UH-60A HELICOPTER, UTILITY 8023489 - GSA … helicopter, utility 8023489 1. aircraft model 2....

NUMBERLOCATIONPIDENTRYORGANIZATION

8.7.DATE

6.REMARKS

4. 5.

UH-60A 8023489HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL

Report Date: of 3803-Mar-2016

SIKORSKY AIRCRAFTAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA SWG. 70400-00003REV. B SYSTEM CONTROLS HAVE BIASED INACCORD. A. LATERAL CONTROL SERVOINPUT ROD P/N 70400-02258-046 HAS BEENSHORTENED 1/4 TURN. B. AFT CONTROLSERVO INPUT ROD P/N 70400-02258-045 HASBEEN LENGTHENED 1/2 TURN. C. FORWARDCONTROL SERVO INPUT ROD P/N 70400-02258-047 HAS BEEN SHORTENED 1/2 TURN. NOTE:WHEN AIRCRAFT RIGGING IS BIASEDRIGGING PIN HOLES ARE TEMPORARILYLOST AT THE ABOVE POINTS (GN1111)

22-Jan-1982 1

NO LOCATION

SIKORSKY AIRCRAFTENGINE STARTERS S/N P-818 & P-802UPDATED AT SIKORSKY AIRCRAFT. BYVENDOR WITH NEW SHAFT STATER P/N 70306-10000-105 (GN1111)

04-May-1982 1

NO LOCATION

394TH TRANS BN (AVIM)UH-60A-82-06/ TB 1-1520-237-20-27 ONE TIMEINSPECTION C/W (HM1111)

04-May-1982 2

APO 09061

394TH TRANS BN (AVIM)TWX UH-60A-82-7 ONE TIME INSP OF MAINMODULE BEAM FASTNERS COMPLETED(LD1111)

22-Jul-1982 1

APO NY 09061

394TH TRANS BN (AVIM)TWX UH-60A-82-8 RECURRING INSP OFENGINE SHAFT ASSY. COMPLETED (LD1111)

22-Jul-1982 2

APO NY 09061

394TH TRANS BN (AVIM)TWX UH-60A-82-9 ONE TIME INSP OF ENGINEGIMBAL MOUNT COMPLETED (LD1111)

22-Jul-1982 3

APO NY 09061

394TH TRANS BN (AVIM)SOF UH-60-82-11 ONE TIME INSP OF SERVOMANIFOLD SCREWS COMPLETED (LD1111)

11-Aug-1982 1

APO NY 09061

394TH TRANS BN (AVIM)SOF UH-60-82-13 ONE TIME INSP OF SERVOINPUT BEARING COMPLETED (LD1111)

16-Aug-1982 1

APO NY 09061

394TH TRANS BN (AVIM)UH-60-82-12 MODIFICATION OF YAW ANDCOLLECTIVE BOOST SERVO COMPLETED(LD1111)

30-Aug-1982 1

APO NY 09061

394TH TRANS BN (AVIM)UH-60-82-14 ONE TIME INSP OF T/R SERVOBOLTS COMPLETED (LD1111)

08-Sep-1982 1

APO NY 09061

394TH TRANS BN (AVIM)UH-60-82-16 ONE TIME INSP OF MIXINGBEARINGS COMPLETED (LD1111)

23-Sep-1982 1

APO NY 09061

394TH TRANS BN (AVIM)SOF UH-60-83-02 ONE TIME INSP OFDIRECTIONAL CONTROL BEARING GAPCOMPLETED (LD1111)

05-Apr-1983 1

APO NY 09061

394TH TRANS BN (AVIM)SOF UH-60-83-04 ONE TIME INSP OF AIR INLETBULLETS FOR CRACKS COMPLETED (LD1111)

25-Apr-1983 1

APO NY 09061

CO B 394TH TRANS BN(AVIM)

SOF UH-60-83-09 ONE TIME INSP OF STABAMPS COMPLETED (AF1111)

11-Oct-1983 1

APO NY 09061


SOF UH-60-83-10/ TB 55-1520-237-20-44 ONETIME REPLACEMENT OF COLLECTIVE BIASTUBE ASSY ROD END BOLT WASHER.COMPLIED WITH AT 150.0 AIRCRAFT HOURS(AF1111)

10-Nov-1983 1

APO NY 09061

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 UH-60-83-12/ TB 55-1520-237-20-46 ONETIME INSPECTION OF TAIL ROTOR SERVOVALVE INPUT LINKAGE COMPLED WITH AT150.0 AIRCRAFT HOURS (AF1111)

14-Nov-1983 1

APO NY 09061


SOF UH-60-84-01 ONE TIME INSP OF XMSNMAST FOR FLAWS COMPLETED (LD1111)

30-Jan-1984 1

APO NY 09061


OCM/ACE PERFORMED AT 0150 A/C HRS, ATHELLINGENGE BY ACE TEAM MEMBER DON ESCHROEDER TSARCOM OCM SEC, ST. LOUIS,MO (DE1111)

16-Feb-1984 1

APO NY 09061


CHAFER DISPENER PLATE (ECP 0196), KICKPLATE (ECP 092R2), STABILATOR GROUNDCABLE (ECP 183), MAIN ROTOR DAMPERCABLE (ECP 223), MIXER BEARINGRETENTION (ECP 239) INSTALLED ON ACFTBY SIKORSKY TEAM AT 152.5 ACFT HRS(RH2650)

22-Mar-1984 1

APO NY 09061


SOF UH-60A-84-02 ONE TIME INSPECTION OFWIRE ROUTING BETWEEN THE #1 AND #2JUNCTION BOXES COMPLETED (JP1111)

27-Mar-1984 1

APO NY 09061


SOF UH-60A-84-06 ONE TIME INSP ON GEARBOX OIL LEVELS COMPLETED (JD1111)

10-May-1984 1

APO NY 09061


SOF UH-60A-84-07 ONE TIME INSP OF ENGINEOUTPUT SHAFTS COMPLETED. ACFT HAS -06BOLTS INSTALLED POINTING AFT.REPLACEMENT REQUIRED BY 255.5 ACFTHRS. (JD1111)

19-May-1984 1

APO NY 09061


SOF UH-60A-84-09 REVISED INSPECTIONREQUIREMENT FOR SOF MSG. UH-60-07COMPLETED (JD1111)

20-May-1984 1

APO NY 09061


SOF UH-60A-84-11 ONE TIME INSPECTION OF"LONGITUDAL LINKS" FOR CRACKSCOMPLETED AT 160.0 ACFT HRS (JD1111)

19-Jul-1984 1

APO NY 09061


SOF UH-60A-84-12 ONE TIME INSPECTION OFM/R SPINDLES FOR DEFECTIVE BOLTSCOMPLETED AT 167.0 ACFT HRS (JD1111)

31-Jul-1984 1

APO NY 09061


SOF UH-60A-84-10 ONE TIME INSPECTION OFTAIL PYLON RADIOUS BLOCKS COMPLETEDAT 171.8 ACFT HRS (JD1111)

04-Sep-1984 1

APO NY 09061


SOF UH-60A-84-13 ONE TIME INSPECTION OFT/R CABLE TURNBUCKLES COMP AT 216.4ACFT HRS (AF1111)

01-Nov-1984 1

APO NY 09061


SOF UH-60A-84-14 ONE TIME INSPECTION FORPROPER INSTALLATION OF T/R CABLESCOMP 216.4 ACFT HRS (AF1111)

01-Nov-1984 2

APO NY 09061


#2 OCM/ACE PERFORMED AT 222 A/C HRS, ATNELLINGEN, GE BY ACE TEAM MEMBER SPAUL AVSCOM OCM SEC, ST. LOUIS, MO(SP1111)

27-Nov-1984 1

APO NY 09061



8.7.DATE

6.REMARKS

4. 5.




ONE TIME INSPECTION OF T700-GE-700ENGINES, FOR GAS GENERATOR ORROTORS. COMPLETED AT 121.6 AIRCRAFTHOURS (LD1111)

19-Dec-1984 1

APO NY 09061


SOF UH-60-84-17 REACURRING INSPECTIONOF MAIN MODULE DOWEL PINS COMPLETEDAT 422.2 AIRCRAFT HOURS (LD1111)

12-Mar-1985 1

APO NY 09061


SOF UH-60-85-01 ONE TIME INSPECTION OFSTAB AMPS FOR PROPER SHAFTSCOMPLETED AT 422.4 AIRCRAFT HOURS(LD1111)

12-Mar-1985 2

APO NY 09061


SOF UH-60-85-02 ONE TIME INSPECTION OFINSTRUMENT MARKINGS COMPLETTED AT422.4 AIRCRAFT HOURS (LD1111)

12-Mar-1985 3

APO NY 09061

CI B 394TH TRANS BN(AVIM)

SOF UH-60-85-03 ONE TIME INSPECTION OFCERTAIN SERIAL # AMPS COMPLETED AT422.4 AIRCRAFT HOURS (LD1111)

12-Mar-1985 4

APO NY 09061


SOF UH-60-85-06 ONE TIME INSPECTION OFALL PRIMARY SERVO'S FOR PROPERRETAINERS COMPLETED AT 228.4 HOURS(LD1111)

25-Mar-1985 1

APO NY 09061


SOF UH-60-85-07 ONE TIME INSPECTION OFALL FLIGHT CONTROL SYSTEMS FOR LOOSEOR MISSING HARDWARE COMPLETED AT235.8 ACFT HRS (LD1111)

16-Apr-1985 1

APO NY 09061


SOF UH-60-85-12 ONE TIME AND REPETITIVEINSPECTION OF PT CASING AND PT NOZZLEBOLTS COMPLETED AT 235.8 ACFT HRS(BW1111)

08-May-1985 1

APO NY 09061


SOF UH-60-85-13 ONE TIME INSPECTION OFM/R SPINDLE ASSY;S P/N 70102-08100-041THRU 059 HISTORICAL DATA COMPLETED AT235.8 AIRCRAFT HOURS (SL1111)

20-May-1985 1

APO NY 09061


SOF UH-85-14 ONE TIME INSP OF M/R SHAFTPART NUMBER -044, 045, 046 COMP 235.8ACFT HRS (PF1111)

22-Jul-1985 1

APO NY 09061


SOF UH-60-85-15 ONE TIME INSP OF MAIN HUBFOR PART NUMBERS 041 + 043 COMPLETEDAT 234.8 ACFT HRS (PF1111)

22-Jul-1985 2

APO NY 09061


SOF UH-60-85-16 ONE TIME CHANGE TOROTOR TACHOMETER RPM LIMITSCOMPLETED AT 235.8 ACFT HRS (PF1111)

22-Jul-1985 3

APO NY 09061


SOF UH-60-85-17 VIBRATION LIMITS TEST ONENGINE OUTPUT SHAFT NOTED #1 1.3, #2 0.16AT 235.8 ACFT HRS (PF1111)

22-Jul-1985 4

APO NY 09061


UH-60A-85-04 INSP & REPLACEMENT OF STABAMP PREVIOUSLY COMPLIED WITH AT 236ACFT HRS (PF1111)

07-Nov-1985 1

APO NY 09061



8.7.DATE

6.REMARKS

4. 5.




UH-60A-85-05 PROHIBIT IN FLIGHT TRAINING &ORERATION IN ECU LOCK-OUT PRIVIOUSLYCOMPLIED WITH AT 236 ACFT HRS (PF1111)

07-Nov-1985 2

APO NY 09061


UH-60A-85-08 PREVIOUSLY COMPLIED WITH(PF1111)

07-Nov-1985 3

APO NY 09061


UH-60A-85-09 IMMEDIATE GROUNDIN OF ALLUH60A HELICOPTERS PREVIOUSLYCOMPLIED WITH AT 236 ACFT HRS (PF1111)

07-Nov-1985 4

APO NY 09061


UH-60A-85-10 ONE TIME INSPECTION OFDIRECTIONAL CONTROL LEVERS PREVIOSLYCOMPLIED WITH AT 236 ACFT HRS (PF1111)

07-Nov-1985 5

APO NY 09061


UH-60A-85-11 ONE TIME INSP OF MAIN ROTORSPINDLES PREVIOUSLY COMPLIED WITH AT236 ACFT HRS (PF1111)

07-Nov-1985 6

APO NY 09061


UH-60A-85-19 ONE TIME INSP OF RECORDSON MAIN ROTOR SHAFT PREVIOUSLYCOMPLIED WITH AT 236 ACFT HRS (PF1111)

07-Nov-1985 7

APO NY 09061


UH-60A-85-20 MAIN ROTOR SPINDLESRETIREMENT LIFE CHANGE PREVIOUSLYCOMPLIED WITH AT 236 ACFT HRS (PF1111)

07-Nov-1985 8

APO NY 09061


UH-60A-85-21 MAIN ROTOR SPINDLES &RETAINING ROD RETIREMENT LIFE CHANGEPREVIOUSLY COMPLIED WITH AT 236 ACFTHRS (PF1111)

07-Nov-1985 9

APO NY 09061


UH-60A-85-22 RESTRICTION ON HELICOPTERWITH SEQUENCE VALVES COMPLIED WITH AT236 ACFT HRS (PF1111)

07-Nov-1985 10

APO NY 09061


#3 OCM/ACE PERFORMED AT 236 A/C HRS, ATNELLINGEN, GE BY ACE TEAM MEMBER WFIMS AVSCOM OCM SEC ST. LOUIS, MO(WF1111)

16-Jan-1986 1

APO NY 09061


SOF UH-60A-86-02/TB 55-1520-237-20-74TORQUE CHECK OF T/R D/S BOLTS COMPLIEDWITH AT 236 ACFT HRS (HM1111)

30-Apr-1986 1

APO NY 09061


SOF UH-60A-86-01 REPLACEMENT OF TAILROTOR DRIVESHAFT VISCOUS DAMPERBEARING S COMPLETED AT 236 ACFT HRS(HM1111)

21-May-1986 1

APO NY 09061


SOF UH-60A-86-07 (MWO 55-1520-237-20-1)REQUIRMENTS FOR UNGROUNDINGCOMPLETED AT 236 ACFT HRS (HM1111)

21-May-1986 2

APO NY 09061


SOF UH-60A-86-03 REVISION OF ONE TIMEINSPECTION OF DRIVESHAFT NUTSPREVIOUSLY COMPLIED WITH AT 236 ACFTHRS (SJ1111)

13-Aug-1986 1

APO NY 09061


SOF UH-60A-86-04 REVISION OFREPLACEMENT OF T/R DRIVESHAFTBEARINGS PREVIOUSLY COMPLIED WITH AT236 ACFT HRS (SJ1111)

13-Aug-1986 2

APO NY 09061



8.7.DATE

6.REMARKS

4. 5.




SOF UH-60A-86-05 EMERGENCY MSG.IMMEDIATE GROUNING OF ALL UH-EH-60.PREVIOUSLY COMPLIED WITH (SJ1111)

13-Aug-1986 3

APO NY 09061


SOF UH-60A-86-06 STABILATOR/AUTO FCSCONTROL PANEL RETROFIT PREVIOUSLYCOMPLIED WITH (SJ1111)

13-Aug-1986 4

APO NY 09061


SOF UH-60A-86-08 REPLACEMENT OFSTABILATOR ACTUATORS COMPLIED WITHAT 239.2 ACFT HRS (SJ1111)

13-Aug-1986 5

APO NY 09061


SOF UH-60A-86-09 ONE TIME INSP OF ENG OILCOOLER PREVIOUSLY COMPLIED WITH(SJ1111)

13-Aug-1986 6

APO NY 09061


SOF UH-60A-86-10 ONE TIME STAKING OFBEARING ON YAW CONTROL LEVERCOMPLIED WITH AT 239.2 ACFT HRS (SJ1111)

13-Aug-1986 7

APO NY 09061


SOF UH-60A-86-11 REVISION TOREQUIREMENTS FOR REPORTINGUNGROUNDING COMPLIED WITH AT 239.2ACFT HRS (SJ1111)

13-Aug-1986 8

APO NY 09061


SOF UH-60A-86-12 ACFT LOCATION ANDCHANGE OUT LISTED SERIAL NUMBEREDYAW AND COLLECTIVE BOOST SERVOSCOMPLIED WITH AT 239.2 ACFT HRS (SJ1111)

13-Aug-1986 9

APO NY 09061


SOF UH-60A-86-13 MAINT. MANDATORYREMOVAL OF AN310-8 NUTS COMPLIED WITH(SJ1111)

14-Aug-1986 1

APO NY 09061


SOF UH-60A-86-14 REVISION TO PREVIOUSMSG CONCERNING LEVER ASSY (SJ1111)

14-Aug-1986 2

APO NY 09061


SOF UH-60A-86-15 REVISION TO PREVIOUSMSG 86-13 CHANGES STATUS SYMBOL FORACFT NOT ABLE TO REPLACE NUTS IN TIMETO A CIRCLE RED X UNTIL REPLACEMENTCOMPLETED (SJ1111)

20-Aug-1986 1

APO NY 09061

203RD AVIATION COSOF UH-60A-86-16 EXTENSION TO SOF UH-60A-86-10 N/A THIS AIRCRAFT, PREVIOUSLYCOMPLIED WITH (HG1111)

27-Oct-1986 1

APO NY 09025

203RD AVIATION COSOF UH-60A-86-17 ONE TIME INSPECTION OFTAIL ROTOR DRIVE SYSTEM N/A THISAIRCRAFT (HG1111)

27-Oct-1986 2

APO NY 09025

203RD AVIATION COSOF UH-60A-86-18 RESRICTING AIRCRAFTFROM RAPPELLING, STABO, AND STATICHOOKUP OPERATIONS AND STATIC HOOKUPOPERATIONS ENTERED ON 2408-13 (HG1111)

27-Oct-1986 3

APO NY 09025

203RD AVIATION CO#4 OCM/ACE PERFORMED AT 0282 A/C HRS,AT SCHWAEBISH HALL, GE BY ACE TEAMMEMBER X AVSCOM OCMSEC, ST LOUIS, MO(HG1111)

04-Nov-1986 1

APO NY 09025

203RD AVIATION COSOF UH-60A-86-20 ONE TIME INSPECTION OFTAIL ROTOR DRIVE SHAFT COUPLINGCOMPLETED AT 289.3 ACFT HRS (WB1111)

13-Nov-1986 1

APO NY 09025



8.7.DATE

6.REMARKS

4. 5.



203RD AVIATION COSOF UH-60A-86-19 REPETITIVE INSPECTIONOF EYEBOLT P/N 70209-02136-102 N/A THISAIRCRAFT (MDS) (WB1111)

13-Nov-1986 2

APO NY 09025

203RD AVIATION COSOF UH-60A-86-21 ONE-TIME INSP OF CREWSEATS OF LOCK PIN ADJUSTMENT N/A THISAIRCRAFT (NORTON SEATS) ACFT HRS 304.6(TM1111)

02-Dec-1986 1

APO NY 09025

203RD AVIATION COSOF UH-60A-86-22 REVISION TO SOF UH-60A-86-17 N/A THIS MDS AIRCRAFT (TM1111)

12-Dec-1986 1

APO NY 09025

203RD AVIATION COSOF UH-60A-86-08 STABILATOR ACTUATORP/N 70400-06641-115 INSTALLED AT 329.1AIRCRAFT HOURS (WB1111)

11-Feb-1987 1

APO NY 09025

203RD AVIATION COSOF UH-60A-87-01 ONE TIME VALIDATION OFCORRECT TORQUE OF T-700 ENGINE FUELDIFFERENTIAL PRESSURE INDICATORCOMPLETED AT 329.1 AIRCRAFT HOURS(WB1111)

13-Feb-1987 1

APO NY 09025

203RD AVIATION COSOF UH-60A-87-02 CORRECTION TO SOF UH-60A-87-01 (HG1111)

18-Feb-1987 1

APO NY 09025

203RD AVIATION COSOF UH-60A-87-03 INSPECTION OF FIRSTTHREE TAIL ROTOR DRIVE SHAFTCOUPLINGS COMPLETED AT 355.7 ACFTHOURS (HG1111)

14-Mar-1987 1

APO NY 09025

203RD AVIATION COSOF UH-60A-87-04 RECURRING INSP OFEYEBOLT P/N 70205-02136-102 ENTERED ONAPPLICABLE FORMS AT 355.7 ACFT HRS(HG1111)

27-Mar-1987 1

APO NY 09025

203RD AVIATION COSOF UH-60A-87-05 AIRCRAFT RESTRICTED TOBELOW 80 KTS AT ATTITUDES AT OR BELOW3000 FT AGL ENTERED ON DA FORM 2408-13AT 355.7 ACFT HRS (HG1111)

13-Apr-1987 1

APO NY 09025

203RD AVIATION COSOF UH-60A-87-06/TB 55-1520-237-50-2 OILCOOLER WEAR INDICATOR COMPLETED @361.3 ACFT HRS (RS1111)

22-May-1987 1

APO NY 09025

203RD AVIATION COSOF UH-60A-87-07 COMPLETED AT 361.3 ACFTHRS (HG1111)

22-May-1987 2

APO NY 09025

203RD AVIATION COSOF-UH-60A-87-08 COMPLETED AT 261.8 ACFTHRS (CC1111)

08-Jul-1987 1

APO NY 09025

203RD AVIATION CO#5 OCM/ACE PERFORMED AT 0366 A/C HRSAT SCHWABISH HALL GE BY ACE TEAMMEMBER P AVSCOM OCMSEC, ST LOUIS, MO(BP1111)

27-Jul-1987 1

APO NY 09025

203RD AVIATION COSOF-UH-60-87-05 AND SOF UH-60-87-09RECORDED AND COMPLETED BYAPPLICATION OF MWO 55-1520-237-50-46CYCLIC STABILATOR SLEW-UP SWITCH. AT425.6 ACFT HRS (WB1111)

10-Sep-1987 1

APO NY 09025

203RD AVIATION COSOF-UH-60-87-10 ONE TIME INSPECTION OFINPUT FLANGE ASSEMBLY COMPLETED AT460.1 ACFT HRS (WB1111)

19-Oct-1987 1

APO NY 09025



8.7.DATE

6.REMARKS

4. 5.



CO C 6/159TH AVIATIONCOMPANY

SOF-UH-60-87-11 ONE TIME INSPECTION OFCARGO DOOR UPPER AND LOWER SUPPORTASSEMBLY COMPLETED AT 468.0 ACFT HRS(203RD AVN CO CHANGED OVER TO C 6-159TH AVN CO) (WB1111)

03-Nov-1987 1

APO NY 09025


TB 55-1520-237-20-93 ONE TIME INSPECTIONAND SUBSEQUENT CONDITIONALINSPECTION OF ENGINE COWLINGCOMPLETED AT 473.1 ACFT HRS (HG1111)

16-Nov-1987 1

APO NY 09025


SOF-UH-60-87-12 ONE TIME INSPECTION FORDEFECTIVE T-700-GE-700/701 ENGINE POWERTURBINE MODULES COMPLETED AT 474.9ACFT HRS (WB1111)

03-Dec-1987 1

APO NY 09025

CO C 6/159TH AVIATIONREGIMENT

TB 55-1520-237-20-86 PITCH BIAS ACTUATORREPLACED WITH FIXED LINK AT 483.9 ACFTHRS (HG1111)

14-Jan-1988 1

APO NY 09025

CO C 6TH BN 159THAVIATION REG.

PMS-2 WAS INITIATED, 496.7 AIRCRAFTHOURS PMS-2 COMPLETED 27 APR 88(TM1111)

08-Feb-1988 1

APO NY 09025


SOF UH-60A-88-01 ONE TIME INSPECTION OFTAIL ROTOR BLADE ASSY COMPLETED AT496.7 ACFT HRS (JS1111)

16-Feb-1988 1

APO NY 09025


SOF UH-60A-88-02 ONE TIME INSPECTION OFTAIL ROTOR GEARBOX OUTPUT SHAFTASSEMBLY, COMPLETED AT 496.7 ACFTHOURS (TM1111)

30-Mar-1988 1

APO NY 09025


PMS-2 COMPLETED 27 APRIL 1988 AT 497.7ACFT HRS (TM1111)

05-May-1988 1

APO NY 09025


SOF UH-60A-88-03/TB 55-1520-237-20-97 LIFEEXTENSION OF THE UH-60A AIRCRAFT MAINMODULE SHAFT COMPLETED AT 504.5 ACFTHRS (TM1111)

13-May-1988 1

APO NY 09025


SOF UH-60A-88-04 REVISION TO ONE TIMEINSPECTION OF THE TAIL ROTOR GEAR BOXOUTPUT SHAFT COMPLETED AT 504.5 ACFTHRS (TM1111)

13-May-1988 2

APO NY 09025


SOF UH-60A-88-05 INITIATION OF APU MAOTINTERMS OF APU OPERATING HOURS ANDSTARTS TO BE COMPLETED BY 13 AUG 88 OR563.0 ACFT HRS. COMPLETED 15 JUNE 88 AT533.0 ACFT HRS (TM1111)

15-Jun-1988 1

APO NY 09025


#6 OCM/ACE PERFORMED AT 0558 A/C HRS.AT SCHWABISH HALL, GE BY ACE TEAMMEMBER T AVSCOM OCMSEC, ST. LOUIS, MO(TM1111)

13-Jul-1988 1

APO NY 09025


SOF UH-60A-88-06 REQUIREMENTS FORREPLACEMENT OF OIL COOLER BEARING AT2000 HRS ENTERED ON TIME CHANGE 2408-15, 719.1 ACFT HRS (HG1111)

13-Jul-1988 2

APO NY 09025



8.7.DATE

6.REMARKS

4. 5.




SOF UH-60A-88-07/TB 55-1520-237-20-98REVISION TO SOF UH-60-88-05 REVISE THEAPU OPERATING HOUR AND STARTSCALCULATIONS FOR LOGGING ANDTRACKING COMPLETETED 558.1 ACFT HRS(WB1111)

15-Jul-1988 1

APO NY 09025


SOF UH-60A-88-08 REVISION TO SOF UH-60A-88-06 REVISION TO OVERHAUL LIFE FOR THETRANSMISSION OIL COOLER BLOWER.COMPLETED 570.2 ACFT HRS (WB1111)

28-Jul-1988 1

APO NY 09025


SOF UH-60A-88-09 ONE TIME INSP OF ARAMANUFACTURED CREW SEATS FOR LOOSECLEVIS SCREWS COMPLETED AT 574.9 ACFTHRS (TM1111)

03-Aug-1988 1

APO NY 09025


SOF UH-GEN-88-02 ONE TIME INSPECTIONFOR INSTALLATION OF CORRECT INTERNALPORTABLE FIR EXTINGUISHER COMPLETEDAT 631.5 ACFT HRS (WB1111)

28-Sep-1988 1

APO NY 09025


GENERAL SOF 88-03/TB 1-500-200-20-26REVISION TO GEN SOF 88-02, ONE TIMEINSPECTION OF CORRECT INTERNALPORTABLE FIRE EXTINGUISHER PREVIOUSLYCOOMPLIED WITH COMLETION OF GENERALSOF 88-02 (TM1111)

04-Oct-1988 1

APO NY 09025


SOF UH-60A 88-10 ONE TIME INSPECTION OFTROOP/GUNNER SEAT AND THREE MANMEDEVAC UPPER SUPPORT INSTALLATIIONCOMPLETED AT 631.5 ACFT HRS (TM1111)

11-Oct-1988 1

APO NY 09025


SOF UH-60A-88-11 REVISION TO SOF UH-60A-86-18 THIS MSG SITES AUTHORITY FORREMOVAL OF THE RESTRICTION EH-60AAIRCRAFT (TM1111)

19-Oct-1988 1

APO NY 09025


SOF UH-60A-88-12 REVISION TO SOF UH-60A-86-10 THIS MSG SITES ADDITIONAL NSN ANDPART NUMBERS TO BE INSP COMPLETED AT643.8 ACFT HRS (WB1111)

02-Nov-1988 1

APO NY 09025


SOF UH-60A-88-13 MSG ONE TIME INSP OFMAIN ROTOR EXPANDABLE RETENSION PINSFOR MISSING SEGMENTS COMPLETED AT655.7 ACFT HRS (RJ1111)

21-Nov-1988 1

APO NY 09025


SOF UH-60A-88-14/ TB 55-1520-237-20-103 ONETIME INSP OF ALL UH-60A HIGHPERFORMANCE HOIST SYSTEM NOTAPPLICABLE THIS MODEL, DESIGN ORSERIES AIRCRAFT (MDS) (WB1111)

15-Dec-1988 1

APO NY 09025


SOF UH-60A-89-03 ONE TIME INSP OF ALL M/RSPINDLES COMPLETED 747.6 ACFT HRS(RJ1111)

04-Feb-1989 1

APO NY 09025


SOF UH-60A-89-01 ONE TIME INSPECTION OFT-700 ENGINE G/G STATOR SHROUDS,COMPLIED WITH AT 716.4 ACFT HRS (WG1111)

10-Feb-1989 1

APO NY 09025


SOF UH-60A-89-02 REVISION TO SOF UH-60A-89-01 COMPLETED 716.4 ACFT HRS (RJ1111)

13-Feb-1989 1

APO NY 09025



8.7.DATE

6.REMARKS

4. 5.




SOF UH-60A-89-11 COMPLETED AT 904.5 ACFTHRS (DH1111)

09-Mar-1989 1

APO NY 09025


SOF UH-60A-89-04 REVISION TO SOF UH-60A-89-03 ONE TIME INSPECTION OF ALL M/RSPINDLES COMPLETED AT 795.6 ACFT HRS(JE1111)

04-Apr-1989 1

APO NY 09025


SOF UH-60A-89-05/ TB 55-1520-237-20-106 ONETIME INSP OF FWD WIRE STRIKEPROTECTION PITOT CUTTER COMPLETED AT795.4 ACFT HRS (JE1111)

15-Jun-1989 1

APO NY 09025


SOF UH-60A-89-06 ONE TIME INSP OF L/H +R/H RELAY PANEL GROUND MODULESCOMPLETED AT 815.3 ACFT HRS (JE1111)

19-Jul-1989 1

APO NY 09025


#7 OCM/ACE PERFORMED AT 0824 A/C HRS,AT SCHWABISCH, HALL, GE. BY ACE TEAMMEMBER C AVSCOM OCMSEC ST. LOUIS, MO(JE1111)

28-Jul-1989 1

APO NY 09025


SOF UH-60A-89-07 CORRECTION TO SOF UH-60A-89-06 COMPLETED (JE1111)

09-Aug-1989 1

APO NY 09025


SOF UH-60A-89-08 ONE TIME OPERATIONALINSP OF THE FUEL BOOST PUMP HOSEINSTALLATION FOR CONNECTION TOSUBMERGED BOOST PUMP COMPLETED AT840.4 (JE1111)

16-Aug-1989 1

APO NY 09025


SOF UH-60A-89-09 CORRECTION OFRETIREMENT LIFE SCHEDULE FOR H-60RETIREMENT LIFE COMPONENTSCOMPLETED AT 840.4 (JE1111)

16-Aug-1989 2

APO NY 09025


SOF UH-60A-89-10 ONE TIME INSP OF T 700-GE-700 ENG GAS GENERATOR ROTOR ANDSTATOR SHROUDS COMPLETED 874.4 ACFTHRS (JE1111)

20-Sep-1989 1

APO NY 09025


SOF UH-60A-89-12 ONE TIME INSPECTION OFOIL COOLER AXIAL FAN BY NEXT 10 HR 14DAY INSPECTION COMPLETED AT 904.5 ACFTHRS (LL1111)

28-Nov-1989 1

APO NY 09025


SOF UH-60A-89-13 COMPLETED AT 910.2 ACFTHRS (DH1111)

11-Dec-1989 1

APO NY 09025


TB 55-1520-237-20-104 DATED 30 SEPT 89 NEWOVERHAUL/RETIREMENT LIFE SCHEDULEFOR H-60 RETIREMENT LIFE COMPONENTSCOMPLETED AT 933.7 ACFT HRS (KH1111)

13-Feb-1990 1

APO NY 09025

T TROOP 4/12ARMORED CAVALRYREG.

ALL SPINDLE NUTS REPLACED AT 989 ACFTHRS DUE TO MORE THAN 50% OF FILM LUBEMISSING (HC1111)

25-Mar-1990 1

APO NY 09092

CO B 7TH BN 159THAVIATION REG.

SOF MSG UH-60-90-01/ TB 55-1520-237-20-113ONE TIME AND RECURRING INSPECTION OFTHE MAIN ROTOR BLADE EXPANDABLE PINS.COMPLETED AT 946.5 ACFT HRS (GG1111)

20-Apr-1990 1

APO NY 09061-0298



8.7.DATE

6.REMARKS

4. 5.




#8 OCM/ACE PERFORMED AT 0948 A/C HRS,AT NELLINGEN GE BY ACE TEAM MEMBER NAVSCOM OCMSEC, ST LOUIS, MO (GG1111)

07-Aug-1990 1

APO NY 09061-0298


SOF MSG UH-60-90-02/ TB 55-1520-237-20-118ONE TIME INSPECTION OF TAIL ROTOR PITCHBEAM RETAINING WASHER, AND PITCH BEAMRETAINING NUT AND EMPHASIZEDRECURRING VISUAL INSPECTION.COMPLETED AT 947.5 AIRCRAFT HOURS(GG1111)

30-Aug-1990 1

APO NY 09061-0298


TB 55-1520-237-20-111 ONE TIME INSPECTIONOF UPPER PRESSURE PLATE AND SPINDLETO HUB ATTACHMENT BOLTS FOR PROPER -NUMBERS. COMPLETED AT 953.0 (GG1111)

24-Sep-1990 1

APO NY 09061-0298

T TROOP 4/2 ARMOREDCAVALRY REG.

AIRCRAFT ARRIVAL IN SWA ACFT HRS UKNAIRCRAFT DEPARTED SWA ON 17 APRIL 91AT 995.5 ACFT HRS (AC1111)

10-Dec-1990 1

APO NY 09092


UH-60-91-ASAM-02 RECURRING INSPECTIONOF M/R BLADE TIP CAPS ( DESERT SHIELDACFT) C/W AT 963.0 ACFT HRS (JE1111)

24-Jan-1991 1

APO NY 09092


PHASE 2 COMPLETED AT 995.5 AIRCRAFTHOURS AT T TROOP 4/2 ACR (SWA)

11-Mar-1991 1

APO NY 09092


UH-60-91-ASAM-01 T/R PITCH BEAMRETAINING NUT WASHER REPLACEMENT C/W989.5 ACFT HRS (JE1111)

10-Apr-1991 1

APO NY 09092


SOF MSG UH-60-91-ASAM-06 ONE TIME INSPOF CARGO HOOK INTERNAL WIRE BUNDLEROUTING C/W 995.1 HRS (JE1111)

12-Apr-1991 1

APO NY 09092


UH-60-91-ASAM-03 EXTENDED TIME BETWEENOVERHAUL HOURS UNDER DESERT SHIELDOPERATION FOR OIL COOLER AND PITCHCHANGE SHAFT (NO EXTENSION THISAIRCRAFT) COMPLIED AT 999.7 HRS (JE1111)

24-Jul-1991 1

APO NY 09092


UH-60-91-ASAM-04 GUIDANCE FORSITUATIONS REQUIRING EXCEEDING THERETIREMENT LIFE OF CERTAIN COMPONENTSCOMPLIED WITH AT 999.7 HRS (JE1111)

24-Jul-1991 2

APO NY 09092


UH-60-91-ASAM-05 ALL H-60 SERIESAIRCRAFT INSPECTION FOR FOURUNSERVICEABLE M/R SPINDLE ASSEMBLIESCOMPLIED WITH AT 989.5 ACFT HRS 8 APR 91(JE1111)

24-Jul-1991 3

APO NY 09092


UH-60-91-ASAM-06 ALL H-60 SERIESAIRCRAFT INSPECTION OF CARGO HOOKINTERNAL WIRE BUNDLE ROUTING COMPLEDWITH AT 999.7 HRS (JE1111)

24-Jul-1991 4

APO NY 09092


UH-60-91-ASAM-07 ADVANCED NOTIFICATIONOF MANUAL CHANGES CONCERNING MAINTRANSMISSION MODULE COMPLIED WITH AT999.7 HRS (JE1111)

24-Jul-1991 5

APO NY 09092



8.7.DATE

6.REMARKS

4. 5.




UH-60-91-ASAM-08 ALL H-60 SERIESAIRCRAFT ONE TIME INSPECTION OF FIREEXTINGUISHING SYSTEM COMPLIED WITH AT999.7 HRS (JE1111)

24-Jul-1991 6

APO NY 09092


UH-60-91-ASAM-09 ALL H-60 SERIESAIRCRAFT CHANGES TO INSPECTPROCEDURES FOR MAIN ROTORELASTOMERIC BEARINGS COMPLIED WITH AT999.7 HRS (JE1111)

24-Jul-1991 7

APO NY 09092


#9 0CM/ACE PERFORMED AT 1001 A/C HRS ATFEUCHT, AA GE BY ACE TEAM MEMBER LAVSCOM OCMSEC, ST, LOUIS, MO (AC1111)

08-Aug-1991 1

APO NY 09092


UH-60-91-ASAM-10 ALL H-60 SERIESAIRCRAFT ONE TIME INSPECTION ANDREPLACEMENT OF MAIN LANDING GEARASSEMBLY COMPLIED WITH 1 AUG 91 @ 999.7ACFT HOURS (JE1111)

01-Oct-1991 1

APO NY 09092


UH-60-92-ASAM-01 ALL H-60 SERIES ACFT.INSPECTION FOR 3 UNSERVICABLE SPINDLEASSY COMPLIED WITH AT 1060.0 ACFT HRS(DG1111)

07-Jan-1992 1

APO NY 09092

DYNCORP (OLR)UH-60-91-ASAM-11 OPERATE WITH BOOSTPUMPS ON WHILE BURNING J-P/4 FUEL C/WAT 1116.4 ACFT HRS (DH1111)

20-Apr-1992 1

FT HOOD TX 76540

DYNCORP (OLR)UH-60-92-ASAM-05/ TB 1-1520-237-20-130 ALLH-60 AIRCRAFT, INSPECTION ANDREPLACEMENT OF MAIN ROTOR BLADEEXPANDABLE PIN C/W 1116.4 ACFT HRS(WN1111)

26-Aug-1992 1

FT HOOD TX 76540

DYNCORP, PROJECTOLR

PMS-2 (PE #3) INSP COMPLETED AT 1116.4ACFT HRS. NEXT PMS-2 DUE AT 1616.4 ACFTHRS. (MW1111)

10-Sep-1992 1

FT HOOD, TX

DYNCORP, PROJECTOLR

TB 1-1520-237-30-2 DESERT STORMREDEPLOYMENT SPECIAL INSPECTION ANDCLEANING REQUIREMENT UH-60A/L AND EH-60 ACFT COMPLETED AT 1116.4 ACFT HRS.(MW1111)

10-Sep-1992 2

FT HOOD, TX

DYNCORP, PROJECTOLR

TB 1-1500-200-20-30 DESERT STORMREDEPLOYMENT CLEANING REQUIREMENTCOMPLETED AT 1116.4 ACFT HRS. (WN1111)

10-Sep-1992 3

FT HOOD, TX

DYNCORP, PROJECTOLR

UH-60-92-ASAM-06/TB 1-1520-237-20-134 ONETIME INSPECTION OF THE PEDAL ADJUSTERASSY. FOR PROPER HARDWARE C/W.(MW1111)

28-Sep-1992 1

FT HOOD, TX

DYNCORP, PROJECTOLR

UH-60-93-ASAM-01/TB 1-1520-237-20-135 ONETIME OPERATIONAL CHECK OF THE XMSNAND GEARBOX CHIP DETECTOR SYSTEMSNOT REQUIRED IAW ATCOM MEMORANDUMDTD 13 OCT 92. (WN1111)

02-Nov-1992 1

FT HOOD, TX

DYNCORP, PROJECTOLR

UH-60-93-ASAM-04/TB 1-1520-237-20-134REVISION TO UH-60-92-ASAM-06 INSP ANDREPLACEMENT OF THE PEDAL ADJUSTERASSY HARDWARE C/W AT 1124.3 ACFT HRS.(HK1111)

10-Dec-1992 1

FT HOOD, TX



8.7.DATE

6.REMARKS

4. 5.



DYNCORP, PROJECTOLR

UH-60-93-ASAM-06/TB 1-1520-237-20-136INSPECTION OF T/R PITCH BEAM ASSY. FORCERTAIN SERIAL NUMBERS C/W AT 1124.3ACFT HRS. (HK1111)

18-Dec-1992 1

FT HOOD, TX

AERATB 1-1520-237-20-XX TRIMBLE TRIMPACK GPSSPECIAL MISSION INSTALLED. (JD1111)

19-Jan-1993 1

LAKEHURST, NJ 08733

C CO 4/227 AVNUH-60-93-ASAM-08/TB 1-1520-237-20-138 BIAST/R RIGGING THREE DEGREES C/W AT 1137.2ACFT HRS. (SD1111)

04-Mar-1993 1

FT HOOD, TX 76545

C CO 4/227 AVNUH-60-93-ASAM-10/TB 1-1520-237-20-141 ESSSSYSTEM INSP C/W AT 1143.2 ACFT HRS.(DH1111)

06-Apr-1993 1

FT HOOD, TX 76545

C CO 4/227 AVNUH-60-93-ASAM-11/TB 1-1520-237-20-142INSPECTION OF CREW RESTRAINT SYSTEMC/W AT 1147.6 ACFT HRS. (DH1111)

26-Apr-1993 1

FT HOOD, TX 76545

C CO 4/227 AVNUH-60-93-ASAM-03/TB 1-1520-237-20-130INSPECTION OF M/R BLADE PINS C/W AT1190.4 ACFT HRS. (DH1111)

25-Jun-1993 1

FT HOOD, TX 76545

CCADACFT COMPLETEDREFURBISHMENT/STANDARDIZATIONPROGRAM 22 AUG 84 BY CCAD AT 1192.4ACFT HRS IAW ATCOM SOW DTD 05 AUG 93WHICH INCLUDED MWO 1-1520-237-55-7 ANDPMS-2 #4. NEXT PMS-2 DUE AT 1692.4 ACFTHRS. (SR1111)

22-Aug-1994 1

CORPC, TX

CCADACFT EXTERIOR PAINTED WITH LOWREFLECTIVE POLYURETHANE ACFT GREEN,MIL-C-46168 IAW TM 55-1500-345-23 DTD 12JUN 86 AND ECP 0245. (SR1111)

22-Aug-1994 2

CORPC, TX

CCADACFT SIX MONTH FILE WILL BE RETAINED ATCCAD IAW TDS # AGEN-X0363, CHG 1, DTD 13JAN 84. (SR1111)

22-Aug-1994 3

CORPC, TX

CCADTB 1-1520-237-20-128 DISCONNECTION OF THEPITCH BIAS ACTUATOR C/W. (SR1111)

22-Aug-1994 4

CORPC, TX

CCADUH-60-93-ASAM-16/TB 1-1520-237-20-146 ONETIME INSPECTION OF THE HYDRALIC PUMPMODULE KNURLED BLEED/ RELEIF KNOBSECURING PIN C/W. (SR1111)

22-Aug-1994 5

CORPC, TX

CCADUH-60-94-ASAM-01/TB 1-1520-237-20-139REWORK OF NIGHT VISION GOGGLE MASTERWARNING PANEL C/W. (SR1111)

22-Aug-1994 6

CORPC, TX

CCADUH-60-94-ASAM-03/10/TB 1-1520-237-20-151ONE TIME REFURBISHMENT OF M/R SPINDLEAND REPLACEMENT OF CERTAIN M/RTHRUST BEARINGS C/W. (SR1111)

22-Aug-1994 7

CORPC, TX

CCADUH-60-94-ASAM-04/TB 1-1520-237-20-136REISSUE OF ONE TIME INSPECTION TOREMOVE SUSPECT T/R PITCH BEAM C/W.(SR1111)

22-Aug-1994 8

CORPC, TX

CCADUH-60-94-ASAM-09/TB 1-1520-237-20-155REMOVAL OF CERTAIN PRIMARY SERVOASSEMBLIES C/W. (SR1111)

22-Aug-1994 9

CORPC, TX



8.7.DATE

6.REMARKS

4. 5.



CCADUH-60-93-ASAM-09/TB 1-1520-237-20-140 ONETIME INSPECTION TO DETERMINECOMPLIANCE WITH SYSTEM MWO'S C/W.(MF1111)

22-Aug-1994 10

CORPC, TX

CCADUH-60-94-ASAM-02/TB 1-1520-237-20-149RETURN FOR EXCHANGE CERTAIN ARA MFDBUCKLE/CROTCH STRAP ASSY'S, P/N 04495-28, C/W, SUBJECT ASSEMBLY NOTINSTALLED. (WF1111)

22-Aug-1994 11

CORPC, TX

CCADUH-60-94-ASAM-05/TB 1-1520-237-20-152 ONETIME REMOVAL OF TAIL ROTOR GEAR BOXESWITH OUTPUT SHAFT P/N 70358-06620-101C/W. SUBJECT P/N NOT INSTALLED IN ACFT.(MF1111)

22-Aug-1994 12

CORPC, TX

CCADUH-60-94-ASAM-06/TB 1-1520-237-20-150COCKPIT STANDARDIZATION OFPILOT/COPILT RESTRAINT RELEASE SYSTEMC/W. (MF1111)

22-Aug-1994 13

CORPC, TX

CCADUH-60-94-ASAM-07/08/TB 1-1520-237-20-154CHANGE TO UH-60 OVERHAUL ANDRETIREMENT LIFE TABLE C/W. (MF1111)

22-Aug-1994 14

CORPC, TX

CCADUH-60-95-ASAM-01/TB 1-1520-237-20-157HOISTING AND RECOVERY OF UH-60/EH-60ESSS FIXED PRVISIONED HELICOPTERS C/W.(MF1111)

22-Aug-1994 15

CORPC, TX

CCADUH-60-95-ASAM-02/TB 1-1520-237-20-159REQUIREMENT TO OPERATE THE FUEL TANKSUBMERGED BOOST PUMPS ON AT ALLTIMES WITH ALL FUELS DURING GROUNDRUNS AND FLIGHT OPERATIONS C/W.(MF1111)

22-Aug-1994 16

CORPC, TX

CCADUH-60-95-ASAM-03/TB 1-1520-237-20-158REQUIRED RESHIMMING OF TAIL ROTORPIVOT BEARINGS PER REVISEDPROCEDURES ADNCERTAIN BLADE ASSY'SWITH SPECIFIED S/N'S WILL BE INSPECTEDFOR COMPOSITE PIVOT BEARING RETAINERSC/W. (MF1111)

22-Aug-1994 17

CORPC, TX

AASF #2, WIARNGAIRCRAFT RECEIVED AT THIS STATION WITH1206.6 ACFT HRS FROM CCAD. (DR4264)

18-Nov-1994 1

MADISON, WI 53704-2517

AASF #2, WIARNG-ASAM-07/TB 1-1520-237-20-164REPLACEMENT CRITERIA FORTROOP/GUNNER SEAT ATTENUATION WIRESC/W. (XK1861)

06-Jan-1995 1


AASF #2, WIARNGUH-60-95-ASAM-05/TB 1-1520-237-20-163CHANGE IN RETIREMENT LIFE FOR CERTAINP/N SERVO BEAM RAILS C/W. (XK1861)

04-Feb-1995 1


AASF #2, WIARNGSOF UH-60-95-02/TB 1-1520-237-20-161CHANGE IN RETIREMENT LIFE FOR CERTAINM/R BLADE CUFFS C/W. (DR4264)

03-Mar-1995 1


AASF #2, WIARNGINSTALLATION OF ELT I/A/W AIRWORTHINESSRELEASE DATED 20 MAR 90 C/W. (DR4264)

24-Mar-1995 1




8.7.DATE

6.REMARKS

4. 5.



AASF #2, WIARNGEMC TEST COMPLETED I/A/W AWR DTD 20MAR 90 FOR INSTALLATION OF ELT. (XR4264)

24-Mar-1995 2

1950 PEARSON ST.MADISON WI.

AASF #2, WIARNGUH-60-95-ASAM-06/TB 1-1520-237-20-168 ONETIME INSPECTION FOR CRACKED MAIN XMSNBEAMS AND IMPLEMENTATION OF 100 HRREACURRING INSP C/W. (DR4264)

09-Aug-1995 1


AASF #2, WIARNGUH-60-95-ASAM-07/TB 1-1520-237-20-164REPLACEMENT CRITERIA FORTROOP/GUNNER SEAT ATTENUATION WIRESC/W. (XK1861)

13-Aug-1995 1



UH-60-96-ASAM-01/TB 1-1520-237-20-170 ALLACFT WITH IMPROVED FLT CONTROLS,REPLACEMENT OF 70400-08159 SERIESBOLTS C/W, N/A THIS ACFT. (XK1861)

14-Oct-1995 1

MADISON,WI

1/147TH CAB WIARNG.SOF UH-60-96-1/TB 1-1520-237-20-172 CHANGEIN RETIREMENT LIFE OF CERTAIN FWDBELLCRANK SUPPORTS AND REMOVAL OFSUSPECT S/N'S C/W. (XK1861)

08-Nov-1995 1

MADISON, WI.53704-2517

1/147TH CAB WIARNG.SOF UH-60-96-02/TB 1-1520-237-20-173 ONETIME INSP FOR SUSPECT TAIL ROTORINBOARD RETENSION PLATES C/W. (XK1861)

30-Nov-1995 1


AASF #2, WIARNGUH-60-95-ASAM-04/TB 1-1520-237-20-160REDUCTION OF TORQUE OF BRIDGE PIVOTBOLTS C/W. (DR4264)

15-Dec-1995 1


1/147TH CAB WIARNG.UH-60-96-ASAM-02/TB 1-1520-237-20-171 ONETIME INSPECTION FOR SUSPECT M/R SHAFTNUT BOLTS C/W. (DR4264)

25-Jan-1996 1


1/147TH CAB WIARNG.UH-60-96-ASAM-03/TB 1-1520-237-20-171REVISION TO ONE TIME INSPECTION FORSUSPECT M/R SHAFT NUT BOLTS REQ'D BYUH-60-96-ASAM-02 C/W. (DR4264)

25-Jan-1996 2


AASF #2 1/147TH AVNUH-60-96-ASAM-04/TB 1-1520-237-20-176 ALLACFT WITH FAST ROPEINSERTION/EXTRACTION SYSTEM (FRIES)BAR MAXIMUN ALLOWABLE LOADREDUCTION C/W N/A THIS ACFT. (XK1861)

26-Jan-1996 1

MADISON, WI

1/147TH CAB WIARNG.UH-60-96-ASAM-10 ALL H-60 SERIESACFT.SPINDLE ASSY &SPINDLE ELASTRO.BRGS. C/W (DR4264)

06-Oct-1996 1


AASF #2 WIARNG.UH-60-97-ASAM-02 ONE TIME INSP. OF TAILDRIVE FLEX COUPLING CONNECTIONS C/W(DR4264)

28-Oct-1996 1


AASF #2 WIARNG.GEN-97-ASAM-03 CHANGE OF PROCEDURESFOR LOADING THE CRYPTO KEYS INNAVSTAR AN/ASN-149 GPS RECEIVER C/W.(DR4264)

22-Jan-1997 1


AASF #2 WIARNG.UH-60-97-ASAM-05 (TB1-1520-237-23-03) ONETIME INSP. FOR REMOVAL & REWORK OFCERTAIN VISCOUS DAMPER BRNG.SUPPORTASSYS. C/W. (DR4264)

22-Jan-1997 2




8.7.DATE

6.REMARKS

4. 5.



AASF #2 WIARNG.UH-60-97-ASAM-08 (TB1-1520-237-20-187) ALLH60 ACFT. WITH CONNECTING LINK ASSY.P/N70400-08155-056 MANUFACTURED BYPURDY MACHINE CO. C/W. (DR4264)

22-Jan-1997 3

MADISON,WI.53704-2517

PROJECT ,OLRFT.LEWIS,WA

ACE INSP. PERFORMED AT 1609 ACFT HRS.AT MADISO,WI BY Q. (CP1111)

29-Jul-1997 1


AASF#2 WIARNG.UH-60-97-ASAM-14 (TB1-1520-237-20-195)ONE TIME INSP. FOR BELLCRANK SUPPORTC/W (JV1079)

11-Aug-1997 1


AASF #2 WIARNG.UH-60-97-ASAM-15 (TB1-1520-237-20-196)ONE TIME INSP. FOR BEARING ROD END C/W.(JV1079)

11-Aug-1997 2

MADISON, WI. 53704-2517

AASF #2 WIARNG.UH-60-97-ASAM-17 (TB1-1520-237-20-199)ONE TIME INSP. FOR THE INTERNAL ENGINEHOIST BRKT. ASSY.C/W (DR4264)

20-Aug-1997 1


AASF #2 WIARNG.UH-60-97-ASAM-19 (TB1-1520-237-20-204)ONE TIME INSP. OF ANVIS / HUD POWERSUPPLY C/W. (DR4264)

04-Oct-1997 1


AASF #2 WIARNG.UH-60-98-ASAM-02 (TB1-1520-237-20-197)ONE TIME INSP. FOR SUSPECT PUSHRODSP/N70400-08155-050 & 51 C/W (RK1861)

04-Oct-1997 2


AASF #2 WIARNG.UH-60-98-ASAM-03 (TB1-1520-237-20-203) ONETIME INSP. FOR SWASHPLATE LINK P/N 70400-08110-054 C/W (DR4264)

10-Nov-1997 1


AASF #2, 1/147TH AVNSOF UH-60-98-01 RISK MANAGEMENT OF 230GALLON EXTERNAL TANKS FLIGHTOPERATIONS C/W, N/A THIS ACFT W/O ESSS.(XK1861)

27-Jan-1998 1

MADISON, WI

AASF #2 WIARNGUH-60-98-ASAM-04 LOOSE HUCK BOLTS ONOVERHAULED PRIMARY SERVOS,COL.& YAWBOOST SERVOS, & T/R SERVOS C/W.(DR4264)

17-Mar-1998 1


AASF #2 / 1-147TH CABACFT RECORDS CONVERTED TO ULLS-A(XK1861)

07-May-1998 1


AASF #2 / 1-147TH CAB /WIARNG

UH-60-98-ASAM-05/TB 1-1520-237-20-203 ALLH60 ACFT WITH SWASHPLATE LINKSMANUFACTURED BY TEC CAGE CODE 65780,P/N 70400-08110-054/-061 C/W (XK1861)

07-May-1998 2


PROJECT OLRACE PERFORMED AT 1692.0 ACFT HRS ATMADISON WI. BY DD. (MF3073)

20-Jul-1998 1

FT. LEWIS WA.

AASF #2 WIARNGUH-60-99-ASAM-01/TB 1-1520-237-20-208RESTORATION OF FULLL SERVICE LIFE ONSWASHPLATE LINK MFD BY TEC C/W.(XR4264)

09-Nov-1998 1




8.7.DATE

6.REMARKS

4. 5.



AASF #2 WIARNGUH-60-99-ASAM-02/TB 1-1520-237-20-207 ALLH-60 HELICOPTERS WITH PROVISIONS TOINSTALL EXTERNAL HOIST AND ALLEXTERNAL HOIST MANUFACTURED BYBREESE. (XR4264)

09-Nov-1998 2


1/147TH CAB WIARNG.AIRCRAFT DIGITAL ELECTRIC CLOCKS P/NPDMME-367-3 INSTALLED I/A/W ECP 454REPLACING ABU-11/A MECHANICAL CLOCKS.(XK1861)

16-Dec-1998 1


AASF #2 WIARNGINSTALLATION OF LOCALLY MANUFACTUREDLOCKING DEVICE I/A/W AWR DTD 07 JAN 99.(XR4264)

04-Feb-1999 1


AASF #2 WIARNGEMC TEST COMPLETED FOR LOCALLYMANUFACTURED LOCK-ING DEVICE I/A/WAWR DTD 7 JAN 99. (XR4264)

04-Feb-1999 3


AASF #2, WIARNGPMS-2 COMPLETED AT 1692.0 ACFT HRS.NEXT PMS-2 DUE AT 2192.0 ACFT HRS.(XK1861)

02-Apr-1999 1


PROJECT OLRACE PERFORMED AT 1692.0 ACFT HRS.(KS0820)

08-Apr-1999 1

AASF#2 MADISON WI.53704

AASF #2 WIARNGUH-60-99-ASAM-10/TB1-1520-237-20-213INSPECTION AND PREVENATIVEMAINTENANACE ON THE NUMBER TWOCROSS FEED BREAKAWAY VALVE C/W.(XK1861)

01-Oct-1999 1

MADISON WI. 53704-2517

AASF #2 WIARNGCYCLIC STICK WIRING BUNDLE RELOCATIONUH-60-00-ASAM-02 C/W. (XR4264)

16-Dec-1999 1

MADISON WI.

AASF #2 WIARNGAWR DTD 17 DEC 99 FOR THE INSTALLATIONOF ELT'S SUPERCEDES AWR DTD 20 MAR 90.(XR4264)

04-Jan-2000 1


AASF #2 WIARNGEMC TEST COOMPLETED I/A/W AWR DTD 17DEC99 FOR INSTALLATION OF ELT. (XR4264)

04-Jan-2000 2


AASF #2 WIARNGUH-60-00-ASAM-04/TB1-1520-237-20-218INSPECT TAIL LANDING GEAR ASSY. FORMISSING BEARING PINS. C/W.G PINS. C/W.(XR4264)

24-Feb-2000 1


AASF #2 WIARNGUH-60-00-ASAM-05/TB1-1520-237-20-219INSPECT FIRE EXTINGUISHER WIRING C/W.219C/W. (XR4264)

17-May-2000 1


AASF #2, WIARNG,1/147TH AVN

UH-60-00-ASAM-06/TB 1-1520-237-20-219REVISION TO UH-60-00-ASAM-05 INSPECTIONOF FIRE EXTINGUISHER WIRING C/W AT2040.3 ACFT HRS. (XK1861)

24-Jun-2000 1


PROJECT OLRJACE PERFORMED AT 2038 ACFT HRS ATMADISON, WI BY HH&V. (KS0820)

25-Jun-2000 1

FT. LEWIS, WA

AASF#2 WIARNG1/147TH AVN BN

UH-60-00-ASAM-07/TB 1-1520-237-20-224INSPECT WIRE HARNESS CONNECTING THE#1 AND #2 JUNCTION BOXES C/W (XC8756)

31-Aug-2000 1

MADISON WI 53704-2517



8.7.DATE

6.REMARKS

4. 5.



AASF#2 WIARNG1/147TH AVN BN

AWR DTD 14 JUL 99 FOR THECOMMUNICATION EAR PLUG INSTALLATIONAND TESTING C/W. (XR4264)

18-Sep-2000 1


AASF #2 WIARNGEMC TEST COMPLETED FORCOMMUNICATION EAR PLUG I/A/W AWR DTD14 JUL 99. (XR4264)

18-Sep-2000 2


AASF #2 WIARNG1/147TH AVN

SOF UH-60-01-01/TB 1-1520-237-20-225 INITIALAND RECURRING INSPECTION OF MLG DRAGBEAM ASSY'S AND REDUCTION OF TORQUEON JACKPAD NUT C/W AT 2102.2 ACFT HRS.(XK1861)

09-Nov-2000 1


AASF #2 WIARNG1/147TH AVN

SOF UH-60-01-02/TB 1-1520-237-20-225 INITIALAND RECURRING INSPECTION OF MLG DRAGBEAM ASSY'S AND REDUCTION OF TORQUEON JACKPAD NUT. UPDATE C/W. (XR4264)

03-Jan-2001 1



SOF UH-60-01-04/TB 1-1520-237-20-228REVISION TO SOF UH-60-98-01 RISKMANAGEMENT OF 230 GAL EXTERNAL TANKOPERATIONS, INSP FOR INSTALLATION OFFUEL MONITORING SYSTEM. N/A THIS ACFT,ESSS HARDPOINTS NOT INSTALLED AT 2134.4ACFT HRS. (XK1861)

08-Jan-2001 1


AASF #2 WIARNGUH-60-01-07/08 TB 1-1520-237-20-232 INSPM/R FLIGHT CONTROL SELF LOCKING BOLTSC/W (XC8756)

14-Jun-2001 1

1950 PEARSON STMADISON WI

PROJECT, OLR FT.LEWIS, WA

ACE. INSP. PERFORMED AT 2192 ACFT HRS.AT MADISON WI. BY HH&Q (GC0981)

10-Sep-2001 1


AASF #2 WIARNGSOFUH-60-02-03 ONE TIME INSP OF THEFLIGHT CONTROL SYS, PITCH TRIM ASSY.C/W (XC3582)

12-Dec-2001 1

1950 PEARSON ST, MSNWI

AASF #2 WIARNGALL UH-60 SERIES ACT, INSPECTION OF APUFUEL LINE GROMMET, SOF UH-60-02-04/TB1-1520-237-20-242 C/W. (XR4264)

31-Jan-2002 1


AASF #2 WIARNG.INSPECT CONTROL ROD JAMNUTS IAW UH-60-02-ASAM-02 (TB1-1520-237-20-246) C/W.(XC3582)

21-Feb-2002 1

MADISON, WI. 53704-2517

AASF #2 WIARNG.UH-60-02-ASAM-04/TB 1-1520-237-20-244INSPECT CREW AND PASSENGER RESTRAINTSYSTEMS (XC8756)

20-Mar-2002 1


AASF #2 WIARNG.UH-60-02-ASAM-06/TB 1-1520-237-20-252INSPECTION OF SWAGE PINS/COLLARS ONBOOST SERVO ASSEMBLIES C/W. (XR4264)

29-Apr-2002 1



ACE PERFORMED AT 2192 ACFT HRS ATMADISON, WI BY P & D, PROJECT OLR, FTLEWIS, WA. (XK1861)

30-May-2002 1




8.7.DATE

6.REMARKS

4. 5.



AASF#2,WIARNG1/147TH AVIATION

UH-60-02-ASAM-08 INSPECT AN/ARC-220WIRING FOR CHAFING (XC8756)

25-Jun-2002 1

MADISON WI 53704

AASF#2, WIARNG1/147TH AVIATION

UH-60-02-ASAM-09 INSP T/R QUADRANT FORCORRECT HARDWARE C/W (XC8756)

28-Jun-2002 1

MADISON, WI 53704

AASF#2 WIARNG1/147TH AVIATION

UH-60-02-ASAM-10 INSP AERIAL REFUELINGPROBE, N/A THIS AIRFRAME (XC8756)

02-Jul-2002 1

MADISON WI 53704

AASF #2 WIARNGREVISION TO UH-60-02-ASAM-08 INSPECTAN/ARC-220 WIRING FOR CHAFING I/A/W UH-60-02-ASAM-11/TB1-1520-237-20-261 C/W.(XR4264)

03-Oct-2002 1


AASF # 2 WIARNGGEN-03-ASAM-01 INSPECTION OF THEBATTERY BOX, CY-8515 C/W. (XR4264)

19-Dec-2002 1



UH-60-02-ASAM-03 INSP PCL QUADRANTWIRING C/W AT 2192.2 A/C HRS (XC8756)

28-Feb-2003 1


1-108TH AVN, CO.DAEC # LE-KU001-0004 (WINDSHIELDS/WINDSCREENS) IN EXTREAMELY ROCKYENVIRONMENT OF SOUTHWEST ASIA, WITHCURRENT OP-TEMPO AIRCRAFT MOVEMENTSAND PARTS AVALIABILITY... TM PROVIDESTHE MOST SERVICABLE COMPONENT TO BEUSED, FROM A VISIBILITY STANDPOINT THEOPERATORS MUST DETERMIN WHEN THEDAMAGE TO THE WINDSCREEN EXCESSIVELYIMPACTS SERVICABLILITY. 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, AEROSPACEENGINEER, KUWAIT,[email protected]

22-Mar-2003 1

BALAD, IRAQ

JR759141

DYNCORPACE/CPCE PERFORMED AT 2192 ACFT HRSBY TEAMMEMBERS "K" & "I" AMCOMOLR/MWO BRANCH. (DM5698)

12-Aug-2003 1

KILLEEN TX.

D CO 1-108TH AVNREGT

12 AUG 03 R-1 AWR FOR UH-60A/LOPERATIONS DURING DESERT COMBATOPERATIONS (AWR1119) LATE ENTRY

12-Aug-2003 2

LSA ANACONDA,BALAD, IRAQ


15 AUG 03 R-4 AWR FOR UH-60A/LHELICOPTERS EQUIPPED WITH AUXILIARYPOWER UNIT (APU) INLET BARRIER FILTERS(AWR911) LATE ENTRY

15-Aug-2003 1




8.7.DATE

6.REMARKS

4. 5.




ISAQ FOR ALL UH-60A/L HELICOPTERSEQUIPPED WITH BALLISTIC PROTECTIONSYSTEM (BPS) (ISAQ 108) LATE ENTRY

30-Sep-2003 1



SOF UH-60-04-01 ALL UH-60A AND UH-60QACFT, ONE TIME INSPECTION OF FORWARDBELLCRANK SUPPORT INSTALLATIONHARDWARE C/W. (XR4264)

03-Oct-2003 1



ISAQ FOR UH-60A/L/Q AND HH-60LHELICOPTERS EQUIPPED WITH AEROSPACEFILTRATION SYSTEMS (AFS) AUXILIARYPOWER UNIT (APU) INLET BARRIER FILTERS(ISAQ 118) LATE ENTRY

21-Oct-2003 1



MAVEN IMPROVED HEATING SYSTEMINSTALLED IAW AWR 10 46 DATED 5 SEP 02.EMC TEST SUCCESFULY COMPLETED ON 2DEC 03 AT 2194.1 A/C HOURS (XS8477)

25-Nov-2003 1



PMS II COMPLETED AT 2192.2 A/C HRS, NEXTPMS II IS DUE AT 2692.2 A/C HRS (XC8756)

25-Nov-2003 2



TB 1-1520-237-20-167 INSPECTION ANDREPAIR OF ST 635 FRAME ASSEMBLY FORT/W STRUT CLEARANCE C/W AT 2192.2 A/CHRS (XC8756)

02-Dec-2003 1



SIGRTONIC TRANSCOM 2 PORTABLEBATTERY POWERED INTERCOM INSTALLEDAND EMC TEST COMPLETED IAW AWR DATED05 JUN 02 AT 2194.9 A/C HRS. (XC8756)

02-Dec-2003 2

MADISON, WIL 53704-2517


INSTALLATION OF OPTION II (MAVEN) CABINHEATER ACCOMPLISHED UNDER AWR 1046NOW COVERED BY ISAQ 110 DATED 06 FEB2004. (XK1861)

22-Mar-2004 1


AASF #2 WIARNG/ 1-147TH AVN

UH-60-04-ASAM-01 GLARE SHIELD LIGHTINGCIRUIT BREAKER REPLACEMENT C/W(XC8756)

22-Mar-2004 2


AASF #2 WIARNG/ 1-147TH AVN

UH-60-04-ASAM-02 T/R D/S FLANGE NUT INSPC/W (XC8756)

15-Apr-2004 1


AASF#2,WIARNG/1-147TH AVN

S.E.I BAMBI BUCKET TEMPORARILYINSTALLED IAW AWR 1054 DATED 16 APR 04,TO INCLUDE SACKSAFOAM DISPENSINGSYSTEM (XC8756)

14-May-2004 1


AASF#2 WIARNG/ 1-147TH AVIATION

AWR 1189 DATED 12 MAY 04 FOR THEINSTALLATION OF EBC-302HM ELT'SSUPERCEDES AWR DATED 17 DEC 99 EMCAND NVG CHECKS P/C/W (XC8756)

25-May-2004 1

1950 PEARSON STMADISON WI

AASF#2 WIARNG/ 1-147TH AVN

UH-60-04-02 DISABLE CABS SYSTEM, N/A THISAIRFRAME CABS NOT INST (XC8756)

11-Jun-2004 1




8.7.DATE

6.REMARKS

4. 5.




14 JUN 04 R-1 AWR FOR INSTALLATION ANDTESTING PROCEDURES OF THE EBC-302HMEMERGENCY LOCATOR TRANSMITTER (ELT)ON UH-60A/L/Q AND HH-60L AIRCRAFT (AWR1189) LATE ENTRY

14-Jun-2004 1


AASF #2/1-147TH AVNBN, WIARNG

SOF UH-60-04-03 CRASHWORTHY EXTERNALFUEL SYSTEM (CEFS) OPERATIONS. N/ATHIS ACFT, ESSS HARDPOINTS NOTINSTALLED. (XK1861)

15-Jul-2004 1


AASF#2, WIARNG/ 1-147TH AVN

AWR 1189 DATED 14 JUNE 04 FOR THEINSTALLATION OF EBC-302HM ELT'SSUPERCEDES AWR DATED 12 MAY 04 EMCAND NVG CHECKS PCW (XC8756)

23-Jul-2004 1


AASF #2/ 1-147TH AVNBN, WIARNG

SOF UH-60-04-04 MAIN ROTOR HUB REWORK,COLLECTION OF HUB PART NUMBERS ANDTIME SINCE NEW DATA FOR DETERMININGCANIDATES FOR HUB REWORK PROGRAM.(XK1861)

25-Aug-2004 1


AASF #2/ 1-147TH AVNBN, WIARNG

UH-60-04-ASAM-04 ALL H-60 HELICOPTERS,REVISIONI TO UH-60-04-ASAM-03 FUELSYSTEM INTEGRITY CHECKS C/W. (XK1861)

25-Aug-2004 2


PROJECT OLR WESTACE PERFORMED AT 2368 ACFT HRS ATMADISON WI. BY E & P (MM6284)

15-Sep-2004 1

FT. LEWIS WA.


TFM-138/KFM-985 STATE RADIO INSTALLEDIAW AWR 913 DTD 1 AUG 03. EMC TESTSUCCESSFULLY COMPLETED ON ACFT8123554 20 NOV 03. (XR4264)

23-Sep-2004 1



UH-60-04-ASAM-05 RESTRAINT SYSTEMINSPECTION C/W AT 2368 A/C HRS (XC8756)

05-Oct-2004 1

MADISON WI 53704

AASF#2, WIARNG/ 1-147TH AVN

S.E.I. BAMBI BUCKET (AWR 1054 DATED 16APR 04) NO LONGER USED FOR MISSIONS,OR TRAINING DUE TO CLIMACTICCONDITIONS (XC8756)

01-Dec-2004 1


AASF#2 WIARNG/ 1-147TH AVN BN

UH-60-05-ASAM-01 REVISION OF FUELSYSTEM INTEGRITY CHECKS, SUPERCEDESUH-60-04-ASAM-03 AND UH-60-04-ASAM-4. C/WAT 2400.4 A/C HRS (XC8756)

05-Jan-2005 1



ISAQ FOR INSTALLATION AND OPERATION OFAIR WARRIOR (AW) BLOCK 1 ON UH-60A/LHELICOPTERS (ISAQ 114) LATE ENTRY

28-Jan-2005 1



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

08-Feb-2005 1


AASF #2/1-147TH AVN,WIARNG

UH-60-05-ASAM-02 BLUE FORCE TRACKERINSTALLATION C/W AT 2426.0 ACFT HRS. BFTNOT INSTALLED ON THIS ACFT. (XK1861)

03-Mar-2005 1




8.7.DATE

6.REMARKS

4. 5.




AWR FOR INSTALLATION AND OPERATIONOF COMMON MISSILE WARNING SYSTEM(CMWS) AND IMPROVED COUNTERMEASURESDISPENSER (ICMD) ON UH-60A/LHELICOPTERS (AWR 1252) LATE ENTRY

10-Mar-2005 1



SOF UH-60-05-01 REACTIVATION OF COCKPITAIRBAG SYSTEM (CABS) C/W AT 2444.2 ACFTH RS. CABS NOT INSTALLED THIS ACFT.(XK1861)

16-Mar-2005 1



24 MAR O5 R-2 AWR FOR INSTALLATION ANDUSE OF THE M-240H MACHINE GUN ON UH-60A/L HELICOPTERS (AWR 1120) LATE ENTRY

24-Mar-2005 1



29 MAR 05 R-2 AWR FOR INFRARED (IR) ANTI-COLLISION LIGHT LENS INSTALLED ON USARMY UH-60A/L/Q AND HH-60L HELICOPTERS(AWR 1223) LATE ENTRY

29-Mar-2005 1



LOCALLY MANUFACTURED LOCKING DEVICE,INSTALLED IAW AWR DTD 07 JAN 99 HASBEEN REMOVED (XC8756)

12-Apr-2005 1



MAVEN IMPROVED HEATING SYSTEM,INSTALLED IAW AWR 1046, DTD 5 SEP 02, ANDISAQ 110 DTD 06 FEB 04 HAS BEEN REMOVED.(XC8756)

12-Apr-2005 2



SIGTRONIC TRANSCOM 2 PORTABLEBATTERY POWERED INTERCOM, INSTALLEDIAW AWR 05 JUN 02 HAS BEEN REMOVED(XC8756)

12-Apr-2005 3



TFM-138/KFM985 STATE RADIO INSTALLEDIAW AWR 913 DTD 01 AUG 03, HAS BEENREMOVED (XC8756)

12-Apr-2005 4



UH-60-05-ASAM-03 AIRCREW RESTRAINTSYSTEM COMPATABILITY INSP C/W (XC8756)

12-Apr-2005 5



UH-60-05-ASAM-04 TAIL LANDING GEAR YOKEINSPECTION C/W (XC8756)

12-Apr-2005 6


AMCOM PROJECT/OLR(EAST)

UH-60-05-ASAM-05 INSPECTION FORSELECTED SERIAL ON RIGHT TIE RODASSEMBLY, COMPLIED WITH AT 2473.7 ACFTHRS. (PG4153)

21-Apr-2005 1

HAAF, GA . 31409

AMCOM OLR EASTUH-60-05-ASAM-07 COMPLIED WITH @ 2473.7ACFT HOURS (BC7066)

25-May-2005 1

HAAF SAV GA

AMCOM OLR EASTUH-60-05-ASAM-08 COMPLIED WITH @ 2473.7ACFT HOURS (BC7066)

25-May-2005 2

HAAF SAV GA


AWR FOR INSTALLATION AND OPERATION OFENGINE INLET BARRIER FILTER (IBF) ON UH-60A/L/Q AND HH-60L HELICOPTERS (AWR1270) LATE ENTRY

26-May-2005 1




8.7.DATE

6.REMARKS

4. 5.




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

29-Jun-2005 1



AWR FOR UH-60A/L/Q AND HH-60LOPERATIONS WITH PILOT AND COPILOTDOORS REMOVED (AWR 1279) LATE ENTRY

06-Jul-2005 1


AASF MD ARNGUH-60-05-ASAM-06 KOCH & SONS TROOPSEAT BUCKLES C/W @ 2480.4 ACFT HOURS.(RG8010)

22-Jul-2005 1

APG(EA), MD 21010


29 JUL 05 R-2 ISAQ FOR UH-60A/L/Q, HH-60LAND AIRBORNE COMMAND AND CONTROLSYSTEM (A2C2S) HELICOPTERS EQUIPPEDWITH THE MELT MANUFACTURING (HELI-GUARD) BALASTIC PROTECTION SYSTEM(BPS) (ISAQ 111) LATE ENTRY

29-Jul-2005 1


AASF MD ARNGUH-60-05-ASAM-09 CEFS BOLT INSTALLATIONC/W (BI4843)

02-Aug-2005 1

APG(EA), MD 21010

AASF MDARNG(WV6Z98)

UH-60-05-ASAM-10 ONE TIME ANDRECURRING INSPECTION OF ENGINE OUTPUTSHAFT ASSY C/W AT 2480.4 ACFT HRS(DD4171)

09-Aug-2005 1

APG-EA, MD 21010

AASF MD ARNGUH-60-05-ASAM-01 FUEL INTEGRITY CHECKSCOMPLETED @ 2480.4 ACFT HOURS.(SS9694)

15-Sep-2005 1

APG(EA), MD 21010

AASF MD ARNGUH-60-05-SOF-02 C/W @ 2480.4 ACFT HRS.(RG8010)

21-Sep-2005 1

APG(EA) MD 21010

AASF MD ARNGAIRCRAFT PLACED ON ESM 09/21/05 @ 2480.4HRS. PMI 2 DUE @ 2830.4 ACFT HRS.(RG8010)

21-Sep-2005 2

APG(EA) MD 21010

AASF MD ARNGUH-60-05-ASAM-07 HYDROLIC BLEEDING C/W@ 2480.4 ACFT HOURS. (RG8010)

24-Sep-2005 1

APG(EA), MD 21010

AASF MD ARNGTAIL ROTOR CONTROL CABLE TENSIONCHECK C/W @ 2480.4 ACFT HOURS. TEMP 25C L/H CABLE 155 R/H CABLE 154 (RG8010)

26-Sep-2005 1

APG(EA), MD 21010

AASF MD ARNGTAIL ROTOR PITCH CONTROL ROD BIAS ECKC/W @ 2480.4 ACFT HOURS.PITCH CONTROLROD INITIAL FINALDIFFERENCERED4.828 5.171.343YELLOW 4.8955.203 .344BLACK4.171 4.453.282BLUE 4.1714.484 .313(RG8010)

26-Sep-2005 2

APG(EA), MD 21010

AASF MD ARNGPMI #1 COMPLETED @ 2480.4 ACFT HOURS.PMI #2 DUE @ 2830.4 ACFT HOURS (RG8010)

29-Sep-2005 1

APG(EA), MD 21010



8.7.DATE

6.REMARKS

4. 5.



AASF MD ARNGUH-60-05-ASAM-11 C/W @ 2480.1 ACFT HOURS(RG8010)

29-Sep-2005 2

APG(EA), MD 21010


22 DEC 05 R-3 AWR FOR UH-60A/LHELICOPTERS EQUIPPED WITH THEELECTRONIC DATA MANAGER (EDM) ANDBLUE FORCE TRACKING (BFT) SYSTEM(QUAD BAY INSTALLATION) (AWR 1300) LATEENTRY

22-Dec-2005 1


C CO 7-101UH-60-06-SOF-01 MAIN ROTOR HUBASSEMBLY C/W @ 2573.3 ACFT HRS(RH6085)

23-Dec-2005 1

BALAD, IRAQ

C CO 7-101TAIL ROTOR PITCH CONTROL ROD BIASCHECK C/W @ 2546.6 ACFT HRSP/C RODINITIAL FINALDIFFERENCERED 5.2074.871 .336 YELLOW5.202 4.874.328BLACK 4.5164.171 .335BLUE4.519 4.180.339(RH6085)

02-Jan-2006 1

BALAD, IRAQ


AWR FOR THE OPERATION OF COMMONMISSILE WARNING SYSTEM (CMWS) ANDIMPROVED COUNTERMEASURES DISPENSER(ICMD) ON UH-60A/L HELICOPTERS (AWR1299) LATE ENTRY

27-Jan-2006 1


B CO 563RD ASBM/R RIG COMPLETED FOR REPLACEMENT OFMAIN TRANSMISSION. AFT PRIMARY SERVO,FORWARD PRIMARY SERVO SHORTENED @2682.2 ACFT HRS. FWD ROD 1/4 TURNSHORTENED AFT ROD 1/4 TURN (RC1157)

26-Feb-2006 1

BALAD, IRAQ


AWR FOR UH-60A/L SERIES HELICOPTERSEQUIPPED WITH THE MICROCLIMATECOOLING SYSTEM WITH DIGITALCONTROLLER (AWR 1323) LATE ENTRY

27-Feb-2006 1


C CO 7-101 GSABMAIN TRANSMISSION, S/N A265-00305, P/N70351-08100-076. LETTER FOR CHIPS/FLAKESEXCEEDING LIMITS, MEC# LE-BAL012-1539REV1, AUTHORIZING RETURN TO SERVICE ASPER CONDITIONS STATED. SUSPECT DEBRISLEFT OVER FROM REBUILD. RECHECK 5-10FLT HRS AND 40 FLT HRS.CURRENT 2758.6A/C HRS (RH6085)

17-Apr-2006 1

BALAD, IRAQ

C CO 7-101 GSABMEC # LE-BAL012-1539 REV 2 PARTICLESFOUND ON MAIN MOD C/D EXCEEDING TMLIMITS. RETURN TO SERVICE AFTERSERVICABILITY CHECK 5-10 HR CHECK @2727.5 A/C HRS. REINSPECT @ 2758.6 A/CHRS. (RH6085)

22-Apr-2006 1

BALAD,IRAQ

C CO 7-101 GSABMEC # LE-BAL012-1539 REV 3 DEBRIS FOUNDON MAIN MOD CHIP DETECTOR WITHINLIMITS. REINSPECT @ PMI. RETURN TOSERVICE. (RH6085)

06-May-2006 1

BALAD, IRAQ



8.7.DATE

6.REMARKS

4. 5.



C C0 7-101 GSABUH-60-06-ASAM-02 M/R P/C ROD ENDJAMNUTS C/W @ 2759.6 A/C HRS. (RH6085)

24-May-2006 1

BALAD, IRAQ

C CO 7-101AWR 764(VIPII) DATED 18NOV03 EMC CK C/W(RH6085)

24-May-2006 2

BALAD, IRAQ

C CO 7-101AWR 1120(M240H) DATED 24MAR05 C/W(RH6085)

24-May-2006 3

BALAD, IRAQ

C CO 7-101AWR 1223(IR STROBE) DATED 29MAR05 C/W(RH6085)

24-May-2006 4

BALAD, IRAQ

C CO 7-101AWR 1270(EIBF) DATED 26MAY05 C/W(RH6085)

24-May-2006 5

BALAD, IRAQ

C CO 7-101AWR 1279(DOORS&WINDOWS) DATED06JUL05 C/W (RH6085)

24-May-2006 6

BALAD, IRAQ

C CO 7-101AWR 1299(CMWS) DATED 30SEP05 C/W(RH6085)

24-May-2006 7

BALAD, IRAQ

C CO 7-101AWR 1300(BFT) DATED 22DEC05 C/W(RH6085)

24-May-2006 8

BALAD, IRAQ

C CO 7-101ISAQ 111(BPS) DATED 29JUL05 C/W(RH6085)

24-May-2006 9

BALAD, IRAQ

C CO 7-101ISAQ 114(AIR WARRIOR) DATED 28JAN05 C/W(RH6085)

24-May-2006 10

BALAD, IRAQ

C CO 7-101ISAQ 118(AIBF) DATED 21OCT05 C/W(RH6085)

24-May-2006 11

BALAD, IRAQ

C CO 7-101PHASE TIMES ADJUSTED IAW UH-60-MIM-06-004 PMI#1 DUE @ 3200.4 A/C HRS PMI#2 DUE@ 2840.4 A/C HRS. (RH6085)

25-May-2006 1

BALAD, IRAQ

C CO 7-101UH-60-MIM-06-005 CHANGES TO LUBRICATIONAND OVERHAUL/RETIREMENT LIFE ITEMS INSUPPORT OF ESM SCHEDULING C/W @ 2831.1A/C HRS (RH6085)

04-Jun-2006 1

BALAD, IRAQ

C C0 7-101T/R G/B CHIP EVENT - ONE FLAKE EXCEEDELIMITS RELEASED FOR FLIGHT AS PER MEC#LE-BAL012-1715. POSTED IN HISTORICALS &LOGBOOK. S/N A006-00990 (RH6085)

04-Jun-2006 2

BALAD, IRAQ


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

06-Jun-2006 1


L3 COMMUNICATIONS /VERTEX

UH-60-06-ASAM-01 INSPECTION OF TAILLANDING GEAR SHOCK STRUT COMPLETEDDURING PMI-2 @ 2836.5 ACFT HRS (DW7677)

23-Jun-2006 1

CAMP AIRFJAN,KUWAIT


UH-60-06-ASAM-02 INSPECTION OF MAINROTOR RIGID CONNECTING LINK/PITCHCONTROL ASSEMBLIES COMPLETED DURINGPMI-2 @ 2836.5 ACFT HRS (DW7677)

23-Jun-2006 2

CAMP ARIFJAN,KUWAIT



8.7.DATE

6.REMARKS

4. 5.




UH-60-06-ASAM-03 INSPECTION OFSWASHPLATE DUPLEX BEARING COMPLETEDDURING PMI-2@ 2836.5 ACFT HRS (DW7677)

23-Jun-2006 3

CAMP AIRFJAN,KUWAIT


UH-60-06-ASAM-04 INSPECTION OF AIRCRAFTCOCKPIT AIRBAG SYSTEM IS N/A THISAIRFRAME. INSPECTION COMPLETED DURINGPMI-2 @ 2836.5 ACFT HRS (DW7677)

23-Jun-2006 4

CAMP ARIFJAN,KUWAIT


UH-60-06-SOF-01 INSPECTION OF M/R HUBASSEMBLY COMPLETED DURING PMI-2 @2836.5 ACFT HRS (DW7677)

23-Jun-2006 5

CAMP AIRFJAN,KUWAIT


UH-60-06-SOF-02 DISABLING OF COCKPITAIRBAG SYSTEM IS NA THIS ACFT.INSPECTION COMPLETED DURING PMI-2 @2836.5 ACFT HRS (DW7677)

23-Jun-2006 6

CAMP ARIFJAN,KUWAIT


MEC REQUEST FOR RIGHT HAND TEXASPATCH, MEC # LE-BAL013-1793 REPAIRAUTHORIZATION APPROVAL. REPAIR CABINFOOR TEXAS PATCH COMPLLETED DURINGPMI-2 @ 2836.5 ACFT HRS. (DW7677)

23-Jun-2006 7

CAMP ARIFJAN,KUWAIT


MEC REQUEST FOR L/H COCKPIT DOORPOST, MEC # LE-BAL013-1792 REPAIRAUTHORIZATION APPROVAL. L/H COCKPITDOOR POST COMPLLETED DURING PMI-2 @2836.5 ACFT HRS. (DW7677)

23-Jun-2006 8

CAMP ARIFJAN,KUWAIT


MEC REQUEST FOR R/H COCKPIT DOORPOST, MEC # LE-BAL013-1791 REPAIRAUTHORIZATION APPROVAL. R/H COCKPITDOOR POST COMPLLETED DURING PMI-2 @2836.5 ACFT HRS. (DW7677)

23-Jun-2006 9

CAMP ARIFJAN,KUWAIT


PMI2 C/W @ 2836.5 ACFT HRS PMI1 DUE @3196.5 A/C HRSPMI2 DUE @ 3556.5 A/C HRS(DW7677)

23-Jun-2006 10

CAMP ARIFJAN,KUWAIT

C. CO. 7-101 GSABUH-60-06-ASAM-05 BLUE FORCE TRACKERHARDWAER C/W @2915.8A/C HRS.

14-Aug-2006 1

BALAD IRAQ

HS427315


31 AUG 06 R-1 AWR FOR UH-60-A/L/Q ANDHH-60L HELICOPTERS TO OPERATE WITHENGINE INLET BARRIER FILTER (EIBF)INSTALLED IN SUPPORT OF DESERT COMBATOPERATIONS (AWR 1270) LATE ENTRY

31-Aug-2006 1



20 SEP06 R-4 AWR FOR UH-60A/LHELICOPTERS WITH VERTICAL SUPPORTPYLON FAIRING MODIFICATIONS (AWR 893)LATE ENTRY

20-Sep-2006 1


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

AIRCRAFT TRANSFERED TO 1-108TH AVN,36TH CAB

10-Oct-2006 1

LSA ANACONDA, IRAQ

JR759141

D CO 1/108TH AVNLATE ENTRY - ACFT TRANSFERED TO OIFTHEATER OF OPERATIONS BY PREVIOUSUNIT

15-Oct-2006 1

BALAD, IRAQ

KJ781803



8.7.DATE

6.REMARKS

4. 5.




UH-60-07-ASAM-01 COMPLIED WITH AT 3196.0AIRCRAFT HOURS.

09-Dec-2006 1

LSA ANACONDA, IRAQ

JR759141



09-Dec-2006 2

LSA ANACONDA, IRAQ

JR759141



17-Dec-2006 1

LSA ANACONDA, IRAQ

JR759141

1-108TH AVN, CO.DMEC# LE-BAL014-0373 (FUSELAGESTRUCTURE) STA. 308 WL.262 BL.34.5 CRACKFOUND AT THE RIGHT SIDE CHANNELTHROUGH THE WEB AND INBOARD CAPANGEL. REPAIR AUTHORIZED AT ACFT HRS.3196.0 IAW SIKORSKY PROCEDURES AJM-BL34-1B AND THE TECHNICAL MANUALS.(TRAVIS W. MESSA) [email protected]

18-Dec-2006 1

LSA ANACONDA, IRAQ

JR759141

1-108TH AVN, 36TH CABUH-60-07-ASAM-04 COMPLIED WITH AT 3198.7AIRCRAFT HOURS.

03-Jan-2007 1

LSA ANACONDA, IRAQ

JR759141


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

04-Jan-2007 1


RG021127

1-108TH AVN, 36THCAB, CO.D

UH-60-07-ASAM-05 (ARC-220 KY-100 START UPPROCEDURES) COMPLIED WITH AT 3311.4AIRCRAFT HOURS. KY-100 S/N- 2699

02-Feb-2007 1

LSA ANACONDA, IRAQ

AH311891


MEC LE-BAL014-0662, WASHER ON THEBLACK MAIN ROTOR BLADE S/N A007-02619UPPER TRAILING EDGE CUFF LUG ISDISBONDED. AUTHORIZATION GRANTED TOREPAIR DE-BONDED WASHER IAW DMWR 1-1615-281, TASK 3-14.6.9, MEC ENTERED IN THENARATIVE OF THE BLACK MAIN ROTORBLADE S/N A007-02619.

05-Feb-2007 1

LSA ANACONDA, IRAQ

JR759141

1-108TH AVN, CO.DUH-60-07-ASAM-06 (HOIST HARNESS) C/W AT3320.0 AIRCRAFT HOURS. N/A THIS ACFT.

23-Feb-2007 1

LSA ANACONDA, IRAQ

JR759141

1-108TH AVN, CO.DUH-60-07-AMAM-01 (CMWS EOMS ECU)COMPLIED WITH AT 3419.7 AIRCRAFT HOURS.

01-Apr-2007 1

LSA ANACONDA, IRAQ

JR759141

1-108TH AVN, CO.DMEC # LE-BAL015-0466 (FLIGHT CONTROLCOMPONENTS) ACFT HRS: 3538.0, UNITEXTENDED FLIGHT CONTROL AND CABIN TUB1000 HOURS INSP'S TO ALING WITH NEXT PMI.INSP'S DUE: 3898.0 ACFT HRS. EXTENDED 61.5FLIGHT HRS APPROVED BY: WALT, A.BUTSCH (GS-13 AEROSPACE ENGINEER)[email protected]

06-May-2007 1

LSA ANACONDA, IRAQ

JR759141



8.7.DATE

6.REMARKS

4. 5.



1-108TH AVN, CO.DUH-60A/L MAIN ROTOR RIG WORK SHEET. #1BLADE (RED) T/R BIAS READINGS:PERFORMED BY: J. SPEAR JS0860DIM-A DIM-B DIFF. RED: 4.7375.072 0.335 BLUE: 4.113 4.4470.334 YELLOW: 4.713 5.044 0.331BLUE: 4.181 4.516 0.335

11-May-2007 1

LSA ANACONDA, IRAQ

JR759141

L3 VERTEX,AEROSPACE

PMI-2 COMPLETED AT: 3538.0 AIRCRAFTHOURS. NEXT PMI-1 DUE @ 3898.0 AIRCRAFTHOURS.

14-May-2007 1

LSA ANACONDA, IRAQ

JR759141

1-108TH AVN, CO.DUH-60-07-ASAM-07 (CEFS BONDING JUMPER)COMPLIED WITH AT 3497.4 AIRCRAFT HOURS.

18-May-2007 1

LSA ANACONDA, IRAQ

JR759141

D CO 1/108 AVN REGTISAQ-128 (FOGS) 2 MAR 07R.3 APPLIED TOAIRCRAFT FOR INSTALLATION OF MWO 1-1520-237-50-94

03-Jul-2007 1

BALAD, IRAQ

DL861165

1-108TH AVN, CO.DUH-60-07-ASAM-08 (HMU/FUEL CONTROL O-RING) COMPLIED WITH AT 3622.0 AIRCRAFTHOURS. N/A THESE AIRCRAFT ENGINES.

20-Jul-2007 1

BALAD, IRAQ

JR759141

1-108TH AVN, CO.DUH-60-07-ASAM-09 (DEFECTIVE DIGITALENGINE CONTROL UNIT) COMPLIED WITH AT3624.8 AIRCRAFT HOURS. N/A THIS AIRCRAFT- ENGINES HAVE ECU'S

24-Jul-2007 1

BALAD, IRAQ

JR759141

D CO 1 108THCOMPLIED WITH UH 60--07-ASAM-10 14 AUG07

14-Aug-2007 1

BALAD IRAQ

MG764295

AASF#1UH-60-08-AMAM-02 (T/R OUTBOARDRETENTION PLATE SHIMS) COMPLIED WITHAT 3689.6 ACFT HRS

28-Nov-2007 1

TOPEKA, KS.

KJ781803

AASF#1UH-60-08-ASAM-04 (PILOT'S LOWER SEATRAIL CHAFING ELECTRICALHARNESS)COMPLIED WITH AT 3689.6 ACFT HRS

28-Nov-2007 2

TOPEKA, KS

KJ781803

AASF#1UH-60-08-ASAM-02 (POWER AVIALABLECONTROL CABLES) COMPLIED WITH AT3689.6 ACFT HRS

29-Nov-2007 1

TOPEKA, KS

KJ781803

AASF#1UH-60-08-AMAM-01 (MLG SHOCK STRUTS)COMPLIED WITH 3689.6 ACFT HRS

30-Nov-2007 1

TOPEKA, KS

KJ781803

AASF#1UH-60-08-ASAM-01 (CE/TROOP SEATATTENUATING WIRES) COMPLIED WITH AT3689.6 ACFT HRS

04-Dec-2007 1

TOPEKA, KS

KJ781803

AASF#1H-60-08-ASAM-05 REPLACEMENT OF TAILROTOR QUADRANT SPRING CAPSULEASSEMBLY CW AT 4462.6 ACFT HRS

12-Dec-2007 1

TOPEKA, KS

KJ781803

AMCOM FT HOODPROJECT OLR

ACE/CPCE PERFORMED AT 3691 AIRCRAFTHOURS BY TEAM MEMBERS K & Q.

09-Jan-2008 1

TOPEKA, KS

WS244328

AASF#1H-60-08-AMAM-04 (COCKPIT DOORJETTISONABLE WINDOWS) C/W AT 3898.0ACFT HRS

15-Jan-2008 1

TOPEKA, KS. 66609

KJ781803

AASF#1H-60-08-SOF-01 (M/R BLADE PIN 10 HR INSP)COMPLIED WITH AT 3691.1 ACFT HRS

30-Jan-2008 1

TOPEKA, KS

KJ781803



8.7.DATE

6.REMARKS

4. 5.



DS2/OLR EAST (RESET)ACFT INDUCTED INTO RESET @ 3700.1 ACFTHOURS BY DS2/OLR EAST (RESET).

04-Mar-2008 1

SAAF, FBNC 28310

JR739474

DS2/OLR EAST (RESET)DURING RESET INSPECTIONS, A CRACK WASFOUND AT THE RIGHT HAND SIDE DOUBLERTHROUGH THE WEB AT FS 328, WL 262, BL34.5. REPAIR WAS AUTHORIZED INACCORDANCE WITH MEC NUMBER F73563. ACOPY OF MEC WILL BE ATTACHED TOHISTORICAL RECORDS. DS2/QC

13-Mar-2008 1

SAAF, FBNC 28310

JR739474

AASF#1CW H-60-08-AMAM-07 AN/ASN-128B/DDOPPLER GPS NAVIGATION SET DGNS 3700.1ACFT HRS.

24-Mar-2008 1

TOPEKA, KS

JM884376

DS2/OLRACE COMPLETED @ 3700.1 ACFT HRS BYTEAM MEMBERS "EE & VV".

09-Apr-2008 1

FT. BRAGG, NC

JS544833

AASF #1H-60-08-ASAM-08 ALL H-60L/M SERIESAIRCRAFT ONE TIME INSP OF SELF-RETAINING FLIGHT CONTROL SELFRETAINING BOLTS. N/A THIS ACFT.

15-Apr-2008 1

TOPEKA, KS

KJ781803

DS2 OLRINSTALLATION OF EII-06-002 REV 1 AND EII-05-051 REV 02 COMPLIED WITH.

30-Apr-2008 1

FT BRAGG, NC

JW496160

DS2/OLR EAST (RESET)FUEL CELLS WERE REMOVED ANDINSPECTED IN ACCORDANCE WITH TB 1-1520-237-30-1 BY DS2/OLR MAINTENANCEPERSONNEL.

30-Apr-2008 2

SAAF, FBNC 28310

JR739474

DS2/OLR EAST (RESET)FUEL INTEGRITY CHECK WAS COMPLETEDON THIS DATE BY DS2/OLR MAINTENANCEPERSONNEL. STATUS: PASSED.

07-May-2008 1

SAAF, FBNC 28310

JR739474

DS2/OLR EAST (RESET)MAIN ROTOR RIG WAS COMPLETED ON THISDATE BY DS2/OLR MAINTENANCE TEAM.READINGS ARE AS FOLLOWS:PRIMARYSERVOSFWD: 3/4 TURNAFT: 3/4 TURNLAT: -1/4MIXER PIN WOULD NOT GO THROUGHMIXERTAIL ROTOR 3* BIAS WAS COMPLETEDON THIS DATE. READINGS ARE AS FOLLOWS:BEFORE AFTER DIFFERENCERED4.225 4.558 0.333YELLOW 4.8265.159 0.333BLUE 4.259 4.5950.336BLACK 4.813 5.146 0.333TAILROTOR CABLE TENSION CHECK WASCOMPLETED ON THIS DATE. READING AREAS FOLLOWS:TEMP: 20*C LEFT: 150,RIGHT:150RIGGING WAS COMPLETED WITHHYDRAULICS ON. A COPY OF RIGGING ISATTACHED TO ACFT PAPERWORK.

15-May-2008 1

SAAF, FBNC 28310

JR739474

DS2/OLR EAST (RESET)COMPLIED WITH CLEANING REQUIREMENTSIN TB 1-1500-200-20-1 ON THIS DATE BYDS2/OLR MAINTENANCE TEAM.

17-May-2008 1

SAAF, FBNC 28310

JR739474

DS2/OLR EAST (RESET)COMPLIED WITH REQUIREMENTS OF TB1-1500-200-20-31 ON AIRCRAFT DESERT OPERATIONCLEANING REQUIREMENTS DATED 10 AUG 04ON THIS DATE BY DS2/OLR MAINTENANCETEAM.

17-May-2008 2

SAAF, FBNC 28310

JR739474



8.7.DATE

6.REMARKS

4. 5.



DS2/OLR EAST (RESET)#2 CROSSBLEED BREAKAWAY VALVEREPLACE DURING RESET BY DS2/OLRMAINTENANCE TEAM.

17-May-2008 3

SAAF FBNC 28310

JR739474

DS2/OLR (RESET)H-60-08-ASAM-06 ON MAIN ROTOR PYLONSLIDING FORWARD FAIRING - COMPLIEDWIITH DURING RESET. DS2/QC.

17-May-2008 4

SAAF, FBNC 28310

JR739474

DS2/OLR EAST (RESET)H-60-08-ASAM-07 ON T700 SERIES ENGINEEXTERNAL WASH PROCEDURES - COMPLIEDWITH DURING RESET. DS2/OLR QC.

17-May-2008 5

SAAF FBNC 28310

JR739474

DS2/OLR EAST (RESET)H-60-08-ASAM-08 ON SELF RETAINING FLIGHTCONTROL BOLTS - NOT APPLICABLE ON THISACFT. DS2/OLR QC

17-May-2008 6

SAAF, FBNC 28310

JR739474

DS2/OLR EAST RESETH-60-08-ASAM-03 ON CHANGES TO CURRENTFUEL SYSTEM INTEGRITY CHECKS -COMPLIED WITH DURING RESET. DS2/OLRQC.

17-May-2008 7

SAAF, FBNC 28310

JR739474

DS2/OLR EAST (RESET)H-60-08-ASAM-05 ON TAIL ROTOR QUADRANTSPRING CAPSULE ASSEMBLY - COMPLIEDWITH DURING RESET. DS2/OLR QC.

17-May-2008 8

SAAF, FBNC 28310

JR739474

DS2/OLR EAST (RESET)TB 1-1520-237-30-1 DTD 21 SEPTEMBER 2007ON AIRCRAFT DESERT OPERATIONS SPECIALINSPECTION AND CLEANING REQUIREMENT -COMPLIED WITH ON THIS DATE BY DS2/OLRMAINTENANCE TEAM.

17-May-2008 9

SAAF, FBNC 28310

JR739474

DS2/OLR EAST (RESET)H-60-08-AMAM-08 ON FLIGHT CONTROLRIGGING UPDATE - COMPLIED WITHINSPECTION ON THIS DATE. SEE ABOVEENTRY. DS2/OLR QC

20-May-2008 1

SAAF, FBNC 28310

JR739474

DS2/OLR EAST (RESET)H-60-08-AMAM-08 - IAW AMAM THE CABINPITCH FIXED LINK, PN: 70400-02270-045,NEEDS TO BE REPLACE WITH PN: 70400-02270-048 @ 4060.1 AIRCRAFT HOURS OR NLT18 MAY 2010. DS2/OLR QC

20-May-2008 2

SAAF, FBNC 28310

JR739474

DS2/OLR EAST (RESET)TB 1-1520-237-30-1 ON AIRCRAFT DESERTOPERATIONS SPECIAL INSPECTION ANDCLEANING REQUIREMENT HAS BEENCOMPLIED WITH @ 3703.1 FLIGHT HOURS ONTHIS DATE. NEXT PMI DUE @4060.1 FLIGHTHOURS.

20-May-2008 3

SAAF, FBNC 28310

JR739474

AASF 1H-60-08-ASAM-10 ELECTRICAL WIRE CHAFEISSUES. CW AT 3740.1 ACFT HRS

09-Jul-2008 1

TOPEKA, KS

JM884376

AASF #1C/W H-60-08-ASAM-11 AT 3749.1 ACFT HRS.9FLIGHT CONTROL INSPECTION)

29-Aug-2008 1

TOPEKA, KS

KJ781803

AASF 1H-60-08-ASAM-12 DATED 15 SEPTEMBER 2008ALL H60 SERIES ACFT PARKER AEROSPACEAIR TURBINE STARTER (ATS). C/W AT 3778.8ACFT HRS.

18-Sep-2008 1

TOPEKA, KS

JM884376

AASF 1H-60-08-ASAM-13 DATED 22 SEPTEMBER 2008ALL H-60 SERIES AIRCRAFT FIREEXTINGUISHING TUBE UNION RING CW ATXXXX.X ACFT HRS

22-Sep-2008 1

TOPEKA, KS

JM884376



8.7.DATE

6.REMARKS

4. 5.



AASF 1H-60-08-ASAM-14 DATED 22 SEPTEMBER 2008ALL H-60 SERIES ACFT SUSPECT ENGINEHARNESSES CW AT XXXX.X ACFT HRS

22-Sep-2008 2

TOPEKA, KS

JM884376

AASF #2H-60-09-SOF-1 DTD 21 OCT O8 HMU THROTTLEVALVES CW 24 OCT 2008 AT 3780.2 ACFT HRS.

24-Oct-2008 1

SALINA, KS

JD508508

AASF #2H-60-09-SOF-02 DTD 7 NOV 2008, ALQ-144REMOVAL, CW ON 7 NOV 2008 AT 3786.2 ACFTHRS.

07-Nov-2008 1

SALINA, KS

JD508508

AASF #2H-60-09-SOF-03 DTD 13 NOV 2008, LIFELIMITED COMPONENTS, CW 20 NOV 2008 AT3795.0 ACFT HRS.

20-Nov-2008 1

SALINA, KS

JD508508

AASF #2H-60-09-ASAM-01 DTD 12 JAN 2009, SPARET700-GE-701C GAS GENERATORROTOR/STATOT ASSY, CW 13 JAN 2009 AT3813.0 ACFT HRS.

13-Jan-2009 1

SALINA, KS

JD508508

AASF #2AWR 1516, ELT PERMANENT INSTALLATION,APPLYED 3813.0 ACFT HOURS. FCCCOMPLETED FOR ALL UNIT ACFT ON THISAIRFRAME.

14-Jan-2009 1

SALINA, KS

JD508508

AASF #2COMPLIED WITH H-60-09-ASAM-05 UPDATEDTO LIFE LIMIT CHANGE FOR T/R QUADRANTSPRING CAPSULES (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

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

21-Apr-2009 1

SALINA, KS

DL861165

FT HOOD AFMAAIRCRAFT 8023489 ACE COMPLETED ATSALINA, KS AT 3855 ACFT HRS BY TEAMMEMBERS RR & Q

23-Apr-2009 1

KILLEEN, TX

AS425855

MO-AVCRADH60-07-ASAM-06 INSTALLATION OF CABLEGUARD PER WO# M80151. REFER: (RSN)1001031, INTERSHOP # 8I0733, OTR#AMOTRL49 AND MEO# A5908 COMPLETED BYMO-AVCRAD CONTACT TEAM ANDINSPECTED BY R. WILSON, T.I. #12RW626133, MO-AVCRAD, Q.C.

06-May-2009 1

SPRINGFIELD, MO.

RW626133

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

06-May-2009 2

SALINA, KS

DL861165

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

24-Aug-2009 1

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 @3911.1ACFT HRS

01-Sep-2009 3

SALINA, KS

DL861165

AASF #2COMPLIED WITH H-60-09-AMAM-06 CARGOHOOK CARTRIDGE ACTUATED DEVICE LIFEREDUCTION @3911.1 ACFT HRS

01-Sep-2009 4

SALINA, KS

DL861165



8.7.DATE

6.REMARKS

4. 5.



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

1109TH AVCRAD (LSI)ACFT STRIPPED WITH PLASTIC MEDIA,REPAINTED WITH MIL-DTL-64159 IAWCONTRACT # FA8101-09-D-0006

26-Oct-2009 1

GROTON CT. 06340

GL544447

1109TH AVCRADH-60-10-ASAM-03 FIRE BOTTLE DISCHARGELINE COMPLIED WITH

12-Nov-2009 1

GROTON CT

JW546464

1109TH AVCRADH-60-10-AMAM-04 ASN-128 DOPLER GPSCOMPLIED WITH

12-Nov-2009 2

GROTON CT

JW546464

B CO 1-108TH AVNREGT

COMPLIED WITH THE REQUIREMENTS OF H-60-10-ASAM-04 STABILITY AUGMENTATIONSYSTEM LINKS, AT ACFT HRS 3931.0

13-Jan-2010 2

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 3958.3 ACFT HRS

03-Feb-2010 2

SALINA, KS

DL861165

AASF #2COMPLIED WITH THE REQUIREMENTS OF H-60-10-ASAM-07, STABILATOR HINGE FITTINGS,AT 3998.7 ACFT HRS

22-Apr-2010 1

SALINA, KS

CS729537

AASF #2COMPLIED WITH THE REQUIRMENTS OF H-60-10-AMAM-12, IMPROVED DRAG BEAM, AT4018.7 ACFT HRS

28-Apr-2010 1

SALINA, KS

CS729537

FT HOOD AFMAAIRCRAFT 8023489 ACE COMPLETED AT 4019ACFT HRS 7 MAY 2010 AT SALINA, KS BYTEAM MEMBERS RR & W

07-May-2010 1

KILLEEN, TX

AS425855

B CO. 1/108TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-08, APU FIREWALL INSP. AT 4020.8ACFT 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 4028.2 ACFT HRS.

24-Jun-2010 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH REQUIREMENTS OFH-60-10-ASAM-12, ENG COMMON COMPONENTRETIREMENT CHANGE TIMES, 4043.1 ACFTHRS.

03-Aug-2010 1

SALINA, KS

CS729537

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-11, COMMON COMPONENTRETIREMENT CHANGE TIMES UPDATE,4043.1 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, 4052.1 ACFT HRS.

17-Aug-2010 1

SALINA, KS

DL861165



8.7.DATE

6.REMARKS

4. 5.



B CO 1/108TH AVNREGT (ASSLT)

COMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-16, RESCUE HOIST CABLE CUTHARNESS CONNECTOR. 4057.1 ACFT HRS

08-Sep-2010 1

SALINA, KS

DL861165

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

15-Oct-2010 1

SALINA, KS

CS729537

MOAVCRAD-URSCOMPLIED WITH H-60-11-ASAM-02 T/RSERVOCYLINDER ASSEMBLY HARDWARE

27-Oct-2010 1

SALINA, KS

KL471143

MOAVCRAD-URSCOMPLIED WITH H-60-ASAM-06 CYCLIC STOPBOLTS

18-Jan-2011 1

SALINA, KS

KL471143

MOAVCRAD-URSCOMPLIED WITH H-60-ASAM-04 AN/ARN-153TCN-500 TACAN REC. BEARING ERROR

18-Jan-2011 2

SALINA, KS

KL471143

MOAVCRAD-URSCOMPLIED WITH H-60-11-AMAM-04 LCFCHANGE 61

18-Jan-2011 3

SALINA, KS

KL471143

MOAVCRAD-URSCOMPLIED WITH H-60-11-ASAM-08, LOS/IFF &IVHMS ACCELEROMETER CONNECTOR

11-Feb-2011 1

SPRINGFIELD, MO

KL471143

MOAVCRAD-URSCOMPLIED WITH H-60-11-AMAM-03, OILCOOLER FAN AXIAL BEARING

11-Feb-2011 2

SPRINGFIELD, MO

KL471143

FT. HOOD AFMAONE TIME FCC REQUIRED PRIOR TO FIRSTFLIGHT WITH THE NEWLY INSTALLEDEQUIPMENT IAW AWR 1346 DATED 15 JUL 10(IVHMS), AWR 1425 DATED 18 AUG 10 (P3I),AWR DATED 30 SEP 10 (5TH SENSOR)COMPLETED ON ACFT 80-23495 @4967.0 ACFTHRS

18-Feb-2011 1

SALINA, KS

BD447755

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

14-Mar-2011 1

SALINA, KS

DL861165

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

14-Mar-2011 2

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

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



8.7.DATE

6.REMARKS

4. 5.



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

MOAVCRAD-URSH-60-11-AMAM-06 MEDEVAC CAROUSELREFURBISHMENT N/A THIS AIRCRAFT

17-Mar-2011 1

SPRINGFIELD, MO

KL471143

MOAVCRAD-URSCOMPLIED WITH H-60-11-ASAM-03 HAMILTONSTANDARD HMU

17-Mar-2011 2

SPRINGFIELD, MO

KL471143

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

17-Mar-2011 3

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 53406641 06-Apr-2011 1

SALINA, KS

DL861165

B CO 1-108TH AVNACFT HAS CMWS B KIT INSTALLED FORTRAINING, CONTROL IND. #05021, DISPENSER# 19939,19737,19834, CONTAINERCOUNTERMEASURE #, 11054,11030,10950,ECU # 2549, EOMS # 5382,1154,8813,8443,5237,SEQUENARS # 11941, 22846.

19-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 PERFORMED AT 4071 AIRCRAFT HOURSAT SALINA, KS BY TEAM MEMBERS K & Q.

26-Apr-2011 1

SALINA, KS

WS2443

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 4093.8ACFT HRS.

05-Jul-2011 1

TOPEKA, KS

JM884376

AASF#1H-60-11-SOF-01 (DISCREPANT SELF LOCKINGDOUBLE HEX NUTS) COMPLIED WITH AT4099.1 ACFT HRS.

23-Jul-2011 1

TOPEKA

TB866532



8.7.DATE

6.REMARKS

4. 5.



AASF#1H-60-11-ASAM-13 (ENG AIR ANTI-ICINGMODULATING VALVE) COMPLIED WITH AT4104.4 ACFT HRS

29-Jul-2011 1

TOPEKA

KJ781803

MOA AVCRAD120 DELTA SOFTWARE UPGRADE 511PROGRAM 4127.1 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 HRS4180.8, COMP HRS 3700.0

08-Oct-2011 1


JP579972

D CO 1-108TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-12-SOF-02. 4185.3 ACFT HRS.

13-Oct-2011 1


TP416505

D CO 1-108THCOMPLIED WITH REQUIREMENTS OF H-60-12-SOF-03. 4192.8 ACFT HRS.

17-Oct-2011 1


TP416505

AASF #1COMPLIED WITH REQUIREMENTS OF H-60-12-SOF-03 AT 4221 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 ENGINECOWLING REPAIR RESTRICTIONS AT 4233ACFT HRS

20-Apr-2012 1

SALINA, KANSAS

KJ781803

AASF #1H-60-12-AMAM-03 TRANSPONDER ANDCOMMON MISSLE WARNING SYTENINSTALLATION COMPLIED WITH AT 4233 ACFTHRS

20-Apr-2012 2

TOPEKA, KS

KJ781803

FT HOOD AFMAACE PERFORMED AT 4268 ACFT HRS ATTOPEKA, KS BY TEAM MEMBERS RR & W

13-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-09 BREEZE EASTERN EXTERNALRESCUE HOIST.

22-Aug-2012 1

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 THE REQUIREMENTS OF H-60-12-ASAM-07 CHAFFING WIRING.

07-Sep-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 1-108THMEC F152364, 48 MONTH FLIGHT CONTROLINSP DUE 29AUG2012 AND WILL BECOME RED"X" ON 29SEP2012. AUTHORIZATIONGRANTED FOR A ONE TIME 45 DAYEXTENSION DUE TO LACK OF MAINTENANCEPERSONNEL DUE TO POST-DEPLOYMENT/MOBILIAZATION.

19-Sep-2012 1

SALINA, KS

JL949482



8.7.DATE

6.REMARKS

4. 5.



B CO 1-108THCOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-17 OUTBOARD RETENTION PLATESHIMS.

19-Sep-2012 2

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 THE REQUIREMENTS OF H-60-13-AMAM-04 @ 4350.1 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


COMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-01 (T/R BEVEL GEAR NDI)

06-Mar-2013 1

SALINA, KS

DL861165

DYNCORP INTLACE PERFORMED AT 4391 ACFT HRS ATSALINA, KS BY TEAM MEMBERS RR & K

21-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

B CO 1-108TH AVNREGT.

COMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-01 (TAIL ROTOR) RED SET 3 DEGREES,YELLOW SET AT 3 DEGREES, BLACK SET AT 3DEGREES, BLUE SET AT 3 DEGREES.

24-Apr-2013 1

SALINA, KS

DL861165


TAIL ROTOR CABLE CHECK POST PMIREADINGS, TEMP. 23C CABLE TENTION LEFT-137, RIGHT -136

24-Apr-2013 2

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

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

AASF #2M/R TRACK AND BALANCE FOR BLADEREPLACEMENT: GND A-B: .56, GND A+B: .39,HVR A-B: .10, HVR A+B: .20 80KTS A-B: .05, 80KTS A+B: .18, 120KTS A-B: .19, 120KTS A+B:.11, 145KTS A-B: .02, 145 A+B: .34

12-Jul-2013 1

SALINA, KS

DL861165


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 EXTRERNALRESCUE HOIST)

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 #2H-60-14-ASAM-03 (EIBF BRACKET) COMPLIEDWITH AT 4509.8 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 1-1520-237-20-2 INSTALLED (AHRUSINGLE)

04-Feb-2014 1

SALINA, KS

DL861165

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

05-Mar-2014 1

SALINA, KS

DL861165

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

21-Mar-2014 1

SALINA, KS

DL861165



8.7.DATE

6.REMARKS

4. 5.



AASF #2COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-05 (LCF CHG 65) AT 4533.8 ACFT HRS

24-Mar-2014 1

SALINA, KS

CS729537

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

27-Mar-2014 1

SALINA, KS

DL861165

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

11-Apr-2014 1

SALINA, KS

DL861165


23-Apr-2014 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-06 (MIXER )

23-Apr-2014 2

SALINA, KS

DL861165

AFM RASM-WACE COMPLETED AT 4538 AIRCRAFT HOURSAT SALINA, KS BY TEAM MEMBERS W & Q.

23-Apr-2014 3

SALINA, KS

WS244328


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 PROCEDURE

11-Dec-2014 1

SALINA, KS

DL861165

FT HOOD AFMA RASMW

ACE COMPLETED AT 4655 AIRCRAFT HOURSAT SALINA, KS BY TEAM MEMBERS RR & K

08-Apr-2015 1

SALINA, KS

AS425855

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

28-May-2015 1

SALINA, KS

DL861165


02-Jun-2015 1

SALINA, KS

DL861165

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-15-AMAM-11 (MODE-S TRANSPONDER) 53406641ADDRESS

10-Jun-2015 1

SALINA, KS

DL861165

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



8.7.DATE

6.REMARKS

4. 5.



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

SCIENCE ANDENGINEERINGSERVICES LLC

H-60-ASAM-07 (MAIN ROTOR DEBONDING ANDTIP RIB CRACKING), NOT COMPLIED WITH

03-Mar-2016 1

HUNTSVILLE

JM866540


DATE AC HRS SHAFT VERTICAL REASON FOR VIB CHECKLONGITUDINALLATERAL

IPS READINGS4.

8023489HELICOPTER, UTILITYUH-60A3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Report Date: 03-Mar-2016 1/3

T/R BOOT REPAIR12-Jan-2000 T/R G/B OU 0.04001940.9

100HR REQUIREMENT14-Apr-2000 #1 ENG OUT 0.06001993.6

100HR REQUIREMENT14-Apr-2000 #2 ENG OUT 0.16001993.6

100HR REQUIREMENT14-Apr-2000 AXIAL FAN 0.050.2701993.6

100HR REQUIREMENT14-Apr-2000 T/R G/B OU 0.18001993.6

REPLACEMENT OF D/S BRNGS.27-Apr-2000 AXIAL FAN 0.120.201998.7

POSTPHASE BALANCE03-Nov-2003 #1 ENG OUT 0.15002192.2

POSTPHASE BALANCE03-Nov-2003 #2 ENG OUT 0.02002192.2

POSTPHASE BALANCE03-Nov-2003 AXIAL FAN 0.10.2602192.2

POSTPHASE BALANCE03-Nov-2003 T/R G/B OU 0.03002192.2

INB. RET. PLATE RETORQUE18-Dec-2003 T/R G/B OU 0.05002201.8

100 HR REQUIREMENT19-Apr-2004 #1 ENG OUT 0.09002297.7

100 HR REQUIREMENT19-Apr-2004 #2 ENG OUT 0.42002297.7

100 HR REQUIREMENT19-Apr-2004 AXIAL FAN 0.070.1202297.7

100 HR REQUIREMENT19-Apr-2004 T/R G/B OU 0.09002297.7

100 HR REQUIREMENT16-Dec-2004 T/R G/B OU 0.09002393.9

100 HR REQUIREMENT16-Dec-2004 AXIAL FAN 0.060.0802393.9

100 HR REQUIREMENT16-Dec-2004 #2 ENG OUT 0.42002393.9

100 HR REQUIREMENT16-Dec-2004 #1 ENG OUT 0.09002393.9

POST PMI 128-Sep-2005 AXIAL FAN 0.170.1202480

POST PMI 128-Sep-2005 #1 ENG HSS 0.1002480

POST PMI 128-Sep-2005 T/R G/B OU 0.08002480

POST PMI 128-Sep-2005 #2 ENG HSS 0.31002480

POST PHASE30-Jun-2006 HSS ENG#1 00.2302836.5

POST PHASE30-Jun-2006 HSS ENG #2 00.2702836.5

POST PHASE30-Jun-2006 OIL COOLER 0.060.0902836.5

POST PHASE30-Jun-2006 TAIL ROTOR 00.102836.5

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.



POST PMI #131-Dec-2006 ENG #1 00.203196.8

POST PHASE #131-Dec-2006 ENG #2 00.2503196.8

POST PHASE #131-Dec-2006 OIL COOLER 0.090.103196.8

POST PHASE #131-Dec-2006 TAIL ROTOR 00.0403196.8

POST PHASE #131-Dec-2006 MAIN ROTOR 00.1103196.8

120 HOUR INSP.03-Feb-2007 #1 ENGINE 00.0703311.4

120 HOUR INSP.03-Feb-2007 #2 ENGINE 00.0803311.4

120 HOUR INSP.03-Feb-2007 OIL COOLER 0.230.2303311.4

120 HOUR INSP.03-Feb-2007 T/R 00.1303311.4

REPLACEMENT OF #2 ENG29-Mar-2007 #2 ENG 00.2903419

POST PHASE14-Apr-2007 T/R 0.03003463.8

120 HR03-Aug-2007 T/R 0.03003651.4

120 HR03-Aug-2007 OIL COOLER 00.0603651.4

120 HR03-Aug-2007 #1 ENG 0003651.4

120 HR03-Aug-2007 #2 ENG 00.1603651.4

POST RESET21-May-2008 #1 ENG 0.4003700.1

POST RESET21-May-2008 #2 ENG 0.47003700.1

POST RESET21-May-2008 OIL CLR 00.2303700.1

POST RESET21-May-2008 TAIL 0.09003700.1

REINSTALLATION OF T/R10-Jun-2008 T/R 0.09003711.3

120 HR13-Nov-2009 T/R 0.04003926.4

120 HR13-Nov-2009 #1 ENG 0.02003926.4

120 HR13-Nov-2009 #2 ENG 0.03003926.4

120 HR13-Nov-2009 OIL COOLER 00.1803926.4

PHASE/IVHMS21-Apr-2011 #1 ENG 0.12004070.9

PHASE/ IVHMS21-Apr-2011 #2 ENG 0.41004070.9

PHASE/ IVHMS21-Apr-2011 OIL COOLER 00.1504070.9




IPS READINGS4.



PHASE/ IVHMS21-Apr-2011 T/R 00.204070.9

POST PHASE30-Apr-2013 T/R 0.12004391.4

POST PHASE30-Apr-2013 OIL COOLER 00.7304391.4

POST PHASE30-Apr-2013 #1 ENG 0.48004391.4

POST PHASE30-Apr-2013 #2 ENG 0.13004391.4

120 HR14-Jan-2014 #2 ENG 0.19004506.4

120 HR14-Jan-2014 #1 ENG 0.37004506.4

120 HR14-Jan-2014 OIL COOLER 0.150.5604506.4

14-Jan-2014 T/R 0.15004506.4

ENG REPLACEMENT13-Aug-2014 #1 ENG 0.39004602.3

ENG REPLACEMENT13-Aug-2014 #2 ENG 0.47004602.3

ENG REPLACEMENT02-Oct-2015 #1 ENG 0.38004731.1

ENG REPLACEMENT02-Oct-2015 #2 ENG 0.44004731.1

6. Remarks




8023489HELICOPTER, 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 4748.610TM 1-1520-237-PMDPERFORM M/R SPINDLE LUGS,M/R CUFF, TIP CAPSINSPECTION

4738.6H

A022 17 Feb 201614TM 1-1520-237-23-914 DAY FLYABLE STORAGEENGINE RUN UP

03 Feb 2016D

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

29 Jan 2016D

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

13 Jan 2016D

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

13 Jan 2016D

A103 04 Feb 201630TM 1-1500-344-23AIRCRAFT WASH DUE 05 Jan 2016D

A110 4744.140TM 1-1520-237-PMSPMS 40 HOUR INSPECTION 4704.1H

A115 05 Feb 201630TM 1-1520-237-23-12LUBE REQUIRMENTS 06 Jan 2016D

A115 4773.140TM 1-1520-237-23-12LUBE REQUIRMENTS 4733.1H

A116 5001.3360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

4641.3H

A116 13 Feb 201612H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

13 Feb 2015M

A117 5001.3360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 4641.3H

A117 13 Feb 201612H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 13 Feb 2015M

A160 02 Apr 201690TM 1-1520-237-23-1290 DAY CORROSIONINSPECTION

03 Jan 2016D

A177 28 Mar 201690AR 95-190 DAY REVIEW/UPDATE OF 365-4 ENTRIES

29 Dec 2015D

A200 4744.1120H-60-08-ASAM-11120 HOUR INSPECTIONREQUIREMENTS ON DOWEL PIN

4624.1H

A210 4744.1120TM 1-1520-237-23-12120 HOUR INSPECTIONREQUIREMENTS

4624.1H

A211 5001.3360H-60-10-AMAM-11APU OIL SAMPLE 4641.3H

A211 13 Feb 201612H-60-10-AMAM-11APU OIL SAMPLE 13 Feb 2015M

A213 4744.1120TM 1-2840-248-23ENGINE COMPRESSORCLEANING

4624.1H

A214 4744.1120TM 1-1520-237-23-12CLEAN TAIL WHEEL ADAPTER 4624.1H

A222 03 Dec 2016360TM 1-1680-377-13&PAMSS SURVIVAL KITINSPECTION

09 Dec 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 4751.4360TM 1-1520-237-23-12STABILATOR ACTUATOR ASSYLUBE

4391.4H

A296 4751.4360TM 1-1520-237-23-12STABILATOR INSPECTION 4391.4H

A298 5086.6360TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 4726.6H

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

A299 5028.1360TM 1-1520-237-23-12SWASHPLATE LUBE 4668.1H

A299 15 Apr 201612TM 1-1520-237-23-12SWASHPLATE LUBE 15 Apr 2015M

A320 4751.4360TM 1-2840-248-23ENGINE INSPECTION &CLEANING

4391.4H

A400 4751.4720TM 1-1520-237-PMIPMI-1 4031.4H

A401 5111.4720TM 1-1520-237-PMIPMI-2 4391.4H

A408 5111.4720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-2, AREA 5 AND 6)

4391.4H

A410 4751.4720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-1, AREA 1 THRU 4)

4031.4H

A415 5111.4720H-60-10-AMAM-11MAIN GEARBOX OIL SAMPLE-PART # 073, 074, 076

4391.4H

A470 5200.11500TM 1-1520-237-23-12REPLACE NUMBER TWOCROSSFEED VALVE

3700.1H

A471 6217.12160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

4057.1H

A472 6217.12160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

4057.1H

A473 6217.12160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

4057.1H

A476 8700.15000TM 1-1520-237-23-12REPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

3700.1H

A477 8700.15000TM 1-1520-237-23-12REPLACEMENT OF STABILATORACTUATOR BOLTS

3700.1H

A480 71925000TM 1-1520-237-23-12REPLACE PIVOT BOLT 70400-08159-101,102,103,104

2192H

A485 71925000TM 1-1520-237-23-12REPLACE BELLCRANK BOLT70400-08159-105,106,107,108

2192H

A496 05 Feb 20166TM 1-1500-204-23-1CF3BR FIRE EXTINGUISHERWEIGHT TEST & INSPECTION

05 Aug 2015M

A501 15 Feb 20166TM 1-1520-237-23-12MAIN ROTOR BLADE PRESSURECHECK

15 Aug 2015M






7. FREQUENCY 4.




INSP

A502 21 Apr 20166TM 1-1520-237-23-12INSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

21 Oct 2015M

A530 06 May 201612DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

06 May 2015M

A532 20 May 201612TM 1-1500-204-23-4COMPASS SWING / RMI 20 May 2015M

A533 10 Jun 201612TM 1-1520-237-23-12PITOT STATIC SYSTEMINSPECTION

10 Jun 2015M

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

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

12 Jun 2015M

A541 22 Jan 201712TM 1-1520-237-23, C4REPLACE DIGITAL CLOCKBATTERY

22 Jan 2016M

A550 05 Mar 201612AWR1346R16IVHUMS BATTERYREPLACEMENT

05 Mar 2015M

A553 20 Jan 201612AR 95-1AIRCRAFT WEIGHINGINVENTORY (365-1)

20 Jan 2015M

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

27 Aug 2014M

A621 27 Jan 201724AR 95-1AIRCRAFT WEIGHING CLASS 2 27 Jan 2015M

A625 19 Sep 201760TM 11-6140-203-23&PREPLACEMENT OF SLABBATTERY (SLAB)

19 Sep 2012M

A630 01 Sep 2020114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Mar 2011M

A633 01 Sep 2020114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Mar 2011M

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

01 Sep 2011M

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

01 Sep 2011M

A642 01 Dec 201872TB 9-1300-385CARGO HOOK CARTRIDGEREPLACEMENT, DODIC MJ21

01 Dec 2012M

A648 17 May 2023180TM 1-1520-237-23REPLACE T/R SPRING CAPSULEASSY

17 May 2008M

A665 03 Apr 201748H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

03 Apr 2013M

A670 30 Aug 201648TM 1-1520-237-23-1CABIN TUB INSPECTION 30 Aug 2012M

A673 03 Apr 201748TM 1-1520-237-23-12FUEL CELL CORROSIONINSPECTION

03 Apr 2013M

A675 02 Oct 201648TM 1-1520-237-23-12FLIGHT CONTROL ROD INSP 02 Oct 2012M

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

0H






7. FREQUENCY 4.




INSP

E040 28 Mar 201690TM 11-5841-294-12APR-39 RADAR/LASERWARNING OPNL CHECK, 5841-01-236-8951

29 Dec 2015D

E108 12 Feb 201630TM 11-5810-262-23KY-58 PMCS/OPNL CHECK(STANDBY)

13 Jan 2016D

E135 13 Jul 20166TM 11-5821-333-12AN/ARC-201(V) SINCGARSRADIO HUB BATT REPL

13 Jan 2016M

E155 06 Mar 2016180TM 11-5810-262-23KY-58 BATTERY REPLACEMENT 08 Sep 2015D

E300 12 Feb 201630AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

13 Jan 2016D

E300 4853.1120AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

4733.1H

E320 18 Feb 2017360AWR 1516 FOR ELTEMERGENCY LOCATORTRANSMITTER G-SWITCH (EBC-406HM)

24 Feb 2016D

E325 06 Mar 201960AWR 1516R2 FOR ELTREPLACEMENT OF ELTBATTERY PN GS-46

06 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: 1/1203-Mar-2016

80234891520010350266 00HELICOPTER, UTILITY

162001231183103A01

3264733BEM007770250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001231183103A01

36403700C001-0334670250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001421089003B01

40964391C00202010SL70250-13101-044SHOCK ABSORBER (TAIL) CCCC COND COND

165001285302405A01Z

10113700A106-0508370106-08100-046MAIN ROTOR DAMPER CCCC COND COND

165001285302405A01Z


165001285302405A01Z


165001285302405A01Z

17103926A1060660070106-08100-046DAMPER ASSY, M/R CCCC COND COND

531501537465205A02H

03700B9410488470103-08108-041SOLID BLADE PIN CCCC COND COND

531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


531501537465205A02H


161501199764605A03A

3062638A107-0212470104-08000-050SWASHPLATE ASSY CCCC COND COND

161501078571806A11 LEFT HAND

11921192A258-0055670351-08080-043ACCESSORY MODULE CCCC COND COND

161501383899206A11 R/H

11992192A258-0476670351-08080-045ACCESSORY MODULE CCCC COND COND

161501503311506A

28572632A265-0030570351-08100-076MAIN TRANSMISSIONMODULE

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






161501353382506E R/H

21832192A264-0041670351-08001-049INPUT MODULE CCCC COND COND

161501353382506E L/H

18402192A264-0296070351-08001-049INPUT MODULE CCCC COND COND

168001074515206F

65554487A0050057170357-06300-042INTERMEDIATE GEARBOX CCCC COND COND

161501376508906G01

45524487A006-0081870358-06600-046TAIL ROTOR GEARBOXASSY

CCCC COND COND

161501524780506H04

5134599C8450797070361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501524780506H04

5134599C8450800570361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501081277506H06 SECTION 1

00A271-0027170361-03001-045SHAFT ASSY, T/R DRV SEC1

CCCC COND COND

NSN PENDING06H08 OIL COOLER


CCCC COND COND

161501082650006H09 SECTION 2 MID

11921192A272-0079270361-05001-045SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501082650006H09 SECTION 2FRONT

11921192A272-0079370361-05001-045SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501158952206H09 # 2 AFT

04057WG30024-00624

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

CCCC COND COND

161501083295306H11 SECTION 3


CCCC COND COND

161501158578806H12 7

31034057A2740164370361-06002-047SHAFT ASSY, T/R DRV SEC7

CCCC COND COND

432001207722807A01 #1

4583692194578ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01 3

9484035248631ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01

4352836K098AABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

481001102247307B05A

03651116443213850-3-1VALVE, SOLENIOD CCCC COND COND

481001102247307B05A L/H

0219297903213850-3-1VALVE, SOLENIOD CCCC COND COND

165001084309607B11

02192B401-0024770651-03201-102ACCUMULATOR CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






168001342049608B20

3561423233570450-01043-124PANEL INDICATOR (PDU) CCCC COND COND

168001342049608B20 CO PILOT

990378148370450-01043-124PANEL INDICATOR (PDU) CCCC COND COND

611501114969609A01 #2GENERATOR

47937001511E28B302-8-DMGENERATOR CCCC COND COND

611501114969609A01 #1

1229389883-A105128B302-8-DMGENERATOR CCCC COND COND

168001310225911C21

045528L513-0035970400-02300-048MIXER ASSEMBLY CCCC COND COND

156001411515611D17

02480F338-0326770209-22103-067SERVO BEAM FITTING CCCC COND COND

156001411515011D17

02480H338-0002470209-22103-069SERVO BEAM FITTING CCCC COND COND

156001411514811D17

02480F338-0264770209-22103-071SERVO BEAM FITTING CCCC COND COND

168001261204411D25

23064487024370400-06641-117STABILATOR ACTUATOR CCCC COND COND

168001261204411D25

52264487V0715070400-06641-117STABILATOR ACTUATOR CCCC COND COND

599601316274311D26 2

63203823262570902-02001-048STABILATOR AMPLIFIER CCCC COND COND

599601316274311D26

03740856A70902-02001-048STABILATOR AMPLIFIER CCCC COND COND

299501169529115A04

182337007584-1287163290-100ENGINE SEQUENCINGUNIT

CCCC COND COND

589501245909019E05A

04529133EESM-C-967292RECEIVER-TRANSMITTERRADAR

CCCC COND COND

584101245909319E05C

045290094FFA3060591INDICATOR HEIGHT CCCC COND COND

660501503528419E06A

04573359765100-20ATTITUDE HEADINGREFERENCE UNIT

CCCC COND COND

661001119718052A

10124838504339769800-2AUTOMAT 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 COMPONENTS5/1203-Mar-2016

00

156001081924402C15J7200

UNKNOWN 0370070209-06051-042TAIL PYLON FITTING RCRC3500

161501481695305A01A6928

A308-00647 1872370070070-10046-055HUB, M/R ROTOR ASSY RCRC5100

161501374720305A01I5143

33896-3504 1657370070102-08200-056MAIN ROTOR SPINDLEASSY

RCRC3100

161501442692605A01I10791

A001-06650 0439170102-08200-069MAIN ROTOR SPINDLEASSY

RCRC6400

161501442692605A01I10100


RCRC6400

161501442692605A01I9938


RCRC6400

161501074515105A01L16676

015152-02042 1024370070351-08186-043MAIN ROTOR SHAFTEXTENDER

RCRC14000

161501127738805A01T13000

A327-00690 4038403870107-08400-046BIFILAR, M/R ROTORASSY

RCRC13000

161501106190305A028776

A00700736 5247442370150-09100-043MAIN ROTOR BLADEASSY

RCRC9600

161501106190305A027888


RCRC9600

161501106190305A0211103


RCRC9600

161501106190305A0211929


RCRC9600

161501113818805B02 BLACK/BLUE10920

A00902283 3471439170101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501113818805B02 RED/YELLOW10083

A00903097 4308439170101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501083681206G01B13402

D257-00389 2136353870102-11101-042O/B RETENTION PLATE(T/R)

RCRC12000

414001329342806H236058

1226 0353852E15-1FAN AXIAL 002520

156001129125607A24 ROLL13470

B112-04549 3230370070410-02500-049SAS ACTUATOR RCRC13000

156001129125607A24 PITCH13301

B112-05265 3399370070410-02500-049SAS ACTUATOR RCRC13000

156001129125607A24 YAW15821

C112-02812 15283670410-02500-049SAS ACTUATOR RCRC13000

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

EDITION MAY 67 IS OBSOLETE

AIRCRAFT COMPONENT HISTORICALRECORD

DA FORM 2408-16-E, OCT 91









Report Date:


00

161501141753211C236311

B23301516 2865448770400-06100-042TAIL ROTOR PITCHCHANGE SHAFT

33622160

165001305695411C2519151

B30000776 266144872227000-17TAIL ROTOR SERVOASSY

RCRC15000

165001143122611D01 LAT26878

B303-04824 32422814274000-1031MAIN ROTOR PRIMARYSERVO

RCRC24400

165001143122611D0127602

B30313245 03538274000-1031MAIN ROTOR PRIMARYSERVO

RCRC24400

165001143122611D0126696

B303-03906 3520263270410-02820-054MAIN ROTOR PRIMARYSERVO

RCRC24400

156001082921311D0516664

B391-00247 0070400-08112-044AFT TIE ROD SUPTFITTING

RCRC17000

168001164416011D066255

MM00898 0439170400-08111-042AFT TIE ROD ASSY RCRC2200

156001286887011D076696

390-01596 0263270400-08117-049AFT BELLCRANK SPTASSY

RCRC4400

304001287243811D0811780

C380-00391 0111670400-08151-061LATERAL SWASHPLATELINK

RCRC11000

161501078569511D097356

D28900585 1567219270400-08150-043LATERAL SERVOBELLCRANK

RCRC5500

168001158965311D1114702

M346-R0075 4038403870400-08104-048AFT WALKING BEAM RCRC11000

156001289269711D1318055

344-01834 0439170400-08115-046LEFT TIE ROD RCRC14000

156001296948611D14 R/H6000

288-00660 0283670400-08114-051RIGHT TIE ROD ASSY RCRC3500

168001090204811D1516856

D35500225 2192219270400-08101-044FORWARD BELLCRANK RCRC15000

156001221261911D16 BRIDGE8100

B367-04250 0283670400-08162-042FWD BELLCRANK SPTASSY

RCRC5600

156001095713211D17 STA297-489L-O/B

19664UNK3489 0070219-02134-046SERVO BEAM FITTING RCRC

20000













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 8023489 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 8 of 12

03-Mar-2016

3500 7200

156001081924402C15J

03700TAIL PYLON FITTING UNKNOWN70209-06051-042 RCRC

COND COND

162001231183103A01

3264733FWD FIXED GEARSHOCK

BEM007770250-12051-045 CCCC

COND COND

162001231183103A01


C001-0334670250-12051-045 CCCC

COND COND

162001421089003B01

40964391SHOCK ABSORBER(TAIL)

C00202010SL70250-13101-044 CCCC

5100 6928

161501481695305A01A

18723700HUB, M/R ROTOR ASSY A308-0064770070-10046-055 RCRC

3100 5143

161501374720305A01I

16573700MAIN ROTOR SPINDLEASSY

33896-350470102-08200-056 RCRC

6400 10791

161501442692605A01I


A001-0665070102-08200-069 RCRC

6400 10100

161501442692605A01I


A001-0680070102-08200-069 RCRC

6400 9938

161501442692605A01I


A001-0750370102-08200-069 RCRC

14000 16676

161501074515105A01L

10243700MAIN ROTOR SHAFTEXTENDER

015152-0204270351-08186-043 RCRC

13000 13000

161501127738805A01T

40384038BIFILAR, M/R ROTORASSY

A327-0069070107-08400-046 RCRC

COND COND

165001285302405A01Z

10113700MAIN ROTOR DAMPER A106-0508370106-08100-046 CCCC

COND COND

165001285302405A01Z


COND COND

165001285302405A01Z


COND COND

165001285302405A01Z

17103926DAMPER ASSY, M/R A1060660070106-08100-046 CCCC

9600 8776

161501106190305A02

52474423MAIN ROTOR BLADEASSY

A0070073670150-09100-043 RCRC

9600 7888

161501106190305A02


A0070256770150-09100-043 RCRC

9600 11103

161501106190305A02


A0070940870150-09100-043 RCRC

9600 11929

161501106190305A02


A0071266370150-09100-043 RCRC

COND COND

531501537465205A02H

03700SOLID BLADE PIN B9410488470103-08108-041 CCCC

COND COND

531501537465205A02H


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

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


HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 9 of 12

03-Mar-2016

COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

161501199764605A03A

3062638SWASHPLATE ASSY A107-0212470104-08000-050 CCCC

10000 10920

1615011138188 BLACK/BLUE05B02

34714391TAIL ROTOR BLADEASSY

A0090228370101-31000-043 RCRC

10000 10083

1615011138188 RED/YELLOW05B02

43084391TAIL ROTOR BLADEASSY

A0090309770101-31000-043 RCRC

COND COND

1615010785718 LEFT HAND06A11

11921192ACCESSORY MODULE A258-0055670351-08080-043 CCCC

COND COND

1615013838992 R/H06A11

11992192ACCESSORY MODULE A258-0476670351-08080-045 CCCC

COND COND

161501503311506A

28572632MAIN TRANSMISSIONMODULE

A265-0030570351-08100-076 CCCC

COND COND

1615013533825 R/H06E

21832192INPUT MODULE A264-0041670351-08001-049 CCCC

COND COND

1615013533825 L/H06E

18402192INPUT MODULE A264-0296070351-08001-049 CCCC

COND COND

168001074515206F

65554487INTERMEDIATEGEARBOX

A0050057170357-06300-042 CCCC

COND COND

161501376508906G01

45524487TAIL ROTOR GEARBOXASSY

A006-0081870358-06600-046 CCCC

12000 13402

161501083681206G01B

21363538O/B RETENTION PLATE(T/R)

D257-0038970102-11101-042 RCRC

COND COND

161501524780506H04

5134599DRIVESHAFT ASSYENGINE

C8450797070361-08014-041 CCCC

COND COND

161501524780506H04

5134599DRIVESHAFT ASSYENGINE

C8450800570361-08014-041 CCCC

COND COND

1615010812775 SECTION 106H06

00SHAFT ASSY, T/R DRVSEC 1

A271-0027170361-03001-045 CCCC

COND COND

NSN PENDING OIL COOLER06H08


A270-0148270361-03009-046 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 10 of 12

03-Mar-2016

COND COND

1615010826500 SECTION 2 MID06H09

11921192SHAFT ASSY, T/R SEC3,4,5

A272-0079270361-05001-045 CCCC

COND COND

1615010826500 SECTION 2 FRONT06H09


A272-0079370361-05001-045 CCCC

COND COND

1615011589522 # 2 AFT06H09


WG30024-0062470361-05001-051 CCCC

COND COND

1615010832953 SECTION 306H11


A273-0027670361-05002-045 CCCC

COND COND

1615011585788 706H12


A2740164370361-06002-047 CCCC

2520 6058

414001329342806H23

03538FAN AXIAL 122652E15-1 00

COND COND

4320012077228 #107A01

4583692PUMP MODULE ASSY,HYDRAUL

194578ABR53023-06 CCCC

COND COND

4320012077228 307A01


248631ABR53023-06 CCCC

COND COND

432001207722807A01


K098AABR53023-06 CCCC

13000 13470

1560011291256 ROLL07A24

32303700SAS ACTUATOR B112-0454970410-02500-049 RCRC

13000 13301

1560011291256 PITCH07A24

33993700SAS ACTUATOR B112-0526570410-02500-049 RCRC

13000 15821

1560011291256 YAW07A24

152836SAS ACTUATOR C112-0281270410-02500-049 RCRC

COND COND

481001102247307B05A

03651VALVE, SOLENIOD 116443213850-3-1 CCCC

COND COND

4810011022473 L/H07B05A

02192VALVE, SOLENIOD 97903213850-3-1 CCCC

COND COND

165001084309607B11

02192ACCUMULATOR B401-0024770651-03201-102 CCCC

COND COND

168001342049608B20

35614232PANEL INDICATOR (PDU) 33570450-01043-124 CCCC

COND COND

1680013420496 CO PILOT08B20

9903781PANEL INDICATOR (PDU) 48370450-01043-124 CCCC

COND COND

6115011149696 #2 GENERATOR09A01

4793700GENERATOR 1511E28B302-8-DM CCCC

COND COND

6115011149696 #109A01

12293898GENERATOR 83-A105128B302-8-DM CCCC

COND COND

168001310225911C21

04552MIXER ASSEMBLY 8L513-0035970400-02300-048 CCCC

2160 6311

161501141753211C23

28654487TAIL ROTOR PITCHCHANGE SHAFT

B2330151670400-06100-042 3362




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 11 of 12

03-Mar-2016

15000 19151

165001305695411C25

26614487TAIL ROTOR SERVOASSY

B300007762227000-17 RCRC

24400 26878

1650011431226 LAT11D01

32422814MAIN ROTOR PRIMARYSERVO

B303-04824274000-1031 RCRC

24400 27602

165001143122611D01


B30313245274000-1031 RCRC

24400 26696

165001143122611D01


B303-0390670410-02820-054 RCRC

17000 16664

156001082921311D05

00AFT TIE ROD SUPTFITTING

B391-0024770400-08112-044 RCRC

2200 6255

168001164416011D06

04391AFT TIE ROD ASSY MM0089870400-08111-042 RCRC

4400 6696

156001286887011D07

02632AFT BELLCRANK SPTASSY

390-0159670400-08117-049 RCRC

11000 11780

304001287243811D08

01116LATERAL SWASHPLATELINK

C380-0039170400-08151-061 RCRC

5500 7356

161501078569511D09

15672192LATERAL SERVOBELLCRANK

D2890058570400-08150-043 RCRC

11000 14702

168001158965311D11

40384038AFT WALKING BEAM M346-R007570400-08104-048 RCRC

14000 18055

156001289269711D13

04391LEFT TIE ROD 344-0183470400-08115-046 RCRC

3500 6000

1560012969486 R/H11D14

02836RIGHT TIE ROD ASSY 288-0066070400-08114-051 RCRC

15000 16856

168001090204811D15

21922192FORWARD BELLCRANK D3550022570400-08101-044 RCRC

5600 8100

1560012212619 BRIDGE11D16

02836FWD BELLCRANK SPTASSY

B367-0425070400-08162-042 RCRC

COND COND

156001411515611D17

02480SERVO BEAM FITTING F338-0326770209-22103-067 CCCC

COND COND

156001411515011D17

02480SERVO BEAM FITTING H338-0002470209-22103-069 CCCC

COND COND

156001411514811D17

02480SERVO BEAM FITTING F338-0264770209-22103-071 CCCC

20000 19664

1560010957132 STA297-489L-O/B11D17

00SERVO BEAM FITTING UNK348970219-02134-046 RCRC

COND COND

168001261204411D25

23064487STABILATOR ACTUATOR 024370400-06641-117 CCCC

COND COND

168001261204411D25

52264487STABILATOR ACTUATOR V0715070400-06641-117 CCCC

COND COND

5996013162743 211D26

63203823STABILATOR AMPLIFIER 262570902-02001-048 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 12 of 12

03-Mar-2016

COND COND

599601316274311D26

03740STABILATOR AMPLIFIER 856A70902-02001-048 CCCC

COND COND

299501169529115A04

18233700ENGINE SEQUENCINGUNIT

7584-1287163290-100 CCCC

COND COND

589501245909019E05A

04529RECEIVER-TRANSMITTER RADAR

133EESM-C-967292 CCCC

COND COND

584101245909319E05C

04529INDICATOR HEIGHT 0094FFA3060591 CCCC

COND COND

660501503528419E06A

04573ATTITUDE HEADINGREFERENCE UNIT

359765100-20 CCCC

COND COND

661001119718052A

1012483AUTOMAT FLT CONTCOMPUTER

8504339769800-2 CCCC

7. SIGNIFICANT HISTORICAL DATA




HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM0077 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

03-Mar-2016

9000 13407

NSN PENDING03A01A

00PISTON MAIN L/GEARSTR

BEM007770250-12065-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM0077 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

03-Mar-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 C001-03346 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

03-Mar-2016

9000 9060

1650011250907 LEFT HAND03A01A

00PISTON, MAIN L/GEARSTR

P-04880-UTC70250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 C001-03346 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

03-Mar-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615013747203MAIN ROTORSPINDLE ASSY

70102-08200-056 33896-3504 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

03-Mar-2016

COND COND

311001158960705A01I02

14602254ELASTOMERICSPHERICAL BEARING

B324-19882SB7002-048 CCCC

13000 16041

5310011269444 RED05A01I04

4971495M/R SPINDLE NUT R479-0074670102-08105-102 RCRC

3100 6638

1560012207228 RED05A01I06

01495TIE ROD (M/R SPINDLE) C504-0921870102-08102-102 RCRC

20000 21808

1615012149140 RED05A01I07

17301495HORN ASSEMBLY A241-0459570102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-056 33896-3504 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

03-Mar-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 A001-06650 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

03-Mar-2016

13000 17391

531001126944405A01I04

00M/R SPINDLE NUT C479-1313770102-08105-102 RCRC

6400 10791

530601460602005A01I06


20000 24391

161501214914005A01I07



