SOF INSPECT M/R BLADE CUFFFOR CRACKS (QC000000) (LK5034)

08-Jan-2003 1

BUCKLEY AFB

HI000000

D CO 1-108TH AVNREGT,

07 FEB 03 R-3 ISAQ FOR THE COCKPITAIRBAG SYSTEM (CABS) INSTALLED ON THEUH-60A/L HELICOPTER (ISAQ 101) LATEENTRY (QC000000) (NO PID)

07-Feb-2003 1

LSA ANACONDA,BALAD, IRAQ

HI000000

DYNCORP OLR,UH-60-02-ASAM-11 (TB 1-1520-237-20-261)MODIFICATION OF POWER AMPLIFIER /COUPLER CONNECTOR C/W AT 2928.2 ACFTHRS. (QC000000) (GD6707)

04-Mar-2003 1

BUCKLEY

HI000000



8.7.DATE

6.REMARKS

4. 5.



1-108TH AVN, CO. D,AEC # LE-KU001-0004(WINDSHEEIELDS/WINDSCREENS) INEXTREAMELY ROCKY ENVIRONMENT OFSOUTHWEST ASIA, WITH CURRENT OP-TEMPO AIRCRAFT MOVEMENTS AND PARTSAVALIABILITY... TM PROVIDES THE MOSTSERVICABLE COMPONENT TO BE USED,FROM A VISIBILITY STANDPOINT THEOPERATORS MUST DETERMINE WHEN THEDAMAGE TO THE WINDSCREEN EXCESSIVELYIMPACTS SERVICABILITY. FROM ASTRUCTURAL STANDPOINT, ANY AMOUNT OFDAMAGE TO THE OUTER LAYER OF THEWINDSCREEN IS ACCEPTABLE. ANY DAMAGETO THE INNER LAYER MUST BE ADDRESSEDAT THE EARLIEST OPPORTUNITY, BYREPLACING THE WINDSCREEN. AUTHORIZEDBY: LAURANCE HOFFMAN, AEROSPCEENGINEER, KUWAIT, LAURANCE. G.HOFFMAN@US. ARMY .MIL (JR759141)

22-Mar-2003 1

BALAD, IRAQ

HI000000

AMCOM PROJECT OLR,ACE/CPCE PERFORMED AT 2928 ACFT HRSBY TEAM MEMBERS W/TT AMCOM PROJECTOLR KILLEEN, TX WAYNE A DORIS (QC000000)(WD0176)

09-Jul-2003 1

BUCKLEY AFB/KILLEENTX 76543

HI000000

COAASF,EMC TEST AND DAILY INSPECTIONSECCESFULLY COMPLETED IAW AWR DATED10 OCT 00 FOR SPECIFIED UH-60A/LHELICOPTERS EQUIPED WITH BAMBIBUCKET. (QC000000) (MC6457)

10-Jul-2003 1

BUCKLEY AFB

HI000000


12 AUG 03 R-1 AWR FOR UH-60A/LOPERATIONS DURING DESERT COMBATOPERATIONS (AWR 1119) LATE ENTRY(QC000000)

12-Aug-2003 1


HI000000


15 AUG 03 R-4 AWR FOR UH-60A/LHELICOPTERS EQUIPPED WITH AUXILIARYPOWER UNIT (APU) INLET BARRIER FILTERS(AWR 911) LATE ENTRY (QC000000)

15-Aug-2003 1


HI000000


30 SEP 03 INTERIM STATEMENT OFAIRWORTHINESS QUALIFICATION (ISAQ) FORALL UH-60A/L HELICOPTERS EQUIPPED WITHBALLASTIC PROTECTION SYSTEM (BPS)(ISAQ 108) LATE ENTRY (QC000000)

30-Sep-2003 1


HI000000

COAASF, BAFBUH-60-04-01 FORWARD BELLCRANKSUPPORT INSTALLATION HARDWAREVERIFICATION COMPLIED WITH 20031001 AT2928.3 ACFT HRS. (QC000000) (MC6457)

01-Oct-2003 1

AURORA CO 80011

HI000000

SSSI/DOL,UH 60-04-ASAM-01, COMPLIED WITH AT 2928.2ACFT HRS REPLACE CIRCUIT BREAKER, P.YATES, TI (QC000000) (PY9561)

01-Mar-2004 1

FT. CARSON, CO 80913-4003

HI000000

SSSI/DOL,UH-60-02-ASAM-03/ TB 1-1520-237-20-245,COMPLIED WITH AT 2928.2 ACFT HRS DURINGPMS2 INSPECTION, P. YATES, TI. (QC000000)(PY9561)

22-Mar-2004 1


HI000000



8.7.DATE

6.REMARKS

4. 5.



SSSI/DOL,UH-60-04-ASAM-02, ALL H-60 AIRCRAFT TAILROTOR DRIVESHAFT NUT. C/W, P. YATES, TI(QC000000) (PY9561)

01-Apr-2004 1


HI000000


14 JUN 04 AWR FOR INSTALLATION ANDTESTING PROCEDURES OF THE EBC-302HMEMERGENCY LOCATOR TRANSMITTER (ELT)ON UH-60-A/L/Q AND HH-60L AIRCRAFT (AWR1189) LATE ENTRY (QC000000)

14-Jun-2004 1


HI000000

SSSI/DOL,UH-60-02-ASAM-09, INSPECT TAIL ROTORQUADRANT INSTALLATION HARDWARE I/A/W(TB 1-1520-237-23-257 NLT 2938.2 ACFT HRS,BUT NLT 26 JUNE 02, COMPLIED WITH AT2928.2 ACFT HRS, P. YATES, TI. (QC000000)(PY9561)

12-Aug-2004 1


HI000000

SSSI/DOL,UH-60-04-02/ OH-58-04-01. UH-60A/L AND OH-58D SERIES HELICOPTERS, DISABLING OFCOCKPIT AIRBAG SYSTEM (CABS) N/A THISAIRCRAFT, MWO NOT APPLIED. P. YATES, TI.(QC000000) (PY9561)

17-Aug-2004 1


HI000000

SSSI/DOL,UH-60-03-02, ALL H-60 SERIES AIRCRAFT,INSPECTION OF MAIN ROTR BLADE CUFFASSEMBLY, COMPLIED WITH AT 2928.2AIRCRAFT HRS, P. YATES, TI. (QC000000)(PY9561)

17-Aug-2004 2


HI000000

SSSI/DOL,UH-60-03, MAIN MODULE PLANETARYCARRIER ASSY, ALL UH-60A AND UH-60QSERIES AIRCRAFT, COMPLIED WITH AT 2928.2ACFT HRS, XMSN FROM CCAD HAD 2297 HRSON COMPONENT. P. YATES, TI. (QC000000)(PY9561)

17-Aug-2004 3


HI000000

SSSI/DOL,UH-60-02-ASAM-03, H-60 SERIES AIRCRAFT,INSPECTION OF ENGINE CONTROLQUADRANT POWER CONTROL LEVER (PCL)WIRING, COMPLIED WITH AT 2928.2 AIRCRAFTHRS. P. YATES, TI. (QC000000) (PY9561)

17-Aug-2004 4


HI000000

SSSI/DOLUH-60-02-ASAM-09, ALL H-60 SERIESAIRCRAFT, TAILROTOR QUADRANTHARDWARE INSTALLATION, COMPLIED WITHAT 2928.2 AIRCRAFT HRS. P. YATES, TI.(QC000000) (PY9561)

17-Aug-2004 5


HI000000

SSSI/DOLUH-60-MIM-04-013, RETIREMENT LIFEEXTENSION FOR CERTAIN MAIN ROTORSPINDLE ASSEMBLIES, CW. P. YATES, TI.(PY9561) (QC000000)

02-Sep-2004 1


HI000000

SSSI/DOLPHASE MAINTENANCE COMPLETED AT 2928.2ACFT HRS, COMPLETED CABIN TUB INSP,1000 HRS FLIGHT CONTROL INSPECTION, M/RAND T/R RIG COMPLETED, NEXT PHASE DUEAT 3428.2 ACFT HRS. P. YATES, TI. (PY9561)(QC000000)

03-Sep-2004 1


HI000000

CO AASFSOF UH-60-04-04 (M/R HUB) COMPLIED WITH.(GP7247) (QC000000)

07-Nov-2004 1

BUCKLEY AFB

HI000000

CO AASFSOF UH-60-04-03 (CRASH WORTHY)COMPLIED WITH. (GP7247) (QC000000)

07-Nov-2004 2

BUCKLEY AFB

HI000000



8.7.DATE

6.REMARKS

4. 5.



CO AASFUH-60-04-ASAM-03 (FUEL SYSTEM INTEGRITYCHECK) COMPLIED WITH. (GP7247)(QC000000)

07-Nov-2004 3

BUCKLEY AFB

HI000000

CO AASFUH-60-04-ASAM-04 COMPLIED WITH. (GP7247)(QC000000)

07-Nov-2004 4

BUCKLEY AFB

HI000000

CO AASFUH-60-04-ASAM-05 (RESTRAINT SYSTEM INSP)COMPLIED WITH. (GP7247) (QC000000)

07-Nov-2004 5

BUCKLEY, AFB CO80011

HI000000

D CO 108TH AVN REGT,LSA ANACONDA

INTERIM STATEMENT OF AIRWORTHINESSQUALIFICATION (ISAQ) FOR INSTALLATIONAND OPERATION OF AIR WARRIOR (AW)BLOCK 1 ON UH-60A/L HELICOPTERS(ISAQ114) LATE ENTRY (NO PID) (QC000000)

28-Jan-2005 1

BALAD, IRAQ

HI000000

D CO 1-108TH AVNREGT, LSA ANACONDA

08 FEB 05 R-5 AWR FOR INSTALLATION ANDOPERATION OF ENGINE INLET BARRIERFILTER (IBF) ON UH-60A/L/Q AND HH-60LHELICOPTERS (AWR 1165) LATE ENTRY (NOPID) (QC000000)

08-Feb-2005 1

BALAD, IRAQ

HI000000


10 MAR 05 AWR FOR INSTALLATION OFCOMMON MISSILE WARNING SYSTEM (CMWS)AND IMPROVED COUNTERMEASURESDISPENSER (ICMD) ON UH-60A/LHELICOPTERS (AWR1252) LATE ENTRY (NOPID) (QC000000)

10-Mar-2005 1

BALAD, IRAQ

HI000000

CO AASFUH-60-05-SOF-01 COMPLIED WITH, SYSTEMNOT INSTALLED ON THIS ACFT. (GP7247)(QC000000)

15-Mar-2005 1

BUCKLEY, AFB CO80011

HI000000


24 MAR 05-R2 AWR FOR INSTALLATION ANDUSE OF THE M-240H MACHINE GUN UH-60A/LHELICOPTERS (AWR1120) LATE ENTRY (NOPID) (QC000000)

24-Mar-2005 1

BALAD, IRAQ

HI000000


AWR FOR INFRARED (IR) ANTI-COLLISIONLIGHT LENS INSTALLED ON US ARMY UH-60A/L/Q AND HH-60L HELICOPTERS (AWR1223) LATE ENTRY (NO PID) (QC000000)

29-Mar-2005 1

BALAD, IRAQ

HI000000

CO AASFUH-60-05-ASAM-04 C/W 20050408 @ 3136 ACFTHRS. (GW4483) (QC000000)

08-Apr-2005 1

BUCKLEY AFB

HI000000

CO ARNG AASFUH-60-05-ASAM-03 AIRCREW RESTRAINTSYSTEM COMPATIBILITY INSP COMPLIEDWITH (BM2318) (QC000000)

19-Apr-2005 1

BUCKLEY AFB CO80011

HI000000

CO AASFUH-60-05-ASAM-05 TIE ROD ASSY. S/NVERIFICATION COMPLIED WITH. (GP7247)(QC000000)

22-Apr-2005 1

BUCKLEY AFB CO

HI000000

CO AASFUH-60-05-ASAM-06 (TROOP SEAT RESTRAINTBUCKLE) (DE3062) (QC000000)

28-Apr-2005 1

BUCKLEY AFB CO

HI000000


26 MAY 05 AWR FOR INSTALLATION ANDOPERATION OF ENGINE INLET BARRIERFILTER (IBF) ON UH-60A/L/Q AND HH-60LHELICOPTERS (AWR 1270) LATE ENTRY (NOPID) (QC000000)

26-May-2005 1

BALAD, IRAQ

HI000000



8.7.DATE

6.REMARKS

4. 5.



CO AASFUH-60-05-ASAM-08 COMPLIED WITH ON20050601. (GP7247) (QC000000)

01-Jun-2005 1

BUCKLEY AFB CO80011

HI000000

CO AASFUH-60-05-ASAM-07 (BLEED OF HYD SYSTEM).(QK2440) (QC000000)

10-Jun-2005 1

BUCKLEY AFB,AURORA CO 80011

HI000000

CO AASFAIRCRAFT PLACED ON ESM 20050624 AT3215.5 ACFT HRS, PMI DUE 3278.2. (DE3062)(QC000000)

24-Jun-2005 1


HI000000

CO AASFUH-60-05-SOF-02 ENHANCED SCHEDULEDMAINTENANCE (ESM) PROGRAMIMPLEMENTATION. (DE3062) (QC000000)

24-Jun-2005 2


HI000000

CO AASFTB 1-1520-237-20-266 H-60 SERIES ACFTPREVENTIVE MAINTENANCE DAILY (PMD) 40HR PREVENTIVE MAINTENANCE SERVICES(PMS), AND 700 HR SPLIT MAINTENANCEINSPECTION (PMI) IMPLEMENTATION.(DE3062) (QC000000)

24-Jun-2005 3


HI000000


29 JUN 05 R-4 AWR FOR UH-60A/L/Q AND HH-60L HELICOPTERS EQUIPPED WITHAEROSPACE FILTRATION SYSTEMS (AFS)AUXILIARY POWER UNIT (APU) INLETBARRIER FILTERS (AWR 1097) LATE ENTRY(NO PID) (QC000000)

29-Jun-2005 1

BALAD, IRAQ

HI000000


06 JUL 05 AWR FOR UH-60A/L/Q AND HH-60LOPERATIONS WITH PILOT AND COPILOTDOORS REMOVED (AWR1279) LATE ENTRY(NO PID) (QC000000)

06-Jul-2005 1

BALAD, IRAQ

HI000000


29 JUL 05 R-2 INTERIM STATEMENT OFAIRWORTHINESS QUALIFICATION (ISAQ) FORUH-60-A/L/Q, HH-60-L AND AIRBORNECOMMAND AND CONTROL SYSTEM (A2C2S)HELICOPTERS EQUIPPED WITH THE MELTMANUFACTURING (HELI-GUARD) BALLISITCPROTECTION SYSTEM (BPS) (ISAQ 111) LATEENTRY (NO PID) (QC000000)

29-Jul-2005 1

BALAD, IRAQ

HI000000


29 JUL 05 R-2 ISAQ FOR ALL UH-60A/LHELICOPTERS EQUIPPED WITHT THEPROTECTIVE MATERIALS COMPANYBALLISTIC PROTECTION SYSTEM (BPS) (ISAQ)LATE ENTRY (NO PID) (QC000000)

29-Jul-2005 2

BALAD, IRAQ

HI000000

PROJECT/OLR (EAST)UH-60-05-ASAM-09 INSPECT FOR SUSPECTCRASHWORTHY EXTERNAL FUEL SYSTEM(CEFS) INSTALLATION BOLTS. COMPLIEDWITH AT 3266.8 ACFT HRS. MWO 1-1520-237-50-86 NOT APPLIED. (PG4153) (QC000000)

09-Aug-2005 1

HAAF, GA 31409

HI000000

PROJECT/OLR (EAST)UH-60-05-ASAM-10 INSPECT FOR SUSPECTENGINE OUTPUT SHAFT SERIAL NUMBERS.COMPLIED WITH AT 3266.8 ACFT HRS. NOBAD SERIAL NUMBERS. (PG4153) (QC000000)

09-Aug-2005 2

HAAF, GA 31409

HI000000


22 SEP 05 R-4 AWR FOR UH-60A/L/Q AND HH-60L HELICOPTERS EQUIPPED WITH SEIINDUSTRIES BAMBI WATER BUCKETS (AWR1054) LATE ENTRY (NO PID) (QC000000)

22-Sep-2005 1

BALAD, IRAQ

HI000000



8.7.DATE

6.REMARKS

4. 5.



CO AASFUH-60-05-ASAM-01 C/W 20051011 @ 3277 ACFTHRS. (GW4483) (QC000000)

11-Oct-2005 1

BUCKLEY AFB

HI000000


ISAQ FOR UH-60A/L/Q AND HH-60LHELICOPTERS EQUIPPED WITH AEROSPACEFILTRATION SYSTEMS (AFS) AUXILIARYPOWER UNIT (APU) INLET BARRIER FILTERS(ISAQ) LATE ENTRY (NO PID) (QC000000)

21-Oct-2005 1

BALAD, IRAQ

HI000000


22 DEC 05 AWR FOR UH-60A/L HELICOPTERSEQUIPPED WITH THE ELECTRONIC DATAMANAGER (EDM) AND BLUE FORCE TRACKER(BFT) SYSTEM (QUAD BAY INSTALLATION)AWR 1300. LATE ENTRY (NO PID) (QC000000)

22-Dec-2005 1

BALAD, IRAQ

HI000000

A CO 2-135 AVNUH-60-06-SOF-01 C/W @ 3342.2 ACFT HRS.(GW4483) (QC000000)

23-Dec-2005 1

BALAD, IRAQ

HI000000


30 DEC 05 R-2 FOR OPERATION OF SPECIFIEDUH60L HELICOPTERS EQUIPPED WITH THEARMY AIRBORNE COMMAND AND CONTROLSYSTEM (A2C2S) LOW RATE INITIALPRODUCTION (LRIP) MODIFICATION PACKAGEWITH INTERNATIONAL MARITIME SATELLITE(INMARSAT) (AWR 1304) LATE ENTRY (NO PID)(QC000000)

30-Dec-2005 1

BALAD, IRAQ

HI000000


27 JAN 06 AWR FOR THE OPERATION OFCOMMON MISSILE WARNING SYSTEM (CMWS)AND IMPROVED COUNTERMEASURESDISPENSER (ICMD) ON UH-60A/LHELICOPTERS (AWR 1299) LATE ENTRY (NOPID) (QC000000)

27-Jan-2006 1

BALAD, IRAQ

HI000000


27 FEB 06 AWR FOR UH-60A/L SERIESHELICOPTERS EQUIPPED WITH THEMICROCLIMATE COOLING SYSTEM WITHDIGITAL CONTROLLER (AWR1323) LATEENTRY (NO PID) (QC000000)

27-Feb-2006 1

BALAD, IRAQ

HI000000

L-3 TASMT/R PITCH CHANGE TBP'D BIAS IS RED .355,BLACK .340, YELLOW .330, BLUE .355(JB967800)

07-Mar-2006 1

BALAD, IRAQ

HI000000


13 APR 06 R-5 AWR FOR UH-60A/LHELICOPTERS EQUIPPED WITH THEELECTRONIC DATA MANAGER (EDM) ANDBLUE FORCE TRACKER (BFT) SYSTEM (QUADBAY INSTALLATION) (AWR 1300) LATE ENTRY(NO PID) (QC000000)

13-Apr-2006 1

BALAD, IRAQ

HI000000

CO.A 2-135TH AVN, LSAANACONDA

MEC # - LE-BAL012-1634 UPPER LEFT SIDETAIL PYLON AREA CRCT DOUBLERMODIFICATION KIT REPAIR IAW- DMWR 1-1520-237 FIG. E-22, PG. E-226, AND E-227.AUTHORIZED BY LAURENCE G. HOFFMAN, GS-13 AEROSPACE ENGINEER. DSN: 312-992-3986 X.7812 ACFT HRS 3631.9 (JR759141)

11-May-2006 1

IRAQ

HI000000



8.7.DATE

6.REMARKS

4. 5.



CO.A 2-135TH AVN, LSAANACONDA

MEC # - LE-BAL012-1646, REV. 1 ACFT HRS.3631.9, 1 IN. LONG GOUGE 0.023 TO 0.037DEPTH ON FITTING P/N- 70070-20588-012(STABILATOR). REV.1 - AFTER REMOVAL OFPROTECTIVE PAINT, LUG MEASUREMENTRESULTS WERE 0.506 THICK, 0.030 DAMAGEDEEPEST POINT. FINAL LUG MATERIALTHICKNESS OF 0.476 EXCEEDED DAMAGELIMITATIONS IN TM 1520-237-23 AUTHORIZEDBY: LAURENCE G. HOFFMAN, GS-13AEROSPACE ENGINEER, DSN- 312-992-3986X.7812 (JR759141)

14-May-2006 1

IRAQ

HI000000

1107TH AVCRADMEC # LE-BAL016-164R1 AT 3631.9 ACFT HRSR/H PYLON STABILATOR HIDGE FITTINGREPLACED AS PER (RL745700)

18-May-2006 1

ARIFJAN, KUWAIT

HI000000

A CO 2-135 AVNUH-60-06-ASAM-01 TAIL SHOCK STRUT C/W 23MAY 06 @ 3631.9 ACFT HRS (GW448300)

23-May-2006 1

BALAD, IRAQ

HI000000

L-3 VERTEXAEROSPACE

PMI-2 COMPLETED C.W @ 3631.9 ACFT HRS.NEXT PMI-2 DUE AT 4331.9 ACFT HRS.(RC3243) (QC000000)

24-May-2006 1

APO AE 09391 (BALAD)

HI000000

L-3 VERTEXAEROSPACE

INSTALLED CRCT DOUBLER MOD KIT AS PERMEC # LE-BAL012-1634 @ 3691.9 ACFT HRS(RC324300)

24-May-2006 2

BALAD, IRAQ

HI000000

A CO 2-135 AVNUH-60-MIM-06-004 IMPLEMENTED. NEXTPHASE DUE AT 3991.9 ACFT HRS PMI-1(GW448300)

25-May-2006 1

BALAD, IRAQ

HI000000


06 JUN 06 R-1 AWR FOR THE OPERATION OFCOMMON MISSILE WARNING SYSTEM (CMWS)AND IMPROVED COUNTERMEASURESDISPENSER (ICMD) ON UH-60A/LHELICOPTERS. (AWR 1324) LATE ENTRY (NOPID) (QC000000)

06-Jun-2006 1

BALAD, IRAQ

HI000000

A CO 2-135 AVNUH-60-06-ASAM-03 SWASHPLATE DUPLEXBRNG C/W 13 JUN 06 @ 3657.7 ACFT HRS(GW448300)

13-Jun-2006 1

BALAD, IRAQ

HI000000

CO. D 1-108TH AVN,36TH CAB, LSAANACONDA

UH-60-MIM-06-005 (DELAYED ENTRY) TBOTIME CHANGE C/W. (JR759141)

14-Jun-2006 1

IRAQ

HI000000

A CO 2-135 AVNUH-60-06-ASAM-04 CRASH SENSOR, PLUGSC/W 23 JUN 06 @ 3678.4 ACFT HRS(GW448300)

23-Jun-2006 1

BALAD, IRAQ

HI000000

A CO 2-135 AVNUH-60-06-SOF-02 CABS C/W. N/A THIS ACFT(GW448300)

10-Jul-2006 1

BALAD, IRAQ

HI000000

A CO 2-135 AVNUH-60-06-ASAM-05 BFT HDWR C/W 03 AUG2006 @ 3753.4 ACFT HRS (GW448300)

03-Aug-2006 1

BALAD, IRAQ

HI000000

A CO 1-135 AVNMEC # F52960 APPLIED FOR CRACK @ STA308, BL 34.5, WL 261. DUE REPAIR AT NEXTPM1 OR RESET, WHICHEVER OCCURS FIRST(GW448300)

19-Aug-2006 1

BALAD, IRAQ

HI000000



8.7.DATE

6.REMARKS

4. 5.




31 AUG 06 R-1 AWR FOR UH-60A/L/Q AND HH-60L HELICOPTERS TO OPERATE WITH ENGINEINLET BARRIER FILTER (EIBF) INSTALLED INSUPPORT OF DESERT COMBAT OPERATIONS(AWR 1270) LATE ENTRY (NO PID) (QC000000)

31-Aug-2006 1

BALAD, IRAQ

HI000000


19 SEP 06 R-5 AWR FOR UH-60A/LHELICOPTERS EQUIPPED WITH AUXILIARYPOWER UNIT (APU) INLET BARRIER FILTERS(AWR 911) LATE ENTRY (NO PID) (QC000000)

19-Sep-2006 1

BALAD, IRAQ

HI000000


20 SEP 06 R-4 AWR FOR UH-60A/LHELICOPTERS WITH VERTICAL SUPPORTPYLON FAIRING MODIFICATIONS(AWR893)(NO PID) (QC000000)

20-Sep-2006 1

BALAD, IRAQ

HI000000

L-3 VERTEXUH-60-03-ASAM-02 C/W @ 3981.3 ACFT HRST/R SERVO RETIREMENT LIFE INCREASE(BS096100)

08-Oct-2006 1

BALAD, IRAQ

HI000000


AIRCRAFT TRANSFERRED TO OIF 06-08 FORTHEATER OPERATIONS. (DELAYED ENTRY)(JR759141)

10-Oct-2006 1

IRAQ

HI000000


AIRCRAFT TRANSFERRED TO 1-108TH AVN,36TH CAB (JR759141)

10-Oct-2006 2

IRAQ

HI000000

D CO 1/108TH AVNMEC# T28021 (12 FEB 04 DELAYED ENTRY)BEARINGS RECEIVED FROM SUPPLY PN:ADU36-1 HAVE A LOT OF GOLD SHOWING ONLINER. SUBJECT BEARING IS ACCEPTABLEFOR USE. SUBJECT PART DOES NOT HAVE AHISTORY OF BEING REJECTED AT THE FIELDBECAUSE OF QUESTIONABLE LOOK ANDTHEREFORE SHOULD BE NO PROBLEM.APPROVED BY BILL PEASTER([email protected]) (SM358850)

10-Oct-2006 3

BALAD, IRAQ

HI000000

L-3 VERTEXLE-BAL013-2250 RIGHT SIDE FUEL CELLREPAIRED I/A/W (MEC) UNTIL CELL IS ABLETO BE REPLACED DURING RESET TEMPREPAIRED AT 3981.3 ACFT HRS (MT025955)

20-Oct-2006 1

BALAD, IRAQ

HI000000

L-3 VERTEXLE-BAL013-2207 REPAIRED CRACK ON RIGHTSIDE DOUBLER FS308, WL262, BL 34.5R I/A/WSIKORSKY REPAIR PROCEDURES AJM-BL-34-1A AT 3981.3 ACFT HRS (MT025955)

20-Oct-2006 2

BALAD, IRAQ

HI000000

L3 HANGAR #5PMI #1 COMPLETED AT 3981.3 AIRCRAFTHOURS. PMI#2 DUE AT 4341.3 AIRCRAFTHOURS. (JR759141)

26-Oct-2006 1

BALAD, IRAQ

HI000000


UH-60-07-ASAM-01 COMPLIED WITH AT 4091.8ACFT HRS. (JR759141)

26-Dec-2006 1

IRAQ

HI000000


UH-60-07-ASAM-02 C/W @ 4131.9 ACFT HRS.(JR759141)

27-Dec-2006 1

IRAQ

HI000000



8.7.DATE

6.REMARKS

4. 5.





27-Dec-2006 2

IRAQ

HI000000



30-Dec-2006 1

IRAQ

HI000000


AIRWORTHINESS RELEASE (AWR) FOR THEOPERATION OF COMMON MISSILE WARNINGSYSTEM (CMWS) AND IMPROVEDCOUNTERMEASURES DISPENSER (ICMD) ONUH-60A/L HELICOPTERS (AWR1299).(RG021127)

04-Jan-2007 1

BALAD, IRAQ

HI000000

1-108TH AVN, CO. D,LSA ANACONDA

UH-60-07-ASAM-05 (ARC-220, KY-100 STARTUPPROCEDURES) COMPLIED WITH AT 4303.6AIRCRAFT HOURS. (JR759141)

23-Feb-2007 1

IRAQ

HI000000


UH-60-07-ASAM-06 (HOIST CABLE) COMPLIEDWITH AT 4303.6 AIRCRAFT HOURS. N/A THISACFT. (JR759141)

25-Feb-2007 1

IRAQ

HI000000

D CO 1-108TH AVNREGT, ANACONDA

THE SUBJECT REPAIR IS AUTHORIZED TOREPAIR DAMAGE TO BOTH RH/LH DOORPOST IAW TM 1-1500-204-23-10 & SIKORSKYREPAIR PROCEDURE CDP-240022-1. JUANQUINTANA. DB3 AEROSPACE ENGINEER, USARMY RDECOM, AMSRD-AMR-AE-M DSN: 312-992-3986 X7812 (RG021127)

01-Mar-2007 1

BALAD, IRAQ

HI000000


MEC # LE-BAL014-0938 (AFT PYLON)AUTHORIZATION GRANTED TO DELAYREPLACEMENT OF STRAP NO LATER THANNEXT MAJOR MAINTENANCE EVENT. BILLMCCANDLESS, DB3 AEROSPACE ENGINEER,US ARMY RDECOM, AMSRD-AMR-AE-M DSN:312-992-3986 X7830 (RG021127)

03-Mar-2007 1

BALAD, IRAQ

HI000000



8.7.DATE

6.REMARKS

4. 5.




MEC # MEC014-0932 (FUSELAGE STRUCTURE)REPAIR IS AUTHORIZED IAW 1-1500-204-23-10AND THE FOLLOWING: THE SUBJECT 0.5"CRACK IS TO THE UPPER FWD CORNER OFTHE TAIL LANDING GEAR STRUT ACCESS, ONTHE LH SIDE OF THE TAIL BOOM SKIN, PN70210-05001-046. 1. NDI THE SUBJECT CRACKTO LOCATE THE END OF THE CRACK. STOPDRILL THE CRACK, PROTECT STRUCTURESBEHIND THE CRACK WITH A .020" STEELPLATE. 2. FABRICATE DOUBLER TO EXTENDAT LEAST TWO RIVETS EITHER SIDE OF THECRACK AND FOLLOWING THE CONTOUR OFTHE ACCESS OPENING, ALSO PICK UP TWOADDITIONAL RIVETS UP ON THE FRAMEADJACENT THE CRACK, USE EXISTING RIVETHOOES ON FRAMES AND STRINGERS.DOUBLER TO BE MADE FROM .020" 301 CRESTO BE INSTALLED ON THE INSIDE BETWEENTHE FRAME AND SKIN. 3. INSTALL DOUBLERIAW TM 1-1500-204-23-10, INSTALL WET WITHEPOXY PRIMER, SEAL EDGES WITH AMS-S-8802. FILL CRACK AND STOP DRILL WITH AMS-S-8802. THIS IS A TEMPORARY REPAIR. RE-EVALUATE AT RESET. REFERENCE LE-BAL014-0539. BILL MCCANDLESS, DB3AEROSPACE ENGINEER, US ARMY RDECOM.AMSRD-AMR-AE-M DSN: 312-992-3986 X7830(RG021127)

03-Mar-2007 2

BALAD, IRAQ

HI000000

L-3 VERTEXMEC # LE-BAL015-0028- AUTHORIZATIONGRANTED TO REPAIR STABILATOR ASREQUESTED ABOVE IAW STANDARDPRACTICES. REPAIR WILL BE REVIEWD BYENGINEERING. POC BILL MCCANDLESS, DB3AEROSPACE ENGINEER, US ARMY RDECOM,AMSRD-AMR-AE-M DSN: 312-992-3986 X7830.(RG021127)

12-Mar-2007 1

BALAD, IRAQ

HI000000

D CO 1-108TH AVNREGT

AUTHORIZATION GRANTED TO REPAIRBLISTERED AREA WITH PU-459 IAW LE-BAL013-2250. EVALUATE REPAIR AT NEXTPMI. CONTACT TASM-LE FOR EXTENSION TORESET AT THAT TIME, REFERENCING THISMEC NUMBER. BILL MCCANDLESS, DB3AEROSPACE ENGINEER, US ARMY RDECOM.AMSRD-AMR-AE-M DSN: 312-992-3986 X7830MEC #LE-BAL015-0055 (RG021127)

13-Mar-2007 1

BALAD, IRAQ

HI000000

L-3 VERTEXMEC # LE-BAL015-0083 AUTHORIZATIONGRANTED TO REPLACE INPUT MOD BEARINGRETAINERS PER DMWR 1-1615-374. POC:WALT A. BUTSH, GS-13 AEROSPACEENGINEER, US ARMY AVN ENGR DIR. DSN:312-992-3886 X7812 (RG021127)

17-Mar-2007 1

BALAD, IRAQ

HI000000

D CO 1-108TH AVNREGT

PMI-2 COMPLETED AT 4301.0 ACFT HRS. NEXTDUE PMI-1 AT 4661.0 ACFT HRS (RG021127)

18-Mar-2007 1

BALAD, IRAQ

HI000000



8.7.DATE

6.REMARKS

4. 5.



1-108TH AVN, CO. D,UH-60-06-ASAM-02 (PITCH CHANGE LINKJAMNUTS) C/W @ 4301.0 AIRCRAFT HOURS,DURING PMI-2. COMPLETED BY L3 VERTEX,AEROSPACE (PID: UNK) (JR759141)

18-Mar-2007 2

BALAD, IRAQ

HI000000


UH-60-07-AMAM-01 (CMWS EOMS, ECUCHECK) COMPLIED WITH AT 4324.8 AIRCRAFTHOURS (JR759141)

07-Apr-2007 1

IRAQ

HI000000

L3 TASMM/R RIGGED FOR REPLACEMENT OFTRANSMISSION. 90DGR. 1) 8.3 2) 8.7 3) 8.3 4)8.4 AVG: 7 HIGH COLLECTIVE 15DGR. LEFTCYCLIC ANGLE 7.5DGR RIGHT CYCLIC7.0DGR. (JM884376)

17-Apr-2007 1

BALAD IRAQ

HI000000


UH-60-07-AMAM-07 (CEFS BONDING JUMPER)COMPLIED WITH AT 4373.5 AIRCRAFT HOURS,N/A THIS AIRCRAFT (JR759141)

18-May-2007 1

IRAQ

HI000000

L-3, LSA ANACONDAMEC # LE-BAL015-0758 REPAIR TO BATTLEDAMAGE TAIL CONE SKIN, STRINGER, FRAMEAT STATION 505, STA. 525.0, STA 545.0, STA.565 AND DRIVESHAFT SUPPORT AT STA. 531AND LOWER TRANSITION SECTION REPAIREDI/A/W DMWR 1-1520-237 WP003900 AND TM 1-150-237-23-6 WP038700 AT 4419.4 ACFT HRS.(MB0414592)

05-Jul-2007 1

BALAD IRAQ

HI000000

1-108TH AVN, CO. DMEC # LE-BAL016-0021 (INLET ENGINE, AIR)ACFT HOURS: 4419.4, CRACK FOUND ONINLET SECTION (P/N: 70302-10100-051) S/N:B334-00168 CRACK WAS FOUND ON TUBE.AUTHORIZATION FOR L3 AEROSPACE TOWELD TUBE IAW (TO 00-25-252) AND DMWR (1-1520-237: WP-0290) WAS APPROVED BYGARRY A. MERCALDI, DB3 ELECTRONICSENGINEER [email protected] MEC'S REF. LE-BAL012-1566.(JR759141)

18-Jul-2007 1

BALAD, IRAQ

HI000000

1-108TH AVN, CO. DUH-60-07-ASAM-08 (HMU/FUEL CONTROL O-RING) COMPLIED WITH AT 4419 AIRCRAFTHOURS. N/A THESE AIRCRAFT ENGINES.(JR759141)

19-Jul-2007 1

BALAD, IRAQ

HI000000

1-108TH AVN, CO. DUH-60-07-ASAM-09 (DEFECTIVE DIGITALENGINE CONTROL UNIT) COMPLIED WITH AT4419.4 AIRCRAFT HOURS. N/A THIS AIRCRAFT- ENGINES HAVE ECU'S (JR759141)

25-Jul-2007 1

BALAD, IRAQ

HI000000

1-108TH AVN, CO. DPOST BATTLE DAMAGE REPAIRS.M/R TRACKFPG: 0.18 80 KNOTS 0.23HVR: 0.12 120 KNOTS 0.18, 145KNOTS 0.23MTP: M. SHAW CW4 (JR759141)

26-Jul-2007 1

BALAD, IRAQ

HI000000

D CO 1 108THCOMPLIED WITH UH 60-07-ASAM-10 14 AUG 07(MG764295)

14-Aug-2007 1

BALAD IRAQ

HI000000

AASF 2H-60-08-AMAM-01, MM, DTD 15 OCT 07, MAINLANDING GEAR SHOCK STRUTS C/W 15 NOV07 @ 4501.1 ACFT. HRS. (JD508508)

15-Nov-2007 1

SALINA, KS

HI000000



8.7.DATE

6.REMARKS

4. 5.



AASF # 2H-60-08-ASAM-02, MM, DTD 05 NOV 07, POWERAVAILABLE CONTROL CABLE, C/W 28 NOV 07@ 4496.6 ACFT. HRS. (JD508508)

27-Nov-2007 1

SALINA, KS

HI000000

AASF # 2H-60-08-ASAM-01, MM, DTD 01 OCT 07 C/W 21JUN 08 @ 4570 ACFT. HRS. (JD508508)

08-Dec-2007 1

SALINA, KS

HI000000

AASF # 2H-60-08-ASAM-05 TAIL ROTOR QUADRANTSPRING CAPSULE ASSY REPLACED BOTH AT4501.9 ACFT HRS 28 DEC 07 (CS729537)

12-Dec-2007 1

SALINA, KS

HI000000

AASF # 2H-60-08-AMAM-02, MM, DTD 26 NOV 07, TAILROTOR OUTBOARD RETENTION PLATESHIMS, C/W 12 DEC 07 @ 4501.1 ACFT. HRS.(JD508508)

12-Dec-2007 2

SALINA, KS

HI000000

AMCOM FT HOODPROJECT OLR

ACE/CPCE PERFORMED AT 4501 AIRCRAFTHOURS BY TEAM MEMBERS K & Q.(WS244328)

18-Dec-2007 1

SALINA, KS

HI000000

AASF # 2H-60-08-ASAM-04, PILOT'S LOWER SEAT RAILCHAFING ELECTRICAL HARNESS. CW 19 DEC2007 AT 4501.1 ACFT. HRS. (JD508508)

19-Dec-2007 1

SALINA, KANSAS

HI000000

AASF # 2H-60-08-AMAM-04, MM, DTD 14 JAN 08,PILOT/COPILOT DOOR JETTISONABLEWINDOW C/W 18 JAN 08 @ 4504.5 ACFT. HRS.(JD508508)

03-Jan-2008 1

SALINA, KS

HI000000

AASF #2H-60-08-ASAM-03, MM, DTD 6 NOV 07,CHANGES TO CURRENT FUEL SYSTEMINTEGRITY CHECKS C/W 3 JAN 08 @ 4502.4ACFT. HRS. (JD508508)

03-Jan-2008 2

SALINA, KS

HI000000

AASF # 2H-60-08-AMAM-04, MM, DTD 14 JAN 08,PILOT/COPILOT DOOR JETTISONABLEWINDOW C/W 16 JAN 08 @ 4504.5 ACFT. HRS.

16-Jan-2008 1

SALINA, KS.

JD508508

AASF # 2, 2917 HEINH-60-08-AMAM-03, MM, DTD 20 DEC 07, MIL-PRF-23699 HIGH TEMPERATURE STABILITY(HTS) OIL C/W 5 MAR 08. (JD508508)

29-Jan-2008 1

SALINA, KANSAS 67401

HI000000

AASF # 2, 2917 HEINH-60-08-SOF-01, MM, DTD 28 JAN 08, MAINROTOR BLADE EXPANDABLE PIN INSPECTIONCHANGE C/W 29 JAN 08 @ 4511.6 ACFT. HRS(JD508508)

29-Jan-2008 2

SALINA, KS 67401

HI000000

AASF # 2, 2917 HEINH-60-08-AMAM-06, MM, DTD 29 JAN 08,COMMON MISSILE WARNING SYSTEM (CMWS)SEQUENCERS C/W 8 MAR 08. (JD508508)

29-Jan-2008 3

SALINA, KS 67401

HI000000

AASF # 2, 2917 HEINH-60-08-AMAM-05, MM, DTD 29 JAN 08,GOODRICH INTERNAL RESCUE HOISTS N/ATHIS ACFT 29 JAN 08. (JD508508)

29-Jan-2008 4

SALINA, KS 67401

HI000000

AASF # 2, 2917 HEINH-60-08-ASAM-06, MM, DTD 26 FEB 08, MAINROTOR PYLON SLIDING FORWARD C/W 27FEB 08. (JD508508)

26-Feb-2008 1

SALINA, KS 67401

HI000000

AASF # 2H-60-08-AMAM-07, MM, DTD 24 MAR 08,AN/ASN-128B/D DOPPLER GPS NAVIGATIONSET (DGNS) C/W 29 APR 08 AT 4304.0 ACFT.HRS.(JD508508)

29-Apr-2008 1

SALINA, KS

HI000000

AMCOM PROJECT OLRANNUAL/ACE EVALUATION COMPLETED AT4610 AIRCRAFT HOURS AT FT. HOOD, TX BYTEAM MEMBERS RR & W (AS5855)

13-Aug-2008 1

KILLEEN, TX

HI000000



8.7.DATE

6.REMARKS

4. 5.



DS2MEC #F80594 TAIL ROTOR BLADEPOLYURETHANE STRIPS REPLACEMENT(RE221756)

21-Aug-2008 1

FT. HOOD, TX

HI000000

DS2MEC #F80598 BEADED PANELS, LEFT ANDRIGHT SIDE, ARE CRACKED AT TABS ATGUNNER'S WINDOW. FABRICATE TWOFINGER DOUBLER, 7075-T6, 0.064 INCHMINIMUM, THICKNESS. CUT FINGERS TO FITAROUND BEADS WITH .125 MINIMUMCLEARANCE. SUPPORT AIRFRAME ACROSSBEAM AT STA. 295. CUT GUNNERS WINDOWLOWER PLATE AT STA. 288.5 FROM W1.221 TOW1.227. REMOVE TWO TABS FROM BEADEDPANEL BY CUTTING ALONG STA. 294, W1. 221,AND W1. 227. ALL FASTENERS SHALL BEINSTALLED WITH EPOXY POLYAMIDE PRIMER.(RE221756)

21-Aug-2008 2

FT. HOOD, TX

HI000000

DS2MEC #F80603 TEXAS PATCH. CUT ANDREMOVE STRAP. FABRICATE A REPAIRSTRAP TO REPLACE REMOVED PORTION OFSTRAP. FABRICATE A REPAIR SPLICE PLATE,0.070 THICK, 7075-T6 ALUMINUM ALLOY,PRIME WITH TWO COATS OF MIL-P-23377,EPOXY PRIMER. INSTALL REPAIR STRAP &SPLICE PLATE USING MONEL RIVETS INPLACE OF MS20470AD ALUMINUM RIVETS.(RE221756)

21-Aug-2008 3

FT. HOOD, TX

HI000000

FT. HOOD PROJECTOLR

INTERIM STATEMENT OF AIRWORTHINESSQUALIFICATION ISAQ 130 FOR UH-60A/LHELICOPTERS EQUIPPED WITH THE DOPPLERGLOBAL POSITIONING SYSTEM (DGNS)PREPLANNED PRODUCT IMPROVEMENT.INSTALLED ON THIS DATE @ 4610 ACFT HRS.(DW828962)

15-Sep-2008 1

(NO LOCATION)

HI000000

DS2UH-60-08-ASAM-08 SELF RETAINING FLIGHTCONTROL BOLTS C/W @ 4609.6 ACFT. HRS.(RE001756)

25-Sep-2008 1

FT. HOOD, TX 76542

HI000000

DS2UH-60-08-AMAM-08 FLIGHT CONTROLRIGGING C/W @ 4609.6 ACFT. HRS. (RE001756)

25-Sep-2008 2

FT. HOOD, TX 76542

HI000000

DS2UH-60-08-ASAM-09 SPINDLE LUGULTRASONIC INSP C/W @ 4609.6 ACFT HRS.(RE001756)

25-Sep-2008 3

FT. HOOD, TX 76542

HI000000

DS2UH-60-08-AMAM-10 CLEANING PROCEDURESFOR ENGINE START CONT. VALVE C/W @4609.6 ACFT HRS. (RE001756)

26-Sep-2008 1

FT. HOOD, TX 76542

HI000000

DS2UH-60-08-ASAM-10 ELECTRICAL WIRINGCHAFFING C/W @ 4609.6 ACFT HRS.(RE221756)

26-Sep-2008 2

FT. HOOD, TX 76542

HI000000

DS2UH-60-08-AMAM-09 SOLID BLADE PINCORROSION C/W @ 4609.6 ACFT HRS.(RE221756)

26-Sep-2008 3

FT. HOOD, TX 76542

HI000000

DS2UH-60-08-ASAM-11 FLIGHT CONTROL RIGGINGC/W @ 4609.6 ACFT HRS. (RE221756)

26-Sep-2008 4

FT. HOOD, TX 76542

HI000000



8.7.DATE

6.REMARKS

4. 5.



DS2UH-60-08-AMAM-11 M/R BLADE ANGLEREVISION C/W @ 4609.6 ACFT HRS. (RE221756)

26-Sep-2008 5

FT. HOOD, TX 76542

HI000000

DS2UH-60-08-ASAM-12 PARKER AEROSPACE AIRTURBINE STARTER C/W @ 4609.6 ACFT HRS.(RE221756)

26-Sep-2008 6

FT. HOOD, TX 76542

HI000000

DS2UH-60-08-ASAM-13 FIRE EXTINGUISHING TUBEUNION RING C/W @ 4609.6 ACFT HRS.(RE221756)

26-Sep-2008 7

FT. HOOD, TX 76542

HI000000

DS2M/R RIGGED FOR COMPLETION OF RESETINSP PRIMARY SERVO CONTROL RODS BIASADJUSTMENTS FWD: -1/4 TURN, AFT: + 1/4TURN, LAT: -7/8 TURN. (RE221756)

26-Sep-2008 8

FT. HOOD, TX 76544

HI000000

DS2T/R BIAS: CABLE TENSION RT - 165 LF - 165TEMP 29CRED INITIAL = 4.656 AFTER = 4.968 ADJ = 0.312YEL INITIAL = 4.656 AFTER = 4.968 ADJ = 0.312BLU INITIAL = 4.062 AFTER = 4.375 ADJ = 0.312BLK INITIAL = 4.062 AFTER = 4.375 ADJ = 0.312(RE221756)

26-Sep-2008 9

FT. HOOD, TX 76544

HI000000

DS2UH-60-08-ASAM-14 SUSPECT ENGINEHARNESS C/W @ 4609.6 ACFT HRS.(RE001756)

03-Oct-2008 1

FT. HOOD, TX 76542

HI000000

DS2UH-60-08-AMAM-12 MAIN TRANSMISSION OILGAUGE TUBE ASSY C/W @ 4609.6 ACFT HRS.(RE221756)

03-Oct-2008 2

FT. HOOD, TX 76542

HI000000

DS2RESET INSP COMPLETED @ 4609.6 ACFT HRS.NEXT PMI-2 DUE @ 4969.6 (RE221756)

17-Oct-2008 1

FT. HOOD, TX 76544

HI000000

DS2COMPLIED WITH H-60-09-SOF-01 @ 4613.1AIRCRAFT HOURS. (CM127059)

24-Oct-2008 1

FT. HOOD, TX 76544

HI000000

AASF #2H-60-09-SOF-02 DATED 7 NOV 08, ALQREMOVAL, C/W 7 NOV 08 @5099.0 ACFT HRS

07-Nov-2008 1

SALINA, KS

JD508508

AASF #2COMPLIED WITH H-60-09-SOF-03 POSSIBLERETIREMENT LIFE OVER-FLIGHT (DELAYEDENTRY)

13-Nov-2008 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH H-60-09-ASAM-01 T701C GASGENERATOR (GG) ROTOR ASSEMBLIES N/ATHIS ACFT (DELAYED ENTRY)

12-Jan-2009 1

SALINA, KS

DL861165

AASF #2AWR 1516, ELT PERMANENT INSTALLATION,APPLYED 4638.9 ACFT HOURS. FCCCOMPLETED FOR ALL UNIT ACFT ON 8023489.

14-Jan-2009 1

SALINA, KS

JD508508

AASF #2COMPLIED WITH H-60-09-ASAM-04 RESCUEHOIST CARTRIDGE ACTIVATION DEVICE (CAD)N/A IS ACFT

26-Feb-2009 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH H-60-09-ASAM-05 UPDATE TOLIFE CHANGE FOR T/R QUADRANT SPRINGCAPSULES (DELAYED ENTRY)

03-Mar-2009 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH H-60-09-ASAM-07 FIREEXTINGUISHER WIRING (BREAKAWAYTHREAD) (DELAYED ENTRY)

06-Apr-2009 1

SALINA, KS

DL861165



8.7.DATE

6.REMARKS

4. 5.



AASF #2COMPLIED WITH H-60-09-ASAM-08 ENGINECOWLING WEIGHT RESTRICTION (DELAYEDENTRY)

21-Apr-2009 1

SALINA, KS

DL861165

FT HOOD AFMAAIRCRAFT 8023495 ACE COMPLETED ATSALINA, KS AT 4683 ACFT HRS BY TEAMMEMBERS RR & Q

24-Apr-2009 1

KILLEEN, TX

AS425855

MO-AVCRADH60-07-ASAM-06 INSTALLATION OF CABLEGUARD COMPLIED WITH PER MO-AVCRADWO#990007 AND INTERSHOP# 960234 I/A/WMEC# F87053, OTR# AMOTRM43 AND MEO#A5908. REFER: (RSN) 1001031.COMPLETED BYMO-AVCRAD CONTACT TEAM ANDINSPECTED BY R. WILSON T.I. MO-AVCRADQ.C.

06-May-2009 1

SPRINGFIELD, MO.

RW626133

AASF #2COMPLIED WITH H-60-09-ASAM-09 FIREEXTINGUISHER WIRING (BREAKAWAYTHREAD) (REVISION TO H-60-09-ASAM-07)

06-May-2009 2

SALINA, KS

DL861165

AASF #2COMPLIED WITH H-60-09-AMAM-04 A2C2S N/ATHIS ACFT

24-Aug-2009 2

SALINA, KS

DL861165

AASF #2COMPLIED WITH H-60-09-AMAM-04 @4736.1ACFT HRS

01-Sep-2009 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH H-60-09-AMAM-06 CARGOHOOK CARTRIDGE ACTUATED DEVICE LIFEREDUCTION @4736.1 ACFT HRS

01-Sep-2009 2

SALINA, KS

DL861165

AASF #2 / B COMPANY 1-108TH AVN REGT

COMPLIED WITH REQUIREMENTS OF H-60-09-ASAM-11 CARGO DOOR EMERGENCYJETTISON HANDLE ASSY

10-Sep-2009 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH H-60-09-AMAM-07 (HHFE)HALON HAND-HELD FIRE EXTINGUISHER

15-Sep-2009 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-01 HMU REPLACEMENT

01-Oct-2009 1

SALINA, KS

DL861165

AASF #2M/R RIG FOR COMPLETION OF BEEDEDPANEL MOD

06-Nov-2009 1

SALINA, KS

DL861165

B CO 1-108TH AVNREGT

COMPLIED WITH THE REQUIREMENTS OF H-60-10-ASAM-04 STABILITY AUGMENTATIONSYSTEM LINKS, AT ACFT HRS 4745.1

13-Jan-2010 1

SALINA, KS

DL861165

AASF #2 / B COMPANY 1-108TH AVN REGT

COMPLIED WITH THE REQUIREMENTS OF H-60-10-AMAM-11,OIL SAMPLING SCHEULECHANGES, AT 4762.8 ACFT HRS

03-Feb-2010 2

SALINA, KS

DL861165

AASF #2COMPLIED WITH THE REQUIREMENTS OF H-60-10-ASAM-07, STABILATOR HINGE FITTINGS,AT 4818.1 ACFT HRS

22-Apr-2010 1

SALINA, KS

CS729537

AASF #2COMPLIED WITH THE REQUIRMENTS OF H-60-10-AMAM-12, IMPROVED DRAG BEAM, AT4818.8 ACFT HRS

28-Apr-2010 1

SALINA, KS

CS729537

FT HOOD AFMAAIRCRAFT 8023495 ACE COMPLETED AT 4829ACFT HRS 7 MAY 2010 AT SALINA, KS BYTEAM MEMBERS RR & W

07-May-2010 1

KILLEEN, TX

AS425855



8.7.DATE

6.REMARKS

4. 5.



B CO. 1/108TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-08, APU FIREWALL INSP. AT 4740.2ACFT HRS

27-May-2010 1

SALINA, KS

DL861165

B CO 108TH AVN REGTAIRWORTHINESS LELEASE (AWR) FOROPERATION OF NCS MAGNUS MODEL RNM101LATTOP ONBOARD AND OPERATION (AWR1648)

03-Jun-2010 1

SALINA, KS

DL861165

B CO 1/108TH AVNCOMPLIED WITH THE REQUIREMENTS OF H-60-10-AMAM-16, COMMON MISSILE WARNINGSYSTEM GUARD DISPENCE SWITCH, N/A THISACFT

23-Jun-2010 1

SALINA, KS

DL861165

B CO 1/108TH AVNCOMPLIED WITH THE REQUIREMENTS OF H-60-10-SOF-02, SPINDLE LUG NDI TBO CHANGE,AT 4847.4 ACFT HRS.

24-Jun-2010 1

SALINA, KS

DL861165

B CO 108TH AVN REGTMEC #F111088 DATED 28 JUN 2010, THUR AEDLE, FOR AN EXTESION OF 76.6 HRS ON A M/RSPINDLE HORN ASSY. EXTENTIONAUTHORIZED. NICHOLAS W HURTA ON 02JULY 2010.

28-Jun-2010 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH REQUIREMENTS OFH-60-10-ASAM-12, ENG COMMON COMPONENTRETIREMENT CHANGE TIMES, 4892.0 ACFTHRS.

03-Aug-2010 1

SALINA, KS

CS729537

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-11, COMMON COMPONENTRETIREMENT CHANGE TIMES UPDATE,4892.0 ACFT HRS.

03-Aug-2010 2

SALINA, KS

CS729537

B COMPANY 1-108THAVN (ASSLT)

COMPLIED WITH THE REQUIREMENTS OF H-60-10-ASAM-15 IMPROVED EXTERNAL STORESSUPPORT SYSTEM(ESSS) FUEL SYSTEM VENTELBOW, 4905.1 ACFT HRS.

17-Aug-2010 1

SALINA, KS

DL861165

B CO 1/108TH AVNREGT (ASSLT)

COMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-16, RESCUE HOIST CABLE CUTHARNESS CONNECTOR. 4921.1 ACFT HRS

08-Sep-2010 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-11-ASAM-02, TAIL ROTOR SERVOCYLINDERASSEMBLY HARDWARE 4939.0 ACFT HRS.

15-Oct-2010 1

SALINA, KS

CS729537

AASF #2H-60-11-AMAM-03, OIL COOLER FAN AXIALBEARING, COMPLIED WITH AT 4948.3AIRCRAFT HOURS.

25-Oct-2010 1

SALINA, KS

MS809227

B CO 1-108TH AVN REGCOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-04 AT4967.0 ACFT HRS

15-Nov-2010 1

SALINA, KS

DL861165

FT. HOOD AFMAINSTALLATION AND PERMANENT CHANGESTO CONFIGURATION IAW AWR (CPX)(ISAQ116) RELEASE DATE 22 NOV 06 R-2 INREFERENCE FOR INSTALLATION OF THEMWO 1-1520-237-50-84 APX-118

08-Dec-2010 1

SALINA, KS

ON909978

FT. HOOD AFMAINSTALLATION AND PERMANENT CHANGESTO CONFIGURATION IAW AWR 1346 DATED 15JUL 2010 R-17 IN REFERENCE FORINSTALLATION OF THE MWO 1-1520-237-50-100 IVHMS

08-Dec-2010 2

SALINA, KS

ON909978



8.7.DATE

6.REMARKS

4. 5.



FT. HOOD AFMAINSTALLATION AS WELL PERMANENTCHANGES TO CONFIGURATION IAW AWR 1425DATED 18 AUG 2010 R-14 IN REFERENCE FORINSTALLATION OF THE MWO 1-1520-237-50-97UPGRADE CMWS P3I

08-Dec-2010 3

SALINA, KS

ON909978

FT. HOOD AFMAINSTALLATION AS WELL AS PERMANENTCHANGES TO CONFIGURATION IAW AWR 1494DATED 20 AUG 09 R-4 IN REFERENCE FORINSTALLATION OF THE MWO 1-1520-237-50-99CMWS 5 TH SENSOR

08-Dec-2010 4

SALINA, KS

ON909978

FT. HOOD AFMAINSTALLATION OF THE AN/AAR-57 IMPROVEDCOUNTERMEASURE DISPENSER SYSTEM(ICMD) COMMON MISSILE WARNING SYSTEM(CMWS) MODERNIZATION P3I MWO 1-1520-237-50-97

08-Dec-2010 5

SALINA, KS

ON909978

FT. HOOD AFMAINSTALLATION OF THE COMMON MISSILEWARNING SYSTEM (CMWS) 5 TH SENSORMWO 1-1520-237-50-99

08-Dec-2010 6

SALINA, KS

ON909978

B CO 1/108TH AVNREGT ASSLT

COMPLIED WITH REQUIREMENTS OF H-60-11-ASAM-04 AT 4967.0 ACFT HRS

09-Dec-2010 1

SALINA, KS

DL861165

B CO 108TH AVN REGTASSLT

COMPLIED WITH REQUIREMENTS OF H-60-11-ASAM-06 AT4967.0 ACFT HRS

28-Dec-2010 1

SALINA, KS

DL861165

B CO 1/108TH AVNREGT

PMI #1 COMPLETED 4967.0 ACFT HRS 29-Jan-2011 1

SALINA, KS

DL861165

B CO 1/108TH AVNREGT (ASSLT)

COMPLIED WITH REQUIREMENTS OF H-60-11-ASAM-08 AT 4975.3 ACFT HRS

09-Feb-2011 1

SALINA, KS

DL861165

B CO 108TH AVNREGT(ASSLT)

COMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-06 AT 4975.3 ACFT HRS

09-Feb-2011 2

SALINA, KS

DL861165

B CO 108TH AVNCOMPLIED WITH REQIUREMENTS OF AWR1346 (IVHMS) DATE 15 JUL 10/R17

14-Mar-2011 1

SALINA, KS

DL861165

B CO 1/108TH AVNCOMPLIED WITH REQUIREMENTS OF AWR1738 DATED 1 FEB 11

14-Mar-2011 2

SALINA, KS

DL861165

B CO 1/108TH AVNCOMPLIED WITH REQUIREMENTS OF AWR1738(AN/APX-118) DATED 1 FEB 11

14-Mar-2011 3

SALINA, KS

DL861165

B CO 1-108TH AVNCOMPLIED WITH REQUIREMENTS OF AWR1054(BAMBI WATER BUCKET) DATED 29 OCT10R9

15-Mar-2011 2

SALINA, KS

DL861165

B CO 1-108TH AVNCOMPLIED WITH REQUIREMENTS OF AWR1120(M-240 INSTALLED) DATED 30 NOV 10R8

15-Mar-2011 3

SALINA, KS

DL861165

B CO 1-108TH AVNCOMPLIED WITH REQUIREMENTS OF AWR1308(RESCUE HOIST) DATED 29 APR 09R5

15-Mar-2011 4

SALINA, KS

DL861165

B CO 1-108TH AVNCOMPLIED WITH REQUIREMENTS OF AWR1467(DGNS-P3I) DATED 1 MAR 10R4

15-Mar-2011 5

SALINA, KS

DL861165



8.7.DATE

6.REMARKS

4. 5.



B CO 1-108TH AVNCOMPLIED WITH REQUIREMENTS OF AWR1309(OREGON AERO SEAT) DATED 4 JUN10R5

15-Mar-2011 6

SALINA, KS

DL861165

B CO 1-108TH AVNCOMPLIED WITH REQUIREMENTS OF AWR1444 (AHRU/AHRS) DATED 29 SEPT 09R2

15-Mar-2011 7

SALINA, KS

DL861165

B CO 1-108TH AVNCOMPLIED WITH REQUIREMENTS OF AWR1347(QUAD BAY INSTALL) DATED 27 DEC10R13

15-Mar-2011 8

SALINA, KS

DL861165

B CO 1-108TH AVNCOMPLIED WITH REQUIREMENTS OF AWR1494(CMWS) DATED 30 SEPT 10R5

15-Mar-2011 9

SALINA, KS

DL861165

B CO 1/108TH AVNCOMPLIED WITH REQUIREMENTS OF AWR1516 DATED 29 OCT 10R6

15-Mar-2011 10

SALINA, KS

DL861165

FT. HOOD AFMACOMPLIED WITH REQUIREMENTS OF AWR1425 (CMWS P3I) DATED 18 AUG 2010 R-14

17-Mar-2011 1

SALINA, KS

BD447755

B CO 1/108TH AVNCOMPLIED WITH REQUIREMENTS OF AWR1750 (NVG) DATED 25 MAR 2011

29-Mar-2011 1

SALINA, KS

DL861165

B CO 1-108TH AVNCOMPLIED WITH REQUIREMENTS H-60-11-ASAM-09 N/A THIS ACFT

29-Mar-2011 2

SALINA, KS

DL861165

B CO 1-108TH AVNCOMPLIED WITH REQUIREMENTS OF AWR1566 (HOIST CABLE GUARD) DATED 18 MAR11R2

04-Apr-2011 1

SALINA, KS

DL861165


COMPLIED WITH REQUIREMENTS OF AWR1428(TDFM-6148) DATED 14 JUL 09R2

04-Apr-2011 2

SALINA, KS

DL861165

B CO 1-108TH AVNACFT MODE S ADDRESS IS 53420745 06-Apr-2011 1

SALINA, KS

DL861165

B CO 1-108TH AVNCOMPLIED WITH REQUIREMENT H-60-11-AMAM-09 (ENGINE COMPONENT OPERATINGHOUR RECORD)

20-Apr-2011 1

SALINA, KS

DL861165

B CO 1-108TH AVNCOMPLIED WITH THE REQUIREMENTS OF H-60-11-AMAM-10( COMMON MAIN ROTORSPINDLE)

20-Apr-2011 2

SALINA, KS

DL861165

B CO 1-108TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-11 (AWR STATUS UPDATE)

20-Apr-2011 3

SALINA, KS

DL861165

FT HOOD AFMAACE COMPLETED AT 5038 AIRCRAFT HOURSAT SALINA, KS BY TEAM MEMBERS K & Q.

27-Apr-2011 1

SALINA, KS

WS244328

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-11-ASAM-04 (AN/ARN-153 TCN-500 TACANRECEIVER BEARING ERROR

18-May-2011 1

SALINA, KS

CS729537

AASF 1H-60-11-AMAM-13 EXTERNAL RESCUE HOISTMOUNT FITTING COMPLIED WITH AT 5060.8ACFT HRS.

05-Jul-2011 1

TOPEKA, KS

JM884376

AASF#1H-60-11-SOF-01 (DISCREPANT SELF LOCKINGDOUBLE HEX NUTS) COMPLIED WITH AT5065.8 ACFT HRS.

23-Jul-2011 1

TOPEKA

TB866532

AASF#1H-60-11-ASAM-13 (ENG AIR ANTI-ICINGMODULATING VALVE) COMPLIED WITH AT5075.5 ACFT HRS

29-Jul-2011 1

TOPEKA

KJ781803



8.7.DATE

6.REMARKS

4. 5.



MOA AVCRAD120 DELTA SOFTWARE UPGRADE 511PROGRAM 6035.3 ACFT HRS

30-Aug-2011 1

TOPEKA

DL897874

1/108TH AVN.H-60-11-AMAM-18, GE-YT706 GE-700 FUELFILTER ASS. DIFFERENTIAL PRESSURESWITCH COOLAR KIT, DOES NOT APPLY TOTHIS ACFT. MH-60M ACFT. ONLY.

22-Sep-2011 1

NORTH FORT HOOD,TEXAS

GB707883

D CO 1-108 AVN H-60-12-SOF-01 TAIL ROTOR INTERMEDIATEGEARBOX COMPLIED WITH AT ACFT HRS5139.4 , COMP HRS 4419.0

08-Oct-2011 1


JP579972

D CO 1-108TH AVNCOMPLIED WITH REQUIRMENTS OF H-60-12-SOF-02. 5148.2 ACFT HRS

13-Oct-2011 1


TB866532

D CO 1-108THCOMPLIED WITH REQUIREMENTS OF H-60-12-SOF-03. 5158.3 ACFT HRS.

16-Oct-2011 1


TP416505

D CO. 1/108TH AVN. MAIN ANDT/R RIG CHECK COMPLETED FOROUT OF RIG DURING HOVER. (2408-13-1 DTD03N0V11 #4). M/R 90-8.5, HIGH COLL 21.3, FWDCYC-3.6, AFT CYC 25.5. 180 -2.1 HIGH COLL.11.1 LEFT CYC. -9.0 RIGHT CYC. 5.9. 270 -10.1HIGH COLL 9.8, FWD CYC. 36.7, AFT CYC. 3.7. 0-AFT. HIGH COLL. 18.6, LEFT CYC. 6.4, RT CYC.8.2, TOTAL HIGH COLL 60.8, FWD CYC 40.30,AFT CYC. 21.80, LEFT CYC. 15.40, RT CYC.14.10T/R BIAS CHK: RED-INT. 4.9, BIAS 5.2,DIFF. 0.30. BLUE- INT. 4.3, BIAS 4.6 DIFF 0.30.YELLOW-INT. BIAS 5.0 DIFF. O.30. @BLACK-INT. 4.3 BIAS 5.0 DIFF 0.30. T/R CABLETENSION L/H 155, R/H 156 @ 25 DEGREESCELSIUS, @ 5167.6 ACFT. HRS.

10-Nov-2011 1


GB707883

AASF #1COMPLIED WITH REQUIREMENTS OF H-60-12-SOF-03 AT 5169.2 ACFT HRS. N/A THIS ACFT

21-Feb-2012 1

TOPEKA, KANSAS

KJ781803

AASF #2*LATE ENTRY* COMPLIED WITHREQUIREMENTS OF H-60-11-ASAM-14 ENGINECOWL REPAIR RESTRICTIONS AT 5178 ACFTHRS

20-Apr-2012 1

SALINA, KANSAS

KJ781803

AASF #1H-60-12-AMAM-03 TRANSPONDER ANDCOMMON MISSLE WARNING SYTENINSTALLATION COMPLIED WITH AT 5178 ACFTHRS

20-Apr-2012 2

TOPEKA, KS

KJ781803

FT HOOD AFMAACE PERFORMED AT 5202 ACFT HRS ATTOPEKA, KS BY TEAM MEMBERS RR & W

15-Jun-2012 1

SALINA, KANSAS

AS425855

B CO 1-108THCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-08 CARGO HOOK MANUAL RELEASESPRING.

17-Jul-2012 1

SALINA, KS

JL949482

B CO 1-108THCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-07 @ 5207.5 AIRCRAFT HOURS.

21-Aug-2012 1

SALINA, KS

JL949482

B CO 1-108THCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-09 BREEZE EASTERN EXTERNALRESCUE HOIST.

22-Aug-2012 1

SALINA, KS

JL949482



8.7.DATE

6.REMARKS

4. 5.



B CO 1-108THCOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-17 TAIL ROTOR SHIMS @ 5207.5AIRCRAFT HOURS.

22-Aug-2012 2

SALINA, KS

JL949482

B CO 1-108THCOMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-15 TRIM ACTUATORS.

31-Aug-2012 1

SALINA, KS

JL949482

B CO 1-108THCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-10 ENGINE ANTI-ICE/START BLEEDVALVE.

11-Sep-2012 1

SALINA, KS

JL949482

B CO 1-108THCOMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-09 HYDRAULIC LINE CHAFE DUE TOMISSING CLAMPS.

11-Oct-2012 1

SALINA, KS

JL949482

B CO 1-108THCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-02 ATTITUDE REFERENCE HEADINGSYSTEM (AHRU) WIRING HARNESSES.

06-Nov-2012 1

SALINA, KS

JL949482

B CO 1-108THCOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-01, ANTI-COLLISION LIGHT POWERSUPPLY.

28-Nov-2012 1

SALINA, KS

JL949482

B CO 1-108THCOMPLIED WITH THE REQUIREMENTS OF H-60-13-AMAM-03, DECU/EDECU TURBINE GASTEMPERATURE BIAS.

29-Nov-2012 1

SALINA, KS

JL949482

B CO 1/108TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-01, FLIGHT CONTROL RIGGING

04-Dec-2012 1

SALINA, KS

DL861165

B CO 1-108TH48 MONTH FLIGHT CONTROL INSPCOMPLETED

20-Dec-2012 1

SALINA, KS

DL861165

B CO 1-108TH AVNCOMPLIED WITH THE REQUIREMENTS OF H-60-13-AMAM-04 @ 5240.2 ACFT HRS

15-Jan-2013 1

SALINA, KS

DL861165

B CO 108TH AVN REGTCOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-03, MAIN ROTOR SPINDLE ANTI-FLAPASSEMBIES

28-Feb-2013 1

SALINA, KS

DL861165

B CO 1/108TH AVNREGT

COMPLIED WITH A REQUIREMENTS OF H-60-13-AMAM-06 (CEFS) NOT INSTALLED

05-Mar-2013 1

SALINA, KS

DL861165

B CO 1-108TH AVNLATE ENTRY COMPLIED WITHREQUIREMENTS OF H-60-12-AMAM-12 (RCCOMPONENT REMOVAL DATES)

05-Mar-2013 2

SALINA, KS

DL861165

DYNCORP INTLACE PERFORMED AT 5278 ACFT HRS ATSALINA, KS BY TEAM MEMBERS RR & K

22-Mar-2013 1

SALINA, KS

AS425855


COMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-04 (GEARBOX INSP)

26-Mar-2013 1

SALINA, KS

DL861165


COMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-05, BREEZE EASTERN VARIABLESPEED ELETRIC RESCUE HOIST

10-Apr-2013 1

SALINA, KS

DL861165


COMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-06 (PMI CHECKLIST CHANGE)

15-May-2013 2

SALINA, KS

DL861165



8.7.DATE

6.REMARKS

4. 5.




COMPLIED WITH REQUIREMENTS OF H-60-13-SOF-01 (AHRS)

31-May-2013 1

SALINA, KS

DL861165

B CO 1-108TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-01 (T/R OUTPUT BEVEL GEAR NDI) AT5297 ACFT HRS

05-Jun-2013 1

SALINA, KS

DL861165

B CO 1-108TH AVNPMI 2 COMPLETED AT 5297 ACFT HRS 07-Jun-2013 1

SALINA, KS

DL861165

AASF #2ALL H-60 SERIES AIRCRAFT H-60-13-AMAM-11MAIN TRANSMISSION FILTER BOWLATTACHMENT HARDWARE REPLACEMENTNLT 31 JAN 2014 C/W AT ACFT HRS.

01-Jul-2013 1

SALINA, KS

CS729537


H-60-14-AMAM-01 DOES NOT APPLY TO THISAIRCRAFT

24-Oct-2013 1

SALINA, KS

DL861165


COMPLIED WITH REQUIREMENTS OF H-60-14-SOF-01 (BREEZE EASTERN EXTERNAL RECUEHOIST INSTALLATION)

01-Nov-2013 1

SALINA, KS

DL861165

AASF #2ALL UH/HH-60 SERIES AIRCRAFT, HEALTHUSAGE MONITORING SYSTEM (HUMS)ACCELEROMETERS, H-60-14-ASAM-02 C/W

10-Dec-2013 1

SALINA, KS

CS729537

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-14AMAM-04 ( MAIN ROTOR HUB NDI)

31-Dec-2013 1

SALINA, KS

DL861165

AASF #2H-60-14-ASAM-03 (EIBF BRACKET) COMPLIEDWITH AT 5387.9 ACFT HRS.

24-Jan-2014 1

SALINA, KS

CS729537

AASF #2 SALINACOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-03 (DISCREPANT CONNECTING LINK)

30-Jan-2014 1

SALINA, KS

DL861165

AASF #2 SALINA KSCWO (MWO) 1-1520-237-20-2 COMPLIED 11-Feb-2014 1

SALINA, KS

DL861165

AASF #2 SALINA KSMWO 1-1520-237-30-3 INSTALLED (AUTORELIGHT AND TRANSIENT DROOPIMPROVEMENT FOR 701D ENG)

14-Feb-2014 1

SALINA, KS

DL861165

AASF #2 SALINA KSCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-08 (AN/ASC-15E CIRCUIT BRAEKERPROTECTION)

05-Mar-2014 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-05 (LCF CHG 65) AT 5410.2 ACFT HRS

24-Mar-2014 1

SALINA, KS

CS729537



8.7.DATE

6.REMARKS

4. 5.



AASF #2"OPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR'S: 1823(IVHMS) 14 MAY 12, 1800R2 (BFT) 22 MAR 13,1787R1 (ARN-123) 28 AUG 13, 1753R2(DGNS)26 JUN 13, 1750R2 (ANVIS) 29 MAR 13, 1738(APX-118) 01 FEB 13, 1682R14 (TDI) 26 FEB 14,1648R2 (LATTOP ONBOARD) 09 MAR 12,1615R2 (CE M-4 MOUNT) 14 MAR 12, 1613R2 (ATO L) 06 JUN 13, 1594R4 (701D/CC) 27 NOV 13,1566R3 (CABLE GUARD) 18 MAR 13, 1520R24(FLIR) 16 MAY 13, 1516R7 (ELT) 11 OCT 12,1494R7 (5TH SENSOR) 29 JUN 12, 1455R4(CAP) 18 SEPT 12, 1444R6 (SINGLE AHRU) 11JUL 13, 1428R4 (TDFM) 24 JUL 13, 1425R17(P3I) 18 SEPT 12, 1418R4 (HF ANTENNA) 31MAY 11, 1346R21 (IVHMS) 24 JAN 14, 1309R7(SEAT CUSHION) 10 FEB 12, 1308R10 (IRH) 18APR 13, 1279R4 (WINDOW AND DOORSREMOVED) 25 MAY 12, 1120R9 (M240) 30 NOV12, 1054R13 (BAMBI BUCKET) 31 OCT 13,1037R12 (SATCOM) 03 JAN 14, 980R9 (HOIST)15 MAR 13, 1310R

25-Mar-2014 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-10

11-Apr-2014 1

SALINA, KS

DL861165

AFM RASM-WACE COMPLETED AT 5416 AIRCRAFT HOURSAT SALINA, KS BY TEAM MEMBERS W & Q.

17-Apr-2014 1

SALINA, KS

WS244328

AASF #2COMPLIED WITH REQUIREMETNS OF H-60-14-AMAM-09

23-Apr-2014 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-14

04-Jun-2014 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-14-SOF-03 (DESCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS)

27-Jun-2014 1

SALINA, KS

CS729537

AASF 2H-60-14-AMAM-16 AHRU 2410 TRACKINGCOMPLIED WITH

18-Jul-2014 1

SALINA, KS

JM884376

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-14-SOF-04 (CHECK LIST CHANGE)

27-Aug-2014 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-15-AMAM-05, AHRS EMERGENCY PROCRDURE

11-Dec-2014 1

SALINA, KS

DL861165

FT HOOD AFMA RASMW

ACE COIMPLETED AT 5549 AIRCRAFT HOURSAT SALINA, KS BY TEAM MEMBERS RR & K

07-Apr-2015 1

SALINA, KS

AS425855

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-15-ASAM-03

27-May-2015 1

SALINA, KS

DL861165

AASSF #2COMPLIED WITH REQUIREMENTS OF H-60-15-AMAM-10

02-Jun-2015 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-15-AMAM-11 (MODE-S TRANSPONDER) ADDRESS53420747

10-Jun-2015 1

SALINA, KS

DL861165



8.7.DATE

6.REMARKS

4. 5.



AASF #2H-60-15-SOF-02 (FRIES RELEASE CABLEINSPECTION) N/A THIS ACFT

29-Sep-2015 1

SALINA, KS

DL861165

AASF #2H-60-15-AMAM-18 (MEDEVAC CAROUSEL)COMPLIED WITH

07-Oct-2015 1

SALINA, KS

DL861165

AASF #2H-60-16-AMAM-01 (EIBF FRAME) COMPLIEDWITH

29-Oct-2015 1

SALINA, KS

DL861165

AASF #2H-60-16-ASAM-01 (INBOARD RETENTIONPLATE RETORQUE CHECK) COMPLIED WITH

12-Nov-2015 1

SALINA, KS

DL861165

AASF #2H-60-16-ASAM-02 (DEFECTIVE FUEL HOSES)COMPLIED WITH

12-Jan-2016 1

SALINA, KS

DL861165

AASF #2H-60-16-AMAM-04 (T-CLIP INSTALLATION)COMPLIED WITH

12-Jan-2016 2

SALINA, KS

DL861165

AASF #2AIRCRAFT TRANSFERRED TO BESTPROGRAM ON 3 FEB 2016 FOR ARMY/BESTPROGRAM BY B COMPANY 1-108TH AVNREGT AT XXXX.X ACFT HRS DATA PLATEREMAINS INSTALLED

03-Feb-2016 1

SALINA, KS

DL861165


DATE AC HRS SHAFT VERTICAL REASON FOR VIB CHECKLONGITUDINALLATERAL

IPS READINGS4.

8023495HELICOPTER, UTILITYUH-60A3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Report Date: 19-Feb-2016 1/4

100 HR15-Oct-1993 #1 ENG D/S 000.32177

100 HR15-Oct-1993 #2 ENG D/S 000.42177

100 HR15-Oct-1993 AXIAL FAN 0.360.602177

100 HR04-Aug-1994 #1 ENG D/S 000.12281

100 HR04-Aug-1994 #2 ENG D/S 000.252281

100 HR04-Aug-1994 AXIAL FAN 0.150.402281

100 HR08-Mar-1995 #1 ENG D/S 000.082379

100 HR08-Mar-1995 #2 ENG D/S 000.382379

100 HR08-Mar-1995 AXIAL FAN 0.070.1202379

MWO 1-1520-237-50-7329-Aug-1995 #1 ENG D/S 000.342424.4

MWO 1-1520-237-50-7329-Aug-1995 #2 ENG D/S 000.312424.4

PMS201-Jan-1998 #1 ENG D/S 000.012446.1

PMS 201-Jan-1998 #2 ENG D/S 000.262446.1

PMS 201-Jan-1998 AXIAL FAN 0.130.0702446.1

GUST LOCK ENGAGED14-Feb-2001 #1 ENG D/S 0.24002500

GUST LOCK ENGAGED14-Feb-2001 #2 ENG D/S 0.46002500

GUST LOCK ENGAGED14-Feb-2001 OIL COOLER 0.160.0702500

100 HR29-Mar-2001 #1 ENG D/S 0.26002746.5

100 HR29-Mar-2001 AXIAL FAN 0.050.1202746.5

100 HR29-Mar-2001 #2 ENG D/S 0.41002746.5

100 HR08-Nov-2001 #1 ENG D/S 000.372844.3

100 HR08-Nov-2001 AXIAL FAN 0.050.0602844.3

100 HR08-Nov-2001 #2 ENG D/S 0.43002844.3

RMVL/REP TAIL TAKEOFF SEA01-Feb-2002 AXIAL FAN 0.190.102871.3

100 HR21-Dec-2004 #2 ENG D/S 000.233029.4

100 HR21-Dec-2004 AXIAL FAN 0.090.4203029.4

100HR01-Apr-2005 T/R 0.06003128

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.



100 HR01-Apr-2005 #2 ENG D/S 000.183128

100 HR01-Apr-2005 #1 ENG D/S 000.213128

100 HR01-Apr-2005 AXIAL FAN 0.130.4203128

120 HR27-Jul-2005 #1 ENG D/S 000.193248.2

120 HR27-Jul-2005 #2 ENG D/S 000.243248.2

120 HR27-Jul-2005 #1 ENG D/S 000.193248.2

120 HR27-Jul-2005 #2 ENG D/S 000.243248.2

120 HR27-Jul-2005 AXIAL FAN 0.110.3603248.2

120 HR27-Jul-2005 T/R 0.12003248.2

POST PHASE27-Oct-2006 2 0.15004069

POST PHASE29-Oct-2006 1 0.4004069

POST PHASE29-Oct-2006 OIL COOLER 0.2400.84069

POST PHASE29-Oct-2006 TAIL ROTOR 0.11004069

REPLACEMENT #1 ENGINE28-Nov-2006 #1 ENG 0.14004071.2

120 HR08-Dec-2006 #1 ENG 0.42004101.5

120 HR08-Dec-2006 #2 ENG 0.19004101.5

120 HR08-Dec-2006 OIL COOLER 0.140.0804101.5

120 HR08-Dec-2006 T/R 0.13004101.5

120 HR15-Feb-2007 #1 0.19004220.6

120 HR15-Feb-2007 #2 0.23004220.6

120 HR15-Feb-2007 AXIAL FAN 0.08004220.6

120 HR15-Feb-2007 T/R 0.12004220.6

XMSN REPLACEMENT17-Apr-2007 #1 0.29004337.8

XMSN REPLACEMENT17-Apr-2007 #2 0.28004337.8

XMSN REPLACEMENT17-Apr-2007 AXIAL FAN 0.08004337.8

T/R BOOT REPLACEMENT22-May-2007 T/R 0.12004387.3

BATTLE DAMAGE, MWO 50-94 (FOGS) INSTALL.26-Jul-2007 #1 ENG 0.36004424.2




IPS READINGS4.



BATTLE DAMAGE, MWO 50-94 (FOGS) INSTALL.26-Jul-2007 #2 ENG 0.41004424.2

BATTLE DAMAGE, MWO 50-94 (FOGS) INSTALL.26-Jul-2007 OIL COOLER 0.120.904424.2

BATTLE DAMAGE, MWO 50-94 (FOGS) INSTALL.26-Jul-2007 T/R 0.03004424.2

REPLACEMENT OF #1 ENGINE30-Jul-2007 #1 ENG 0.37004424.2

#1 ENG REPL30-Jul-2007 #1 ENG 0.37004424.2

120 HR21-Jun-2008 #1 ENG 0.23004570

120 HR21-Jun-2008 #2 ENG 0.38004570

120 HR21-Jun-2008 OIL COOLER 0.120.1204570

120 HR21-Jun-2008 TAIL ROTOR 0.07004570

REPLACED DURING RESET16-Oct-2008 #1 ENG 0.16004609.6

REPLACED DURING RESET16-Oct-2008 #2 ENG 0.24004609.6

COMPLETION OF RESET16-Oct-2008 AXIAL FAN 00.0104609.6

COMPLETION OF RESET16-Oct-2008 M/R 0.13004609.6

COMPLETION OF RESET16-Oct-2008 T/R 0.02004609.6

POST MAINTANENCE13-Nov-2009 #1 ENG 0.36004738.9

POST MAINTANENCE13-Nov-2009 #2 ENG 0.02004738.9

POST MAINTANENCE13-Nov-2009 OIL COOLER 00.2204738.9

POST MAINTANENCE13-Nov-2009 TAIL ROTOR 0.08004738.9

POST MAINTANENCE13-Nov-2009 MAIN ROTOR 0.28004738.9

POST PHASE28-Jan-2011 #1 ENG 0.304004967

POST PHASE28-Jan-2011 #2 ENG 0.25004967

POST PHASE28-Jan-2011 OIL COOLER 0.740.0904967

POST PHASE28-Jan-2011 T/R 0.16004867

POST PHASE28-Jan-2011 M/R 0.23004967

T/R PADDLE REINSTALL AFTER RETORQUE11-Feb-2011 T/R 0.06004977.9

ENG REPLACEMENT07-Jun-2011 #1 ENG 0.3005050.8

RIGGING CHANGE10-Aug-2011 T/R 00.0605078.1




IPS READINGS4.



120 HRS INSP.15-Aug-2011 T/R 000.65085.6

120 HRS INSP15-Aug-2011 OIL COOLER 0.17005085.6

120 HRS INSP.15-Aug-2011 #1 HHS 0.45005085.6

120 HRS INSP.15-Aug-2011 #2 HHS 0.2005085.6

#1 ENGINE REMOVAL/REINSTALLATION31-Oct-2011 #1 0.24005167.4

POST PMI 207-Jun-2013 T/R 0.17005300

POST PMI 207-Jun-2013 #1 ENG 0.14005300

POST PMI 207-Jun-2013 #2 ENG 0.15005300

POST PMI 207-Jun-2013 OIL COOLER 00.3105300

120 HR19-Mar-2014 T/R 0.09005410.2

120 HR19-Mar-2014 OIL COOLER 0.070.3405410.2

120 HR19-Mar-2014 #1 ENG 0.15005410.2

120 HR19-Mar-2014 #2 ENG 0.54005410.2

ENG REPLACED18-Dec-2015 #1 ENG 0.46005620.7

ENG REPLACED18-Dec-2015 #2 ENG 0.05005620.7

6. Remarks



PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN

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

8023495UH-60AHELICOPTER, UTILITY

3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE

Report Date: Page 1 of 818-Feb-2016

OM02-Jun-1986

LSSI (NO PID)(QC000000)

1501-Dec-1986

H, IREPLACEMENT OF STABILATORACTUATORS, P/N 70400-06641-115

55-1520-237-20-77MWO:

Mnt LevelPriority

DN25-May-1983

DYNCORP, FTHOOD, TX (NOPID) (QC000000)

201-Jan-1984

H, IMODIFICATION OF MAIN ROTORSERVO INPUT PUSHROD ASSEMBLY(UH-60A HELICOPTERS)

55-1520-237-50-13MWO:

Mnt LevelPriority

OE30-Apr-1986

HHC 1/27 CAVFT CAMPBELL,KY (NO PID)(QC000000)

0.201-May-1986

H, IRELOCATION OF THE AUTOMATICFLIGHT CONTROL SYSTEM (AFCS)PANEL

55-1520-237-20-01MWO:

Mnt LevelPriority

DN01-Jan-1981

DIV AMO, FTCAMPBELL, KY(NO PID)(QC000000)

2401-Nov-1985

H, IINSTALLATION OF HM020 INTERNALAUXILIARY FUEL SYSTEM

55-1520-H60-50-60MWO:

Mnt LevelPriority

DN23-Jan-1989


3001-Nov-1989

H, IMODIFICATION OF MAIN ROTOR HEADANTI-FLAP BRACKETS (UH-60A ANDEH-60A HELICOPTERS)

55-1520-237-50-44MWO:

Mnt LevelPriority

DR29-Mar-2005

1-108TH AVN,CO.D (LATEENTRY)

1001-Oct-2006

SGT REYES,JORGE B

INSTALLATION OF UPPER INFRARED(IR) ANTI-COLLISION LIGHT LENSINSTALLED ON US ARMY UH-60A/L/QAND HH-60L HELICOPTERS

1-1520-237-50-ACLMWO:

Mnt LevelPriority

DN29-Jul-1994

1106TH AVCRADFRESNO, CA(NO PID)(QC000000)

18604-Aug-1997

H, IINSTALLATION OF ELECTRICALLYHEATED GLASS CENTER WINDSHIELD(UH-60A HELICOPTER)

1-1520-237-50-70MWO:

Mnt LevelPriority

DN01-May-1994


12404-Dec-1997

H, IINCORPORATION OF IMPROVED FIREEXTINGUISHER CIRCUIT ANDHELLFIRE CONNECTOR (UH-60 A/LAND EH-60A)

1-1520-237-50-66MWO:

Mnt LevelPriority

DN04-Apr-1994


269604-Dec-1997

H, IINCORPORATION OF UH-60AREFURBISHMENT/STANDARDIZATIONPROGRAM

1-1520-237-55-7MWO:

Mnt LevelPriority

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

DA FORM 2408-5 E, OCT 91 EQUIPMENT MODIFICATION RECORD

PIDMWODATE HRS






DN07-Mar-1995


5504-Dec-1997

H, IINCORPORATION OF IMPROVEDAIRSPEED SYSTEM (UH-60AHELICOPTERS)

1-1520-237-50-22MWO:

Mnt LevelPriority

OM24-Sep-2002

DYNCORP OLRKILLEEN TX(GD6707)(QC000000)

204-Mar-2003

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

UH-60-02-ASAM-11MWO:

Mnt LevelPriority

DR13-Apr-2001


8004-Mar-2003

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

1-1520-237-50-77MWO:

Mnt LevelPriority

DN01-Aug-1991

DYNCORP, OLR,FT HOOD, TX(NO PID)(QC000000)

3.505-Nov-1990

H, ISTAB GROUNDING STRAP55-1520-237-50-54MWO:Mnt LevelPriority

DR11-Aug-2000

DYNCORP OLRKILLEEN, TX(JC1523)(QC000000)

306-Aug-2001

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

1-1520-237-50-79MWO:

Mnt LevelPriority

OT07-Jul-1989

W3EM64 (NOPID) (QC000000)

406-Sep-1989

H, ITBO/REPLACE LIFE REVISIONSCHEDULE

55-1520-237-20-104MWO:

Mnt LevelPriority

DR14-Aug-2009

FT. HOOD AFMA 91207-Dec-2010

CIV NOVOA,ORLANDO

INTEGRATED VEHICLE HEALTHMANAGEMENT SYSTEM (IVHMS)

1-1520-237-50-100.MWO:

Mnt LevelPriority

DR13-Oct-2009


CIV NOVOA,ORLANDO

MODIFICATION: INSTALLATION OFPREPLANNED PRODUCTIMPROVEMENT FOR THE COMMONMISSILE WARNING SYSETM (CMWSP3I) ON UH-60A/L HELICOPTERS

1-1520-237-50-97(R1)MWO:

Mnt LevelPriority

DR15-Jul-2009


CIV NOVOA,ORLANDO

COMMON MISSILE WARNING SYSTEM(CMWS) FIFTH SENSOR

1-1520-237-50-99 (D1)MWO:

Mnt LevelPriority



PIDMWODATE HRS






DR25-Apr-2006


CIV NOVOA,ORLANDO

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE AN/APX-118 TRANSPONDER MODE STRANSPONDER (CXP) ON UH-60A/LAIRCRAFT (NSN 1520-01-035-0266)(NSN 1520-01-298-4532)

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

Mnt LevelPriority

DN02-Jun-2006

MISSOURIAVCRADSPRINGFIELD,MO

4008-Jul-2009

SGT LEBBIN,DAVID L

INSTALLATION OF RESCUE HOISTCABLE GUARD DEFLECTOR

1-1520-237-50-MEDMWO:

Mnt LevelPriority

FN13-Jun-2013

AASF #2 SALINAKS

411-FEB-2014

SGT LEBBIN,DAVID L

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

1-1520-237-20-2MWO:

Mnt LevelPriority

DM01-Sep-1991


211-Mar-1993

H, IIMPROVED ENGINE COWLINGRELEASE HANDLE ASSEMBLY

1-1520-237-50-64MWO:

Mnt LevelPriority

FR03-Oct-2007

AASF #2 SILINAKS

5011-Nov-2009

SGT LEBBIN,DAVID L

INSTALLATION OF OPTION II CABINHEATER SYSTEM

SSI NO. 50-36 REV.AMWO:

Mnt LevelPriority

DN30-Apr-1997

DYNCORP-OLR,KILLEEN, TX(LM2968)(QC000000)

5212-Apr-1990

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

1-1520-237-50-56MWO:

Mnt LevelPriority

DN05-Oct-1994


18412-Apr-1990

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

1-1520-237-50-62MWO:

Mnt LevelPriority

DR08-Nov-1996

DYNCORP-OLR,KILLEEN, TX(LM2968)

17812-Apr-1990

H, IINSTALLATION OF AN/ASN-128BDOPPLER/GPS NAVIGATION SYSTEMIN UH-60A/L HELICOPTER

1-1520-237-50-75MWO:

Mnt LevelPriority

DN31-Oct-1996


3512-Apr-1994

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

1-1520-237-50-74MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN26-Mar-1984

OLR FTCAMPBELL, KY(NO PID)(QC000000)

20012-Dec-1984

H, IMODIFICATION TO INSTALL ROTORBLADE DE-ICE KIT (UH-60AHELICOPTERS)

55-1520-237-50-5MWO:

Mnt LevelPriority

DN26-Mar-1984

DAAJ, FTCAMPBELL, KY(NO PID)(QC000000)

412-Dec-1984

H, IIMPROVED ANTI-ICING MODULATINGVALVE SENSE LINE INSTALLATION(UH-60A HELICOPTERS)

55-1520-237-50-3MWO:

Mnt LevelPriority

DR01-Nov-2006

1-108TH AVN,CO. D.(JR759141)

1012-Jul-2007

H, IMODIFICATION FOR THE DAULINSTALLATION OF ATTITUDEHEADING REFERENCE UNITS (AHRU)

1-1520-237-50-94MWO:

Mnt LevelPriority

DN08-Nov-1984

SIKORSKI (NOPID) (QC000000)

312-Jun-1984

H, IKICK PLATES55-1520-237-50-10MWO:Mnt LevelPriority

DN24-Oct-1984


112-Jun-1984

H, IMAIN ROTOR DAMPER CABLES55-1520-237-50-17MWO:Mnt LevelPriority

DN08-Nov-1984


112-Jun-1984

H, ICHAFF DISP.55-1520-237-50-30MWO:Mnt LevelPriority

DN08-Nov-1984


1.512-Jun-1984

H, ISTAB. GROUND55-1520-237-50-29MWO:Mnt LevelPriority

DN24-Oct-1984


112-Jun-1984

H, IMIXER RET55-1520-237-50-27MWO:Mnt LevelPriority

DU10-Aug-1987

DYNCORP FTHOOD, TX (NOPID) (QC000000)

614-Dec-1987

H, IINCORPORATION OF STABILATORSLEW-UP SWITCH (UH-60AHELICOPTER)

55-1520-237-50-46MWO:

Mnt LevelPriority

DM14-Apr-2008

AASF #2 SALINA 814-FEB-2014

SGT LEBBIN,DAVID L

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

1-1520-237-30-3MWO:

Mnt LevelPriority

DM30-Jan-2003

PROJECT/OLR(EAST) HAAF,GA (PG4153)(QC000000)

16014-Sep-2005

H, IINSTALLATION OF BLUE FORCETRACKER

1-1520-237-50-BFTMWO:

Mnt LevelPriority



PIDMWODATE HRS






DN23-Apr-2004


2514-Sep-2005

H, IINSTALLATION OF BALLISTICPROTECTION SYSTEM

1-1520-237-50-BPSMWO:

Mnt LevelPriority

DR21-Apr-2006


72014-Sep-2005

H, IINSTALLATION OF COMMON MISSILEWARNING SYSTEM (CMWS) ANDIMPROVED COUNTERMEASURESDISPENSER SYSTEM (ICDS)

1-1520-237-50-CMWSMWO:

Mnt LevelPriority

DR03-Dec-2005


3114-Sep-2005

H, IINSTALLATION OF ELECTRONIC DATAMANAGEMENT (EDM) SYSTEM FORBLUE FORCE TRACKING

1-1520-237-50-EDMMWO:

Mnt LevelPriority

DR28-Feb-2005


7514-Sep-2005

H, IMODIFICATION 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

DM08-Feb-2005


28914-Sep-2005

H, IENGINE INLET BARRIER FILTER1-1520-237-50-90MWO:Mnt LevelPriority

DN30-Jun-2004

FT HOODPROJECT OLR(DW828962)

7615-Sep-2008

H, IMODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE DOPPLERGPS NAVIGATION SET (DGNS)

1-1520-237-50-92MWO:

Mnt LevelPriority

DN15-Jan-1989

DYNCORP (NOPID) (QC000000)

1216-Nov-1989

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

1-5945-237-50-1MWO:

Mnt LevelPriority

DN17-Jan-1989


216-Nov-1989

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

55-1520-237-50-52MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN09-Jun-1988


8016-Nov-1989

H, IINCORPORATION OF STABILATORAMPLIFIER IMPROVEMENTS(INCLUDES MODIFICATION OFSTABILIZATION TEST SET) (UH-60AHELICOPTERS)

55-1520-237-50-42MWO:

Mnt LevelPriority

DR04-Jun-2001


30017-Apr-2002

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

1-1520-237-50-76MWO:

Mnt LevelPriority

DM18-Apr-1988


117-Nov-1988

H, IINSTALLATION OF IMPROVEDCARTRIDGE ACTUATED DEVICE

55-4030-237-50-1MWO:

Mnt LevelPriority

DR15-Jul-1985

PROJ OLR, FTCAMPBELL, KY(NO PID)(QC000000)

4017-Sep-1986

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

55-1520-237-50-34MWO:

Mnt LevelPriority

DM12-Aug-1983

OLR FTCAMPBELL, KY(NO PID)(QC000000)

4818-Jul-1983

H, IUPPER CARGO TRACK ASSEMBLY55-1520-237-50-12MWO:Mnt LevelPriority

DN15-Jan-1991


818-Jul-1991

H, IINCORPORATION OF ENGINE DRIVESHAFT BALANCING PROCEDURE (UH-60A/EH-60A HELICOPTERS)

55-1520-237-50-58MWO:

Mnt LevelPriority

DN01-Sep-1986

DYNCORP FTCAMPBELL, KY(NO PID)(QC000000)

105419-Jan-1988

H, IINCORPORATION OF ANVISCOMPATIBLE LIGHTING SYSTEM

55-1520-237-50-20MWO:

Mnt LevelPriority

DN30-Apr-1987

DYNCORP FTCAMPBELL, KY(NO PID)(QC000000)

6719-Jan-1988

H, IINCORPORATION OF WIRE STRIKEPROTECTION SYSTEM (WSPS) (UH-60A HELICOPTER)

55-1520-237-50-24MWO:

Mnt LevelPriority

DN15-Nov-1990


419-Jul-1991

H, IINSTALLATION OF IMPROVEDTIEDOWN RING EYEBOLT (UH-60A/LAND EH-60A)

1-1520-237-50-61MWO:

Mnt LevelPriority



PIDMWODATE HRS






DM22-Feb-1991

DYNCORP, OLRFT HOOD, TX(NO PID)(QC000000)

83219-May-1993

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

1-1520-237-50-59MWO:

Mnt LevelPriority

DR21-Jun-2006

FT HOOD OLRREGIONKILLEEN TX

21520-Aug-2008

SGT LEBBIN,DAVID L

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

BFT60-001MWO:

Mnt LevelPriority

DR30-Apr-1991


13220-May-1993

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

1-1520-237-50-63MWO:

Mnt LevelPriority

DU30-Mar-1987

LSSI (NO PID)(QC000000)

4021-Apr-1986

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

55-1520-237-50-36MWO:

Mnt LevelPriority

DN01-Oct-1990


1221-Jun-1990

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

55-1520-237-50-39MWO:

Mnt LevelPriority

DN15-Aug-1988

DYNCORP, OLR,FT HOOD TX (NOPID) (QC000000)

2421-Jun-1990

H, IMODIFICATION OF WIRE STRIKEPROTECTION SYSTEM (WSPS) (UH/EH-60A HELICOPTER)

55-1520-237-50-47 C1MWO:

Mnt LevelPriority

DO04-Apr-1986

DYNCORP, OLR,FT HOOD TX (NOPID) (QC000000)

521-Jun-1990

H, IINSTALLATION OF MODIFIED OILSHIELDS

55-1520-237-50-53MWO:

Mnt LevelPriority

DM15-Nov-1989


2221-Jun-1990

H, IMODIFICATION OF DOWEL PINRETENTION MAIN GEARBOX

55-1520-237-50-43MWO:

Mnt LevelPriority

DN01-Feb-1993


43621-Sep-1994

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

1-1520-237-50-69MWO:

Mnt LevelPriority



PIDMWODATE HRS






DM11-Oct-1983

PROJECT OLRFT C KY (NOPID) (QC000000)

0.523-Feb-1984

H, IIMPROVED CARGO HOOK KEEPERINSTALLATION FOR UH-60AHELICOPTERS

55-1520-237-50-15MWO:

Mnt LevelPriority

DN01-Oct-1982


2823-Feb-1984

H, IINCORPORATION OF A ENGINEPRIME/BOOST SYSTEM (UH-60AHELICOPTERS)

55-1520-237-50-7MWO:

Mnt LevelPriority

DM01-Apr-1985


15223-Feb-1984

H, IINCORPORATION OF FUEL BOOSTPUMP SYSTEM

55-1520-237-50-25MWO:

Mnt LevelPriority

DN15-Dec-1984


225-Jan-1985

H, IMODIFICATION OF MAIN ROTORSLIDING COVER (UH-60AHELICOPTERS)

55-1520-237-50-32MWO:

Mnt LevelPriority

DU13-Jun-1985


425-Sep-1985

H, IMODIFICATION OF IMPROVED MAINROTOR-TAIL ROTOR PITCH CONTROLROD BOLTS (UH-60A HELICOPTERS)

55-1520-237-50-31MWO:

Mnt LevelPriority

DN24-Mar-1988


126-Apr-1988

H, IMODIFICATION OF WIRE STRIKEPROTECTION SYSTEM (WSPS) (UH/EH-60A HELICOPTER)

55-1520-237-50-47MWO:

Mnt LevelPriority

DU31-May-1995


3629-Aug-1995

H, IMODIFICATION OF THE ENGINE TRIMBALANCE HARDWARE (EH/UH-60AAND UH-60L HELICOPTERS)

1-1520-237-50-73MWO:

Mnt LevelPriority

DU30-Nov-1983


130-Dec-1983

H, ICARGO HOOK EXTERNAL SPRINGRETROFIT KIT

55-1520-237-50-28MWO:

Mnt LevelPriority




8023495HELICOPTER, 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

A001 10 Feb 20167H-60-09-ASAM-11CARGO DOOR WINDOWJETTISON LEVER

03 Feb 2016D

A020 5630.710TM 1-1520-237-PMDPERFORM M/R SPINDLE LUGS,M/R CUFF, TIP CAPSINSPECTION

5620.7H

A022 10 Feb 201614TM 1-1520-237-23-914 DAY FLYABLE STORAGEENGINE RUN UP

27 Jan 2016D

A092 28 Feb 201630TM 11-6140-203-23&P30 DAY SLAB BATTERYINSPECTION (D8565/11-1)

29 Jan 2016D

A100 19 Feb 201630DA PAM 738-751#1 ENGINE HISTORY RECORDERREADING DUE

20 Jan 2016D

A101 19 Feb 201630DA PAM 738-751#2 ENGINE HISTORY RECORDERREADING DUE

20 Jan 2016D

A103 13 Feb 201630TM 1-1500-344-23AIRCRAFT WASH DUE 14 Jan 2016D

A110 5636.740TM 1-1520-237-PMSPMS 40 HOUR INSPECTION 5596.7H

A115 13 Feb 201630TM 1-1520-237-23-12LUBE REQUIRMENTS 14 Jan 2016D

A115 5660.740TM 1-1520-237-23-12LUBE REQUIRMENTS 5620.7H

A116 5934.2360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

5574.2H

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

05 Jun 2015M

A117 5934.2360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 5574.2H

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

A160 15 Mar 201690TM 1-1520-237-23-1290 DAY CORROSIONINSPECTION

16 Dec 2015D

A177 30 Mar 201690AR 95-190 DAY REVIEW/UPDATE OF 365-4 ENTRIES

31 Dec 2015D

A200 5636.7120H-60-08-ASAM-11120 HOUR INSPECTIONREQUIREMENTS ON DOWEL PIN

5516.7H

A210 5636.7120TM 1-1520-237-23-12120 HOUR INSPECTIONREQUIREMENTS

5516.7H

A211 5934.2360H-60-10-AMAM-11APU OIL SAMPLE 5574.2H

A211 05 Jun 201612H-60-10-AMAM-11APU OIL SAMPLE 05 Jun 2015M

A213 5647.7120TM 1-2840-248-23ENGINE COMPRESSORCLEANING

5527.7H

A214 5636.7120TM 1-1520-237-23-12CLEAN TAIL WHEEL ADAPTER 5516.7H

A222 13 Apr 2016360TM 1-1680-377-13&PAMSS SURVIVAL KITINSPECTION

19 Apr 2015D

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 28 Apr 2016120MWO 1-1520-237-50-77INSPECT BATTERYCOMPARTMENT FORCORROSION (SLAB)

30 Dec 2015D

A295 5657360TM 1-1520-237-23-12STABILATOR ACTUATOR ASSYLUBE

5297H

A296 5657360TM 1-1520-237-23-12STABILATOR INSPECTION 5297H

A298 5938.9360TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 5578.9H

A298 07 Jun 201612TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 07 Jun 2015M

A299 5934.2360TM 1-1520-237-23-12SWASHPLATE LUBE 5574.2H

A299 04 Jun 201612TM 1-1520-237-23-12SWASHPLATE LUBE 04 Jun 2015M

A320 5657360TM 1-2840-248-23ENGINE INSPECTION &CLEANING

5297H

A400 5657720TM 1-1520-237-PMIPMI-1 4937H

A401 6017720TM 1-1520-237-PMIPMI-2 5297H

A408 6017720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-2, AREA 5 AND 6)

5297H

A410 5657720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-1, AREA 1 THRU 4)

4937H

A415 6017720H-60-10-AMAM-11MAIN GEARBOX OIL SAMPLE-PART # 073, 074, 076

5297H

A470 6109.61500TM 1-1520-237-23-12REPLACE NUMBER TWOCROSSFEED VALVE

4609.6H

A471 71272160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

4967H

A472 71272160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

4967H

A473 71272160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

4967H

A476 9031.95000TM 1-1520-237-23-12REPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

4031.9H

A477 9609.65000TM 1-1520-237-23-12REPLACEMENT OF STABILATORACTUATOR BOLTS

4609.6H

A480 9031.95000TM 1-1520-237-23-12REPLACE PIVOT BOLT 70400-08159-101,102,103,104

4031.9H

A485 9031.95000TM 1-1520-237-23-12REPLACE BELLCRANK BOLT70400-08159-105,106,107,108

4031.9H

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

19 Jan 2016M

A501 10 Mar 20166TM 1-1520-237-23-12MAIN ROTOR BLADE PRESSURECHECK

10 Sep 2015M






7. FREQUENCY 4.




INSP

A502 01 Apr 20166TM 1-1520-237-23-12INSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

01 Oct 2015M

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

11 Sep 2015M

A532 14 Apr 201612TM 1-1500-204-23-4COMPASS SWING / RMI 14 Apr 2015M

A533 24 Jan 201612TM 1-1520-237-23-12PITOT STATIC SYSTEMINSPECTION

24 Jan 2015M

A534 28 Feb 201724TM 1-1500-204-23-1FIRST AID KIT INSPECTION 28 Feb 2015M

A538 09 Oct 201612TM 1-1520-237-23-12FAT/OAT GAUGEINSPECTION/TEST

09 Oct 2015M

A541 16 May 201612TM 1-1520-237-23, C4REPLACE DIGITAL CLOCKBATTERY

16 May 2015M

A550 04 Aug 201612AWR1346R16IVHUMS BATTERYREPLACEMENT

04 Aug 2015M

A553 09 Jun 201612AR 95-1AIRCRAFT WEIGHINGINVENTORY (365-1)

09 Jun 2015M

A580 27 Aug 201624TM 11-6140-203-23&PRETURN SLAB TO AVIM FORCAPACITY CHECK (VEREY 24MONTH)

27 Aug 2014M

A621 20 Jun 201724AR 95-1AIRCRAFT WEIGHING CLASS 2 20 Jun 2015M

A625 22 Nov 201760TM 11-6140-203-23&PREPLACEMENT OF SLABBATTERY (SLAB)

22 Nov 2012M

A630 01 May 2022114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Nov 2012M

A633 01 May 2022114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Nov 2012M

A638 01 May 2022114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

01 Nov 2012M

A640 01 May 2022114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

01 Nov 2012M

A642 01 Jul 202172TB 9-1300-385CARGO HOOK CARTRIDGEREPLACEMENT, DODIC MJ21

01 Jul 2015M

A648 28 Dec 2022180TM 1-1520-237-23REPLACE T/R SPRING CAPSULEASSY

28 Dec 2007M

A665 08 Nov 201648H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

08 Nov 2012M

A670 25 Sep 201648TM 1-1520-237-23-1CABIN TUB INSPECTION 25 Sep 2012M

A673 08 Nov 201648TM 1-1520-237-23-12FUEL CELL CORROSIONINSPECTION

08 Nov 2012M

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

A695 6157.2720H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

5437.2H






7. FREQUENCY 4.




INSP

A695 04 Jun 201848H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

04 Jun 2014M

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

0H

E040 29 Mar 201690TM 11-5841-294-12APR-39 RADAR/LASERWARNING OPNL CHECK, 5841-01-236-8951

30 Dec 2015D

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

12 Jan 2016D

E155 13 Apr 2016180TM 11-5810-262-23KY-58 BATTERY REPLACEMENT 16 Oct 2015D

E300 11 Feb 201630AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

12 Jan 2016D

E300 5740.7120AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

5620.7H

E320 22 Jan 2017360AWR 1516 FOR ELTEMERGENCY LOCATORTRANSMITTER G-SWITCH (EBC-406HM)

28 Jan 2016D

E325 11 Mar 201960AWR 1516R2 FOR ELTREPLACEMENT OF ELTBATTERY PN GS-46

11 Mar 2014M




h

CONDITION ITEMS

kjifdcba g.

RMVL HR

RMVL HRSWUC HRS)COMPO/H

NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE

SINCEPREVSER NO.ANDNOMENCLATURE DUE

REPLACE

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

3. PART NUMBER ORMODEL

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

Report Date: 1/1225-Feb-2016

80234951520010350266 00HELICOPTER, UTILITY

156001095713502C12D

00UNK349570219-05001-042TAIL CONE FITTING CCCC COND COND

162001231183103A01

47755169C0010270970250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001231183103A01

6395169IA0157070250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001421089003B01

6563632BMC-33570250-13101-044SHOCK ABSORBER (TAIL) CCCC COND COND

161501161437305A01I02

16655297C32406979SB7001-048SPHERICAL BEARINGASSY

CCCC COND COND

165001285302405A01Z

446446100070170106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z

17444610R106-0083370106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z


165001285302405A01Z


531501537465205A02H

04610B9410558870103-08108-041SOLID BLADE PIN CCCC COND COND

531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


161501199764605A03A

04419015152-175270104-08000-050SWASHPLATE ASSY CCCC COND COND

161501078571806A11

4992468A258-0039070351-08080-043ACCESSORY 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






161501078571806A11

5252446A258-0443070351-08080-043ACCESSORY MODULE CCCC COND COND

161501503311506A

27434419A265-0035670351-08100-076MAIN TRANSMISSIONMODULE

CCCC COND COND

161501353382506E

04419A264-0762970351-08001-049INPUT MODULE CCCC COND COND

161501353382506E

04419A264-0764470351-08001-049INPUT MODULE CCCC COND COND

168001074515206F

04424A005-0354670357-06300-042INTERMEDIATE GEARBOX CCCC COND COND

161501376508906G01

04419A006-0315470358-06600-046TAIL ROTOR GEARBOXASSY

CCCC COND COND

161501081277506H06

00A271-0028370361-03001-045SHAFT ASSY, T/R DRV SEC1

CCCC COND COND

161501158951706H08

04610WG30027-00059

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

CCCC COND COND

161501082650006H09

00A272-0082670361-05001-045SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501294167406H09

04967UNK70361-05001-050DRIVESHAFT ASSY SECTIII, IV, V

CCCC COND COND

161501158952206H09

04301WG10208-00210

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

CCCC COND COND

NSN PENDING06H11

00A2730028170361-05001-044SHAFT ASSY, T/R DRV SEC6

CCCC COND COND

161501158578806H12

04293WG10564-00042

70361-06002-047SHAFT ASSY, T/R DRV SEC7

CCCC COND COND

432001207722807A01 2

7934831185923ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01 BU

15224301K0675A53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01 1

11965166252896ABR70652-02300-050PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

481001102247307B05A

1439461018663213850-3-1VALVE, SOLENIOD CCCC COND COND

481001102247307B05A

0292825303213850-3-1VALVE, SOLENIOD CCCC COND COND

165001222431607B11

80246134050A3197170-5ACCUMULATOR CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






168001342049608B20

168246103665100-601561-000PANEL INDICATOR (PDU) CCCC COND COND

168001342049608B20

16824610676100-601561-000PANEL INDICATOR (PDU) CCCC COND COND

611501114969609A01

02928610E28B302-8-DMGENERATOR CCCC COND COND

611501114969609A01

03658124-A220770550-02031-111GENERATOR CCCC COND COND

168001310225911C21

0546043565270400-02300-048MIXER ASSEMBLY CCCC COND COND

168001261204411D25

30195485B2920355070400-06641-117STABILATOR ACTUATOR CCCC COND COND

168001261204411D25

10454851605DL2155M20STABILATOR ACTUATOR CCCC COND COND

599601316274311D26

25304610265170902-02001-048STABILATOR AMPLIFIER CCCC COND COND

599601316274311D26

45464610P52570902-02001-048STABILATOR AMPLIFIER CCCC COND COND

299501169529115A04

168246100282163290-100ENGINE SEQUENCINGUNIT

CCCC COND COND

599601415867319D01A

044241092BBAM-7351/URCAMPLIFIER, RADIOFREQUENCY

CCCC COND COND

584101421416219E05A

054031075AAHG7209AD01RECEIVER-TRANSMITTER,RADAR

CCCC COND COND

584101245909219E05C

05403155BSM-C-967226INDICATOR HEIGHT CCCC COND COND

660501503528419E06A

05463342765100-20ATTITUDE HEADINGREFERENCE UNIT

CCCC COND COND

661001490516852A

724461006075668825050-1-001AUTOMAT FLT CONTCOMPUTER

CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






SIGNIFICANT HISTORICAL EVENTS7.




kjigfdcbaRMVL HR RMVL HRS

NOMEN HRS)COMPO/HO/HLOCATIONNSNWUC

he (ACFTLIFESINCEPRESER NO.ANDAND

INST HRSP/N DUEREPLACE

INST HRSTIMENO.COMPONENTNOMENCLATURE

NOMEN REP.O/H OCOMP6.

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

Report Date:

TIME CHANGE COMPONENTS5/1225-Feb-2016

00

156001081924402C15J19942

B33000027 5355529770209-06051-043TAIL PYLON FITTING 0020000

161501450483405A01A8732

15152-00956 978461070103-08112-047HUB, M/R ROTOR ASSY 005100

161501442692605A01I BLUE11367

A001-06402 0496770102-08200-069MAIN ROTOR SPINDLEASSY

006400

161501442692605A01I11010

A001-07635 0461070102-08200-069MAIN ROTOR SPINDLEASSY

006400

161501442692605A01I8833

A00102249 2790522370102-08200-069MAIN ROTOR SPINDLEASSY

006400

161501442692605A01I11066

A00104735 631529770102-08200-069MAIN ROTOR SPINDLEASSY

006400

161501074515105A01L17308

A286-00621 1302461070351-08186-043MAIN ROTOR SHAFTEXTENDER

0014000

161501127738805A01T13956

015152-00406 3936489270107-08400-046BIFILAR, M/R ROTORASSY

0013000

161501106190305A0214210

A007-14816 0461070150-09100-043MAIN ROTOR BLADEASSY

009600

161501106190305A0211474

A00702644 3476535070150-09100-043MAIN ROTOR BLADEASSY

009600

161501106190305A0210665


009600

161501106190305A0213100


009600

161501113818805B028310

A009-05401 6300461070101-31000-043TAIL ROTOR BLADEASSY

0010000

161501113818805B02 TAIL10899

A00900502 4178507770101-31000-043TAIL ROTOR BLADEASSY

0010000

161501083681206G01B12541

A257-00336 4069461070102-11101-042O/B RETENTION PLATE(T/R)

0012000

311001329857306H18B F7130

B626-55819 5475517SB1138-102BEARING BALLANNULAR

002160

311001329857306H18B A7127

B626-80322 5505517SB1138-102BEARING BALLANNULAR

002160

414101329342806H237130

9F930033SB 3804461070361-03005-107FAN AXIAL 012520

156001129125607A2417610

C11205382 0461070410-02500-049SAS ACTUATOR 0013000

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

156001129125607A2417610

C11205730 0461070410-02500-049SAS ACTUATOR 0013000

156001129125607A2417610

C11205762 0461070410-02500-049SAS ACTUATOR 0013000

161501141753211C236770

233-03809 956461070400-06100-042TAIL ROTOR PITCHCHANGE SHAFT

012160

165001305695411C2513318

B300-01290 2101441970410-06520-046SERVO ASSY, TAILROTOR

0011000

165001143122611D01 FWD25673

B30300526B 3337461070410-02820-054MAIN ROTOR PRIMARYSERVO

0024400

165001143122611D01 LAT25831

B30302899 3179461070410-02820-054MAIN ROTOR PRIMARYSERVO

0024400

165001143122611D01 AFT27507

B30309316B 1503461070410-02820-054MAIN ROTOR PRIMARYSERVO

0024400

156001158968511D0413956

A845-026343 3936489270400-08102-045AFT BELLCRANK 0013000

156001082921311D0517000

A39100263 6670400-08112-044AFT TIE ROD SUPTFITTING

0017000

168001164416011D066619

MM00535 0441970400-08111-042AFT TIE ROD ASSY 002200

156001286887011D076846

39001411 0244670400-08117-049AFT BELLCRANK SPTASSY

004400

304001287243811D0815610

1515202403 0461070400-08151-061LATERAL SWASHPLATELINK

0011000

161501078569511D097737

A28900535 2373461070400-08150-043LATERAL SERVOBELLCRANK

005500

168001158965311D1111000

B346-00301 6670400-08104-048AFT WALKING BEAM 0011000

156001289269711D1318310

344-01260 0431070400-08115-046LEFT TIE ROD ASSY 0014000

156001296948611D145946

28800063 0244670400-08114-051RIGHT TIE ROD ASSY 003500

168001090204811D1515356

D35500236 2090244670400-08101-044FORWARD BELLCRANK 0015000

156001221261911D169232

B367-04248 0363270400-08162-042FWD BELLCRANK SPTASSY

005600

156001095713211D17 L/H O/B20000

UNK3495 0070219-02134-046SERVO BEAM FITTING 0020000













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 8023495 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 8 of 12

25-Feb-2016

COND COND

156001095713502C12D

00TAIL CONE FITTING UNK349570219-05001-042 CCCC

20000 19942

156001081924402C15J

53555297TAIL PYLON FITTING B3300002770209-06051-043 00

COND COND

162001231183103A01

47755169FWD FIXED GEARSHOCK

C0010270970250-12051-045 CCCC

COND COND

162001231183103A01


IA0157070250-12051-045 CCCC

COND COND

162001421089003B01

6563632SHOCK ABSORBER(TAIL)

BMC-33570250-13101-044 CCCC

5100 8732

161501450483405A01A

9784610HUB, M/R ROTOR ASSY 15152-0095670103-08112-047 00

COND COND

161501161437305A01I02

16655297SPHERICAL BEARINGASSY

C32406979SB7001-048 CCCC

6400 11367

1615014426926 BLUE05A01I

04967MAIN ROTOR SPINDLEASSY

A001-0640270102-08200-069 00

6400 11010

161501442692605A01I


A001-0763570102-08200-069 00

6400 8833

161501442692605A01I


A0010224970102-08200-069 00

6400 11066

161501442692605A01I


A0010473570102-08200-069 00

14000 17308

161501074515105A01L

13024610MAIN ROTOR SHAFTEXTENDER

A286-0062170351-08186-043 00

13000 13956

161501127738805A01T

39364892BIFILAR, M/R ROTORASSY

015152-0040670107-08400-046 00

COND COND

165001285302405A01Z

44644610DAMPER ASSY, M/R 0070170106-08100-046 CCCC

COND COND

165001285302405A01Z

17444610DAMPER ASSY, M/R R106-0083370106-08100-046 CCCC

COND COND

165001285302405A01Z


COND COND

165001285302405A01Z


9600 14210

161501106190305A02

04610MAIN ROTOR BLADEASSY

A007-1481670150-09100-043 00

9600 11474

161501106190305A02


A0070264470150-09100-043 00

9600 10665

161501106190305A02


A0070997170150-09100-043 00

9600 13100

161501106190305A02


A0071184770150-09100-043 00

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

25-Feb-2016

COND COND

531501537465205A02H

04610SOLID BLADE PIN B9410558870103-08108-041 CCCC

COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

161501199764605A03A

04419SWASHPLATE ASSY 015152-175270104-08000-050 CCCC

10000 8310

161501113818805B02

63004610TAIL ROTOR BLADEASSY

A009-0540170101-31000-043 00

10000 10899

1615011138188 TAIL05B02

41785077TAIL ROTOR BLADEASSY

A0090050270101-31000-043 00

COND COND

161501078571806A11

4992468ACCESSORY MODULE A258-0039070351-08080-043 CCCC

COND COND

161501078571806A11

5252446ACCESSORY MODULE A258-0443070351-08080-043 CCCC

COND COND

161501503311506A

27434419MAIN TRANSMISSIONMODULE

A265-0035670351-08100-076 CCCC

COND COND

161501353382506E

04419INPUT MODULE A264-0762970351-08001-049 CCCC

COND COND

161501353382506E

04419INPUT MODULE A264-0764470351-08001-049 CCCC

COND COND

168001074515206F

04424INTERMEDIATEGEARBOX

A005-0354670357-06300-042 CCCC

COND COND

161501376508906G01

04419TAIL ROTOR GEARBOXASSY

A006-0315470358-06600-046 CCCC

12000 12541

161501083681206G01B

40694610O/B RETENTION PLATE(T/R)

A257-0033670102-11101-042 00

COND COND

161501081277506H06

00SHAFT ASSY, T/R DRVSEC 1

A271-0028370361-03001-045 CCCC

COND COND

161501158951706H08


WG30027-0005970361-03009-047 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 10 of 12

25-Feb-2016

COND COND

161501082650006H09

00SHAFT ASSY, T/R SEC3,4,5

A272-0082670361-05001-045 CCCC

COND COND

161501294167406H09

04967DRIVESHAFT ASSY SECTIII, IV, V

UNK70361-05001-050 CCCC

COND COND

161501158952206H09

04301SHAFT ASSY, T/R SEC3,4,5

WG10208-0021070361-05001-051 CCCC

COND COND

NSN PENDING06H11


A2730028170361-05001-044 CCCC

COND COND

161501158578806H12


WG10564-0004270361-06002-047 CCCC

2160 7130

3110013298573 F06H18B

5475517BEARING BALLANNULAR

B626-55819SB1138-102 00

2160 7127

3110013298573 A06H18B

5505517BEARING BALLANNULAR

B626-80322SB1138-102 00

2520 7130

414101329342806H23

38044610FAN AXIAL 9F930033SB70361-03005-107 01

COND COND

4320012077228 207A01

7934831PUMP MODULE ASSY,HYDRAUL

185923ABR53023-06 CCCC

COND COND

4320012077228 BU07A01


K0675A53023-06 CCCC

COND COND

4320012077228 107A01


252896ABR70652-02300-050 CCCC

13000 17610

156001129125607A24

04610SAS ACTUATOR C1120538270410-02500-049 00

13000 17610

156001129125607A24

04610SAS ACTUATOR C1120573070410-02500-049 00

13000 17610

156001129125607A24

04610SAS ACTUATOR C1120576270410-02500-049 00

COND COND

481001102247307B05A

14394610VALVE, SOLENIOD 18663213850-3-1 CCCC

COND COND

481001102247307B05A

02928VALVE, SOLENIOD 25303213850-3-1 CCCC

COND COND

165001222431607B11

8024613ACCUMULATOR 4050A3197170-5 CCCC

COND COND

168001342049608B20

16824610PANEL INDICATOR (PDU) 3665100-601561-000 CCCC

COND COND

168001342049608B20

16824610PANEL INDICATOR (PDU) 676100-601561-000 CCCC

COND COND

611501114969609A01

02928GENERATOR 610E28B302-8-DM CCCC

COND COND

611501114969609A01

03658GENERATOR 124-A220770550-02031-111 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 11 of 12

25-Feb-2016

COND COND

168001310225911C21

05460MIXER ASSEMBLY 43565270400-02300-048 CCCC

2160 6770

161501141753211C23

9564610TAIL ROTOR PITCHCHANGE SHAFT

233-0380970400-06100-042 01

11000 13318

165001305695411C25

21014419SERVO ASSY, TAILROTOR

B300-0129070410-06520-046 00

24400 25673

1650011431226 FWD11D01

33374610MAIN ROTOR PRIMARYSERVO

B30300526B70410-02820-054 00

24400 25831

1650011431226 LAT11D01


B3030289970410-02820-054 00

24400 27507

1650011431226 AFT11D01


B30309316B70410-02820-054 00

13000 13956

156001158968511D04

39364892AFT BELLCRANK A845-02634370400-08102-045 00

17000 17000

156001082921311D05

66AFT TIE ROD SUPTFITTING

A3910026370400-08112-044 00

2200 6619

168001164416011D06

04419AFT TIE ROD ASSY MM0053570400-08111-042 00

4400 6846

156001286887011D07

02446AFT BELLCRANK SPTASSY

3900141170400-08117-049 00

11000 15610

304001287243811D08

04610LATERAL SWASHPLATELINK

151520240370400-08151-061 00

5500 7737

161501078569511D09

23734610LATERAL SERVOBELLCRANK

A2890053570400-08150-043 00

11000 11000

168001158965311D11

66AFT WALKING BEAM B346-0030170400-08104-048 00

14000 18310

156001289269711D13

04310LEFT TIE ROD ASSY 344-0126070400-08115-046 00

3500 5946

156001296948611D14

02446RIGHT TIE ROD ASSY 2880006370400-08114-051 00

15000 15356

168001090204811D15

20902446FORWARD BELLCRANK D3550023670400-08101-044 00

5600 9232

156001221261911D16

03632FWD BELLCRANK SPTASSY

B367-0424870400-08162-042 00

20000 20000

1560010957132 L/H O/B11D17

00SERVO BEAM FITTING UNK349570219-02134-046 00

COND COND

168001261204411D25

30195485STABILATOR ACTUATOR B2920355070400-06641-117 CCCC

COND COND

168001261204411D25

1045485STABILATOR ACTUATOR 1605DL2155M20 CCCC

COND COND

599601316274311D26

25304610STABILATOR AMPLIFIER 265170902-02001-048 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 12 of 12

25-Feb-2016

COND COND

599601316274311D26

45464610STABILATOR AMPLIFIER P52570902-02001-048 CCCC

COND COND

299501169529115A04

16824610ENGINE SEQUENCINGUNIT

0282163290-100 CCCC

COND COND

599601415867319D01A

04424AMPLIFIER, RADIOFREQUENCY

1092BBAM-7351/URC CCCC

COND COND

584101421416219E05A

05403RECEIVER-TRANSMITTER, RADAR

1075AAHG7209AD01 CCCC

COND COND

584101245909219E05C

05403INDICATOR HEIGHT 155BSM-C-967226 CCCC

COND COND

660501503528419E06A

05463ATTITUDE HEADINGREFERENCE UNIT

342765100-20 CCCC

COND COND

661001490516852A

7244610AUTOMAT FLT CONTCOMPUTER

06075668825050-1-001 CCCC

7. SIGNIFICANT HISTORICAL DATA




HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 C00102709 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

25-Feb-2016

9000 9394

165001125090703A01A

25942594PISTON, MAIN L/GEARSTR

P0337770250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 C00102709 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

25-Feb-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 IA01570 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

25-Feb-2016

9000 9932

1650011250907 L/SIDE03A01A

4036438PISTON, MAIN L/GEARSTR

C3620256470250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 IA01570 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

25-Feb-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615014426926MAIN ROTORSPINDLE ASSY

70102-08200-069 A001-06402 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

25-Feb-2016

COND COND

3110011589607 BLUE05A01I02

609254ELASTOMERICSPHERICAL BEARING

B324-21863SB7002-048 CCCC

13000 17967

5310011269444 BLUE05A01I04

00M/R SPINDLE NUT F479-0013370102-08105-102 RCRC

6400 11367

5306014606020 BLUE05A01I06

00TIE ROD (M/R SPINDLE) C504-0382738023-10372-101 RCRC

20000 24967

1615012149140 BLUE05A01I07

00HORN ASSEMBLY E241-0024770102-08111-047 RCRC


