18-may-2017 automated cads & pads projections page 1 …

Inspection # Till DueShelf LifeSerial NumberMFG DateLot #NarrativePart NumberDODIC

PROJECTEDDAYS: CURRENT HRS: Ser No.MDS:

Sorted By: Days to InspectionAUTOMATED CADS & PADS PROJECTIONSReport Date: of 118-May-2017

PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN

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

9200307CH-47DHELICOPTER, CARGO

3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE

Page 1 of 11

DU30-Jun-1992

LMLM / OLR(GM0923)

14.022 Dec 1992

CIV CONTROL ,QUALITY

MODIFICATION INSTRUCTIONS FORINSTALLATION OF IMPROVEDCLAMSHELL DOOR FITTING ANDLATCH FOR CH47D HELICOPTERS(NSN 1520-01-088-3669) (EIC: RCD)

1-1520-240-50-62MWO:

Mnt LevelPriority

DR01-Apr-1994

BOEING HELPHILA PA(GM0923)

14.019 Nov 1993


IMPROVED/ADJUSTABLE ENGINE AFTMOUNT LINK ASSEMBLY FOR CH-47DAND MH-47E HELICOPTERS) (NSN1520-01-088-3669) (EIC: RCD) AND(NSN 1520-01-282-3747) (EIC: RCE)

1-1520-240-50-60MWO:

Mnt LevelPriority

DU30-Jun-1993

LSSI / OLR(GM0923)

15.021 Mar 1994


MODIFICATION INSTRUCTIONS TOINSTALL NEW JAM NUT ANDMODIFIED WASHER ON LAGDAMPNERS (PISTON ROD END) FORCH-47D HELICOPTERS (NSN 1520-01-088-3669) (EIC RCD)

1-1520-240-50-64MWO:

Mnt LevelPriority

DR01-Apr-1994

LM2/OLR(GM0923)

14.012 Jul 1994


MODIFICATION INSTRUCTIONS FORAFT ENGINE FAIRING MODIFICATIONTO ALLEVIATE CORROSION FOR CH-47D HELICOPTERS (NSN 1520-01-088-3669) (EIC: RCD)

1-1520-240-50-49MWO:

Mnt LevelPriority

DR01-Feb-1991

LSSI/OLR(GM0923)

12.022 Jul 1994


WIRING MODIFICATION AND AN/APR-39A(V)1 RADAR WARNING SYSTEMINSTALLATION IN CH-47DHELICOPTER

1-1520-240-50-54MWO:

Mnt LevelPriority

DU01-Apr-1994

LSSI / OLR(GM0923)

14.022 Jul 1994


MODIFICATIONS INSTRUCTIONS FORINSTALLING ROTARY WING HEADPITCH HOUSING/LAG DAMPERIMPROVED BOLTS AND BUSHINGS TOREPLACE THE BOLTS AND BUSHINGSINSTALLED AT THE FACTORY/DEPOTAND VIA MWO 1-1520-240-50-37, PARTNUMBERS SK33346-2 (UPPERBUSHING), SK33346

1-1520-240-50-69MWO:

Mnt LevelPriority

DN23-Jan-1989

LSSI / OLR(GM0923)

90.026 Aug 1994


INSTALLATION OF OMEGA/VLFNAVIGATION SYSTEM COMPLETEPROVISION ONLY IN CH-47DHELICOPTERS

55-1520-240-50-30MWO:

Mnt LevelPriority

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

DA FORM 2408-5, AUG 2004 EQUIPMENT MODIFICATION RECORD

PIDMWODATE HRS





Page 2 of 11

DR31-Dec-1993

LMLM / OLR(GM0923)

13.007 Sep 1994


MODIFICATION INSTRUCTIONS FORHELICOPTER INTERNAL CARGOHANDLING SYSTEM (HICHS) RAMPCENTERLINE ATTACHMENT FORCH47D HELICOPTERS (NSN 1520-01-088-3669) (EIC: RCD)

1-1520-240-50-59MWO:

Mnt LevelPriority

DR31-Jan-1996

LMLM / OLR(GM0923)

212.031 Jul 1996


INSTALLATION OF HEADS UP DISPLAY(HUD) AN/AVS-7 IN CH-47DHELICOPTERS (NSN 1520-01-088-3669)(EIC:RCD)

1-1520-240-50-56MWO:

Mnt LevelPriority

DR31-Oct-1995

LMLM / OLR(GM0923)

65.031 Jul 1996


MODIFICATION INSTRUCTIONS FORINSTALLATION OF NVG/ANVISLIGHTING UPDATE CH-47DHELICOPTERS (NSN 1520-01-088-3669)(EIC: RCD)

1-1520-240-50-52MWO:

Mnt LevelPriority

DN31-Jan-1989

LMLM / OLR(GM0923)

80.031 Jul 1996


INSTALLATION OF THE SINGLECHANNEL GROUND RADIO/AIRBORNERADIO SYSTEM (SINCGARS) VHF FMHOMING AN/ARC-201 COMPLETEPROVISIONS ONLY RADIO SYSTEM INCH-47D HELICOPTERS

55-1520-240-50-28MWO:

Mnt LevelPriority

DN01-Mar-1989

LMLM / OLR(GM0923)

115.031 Jul 1996


INSTALLATION OF AN/ARC-199, HF-SSB, RADIO SET COMPLETEPROVISION ONLY IN CH-47DHELICOPTERS

55-1520-240-50-29MWO:

Mnt LevelPriority

DU30-Apr-1996

AASF-PSBPHILIPSBURGPA (GM0923)

25.008 Apr 1997


MODIFICATION INSTRUCTIONS TOREPLACE LOWER PITCH CHANGELINK ELASTOMERIC BEARING WITHTEFLON BEARING FOR CH-47D ANDMH-47E HELICOPTERS NSN 1520-01-088-3669 (EIC: RCD) AND NSN 1520-01-282-3747 (EIC: RCE)

1-1520-240-50-63MWO:

Mnt LevelPriority

DR31-May-1996

LMLM / OLR(GM0923)

28.030 Jun 1997


INSTALLATION OF ALTITUDE VOICEWARNING SYSTEM RADARALTIMETER AN/APN-209(V) IN CH-47DHELICOPTERS (NSN 1520-01-088-3669)(EIC: RCD)

1-1520-240-50-61MWO:

Mnt LevelPriority



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Page 3 of 11

DU24-Feb-1997

LMLM / OLR(GM0923)

8.030 Jun 1997


MODIFICATION INSTRUCTIONS FORNON-METALLIC SPLINE ADAPTERSFOR COMBINING TRANSMISSIONCOOLING FAN DRIVE SHAFT ON CH-47D AND MH-47E HELICOPTERS (NSN1520-01-088-3669) (EIC: RCD) (NSN1520-01-282-3747) (EIC: RCE)

1-1520-240-50-67MWO:

Mnt LevelPriority

DR29-Aug-1997

LMLM / OLR(GM0923)

60.030 Jun 1997


MODIFICATION INSTRUCTIONS FOREASILY REPLACEABLE CABIN ESCAPEHATCH FOR CH-47D HELICOPTER,NSN 1520-01-088-3669 (EIC:RCD) ANDMH-47E HELICOPTER, NSN 1520-01-282-4787 (EIC:RCE)

1-1520-240-50-76MWO:

Mnt LevelPriority

DN15-Jul-1991

LMLM / OLR(GM0923)

2.030 Jun 1997


INSTALLATION OF IMPROVEDFREQUENCY MODULATION (IFM)BYPASS IN CH-47D HELICOPTER

1-1520-240-50-46MWO:

Mnt LevelPriority

DR14-Apr-1997

LM2/OLR(GM0923)

29.027 Apr 1998


MODIFICATION INSTRUCTIONS FORINSTALLING THE COCKPITEMERGENCY RAMP CONTROLSYSTEM ON CH-47D HELICOPTERS(NSN 1520-01-088-3669) (EIC: RCD)

1-1520-240-50-48MWO:

Mnt LevelPriority

DN01-Apr-1992

LMLM / OLR(GM0923)

2.012 May 1998


MODIFICATION INSTRUCTIONS FORIMPROVED FORWARD TRANSMISSIONOIL COOLER AIR INLET DUCT CH-47DHELICOPTERS

1-1520-240-50-57MWO:

Mnt LevelPriority

DR29-Aug-1997

LM2/OLR J. SIMS(GM0923)

109.029 Oct 1998


INSTALLATION OF AN/ASN-128BDOPPLER/GPS NAVIGATION SYSTEMIN CH-47D HELICOPTERS (NSN 1520-01-088-3669 (EIC: RCD)

1-1520-240-50-73MWO:

Mnt LevelPriority

DU03-Dec-1998

AASF-FTIGANVILLE PA(GM0923)

5.012 Oct 1999


DEMODIFICATION OF MWO 1-1520-240-50-67, MODIFICATION INSTRUCTIONSFOR NON-METALLIC SPLINEADAPTERS FOR COMBININGTRANSMISSION COOLING FAN DRIVESHAFT ON CH-47D AND MH-47EHELICOPTERS (NSN 1520-01-088-3669)(EIC: RCD) (NSN 1520-01-282-3747)(EIC: RCE)

1-1520-240-50-67 DEMODMWO:

Mnt LevelPriority



PIDMWODATE HRS





Page 4 of 11

DU17-Mar-2000

LMLM/OLR#12315(RG1913)

12.020 Mar 2000


MODIFICATION INSTRUCTIONS FORIMPROVED NVG LIGHTING BEZEL FORTURN AND SLIP INDICATOR, RADARALTIMETER, AND VERTICAL GYROINDICATOR AND MODIFICATIONINSTRUCTIONS OF FORWARD PYLONDRAIN HOLES AND REPLACEMENT OFNO. 1 AND NO.2 PDP AC BUS THECIRCUIT BREAKE

1-1520-240-50-71MWO:

Mnt LevelPriority

DR04-Apr-1997

LMLM/OLR#123215(RG1913)

12.020 Mar 2000


MODIFICATION INSTRUCTIONS FORINSTALLATION OF STAINLESS STEELBELLCRANKS IN COMBININGTRANSMISSION AREA FOR CH-47DAND MH-47E HELICOPTERS (NSN 1520-01-088-3669) (EIC: RCD) (NSN 1520-01-282-3747) (EIC: RCE)

1-1520-240-50-65MWO:

Mnt LevelPriority

DR01-Feb-2000


6.020 Mar 2000


MODIFICATION INSTRUCTIONS FORINSTALLING A HAND HOLD IN THECENTER CARGO HOOKCOMPARTMENT ON CH-47D AND MH-47E HELICOPTERS (NSN 1520-01-088-3669) (EIC: RCD) AND (NSN 1520-01-282-3747) (EIC: RCE)

1-1520-240-50-79MWO:

Mnt LevelPriority

DR30-Nov-1998


126.020 Mar 2000


INSTALLATION OF AN/ARC-220 ANDTSEC/KY-100 IN CH-47DHELICOPTERS (NSN 1520-01-088-3669)(EIC: RCD)

1-1520-240-50-74MWO:

Mnt LevelPriority

DR01-Jul-2000


6.020 Mar 2000


MODIFICATION INSTRUCTIONS FORON/OFF SWITCH FOR THE AFT WHITEPOSITION LIGHT ON CH-47D AND MH-47E HELICOPTERS (NSN 1520-01-088-3669) AND(EIC: RCD) (NSN 1520-01-282-3747) (EIC: RCE)

1-1520-240-50-75MWO:

Mnt LevelPriority

DR01-May-2000


684.020 Mar 2000


MODIFICATION INSTRUCTIONS FORINSTALLATION OF FULL AUTHORITYDIGITAL ENGINE CONTROLS (FADEC)ON CH-47D HELICOPTERS (NSN 1520-01-088-3669) (EIC: RCD)

1-1520-240-50-83MWO:

Mnt LevelPriority



PIDMWODATE HRS





Page 5 of 11

DR31-Mar-2000


136.020 Mar 2000


MODIFICATION INSTRUCTIONS FOREXTENDED RANGES FUEL SYSTEMON CH-47D HELICOPTERS (NSN 1520-01-088-3669) (EIC: RCD)

1-1520-240-50-84MWO:

Mnt LevelPriority

DR01-Feb-2000


6.020 Mar 2000


MODIFICATION INSTRUCTION TORETROFIT IMPROVED AFT PYLONCLAMSHELL DOOR LATCHCONFIGURATION ON CH-47D AND MH-47E HELICOPTERS (NSN 1520-01-088-3669) (EIC: RCD) AND (NSN 1520-01-282-3747) (EIC: RCE)

1-1520-240-50-80MWO:

Mnt LevelPriority

DR30-Sep-1999


12.020 Mar 2000


ADDITION OF VACUUM RELIEF VALVETO THE PRESSURE REFUELINGSYSTEM FOR CH-47D HELICOPTERS(NSN 1520-01-088-3669) (EIC: RCD)

1-1520-240-50-81MWO:

Mnt LevelPriority

DR06-Apr-2001

LM2/OLR(JS7868)

64.028 Mar 2002


MODIFICATION INSTRUCTIONS FORINSTALLING IMPROVED AFT PYLONWORK PLATFORM DOOR LATCHESON CH-47D AND MH-47EHELICOPTERS (NSN 1520-01-088-3669)(EIC: RCD) (NSN 1520-01-282-3747)(EIC: RCE)

1-1520-240-50-77MWO:

Mnt LevelPriority

DN07-Jun-2001

G CO 104TH AVNKANDAHAR(GM0923)

30.027 Jul 2003


INSTALLATION OF FLIGHTCREWSEATS FOR MH-47DHELICOPTERS

1-1520-H47-50-97MWO:

Mnt LevelPriority

DM06-Mar-2003

FCT ATKANDAHAR(GM0923)

15.031 Jul 2003


CH-47D BLUE FORCE TRACKING (BFT)CARGO BAY INSTALLATION ANDASSEMBLY

1-1520-240-50-BFT R2MWO:

Mnt LevelPriority

DR01-Sep-2002

G CO 104TH AVN(GM0923)

25.017 Oct 2003


MODIFICATION INSTRUCTIONS FORSEALED LEAD ACID BATTERYINSTALLATION ON CH-47DHELICOPTERS (NSN 1520-01-088-3669)(EIC: RCD)

1-1520-240-50-82MWO:

Mnt LevelPriority



PIDMWODATE HRS





Page 6 of 11

DR01-Sep-2002

DYNCORP OLREUROPE(RN1423)

620.001 Mar 2004


MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE AN/ALE-147 COUNTERMEASURES DISPENSERSYSTEM (CMDS) ON THE CH-47DAIRCRAFT (NSN 1520-01-088-3669)(EIC RCD)

1-1520-240-55-12MWO:

Mnt LevelPriority

DU01-Aug-2004

DOL AVIM, FTDRUM NY(RN1423)

48.003 Mar 2004


CH-47D HELICOPTERS, QUICKREACTION MODIFICATION TO AN/PRC-117F SATCOM RADIO ASSEMBLY

AN/PRC-117FMWO:

Mnt LevelPriority

DN07-Jun-2001

AASF # 2/L3BIRMINGHAM

30.002 Jun 2006

CIVBRENGELMAN,GEORGE D

DEMODIFICATION OF MWO 55-1520-H47-50-097 , INSTALLATION OFFLIGHT CREWSEATS FOR MH-47DHELICOPTERS

55-1520-H47-50-097 DEMODMWO:

Mnt LevelPriority

DR22-Aug-2005

DYNCORPPROJECT OLR,FTCKY

21.023 Jan 2007

DAC STEVENS,JOSEPH

MODIFICATION INSTRUCTIONS FORINSTALLATION OF THECRASHWORTHYCREW CHIEF SEATAND FRAME KIT ON CH-47DHELICOPTERS (NSN 1520-01-088-3669)

1-1520-240-50-96MWO:

Mnt LevelPriority

DR15-Mar-2006


6.023 Jan 2007

DAC STEVENS,JOSEPH

INSTALLATION INSTRUCTIONS FORMASTER CAUTION PROTECTIVESHIELD ON CH-47D HELICOPTERS(NSN 1520-01-088-3669) (EIC: RCD)

1-1520-240-50-101MWO:

Mnt LevelPriority

DN09-Jul-2005


32.023 Jan 2007

DAC STEVENS,JOSEPH

RELOCATION OF THE FLUX VALVE1-1520-240-50-FLUXMWO:

Mnt LevelPriority

DR02-Mar-2005

DYCORP OLR,FTCKY

620.023 Jan 2007

DAC STEVENS,JOSEPH

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE COMMONMISSILE WARNING SYSTEM (CMWS)ON THE CH-47D AIRCRAFT W/ALE-47(NSN 1520-01-088-3669) (EIC RCD)

1-1520-240-55-14MWO:

Mnt LevelPriority

DN01-Jul-2003


9.023 Jan 2007

DAC STEVENS,JOSEPH

ADVANCED HEADS UP DISPLAY (HUD)AN/AVS-7(V) AND T55-GA-714AENGINE TORQUE INDICATINGSYSTEM

1-1520-240-50-88MWO:

Mnt LevelPriority



PIDMWODATE HRS





Page 7 of 11

DN12-May-2004


637.023 Jan 2007

DAC STEVENS,JOSEPH

INSTALLATION OF THE ELECTRICALAND AIRFRAME PROVISIONS FORENGINE AIR PARTICLE SEPARATORSHORT RAIL FOR CH-47DHELICOPTERS (NSN 1520-01-088-3669)(EIC RCD)

1-1520-240-50-93MWO:

Mnt LevelPriority

DR07-Sep-2004


240.025 Jan 2007

DAC STEVENS,JOSEPH

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE AIRWARRIOR MICROCLIMATE COOLINGAND MASK BLOWER SYSTEMS ON CH-47D HELICOPTERS (NSN 1520-01-088-3669) (EIC RCD)

1-1520-240-50-91MWO:

Mnt LevelPriority

DR18-Apr-2006


17.025 Jan 2007

DAC STEVENS,JOSEPH

M4 RIFLE MOUNT INSTALLATION FORTHE CH-47D HELICOPTERS (NSN 1520-01-088-3669) (EIC: RCD)

1-1520-240-50-104MWO:

Mnt LevelPriority

DR31-Jan-2007

DYNCORPPROJECT OLR,BIRMINGHAM,AL

36.008 Feb 2007

DAC STEVENS,JOSEPH

INSTALLATION OF ELECTRICHYDRAULIC PUMP FOR CH-47DHELICOPTERS

1-1520-240-50-109MWO:

Mnt LevelPriority

DR15-Mar-2006


2.008 Feb 2007

DAC STEVENS,JOSEPH

INSTALLATION OF THE AVIONICSCOOLING FAN GUSSET FOR THE CH-47 HELICOPTERS (NSN 1520-01-088-3669) (EIC: RCD)

1-1520-240-50-102MWO:

Mnt LevelPriority

DR12-Feb-2006


140.008 Feb 2007

DAC STEVENS,JOSEPH

INSTALLATION OF BLUE FORCETRACKING ON CH-47D HELICOPTERS(CARGO COMPARTMENT INSTALL,REV. 3)

1-1520-240-50-BFT47 (REV 3)MWO:

Mnt LevelPriority

DR17-Nov-2004


72.008 Feb 2007

DAC STEVENS,JOSEPH

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE AN/APX-118 MODE S TRANSPONDER (CXP) ONTHE CH-47D AIRCRAFT (NSN 1520-01-088-3669) (EIC RCD)

1-1520-240-50-90MWO:

Mnt LevelPriority

DR04-Sep-2007

DYNCORPPROJECT OLR

22.013 Mar 2007

DAC STEVENS,JOSEPH

LEFT HAND CRASHWORTHY SEATSYSTEM INSTALLATION FOR CH-47DHELICOPTERS.

1-1520-240-50-99MWO:

Mnt LevelPriority



PIDMWODATE HRS





Page 8 of 11

DR26-Oct-2007

DYNCORPPROJECT OLR

22.013 Mar 2007

DAC STEVENS,JOSEPH

INSTALLATION OF THE AFT PYLONSTEP DOUBLER ON THE CH-47DHELICOPTERS.

1-1520-240-50-111MWO:

Mnt LevelPriority

DR14-Mar-2006

DYNCORPPROJECT OLR,BIRMINGHAM AL

7.002 May 2007

DAC STEVENS,JOSEPH

INSTALLATION OF THE NEW BRACKETFOR THE MA-16 INERTIA REELINSTALLED ON THE PILOT AND CO-PILOT SEATS FOR THE CH-47DHELICOPTERS (NSN 1520-01-088-3669)(EIC:RCD)

1-1520-240-50-97MWO:

Mnt LevelPriority

DR18-Feb-2004


66.015 May 2007

DAC STEVENS,JOSEPH

MODIFICATION INSTRUCTIONS FORCARGO LOADMASTER RADARALTIMETER INSTALLATION ON CH-47DHELICOPTERS (NSN 1520-01-282-3747)(EIC: RCD)

1-1520-240-50-72 C1MWO:

Mnt LevelPriority

DR19-Feb-2007


212.018 May 2007

DAC STEVENS,JOSEPH

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE DOPPLERGPS NAVIGATION SET PREPLANNEDPRODUCT IMPROVEMENT (DGNS P3I)ON THE CH-47D HELICOPTER (NSN1520-01-088-3669) (EIC RCD)

1-1520-240-50-95MWO:

Mnt LevelPriority

DR30-Mar-2007

AASF #2BIRMINGHAM AL

502.008 Jun 2007

CIV EMERSON,AMON L

MODIFICATION OF THE CH-47DSERIES HELICOPTER- MODERNIZEDSIGNAL PROCESSING UNIT

1-1520-MSPU-CH-47-50-1MWO:

Mnt LevelPriority

DR10-Jun-2008

DYNCORPPROJECT OLR

16.018 Sep 2007

CIV VIEYRA ,TIMOTHY D

INSTALLATION OF CMWS P3IUPGRADE ON CH-47D HELICOPTERS

1-1520-240-50-116MWO:

Mnt LevelPriority

DR09-Jun-2008

DYNCORPPROJECT OLRFTCKY

70.001 Feb 2008

D, LMODIFICATION OF CH-47DHELICOPTERS FOR THEINSTALLATION OF THE CMWS 5THELECTRO-OPTIC MISSLE SENSOR.

1-1520-240-50-120MWO:

Mnt LevelPriority

DR04-Sep-2007

DYNCORP 2.021 Oct 2008

CV1 DAVIS,SHARRON J

INSTALLATION OF THE RECESSEDHEADREST RETROFIT ON THECRASHWORTHY CREW CHIEF SEATON THE CH-47D HELICOPTERS.

1-1520-240-50-114MWO:

Mnt LevelPriority



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Page 9 of 11

DR04-Sep-2007


CV1 DAVIS,SHARRON J

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE ARMORSEAT COMPENSATOR FOR THECOCKPIT SEATS ON H-47HELICOPTERS (NSN 1520-01-088-3669)(EIC: RCD)

1-1520-240-50-115MWO:

Mnt LevelPriority

DR08-Feb-2007


CV1 DAVIS,SHARRON J

MODIFICATION INSTRUCTIONS FORINSTALLATION OF THE FUELCROSSFEED BREAKAWAY FITTINGON H-47 HELICOPTERS (NSN 1520-01-088-3669) (EIC: RCD) (NSN 1520-01-513-8008) (EIC: N/A)

1-1520-240-50-98MWO:

Mnt LevelPriority

MN18-Dec-2008

BAE SYSTEMS 480.018 Dec 2008

R, BADVANCED THREAT INFRAREDCOUNTERMEASURES (ATIRCM)AN/ALQ-212 (V). DRAFT MWO

1-1520-240-23-XXMWO:

Mnt LevelPriority

DR17-Feb-2009

AFMARASM-E/CSC

6.023 Sep 2010

CIV BARNES,JAMES

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE P3 DRAINLINE ON THE CH-47D HELICOPTERSMWO 1-1520-240-50-100

1-1520-240-50-100MWO:

Mnt LevelPriority

DR26-Mar-2008

AFMA RASMEAST

3.623 Sep 2010

CIV GUYETTE,PAUL

INSTALLATION OF AVIATIONVIBRATION ANALYZER (AVA) SINGLECAMERA TRACKER BRACKET (TTS54785) FOR ALL CH47D HELICOPTERS

1-1520-240-50-117MWO:

Mnt LevelPriority

DR25-Apr-2008

AFMA RASMEAST

26.423 Sep 2010

CIV GUYETTE,PAUL

INSTALLATION OF AFT PYLONACCESS PANELS ON CH-47DHELICOPTERS

1-1520-240-50-118MWO:

Mnt LevelPriority

DU30-Jan-2003

CCAD 51.013 Aug 2012

C, SRECAP RERMNTS FOR CH-47 FWD &AFT ROTARY WNG HEAD ASSY, P/N1452003-10 (FWD) & 1452004-20 (AFT)

DMWR 55-1615-296 AEDT3332

MWO:

Mnt LevelPriority

OR01-Nov-1999

CCAD 0.513 Aug 2012

C, SREVISION TO SOF CH-47-00-01CH-47-00-ASAM-02MWO:Mnt LevelPriority

OM08-Nov-2000

CCAD 4.013 Aug 2012

C, SAL H-47 SERIES AIRCRAFT, FORWARDAND AFT ROTOR HUB LIGHTENINGHOLE INSPECTIONS

CH-47-01-ASAM-03MWO:

Mnt LevelPriority



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Page 10 of 11

OM14-Dec-2000

CCAD 0.513 Aug 2012

C, SAL H-47 SERIES AIRCRAFT, ONE TIMEINSPECTION OF ROTOR HEADASSEMBLY DROOP STOP BOLTS FORPROPER LENGTH


Mnt LevelPriority

DU21-Jul-2005

CCAD 1.013 Aug 2012

C, SVERTICAL HINGE PIN BEARINGS INSP.CH-47-05-ASAM-03MWO:Mnt LevelPriority

FT15-Sep-2006

CCAD 0.513 Aug 2012

C, SH-47 AIRCRAFT, AFT CRITICALDYNAMIC COMPONENTS

CH-47-06-SOF-06MWO:

Mnt LevelPriority

DU20-Feb-2001

CCAD 0.513 Aug 2012

C, SALL H-47 SERIES A/C, UNGROUNDINGREQUIREMENTS FOR ACFT WITHINCORRECTLY INST DROOP STOPS.

TB 1-1520-240-20-137MWO:

Mnt LevelPriority

DU20-Jan-2002

CCAD 2.013 Aug 2012

C, SALL H-47 SERIES A/C, INSP OF THROTARY WING HEAD TIE BAR ASSY'S

TB 1-1520-240-20-146MWO:

Mnt LevelPriority

OM01-Aug-2008

CCAD 0.513 Aug 2012

C, SALL CH-47D AND CH-47F SERIESAIRCRAFT, AFT ROTOR HEAD PITCHVARYING HOUSING RETIREMENTLIFE, H-47-08-AMAM-05

H-47-08-AMAM-05MWO:

Mnt LevelPriority

OM11-Feb-2008

CCAD 0.513 Aug 2012

C, SALL H-47 AIRCRAFT, PITCH HORNBUSHING

H-47-08-ASAM-01MWO:

Mnt LevelPriority

DU28-Jul-2000

CCAD 0.513 Aug 2012

C, SMANDATORY INSP OF HHP ON ALLCH47D, MH47D AND MH47E ACFT.

TB 1-1520-240-20-122MWO:

Mnt LevelPriority

DU15-Dec-2000

CCAD 0.513 Aug 2012

C, SINSP FOR UNTESTED (FSP) TIE BARPIN ASSY'S P/N 114R2168-3 &114R2168-4.

TB 1-1520-240-20-133MWO:

Mnt LevelPriority

DU15-Dec-2000

CCAD 0.513 Aug 2012

C, SCH/MH-47 A/C, ONE TIME INSP OF AFTR/H ASSY'S & ENGINE CROSS SHAFTADAPTER ASSY'S.

TB 1-1520-240-20-134MWO:

Mnt LevelPriority



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Page 11 of 11

DU06-Feb-2001

CCAD 0.513 Aug 2012

C, SINSPECTION OF DROOP STOPSTB 1-1520-240-20-136MWO:Mnt LevelPriority

OM21-Jul-2005

CCAD 0.513 Aug 2012

S, MCONDUCT AN INSPECTION OF THEAFT ROTOR HEAD P/N'S 145R2004-18AND -20 SUSPECT PITCH HOUSING.

CH-47-05-ASASM-02MWO:

Mnt LevelPriority

DR24-May-2010

FT HOOD AFMADYNCORP INTL

1,220.027 Sep 2012

CIV SOWA ,BRUCE M

MODIFICATION INSTRUCTIONS FORINSTALLATION OF INFRAREDSUPPRESSION SYSTEM (IRSS) ONTHE CH-47D HELICOPTER (NSN 1520-01-088-3669)(EIC:RCD).

1-1520-240-50-119MWO:

Mnt LevelPriority



PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN -


SWASHPLATE ASSY 92003072007A95861. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 21

24-Jan-2002 DT

CSMITH26-Mar-2012

2.0CCADSWASHPLATE LOWER SEALRETAINER SELF LOCKING NUTINSPECTION

CH-47-02-SOF-01MWO:

Priority Mnt Level

04-Jan-2005 FT

CSMITH26-Mar-2012

1.0CCADH-47 SERIES AIRCRAFT,SWASHPLATE ROTATING RING

CH-47-05-SOF-01MWO:

Priority Mnt Level

11-Feb-2008 DT

CSMITH26-Mar-2012

10.0CCADREAMING OF SWASHPLATEBUSHING TO .6250-.6257 DEPOTLEVEL MAINT PERFORMED BY L3AUTHORIZED BY MICHAEL J. FOLEY,LEAD LIAISON ENGINEER, AMRDEC

DMWR 55-1615-297MWO:

Priority Mnt Level

12-Jun-2008 OM

CSMITH26-Mar-2012

0.5CCADFWD & AFT SWASHPLATE ASSYRETAINING SPACERS

H-47-08-AMAN-04MWO:

Priority Mnt Level


EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991

PIDMWODATE HRS



DRIVESHAFT ASSY, SEC 2-6 92003072008A138061. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 2 of 21

10-Oct-1996 OM

FR462627-Sep-2010

1.0CCAD/W0MUAAALL CH-47D, MH-47D, AND MH-47EAIRCRAFT, ONE TIME RECORDSCHECK, VISUAL INSPECTION FOR,AND REMOVAL OF CERTAIN SERIALNUMBERED 145D3400-23/-25/-32FORWARD SYNCHRONIZING DRIVESHAFT ASSEMBLIES


Priority Mnt Level

22-Oct-2002 DR

FR462627-Sep-2010

22.0CCAD/W0MUAARECAPPED DMWR, 55-1615-322, CH1MWO:

Priority Mnt Level



PIDMWODATE HRS




Page 3 of 21

22-Oct-2002 DR

GB886728-Jan-2013

22.0CCADRECAPPED DMWR, 55-1615-322, CH1MWO:

Priority Mnt Level



PIDMWODATE HRS



COMBINING TRANSMISSION 92003072010A90911. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 4 of 21

28-Jan-2015 FI

28-Jan-20153.0MO TASMGMSPU ACCELEROMETERS MOUNT

INSERT REPLACEMENT.MEC-F193343MWO:

Priority Mnt Level



PIDMWODATE HRS



XMSN ASSY ENGINE MECH 9200307A11-460DRGI1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 5 of 21

27-Jan-2000 OT

miranda.m.moore14-May-2007

0.5CCAD C.C.TEXAS 78419-5260 (PS8343)

ALL CH-47D, MH-47D AND MH-47ESERIES AIRCRAFT, ONE-TIMEINSPECTION OF ENGINETRANSMISSIONS RECORDS FORSUSPECT GEARS ANDREPLACEMENT OF SUSPECTTRANSMISSIONS

CH-47-00-04MWO:

Priority Mnt Level

06-Mar-2003 DU

miranda.m.moore14-May-2007

0.5CCAD C.C.TEXAS 78419-5260 (PS8343)

RECAPITALIZATION REQUIREMENTSENGINE MECHANICAL P/N 145D6300-10/11/14/15

DMWR 55-1615-323MWO:

Priority Mnt Level

31-May-2006 OR

darrel.e.dust23-Oct-2008

1.0AMCOMPROJECT OLRHAAF GA 31409

CH-47D AIRCRAFT DESERTOPERATIONS SPECIAL INSPECTIONAND CLEANING

1-1520-240-30-02CH1MWO:

Priority Mnt Level

23-May-2008 OU

karen.l.hall24-May-2008

0.5D CO 2-3 CABBIAP, IRAQ09322

CONDUCT A RECORDS CHECK OFTHE DA FORM 2408-16-1 TODETERMINE IF ONE OF THESUSPECTED SERIAL NUMBEREDPINION GEARS COMPLIED WITH

H-47-08-SOF-01MWO:

Priority Mnt Level



PIDMWODATE HRS



AFT SEC 1 D/S ASSY 9200307A16951. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 6 of 21

10-Feb-2011 DT

GB886724-Sep-2012

22.0CCADRECAPPED55-1615-322,CHG-10 RDMWO:

Priority Mnt Level



PIDMWODATE HRS



BLADE ASSY ROT WING FWD 9200307A1756E1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 7 of 21

21-Jul-2005 ON

GM251014-Feb-2013

0.0BOEING PHILAROTOR BLADE ROOT END FIBERDISTORTATION


Priority Mnt Level



PIDMWODATE HRS




Page 8 of 21

18-Jul-1983 OT

GM251018-Jul-1983

0.0BOEING HELIBOROSCOPE INSPECTION OF PARTNUMBER 114R1702 ROTOR BLADES

55-1520-241-20-24MWO:

Priority Mnt Level

21-Jul-2005 OT

GM251021-Jun-2005

0.0BOEING HELIH-47 SERIES AIRCRAFT, ROTORBLADE, ROOT END FIBERDISTORTION

CH-47-05-SOF-02MWO:

Priority Mnt Level



PIDMWODATE HRS




Page 9 of 21

21-Jul-2005 OT

GM251002-May-2013

0.0BOEING PHILAH-47 SERIES AIRCRAFT, ROTORBLADE, ROOT END FIBERDISTORTION

CH-47-05-SOF-02MWO:

Priority Mnt Level



PIDMWODATE HRS



SHAFT ASSY, ENG DRIVEN 9200307A-21001. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 10 of 21

16-Dec-2008 OT

jorge.l.alvarez17-Dec-2008

1.0D CO 2/104GSAB

H-47-09-SOF-02 INSP FORSPECIFIED SN: ON ENGINE DRIVESHAFTS AND ADAPTERS

H-47-09-SOF-02MWO:

Priority Mnt Level



PIDMWODATE HRS



SHAFT ASSY, ENG DRIVEN 9200307A-21011. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 11 of 21

16-Dec-2008 OT


1.0D CO 2/104GSAB


H-47-09-SOF-02MWO:

Priority Mnt Level



PIDMWODATE HRS



DRIVESHAFT ASSY, SEC 2-6 9200307A-29231. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 12 of 21

22-Oct-2002 DR

casey.j.haugen26-Sep-2007

1.0CCAD/009443RECAPPED 55-1615-322MWO:

Priority Mnt Level

24-Sep-2003 DN

miranda.m.moore0.0RECAPPEDT3813MWO:

Priority Mnt Level

17-Aug-2005 DM

miranda.m.moore0.0RECAPPEDMEO#T5295 REV. AMWO:

Priority Mnt Level



PIDMWODATE HRS



ADAPTER ASSY ENG D/S OUTB 9200307A47011. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 13 of 21

01-Oct-2002 DR

GA344001-Sep-2011

17.0CCAD/W0MUAARECAPPEDDMWR 55-1650-322, C 10 2MWO:

Priority Mnt Level



PIDMWODATE HRS



SHAFT ASSY, AFT VERTICAL 9200307A5081. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 14 of 21

26-Jul-2000 DM

RO730617-Mar-2010

0.1CCADINSPECT FWD & AFT SLIDER SHAFTSEALS

TB1-1520-240-20-123MWO:

Priority Mnt Level

03-Aug-2004 DU

RO730617-Mar-2010

89.8CCADRECAPITALIZATION REQUIREMENTSFOR AFT VERTICAL SHAFT P/N145D3300-6

DMWR 55-1615-322MWO:

Priority Mnt Level

15-Sep-2006 OT

RO730617-Mar-2010

2.0CCADH-47 AIRCRAFT, AFT CRITICALDYNAMIC COMPONENTS

CH-47-06-SOF-06MWO:

Priority Mnt Level



PIDMWODATE HRS



ADAPTER ASSY ENG D/S INB 9200307A-78091. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 15 of 21

16-Dec-2008 OT


1.0D CO 2/104GSAB


H-47-09-SOF-02MWO:

Priority Mnt Level



PIDMWODATE HRS




Page 16 of 21

29-Sep-2000 DT

FR462605-Nov-2008

22.0CCADRECAPPEDDMWR 55-1615-322 CH-10MWO:

Priority Mnt Level



PIDMWODATE HRS



AFT TRANSMISSION 9200307A9-6121. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 17 of 21

14-May-1998 OM

quality.control18-May-1998

0.5AASF #1, CT(XS7987)

C/MH-47D/E, ONE TIME INSPECTIONFOR AFT TRANSMISSIONS WITHSUSPECTED IMPROPERLY SHIMMEDINPUT PINION GEAR ASSEMBLY


Priority Mnt Level

26-Aug-1999 DT

quality.control27-Aug-1999

0.5LMALC/OLRHAAF GA(PL6142)

CH-47D, MH-47D, AND MH-47EAIRCRAFT, INSPECTION OF H-47AIRCRAFT FOR FORWARD AND AFTTRANSMISSION GEAR/BEARINGASSEMBLIES IDENTIFIED BY SERIALNUMBER PREFIX "VB"

CH-47-99-04MWO:

Priority Mnt Level

06-Dec-1999 OT

quality.control06-Dec-1999

0.5AASF #1 CT(XB9987)

ALL H-47 SERIES AIRCRAFT,INCREASE OF OPERATINGLIMITATIONS FOR FORWARD ANDAFT TRANSMISSION GEAR/BEARINGASSEMBLIES IDENTIFIED BY SERIALNUMBER PREFIX "VB"

CH-47-00-03MWO:

Priority Mnt Level

28-Feb-2005 FN

darrel.e.dust01-Oct-2010

1.0AFMA RASM-E/CSC HAAF GA31409

CH-47D AIRCRAFT DESERTOPERATIONS SPECIAL INSPECTIONAND CLEANING

1-1520-240-30-02MWO:

Priority Mnt Level

08-Nov-2007 OM

george.d.brengelman 12-Jun-2008

2.0L3/VERTEXAEROSPACECFS

H-47 SERIES AIRCRAFT, AFTTRANSMISSION TOROT SHAFT SEALRETAINER ASSY. H-47-AMAM-01

H-47-08-AMAM-01MWO:

Priority Mnt Level



PIDMWODATE HRS



ENGINE ASSY TURBINE 9200307GA751891. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 18 of 21

03-Feb-2015 FT

03-Feb-20150.1AASF #3

PEORIA, ILENGINE CHIP DETECTORH-47-15-AMAM-01MWO:

Priority Mnt Level



PIDMWODATE HRS



ENGINE ASSY TURBINE 9200307GA752131. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 19 of 21

30-Jan-2004 FR

chris.poyner11-Apr-2012

200.0AMCOMAFMA/URS

INSPECTION AND REPAIR FOR T55SERIES ENGINE RESET PROGRAM(T55-L-712 AND T55-GA-714A)

1-2840-265-23MWO:

Priority Mnt Level

12-Jul-2005 DM

RH309822-Feb-2009

1.0W0MUAAT55-GA-714A ENGINE, P/N 2-001-020-39, DEPOT MAINTENANCE WORKREQUIREMENT (DMWR) 1-2840-265

MEO P5092 REV BMWO:

Priority Mnt Level

03-Feb-2015 FT

robert.d.childers03-Feb-2015

0.1AASF #3 PIA ILENGINE CHIP DETECTORH-47-15-AMAM-01MWO:

Priority Mnt Level



PIDMWODATE HRS



DRIVESHAFT ASSY, SEC 2-6 9200307NC7711. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 20 of 21

22-Oct-2002 DR

FR462618-Nov-2011

0.5CCADRECAPPED 55-1615-322MWO:

Priority Mnt Level



PIDMWODATE HRS



CYLINDER ACT SWIVEL AFT 9200307UR590BANS1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 21 of 21

23-May-2003 DR

LU605201-Aug-2011

57.0CCAD/WOMUAARECAPPEDDMWR 55-1650-400MWO:

Priority Mnt Level

09-Jan-2006 OM

LU605201-Aug-2011

1.0CCAD/WOMUAAH-47 SERIES AIRCRAFT, UPPERBOOST ACTUATORS (UBA)


Priority Mnt Level



CH-47D WP1JB09200307

1DATE _________________ NUMBERS OF PAGES IN FLIGHT PACK

00

2627

2525

2625

2724

02 May 2017

02 May 2017

09 May 2017

11 May 2017

15 May 2017

4507.1

4443.5

100.61343419.2

12. LOCAL USE

63.6

c. NEXT PHASE/SCHEDULED INSP DUE ATPID

115 May 2017LAST GENERATION PHASE/SCHEDULED

OPERATION SINCE DATE COMPLETED

PMD DUEe.b. NEXT PHASE/SCHEDULED INSP (NO.)a. HOURS OF d. HOURS OF

SCHEDULED INSPECTION INFORMATION11.

TOTALOTHER

ELECT TODAY

ARM 000CURRENT

VHOURS

ACFTCYCLES

AUTOROTATIONSSTD

LANDINGSHSF/AIRCRAFT

FLIGHT DATASYSTEM STATUS 10.9.

TOTAL

TODAY

CURRENT

DATE STARTSHOURSNO. 2NO. 1 HR METER NUMBER 2NUMBER 1

ENGINE HIT READINGS APU HISTORY6. 7. 8. ENGINE STARTS

PEORIA, IL 61607-1497

1.AIRCRAFT SERIAL NUMBER 2. MODEL 4. STATION 5. NAME OF CE/MECH3. UIC

HOVER TOUCHDOWN

OPERATION TO NEXT

INSPECTION

EDITION OF OCT 91 IS OBSOLETE For use of this form, see DA PAM 738-751; the proponent agency is DCS, G-4

AIRCRAFT STATUS INFORMATION RECORDDA FORM 2408-13, MAR 2014

PART I - FAULT INFORMATION

9200307 CH-47D

2. MODEL1. AIRCRAFT SERIAL NUMBER

PART II - CORRECTING INFORMATION

4. PAGE3. DATE

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 14359.8 X

00

AFT 3MAN TRROP SEAT LATCH POST ON 2ND 3MAN SEAT ON L/HSIDE BROKE AIRCRAFT RESTRICTED TO 29 PASSENGERS

PID

SYS DATE ACFT HRSNO

V WUC

FAULTS/REMARKS

ROUNDS ACTION CODE

STATUS DATE TIMEPIDTIME

ACTION

A 1 02:57:00

HRS

joshua.r.childers10-Dec-2016

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 14022.2 K

00

OPERATE WITHIN LIMITATIONS AND RESTRICTIONS SPECIFIED INTHE ENCLOSED AIRWORTHINESS RELEASE DATED: 30APR14(HYDRO-MECH ASSY), 08APR14 R1 (TRACKING WEDGES),21JAN14 R3 (IPAD), 20MAR13 R4 (EMC-100 ECU), 10DEC13 R16(MSPU), 10JUL12 (IRSS), 10OCT13 (EAWIS), 16MAY12 R1 (LOGBOOK LAPTOP), 02MAY12 (DUAL EMD) 24OCT13 R2 (DGNS),09MAY11 (RAMP GUNNER SEAT), 19JUL10-R1 (GARMIN 496),12JAN10 (DGNS P31), 11JAN10 (ATIRCM), 09NOV09 R2 (MILTOPEMSD), 25JUN09 (BFT/SINGLE EDM), 10SEP09 (OREGON AERO),25JUN09 (P3 CHECKVALVE&DECU), 10APR09 (CMWS), 13FEB09-R1 (ELT EBC-406HM), 20NOV08 R4 (SATCOM), 18JAN08 (ERFS IICONTROL), 16OCT07-R1 (EPUSHA), 18SEP08 (M240 CATCH BAG),07FEB07 R7 (BFT), 01FEB07 (HOVER POWER CHECKS), 17AUG06(ADV HUD SDC), 31OCT05 (UPPER CLAMSHELL DOOR LATCH),30SEP05 (SPLIT RING), 06SEP05 (FLUX VALVE RELOCATION),29JUN05 (CREW CHIEF SEAT), 28NOV03-R1 (BUBBLE WINDOWLOCATION), 26NOV03 (EXT. LENGTH FLARE CABLE). OPERATEAIRCRAFT AS PRESCRIBED IN THE ENCOLSED AIRWORTHINESSRELEASE DATED 26MAR08 (AVA SINGLE CAM. MOUNT).

AWR WRITE UP WILL BE SIGNED OFFAS NEW AWRS ARE RELEASED ORAIRCRAFT HAS NEW AWRS ADDED

PID

SYS DATE ACFT HRSNO

V WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 6 02:07:00

HRS

robert.d.childers07-May-2014

DA FORM 2408-13-1, OCT 91, MAY BE USED. For use of this form, see DA PAM 738-751; the proponent agency is DCSLOGDA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORD


9200307 CH-47D



4. PAGE3. DATE

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 23907.1 O

06

AIRCRAFT RESTRICTED TO FLIGHT OPERTION AT A MAXIMUM OF100 PERCENT DUAL ENGINE TORQUE, FOR AIRCRAFT THATEXCEED THE 100 PERCENT TORQUE LIMIT CHANGE THE STATUSSYMBOL TO RED X . THE RED X ENTRY SHALL STATE AIRCRAFTSXCEEDED 100PERCENT DUAL ENGINE TORQUE LIMIT ATION,REPLACE FWD AND AFT NMAIN TRANSMISSION IN ACCORDANCEWITH SAFETY OF FLIGHT CH-47-00-03 AIRCRAFT WHICH EXCEEDTHIS LIMITATION ARE AUUTHORIZED A ONE TIME FLIGHT TO THENEAREST MAINTENANCE FACILITY(TRANSCRIBED FROM ULLS-A(E) PHASE: WJEQB03250002 ON Oct 4 2013 4:59AM)

PID

SYS DATE ACFT HRSNO

V WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 1005 12:36:00

HRS

james.cloud29-Sep-2013

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

O 14432.2 O

00

INSP A530 - AIRCRAFT EQUIPMENT INVENTORY (DA FORM 2408-17). Due at: 29-May-2017. Upgrade to Red X Status on 29-Jun-2017

PID

SYS DATE ACFT HRSNO

- WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 1 07:22:00

HRS

COMGEN28-Apr-2017



9200307 CH-47D



4. PAGE3. DATE

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 14022.2 K

00

PERFORM DAILY VISUAL INSPECTIONS REQUIRED BY THEENCLOSED AIRWORTHINESS RELEASE DATED: 08APR14(TRACKING WEDGES), 10OCT13 (EAWIS), 02MAY12 (DUAL EDM),09MAY11 (RAMP GUNNER SEAT),25JUN09 (BFT/SINGLE EDM),13FEB09-R1 (ELT EBC-406HM), 18JAN08 (ERFS II CONTORL),16OCT07-R1 (EPUSHA), 18SEP08 (M240 CATCH BAG), 07FEB07 R7(BFT), 10APR09 (CMWS), 25JUN09 (P3 CHECKVALVE&DECU),20NOV08 (SATCOM), 31OCT05 (UPPER CLAMSHELL DOOR LATCH),06SEP05 (FLUX VALVE RELOCATION), 29 JUN05 (CREW CHIEFSEAT) IN CONJUNTION WITH PMD. PERFORM SPECIALINSPECTIONS REQUIRED BY THE ENCLOSED AIRWORTHINESSRELEASE DATED: 30SEP05 (SPLIT RING).

AWR WRITE UP WILL BE SIGNED OFFAS NEW AWRS ARE RELEASED ORAIRCRAFT HAS NEW AWRS ADDED

PID

SYS DATE ACFT HRSNO

- WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 7 02:09:00

HRS


DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 24432.2 V

09

CABIN EMERGENCY LIGHTING WOULD NOT RESET

PID

SYS DATE ACFT HRSNO

/ WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 2 07:05:00

HRS

joshua.a.biagioni27-Apr-2017



9200307 CH-47D



4. PAGE3. DATE

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 14415.8 X

04

#2 ENGINE SEEPING OIL ON ENGINE DECK QUICK DISCONNECT

PID

SYS DATE ACFT HRSNO

/ WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 1 09:20:00

HRS

vernon.r.jabson12-Apr-2017

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 24377.2 X

07

HYDRAULIC RETURN LINE AT STA 545 L/H SIDE OF RAMP CROWNSEEPING AT SWAGE

PID

SYS DATE ACFT HRSNO

/ WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 3 11:38:00

HRS

kyle.w.waller10-Feb-2017

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 24357.6 X

02

L/H UPPER C-BOX CLAM SHELL DOOR IRSS BRACKET CRACKED

PID

SYS DATE ACFT HRSNO

/ WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 3 10:24:00

HRS

david.d.shadowens09-Dec-2016



9200307 CH-47D



4. PAGE3. DATE

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 24357.6 X

07

#1 FLT HYD COOLER DRAIN TUBE NOT INSTALLED

PID

SYS DATE ACFT HRSNO

/ WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 4 10:26:00

HRS

david.d.shadowens09-Dec-2016

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT PID

SYS DATE ACFT HRSNO

WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

HRS

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT PID

SYS DATE ACFT HRSNO

WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

HRS


DATE _______________________________________ Page ___________

12. CAT 13. MMH8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID

7. FAULT

6. FAULT NUMBER5. FAULT DATE

2. SERIAL NUMBER 3. SYSTEM CODE1. STATUS 4. TIME

DA FORM 2408-13-2, NOV 91, MAY BE USED. For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

DA FORM 2408-13-2, OCT 1997 RELATED MAINTENANCE ACTIONS RECORD

Page ___________

NUMBER PIDENTRY

ORGANIZATION LOCATION8.7.

DATE6.

REMARKS4. 5.

CH-47D 9200307HELICOPTER, CARGO2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL

Page 1 of 20

BOEING HELICOPTERSALIGMENT CHECK OF THE ACFT DRIVESYSTEM, ENGINE TO COMBINER SHAFTALIGMENT COMPLETED. LENGHT OFADJUSTABLE LINK, CENTER LINE OFBEARING IS 4.67IN L/S 4.68IN R/S K. L. MRUKCIV (GM0923)

19-Nov-1993 1

PHILA PA.

quality.control

BOEING HELICOPTERSAIRFRAME S/N M3448 AIRCRAFT S/N 62-2119CH47A INDUCTED AND CONVERTED TOCH47D S/N 9200307 ON 14 DEC 93 TOTAL TIMEAT MODIFICATION 163.0 ACFT HRS K. L. MRUKCIV (GM0923)

14-Dec-1993 1

PHILA PA

quality.control

BOEING HELICOPTERSAIRCRAFT S/N 9200307 TEST FLOWN ANDACCEPTED AT 171.3 ACFT HRS K. L. MRUKCIV (GM0923)

12-Jan-1994 1

PHILA PA

quality.control

AASF-PSBAIRCRAFT RECEIVED BY CO G 104TH AVN UICWV7SAA (GM0923)

01-Feb-1994 1

PHILIPSBURG, PA.16866

quality.control

AASF-PSBAVSCOM AMSAV-E 70-62 MSG AWR FOREMERGENCY LOCATOR TRANSMITTER ELT &TEST PROCEDURES ON ALL ARMY AIRCRAFTAWR DTD 17 DEC 99 (GM0923)

01-Feb-1994 2


quality.control

AASF-PSBCH47-94-ASAM-04 TB1-1520-240-20-69 ONETIME INSP. OF PILOT & CO-PILOT SEAT BELTSFPR PROPER HARDWARE (PIN)INSTALLATION (GM0923)

12-Feb-1994 1


quality.control

AASF-PSBCH47-94-ASAM-05 TB1-1520-240-20-71 ONETIME INSP. OF 5000 LB TIEDOWNRECEPTACLE ASSEMBLIES (GM0923)

03-May-1994 1


quality.control

AASF-PSBCH47-94-ASAM-06 TB1-1520-240-20-70 ONETIME AND RECURRING INSPECTION OFHYDRAULIC PUMPING UNITS (GM0923)

03-May-1994 2


quality.control

AASF-PSBOCM/ACE PERFORMED AT 252 ACFT HRS ATPHILIPSBURG PA BY ACE TEAM MEMBER R S.HAELD (GM0923)

25-Aug-1994 1


quality.control

AASF-PSBSOF CH47-95-01 TB1-1520-240-20-02 ONE TIMEVISUAL INSPECTION OF UPPER BOOSTACTUATOR SERIAL NUMBERS TO ENSUREPROPER SCREWS ARE INSTALLED (GM0923)

08-Dec-1994 1


quality.control

AASF-PSBCH47-95-ASAM-01 ONE TIME AND RECURRINGDAILY INSP. OF THRUST IDLER ASSY. P/N145C1408-1 (GM0923)

03-Jan-1995 1


quality.control

AASF-PSBCH47-95-ASAM-02 ONE TIME TORQUEVERIFICATION OF THE NUTS SECURING THE#1 & #2 PTU MOTOR/PUMP P/N 145HS140-8(GM0923)

25-Jan-1995 1


quality.control

AASF-PSBCH47-95-ASAM-04 TB1-1520-240-20-75 ONETIME INSP. FOR STRATOPOWER HYD. PUMPSAND COORDINATE A TURN-IN PROGRAM(GM0923)

29-Mar-1995 1


quality.control

AASF-PSBSOF CH47-95-02 TB1-1520-240-20-76 ONE TIMEINSP. & TORQUE CHECK OF FWD & AFTLOWER DRIVE LINK TO SWASHPLATERETAINING HARDWARE (GM0923)

09-May-1995 1


quality.control

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, OCT 1991

NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 2 of 20

AASF-PSBCH47-95-ASAM-05 TB1-1520-240-20-77INSPECTION AND LUBRICATION OF FLIGHTCONTROL ROD END BEARINGS COMPLETEDDURING PHASE MAINTENANCE AT 363.0 ACFTHRS (GM0923)

03-Jun-1995 1


quality.control

AASF-PSBPHASE 1 COMPLETED AT 350.0 ACFT HRSNEXT PHASE INSPECTION DUE IS #2 AT 550.OACFT HRS (GM0923)

13-Jul-1995 1


quality.control

AASF-PSBCH47-95-ASAM-06 TB1-1520-240-20-77REVISION OF INSPECTION AND LUBRICATIONOF FLIGHT CONTROL ROD END BEARINGS(GM0923)

22-Aug-1995 1


quality.control

AASF-PSBCH47-95-ASAM-07 TB1-1520-240-20-79 ONETIME RECORD CHECK AND RECURRINGINSPECTION OF ROTOR HEAD PVH LAGDAMPER WITH MWO1-1520-240-50-69 APPLIED(GM0923)

12-Sep-1995 1


quality.control

AASF-PSBACE/AACE PERFORMED AT 370.0 ACFT HRSBY ACE TEAM MEMBER G AT PHILIPSBURG,PA. ATCOM OCM SEC ST LOUIS MO A. P.BREAUX (GM0923)

14-Sep-1995 1


quality.control

AASF-PSBCH47-95-ASAM-08 TB1-1520-240-20-78 ONETIME AND PHASE INSPECTION, INSPECT AFTROTOR VERTICAL SHAFT FOR CLEARANCEBETWEEN DUST SEAL (GM0923)

16-Sep-1995 1


quality.control

AASF-PSBCH47-96-ASAM-01 TB1-1520-240-20-80INSPECT AND IDENTIFY P/N 114L2329-2 AFTLDG GEAR LOWER DRAG LINKS ARESUSCEPTIBLE TO STRESS CORROSIONCRACKING (GM0923)

08-Nov-1995 1


quality.control

AASF-PSBCH47-96-ASAM-03 TB1-1520-240-20-82 ONETIME VISUAL INSPECTION OF PRESSUREGAUGES FOR OBSTRUCTED RELIEF (DRAIN)HOLES BY IDENTIFICATION TAPE LOCATION(GM0923)

26-Feb-1996 1


quality.control

AASF-PSBCH47-96-ASAM-04 TB1-1520-240-20-83 ONETIME INSP. OF FWD & AFT ROTOR HEADS TOENSURE FLOW OF OIL TO HORIZONTALHINGE PIN BEARINGS (GM0923)

11-Jun-1996 1


quality.control

AASF-PSBCH47-96-ASAM-05 TB1-1520-240-20-84 ONETIME INSP. OF FWD CONTROL INSTALLATIONFOR MANUFACTURER OF BOLT P/N 114R3650-3 (GM0923)

02-Jul-1996 1


quality.control

AASF-PSBCH47-96-ASAM-06 TB1-1520-240-20-85 ONETIME RECORD CHECK & RECURRING INSP. OFTHE UPPER BOOST ACTUATORS AND PULLTEST ON SWASHPLATES. (RB9919)

02-Jul-1996 2

PHILIPSBURG,PA.16866

quality.control

AASF-PSBCH47-96-ASAM-07 TB1-1520-240-20-86INSPECT BOND LINES (SECURITY) OFCUSHION MATERIAL ATTATCHED TO #1 & #2ENGINE FOD SCREENS. (RB9919)

19-Jul-1996 1


quality.control

AASF-PSBCH47-96-ASAM-08 TB1-1520-240-20-88 ONETIME INSP. & REMOVAL OF CERTAIN SERIALNUMBER 145S102-3 FWD XMSN MAINLUBRICATION PUMP. (RB9919)

22-Aug-1996 1


quality.control


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 3 of 20

AASF-PSBCH47-96-ASAM-09 TB1-1520-240-20-89INSPECT C-XMSN DOOR LWR LATCHES FORWEAR TO PRELUDE IN-FLT LOSS & ADDITIONOF LATCH P/C/W. (GM0923)

15-Sep-1996 1

PHILIPSBURG PA 16866

quality.control

AASF-PSBPHASE #2 COMPLETED AT 550 ACFT HRSNEXT PHASE DUE IS #3 AT 750 ACFT HRS.(GM0923)

20-Sep-1996 1


quality.control

AASF-PSBCH47-97-ASAM-01 ONE TIME RECORDSCHECK & REMOVAL OF CERTAIN SERIALNUMBERED SYNCHRONIZING DRIVE SHAFTASSY'S COMPLIED WITH. (GM0923)

15-Oct-1996 1


quality.control

AASF-PSBSOF MSG CH47-97-01 ONE TIME VISUAL INSPOF FWD XMSN MOUNTING (BARREL) NUTSCOMPLIED WITH AT 560.6 ACFT HRS.(GM0923)

15-Nov-1996 1


quality.control

AASF-PSBCH47-97-ASAM-02 TB1-1520-240-20-92INSTALLATION OF GUARD AROUND CARGOHOOK RELEASE SWITCH ON WINCH / HOISTOPERATORS GRIP ASSY. P/N 114ES250-2COMPLIED WITH. (GM0923)

08-Jan-1997 1


quality.control

AASF-PSBGEN MSG 97-ASAM-03 INVENTORY OF AN/ASN-149 GLOBAL POSITIONING SYS &PROCEDURES FOR LOADING CRYPTO TOPREVENT NAVIGATION ERROR COMPLIEDWITH, EQUIP. NOT INSTALLED. (GM0923)

16-Jan-1997 1


quality.control

AASF-PSBCH47-97-ASAM-03 TB1-1520-240-20-94 ONETIME & RECURRING INSP OF CABIN & RAMPFLOOR 5,000 LB TIE DOWN FITTINGS FORSECURITY COMPLIED WITH. (GM0923)

12-Feb-1997 1


quality.control

AASF-PSBCH47-97-ASAM-04 TB1-1520-240-20-96 ONETIME VISUAL INSP & REPLACEMENT OFCERTAIN P/N CRISSAIR CHECK VALVESINSTALLED IN #1 & #2 FLT CONTROL MODULECOMPLIED WITH. (GM0923)

21-Mar-1997 1


quality.control

AASF-PSBCH47-97-ASAM-05 TB1-1520-240-20-93 ONETIME INSP FOR & REPLACEMENT OF AN320-12CASTELLATED NUTS MADE BY GREER INCWITH "G" CODE COMPLIED WITH. (GM0923)

21-Mar-1997 2


miranda.m.moore

AASF-PSBCH47-97-ASAM-06 021555ZAPR97 NAVSTARAN/ASN-149V1 GPS LOCKUP WITH C11702/URDISPLAY WHEN TRACKING SATELLITE PRN30. N/A SYSTEM NOT INSTALLED. (GM0923)

09-Apr-1997 1


quality.control

AASF-PSBCH47-97-ASAM-07 TB1-1520-240-20-95 ONETIME / RECURRING INSP OF POWERDISTRIBUTION FEEDER WIRING & CIRCUITBREAKERS & INSTALLATION OF A COVER TOPREVENT WATER INTRUSION COMPLIEDWITH. (GM0923)

21-Apr-1997 1


quality.control

AASF-PSBCH47-97-ASAM-08 TB1-1520-240-20-97 INSP &LUBE FLT CONTROL ROD END BEARINGS INTHE FLT CONTROL CLOSET COMPLIED WITH.(GM0923)

24-Apr-1997 1


quality.control

AASF-FTIGCH47-97-ASAM-09 OPERATION OF T-62T-2BAPU & REPORT OF APU FLIGHT HOURSCOMPLIED WITH. (GM0923)

03-Jun-1997 1

ANNVILLE PA 17003-5005

quality.control


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 4 of 20

AASF-FTIGCH47-97-ASAM-10 / TB1-1520-240-20-99 ONETIME INSP OF ANVIS/HUD SIGNAL DATACONVERTER P/N CV-4229(V)1 FOR DEFECTIVEPOWER SUPPLY MUDULE (CARD) P/N 125118-001 DATE CODE 9601 AND NEWER ARESUSPECT C/W. EQUIP. NOT INSTALLED(GM0923)

07-Oct-1997 1


quality.control

AASF-FTIGCH47-98-ASAM-01 RECORDS CHECK FORINCIDENTS OF UNCOMMANDED CONTROLINPUTS OR LOCK UPS C/W. (GM0923)

17-Oct-1997 1


quality.control

AASF-FTIGCH47-98-ASAM-02/TB1-1520-240-20-100EXTENSION FOR REPLACEMENT OF AFT LDGGEAR DRAG LINK ASSY THAT ARESUSCEPTIBLE TO STRESS CORROSIONCRACKING C/W (GM0923)

24-Oct-1997 1


quality.control

AASF-FTIGAIRFRAME #1 ENGINE MOUNT STRUCTURENDI COMPLETED AT 725.1 ACFT HRS.(GM0923)

18-Feb-1998 1


quality.control

AASF-FTIGS.O.F. MSG CH-47-98-01 (TB1-1520-240-20-103)ONE TIME INSP. OF AFT UPPER BOOSTACTUATOR TO STATIONARY SWASHPLATERETAINING HARDWARE COMPLIED WITH.(RN1423)

19-Mar-1998 1

ANNVILLE, PA 17003-5005

quality.control

AASF-FTIGAIRFRAME #2 ENGINE MOUNT STRUCTURENDI COMPLETED AT 750.0 ACFT HRS (GM0923)

04-May-1998 1

ANNVILLE, PA 17003

quality.control

AASF-FTIGPHASE #3 COMPLETED AT 750.0 ACFT HRSNEXT PHASE DUE IS #4 AT 950.0 ACFT HRS(GM0923)

04-May-1998 2

ANNVILLE, PA 17003

quality.control

AASF-FTIGCH-47-98-ASAM-03 (TB1-2835-205-20-3)MANDATORY TORQUE CHECK ANDREPLACEMENT OF APU BOLTS REPEATATIVEINSP & BOLT REPLACEMENT C/W AT 750.0ACFT HRS (RN1423)

04-May-1998 3

ANNVILLE, PA

quality.control

AASF-FTIGCH-47-98-ASAM-04 TB1-1520-240-20-102 ONE-TIME COMPONENT S/N INSP.FORTRANSMISSION WITH SUSPECTEDIMPROPERLY SHIMMED INPUT PINION GEARASSY. C/W. (RB9919)

15-May-1998 1

ANNVILLE,PA

quality.control

AASF-FTIGSOF MSG CH47-98-02 TB1-1520-240-20-105FLIGHT RESTRICTIONS AND REPETITVEINSPECTION OF C-XMSN FAN DRIVE SHAFTCOMPLIED WITH (GM0923)

17-Jul-1998 1


quality.control

AASF-FTIGACE PERFORMED AT 818.7 ACFT HRS BYTEAM MEMBER "T" MWO BRANCH ATCOM.(RB9919)

02-Sep-1998 1

ANNVILLE,PA.17003-5005

quality.control

AASF-FTIGCH47-98-ASAM-05 TB1-1520-240-20-101REVISION TO CH47-98-ASAM-02 IDENTIFY &INSPECT AFT LANDING GEAR DRAG LINKPROCEDURES AND LIFTING OF ROLL ONLANDING RESTRICTIONS C/W (GM0923)

23-Sep-1998 1


quality.control

AASF-FTIGCH-47-99-ASAM-01 (TB1-1520-240-20-106) ONETIMEINSP OF BLADE LAG DAMPNERS WITHELASTOMERIC BEARINGS FOR IMPROPERADJUSTMENT OF ROD ENDS C/W. (RN1423)

11-Feb-1999 1


quality.control


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 5 of 20

AASF-FTIGCH47-99-ASAM-02 TB1-1520-240-20-107 FLIGHTCONTROL LOCKUP/UNCOMMANDED INPUTS,INSPECT FOR SUSPECTED SERVOCYLINDER(GM0923)

18-Feb-1999 1

ANNVILLE, PA.17003-5005

quality.control

AASF-FTIGCH47-99-ASAM-03(TB55-1520-240-20-108)ONETIME AND RECURRING INSP OF HOIST/CARGOHOOK CONTROL PANEL AND WATERINTRUSION IN THE COCKPIT (GM0923)

27-Feb-1999 1

ANNVILLE,PA 17003-5005

quality.control

AASF-FTIGCH47-99-ASAM-04 TB1-1520-240-20-109INSPECTION OF FORWARD AND AFTLONGITUDINAL CYCLIC TRIM YOKES FORBUSHING INSTALLATION AND MAINTENANCEMANUAL REVISION (GM0923)

16-Mar-1999 1

ANNVILLE, PA. 17003-5005

quality.control

AASF-FTIGCH47-99-ASAM-05 TB1-1520-240-20-110EXTENSION FOR REPLACEMENT OF THE AFTLDG GEAR LOWER DRAG LINK ASSYSUSCEPTIBLE TO STRESS CORROSIONCRACKING PREVIOUSLY REQUIRED BY CH47-96-ASAM-01 TB1-1520-240-20-80/CH47-98-ASAM-02 TB1-1520-240-20-100 AND CH47-96-ASAM-05 TB1-1520-240-20-101 DUE NLT 31OCT 2000 (GM0923)

30-Apr-1999 1


quality.control

AASF-FTIGSOF CH47-99-01 TB1-1520-240-20-111 ONETIME INSP OF SYNCH-SHAFT MOUNTBRACKETS FOR PROPER CLEARANCE TOSYNCH-SHAFT (GM0923)

01-Jul-1999 1


quality.control

AASF-FTIGPHASE #4 COMPLETED AT 950.0 ACFT HRSNEXT PHASE DUE IS #1 AT 1150.0 ACFT HRS.(GM0923)

30-Jul-1999 1


quality.control

AASF-FTIGSOF CH47-99-02 IMMEDIATE GROUNDINGSECONDARY PLANETARY GEAR FAILURES,AWAITING FURTHER INSTRUCTIONS (GM0923)

09-Aug-1999 1


quality.control

AASF-FTIGACE COMPLETED AT 954 ACFT HRS BY ACEMEMBER 'G' AMCOM OLR/MWO BRANCHEH9090 (GM0923)

13-Aug-1999 1

ANNVILLE, PA.17003-5005

quality.control

AASF-FTIGSOF CH47-99-03 TB55-1520-240-20-113INSPECT/RECORD CHECK OF FWD AND AFTTRANSMISSION S/N'S FOR MG IF SOANNOTATED ACFT IS RELEASED FOR FLT(GM0923)

26-Aug-1999 1


quality.control

AASF-FTIGSOF CH47-99-04 TB1-1520-240-20-114INSPECT/RECORDS CHECK FWD AND AFTTRANSMISSION FOR GEAR BEARING ASSYS/N'S FOR 'VB', UNGROUNDINGPROCEEDURES (GM0923)

27-Aug-1999 1


quality.control

AASF-FTIGSOF CH47-99-05 TB1-1520-240-20-115REPLACEMENT// ORDERING INSTRUCTIONSOF SUSPECTED FWD & AFT XMSN WITHSUBJECT GEAR BEARING ASSY'S (GM0923)

16-Sep-1999 1


quality.control

AASF-FTIGSOF CH47-00-01 TB1-2835-205-20-04OPERATIONAL RESTRICTION AND REVISIONTO HISTORICAL RECORD REQUIREMENTS(GM0923)

14-Oct-1999 1


quality.control


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 6 of 20

AASF-FTIGSOF CH47-00-02 REVISION TO CH47-00-01HISTORICAL RECORD KEEPING &OPERATIONAL RESTRICTION OF APU'SBETWEEN 2100 & 5360 STARTS, ABOVEWHICH UNIT BE COMES NONSERVICABLE(GM0923)

08-Nov-1999 1


quality.control

AASF-FTIGSOF CH47-00-03 TB1-1520-240-20-116 ACFTRESTRICTED TO FLT OPERATIOS AT AMAXIMUM OF 100% DUAL ENGINE TORGUEDOES NOT APPLY FWD & AFT XMSN'SREPLACED WITH MG SUFFIX S/N (GM0923)

08-Dec-1999 1


quality.control

AASF-FTIGSOF CH47-00-04 TB1-1520-240-20-117 ONE-TIME RECORD CHECK OF ENGINE XMSNPINION P/N 145D6301 & SPIRAL BEVEL GEAR145D6302 FOR S/N'S PRECEDED BY 'P'(GM0923)

28-Jan-2000 1


quality.control

AASF-FTIGGEN MSG-00-ASAM-01 ALSE ALL ARMY ACFTUPDATE OF NIGHT VISION GOGGLES,REVISION TO PUBLICATIONS & ACFTLIGHTING CONFIGURATION (GM0923)

26-Feb-2000 1


quality.control

AASF-FTIGCH47-00-ASAM-01 TB1-1520-240-20-119 INITIALAND RECURRING INSPECTION OF FUEL PODSFOR CORROSION & ELECTRICAL BONDINGBETWEEN FUEL CAP & FUSELAGE (GM0923)

28-Apr-2000 1


quality.control

AASF-FTIGSOF CH47-00-05 TB1-1520-240-20-120 ONE-TIME VISUAL INSP OF PITCH HOUSINGS FORS/N PREFIX OF TM REQD NLT 15 MAY 00(RB9919)

02-May-2000 1


quality.control

AASF-FTIGSOF CH47-00-06 AUTHORIZED OPERATIONALUSE OF APU CONTAINMENT DEVICE WITHOUT RESTRICTIONS IAW LOI CH47-2000-01(GM0923)

08-May-2000 1


quality.control

AASF-FTIGCH47-00-ASAM-02 TB1-1520-240-20-118 INSPHORIZ HINGE PIN SHOULDERED BOLTS FORP/N 114R2201-1 (RB9919)

23-May-2000 1


quality.control

AASF-FTIGCH47-00-ASAM-03 UTILITY #1 & #2 HYD.SYSTEM FLUID SAMPLES DUE EVERY 50 HRSOR 100 DAYS. (RB9919)

02-Jun-2000 1


quality.control

AASF-FTIGCH47-00-ASAM-04,TB1-1520-240-20-122RECORDS CHECK OF HORIZONTAL HINGEPINS WITH S/N PRIOR TO UW2407 REQUIRESA HARDNESS TEST BY 4800 TSN. (RB9919)

27-Jul-2000 1


quality.control

AASF-FTIGCH47-00-ASAM-05,TB1-1520-240-20-123INSPECT FWD AND AFT SLIDER SHAFT SEALSIAW TASK 6-58. (RB9919)

27-Jul-2000 2


quality.control

CT AVCRADCH-47-00-ASAM-06 9TB 1-1520-240-20-126)INSP FOR DEFECTIVE FADAC P3 DRAINCARTRIDGE FOR "C" PREFIX AFTER S/N. @1100.0 ACFT HRS (SR0934)

02-Oct-2000 1

GROTON, CT. 06340

quality.control

CT AVCRADCH-47-00-ASAM-07 (TB 1-1520-240-20-125) INSPFOR UNTESTED P/N 114R3650-7 BOLTS FORACCEPTABLE MFG CODES 56878, SPS, 84256@ 1100 ACFT HRS (SR0934)

04-Oct-2000 1

GROTON, CT. 06340

quality.control


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 7 of 20

LSIPAINT REMOVED FROM BILGE AREA USINGPMB PAINTED I/A/W CONTRACT# F34601-97-0-0423. MIL-C-22750 @ 1100.0 ACFT HRS(RL8948)

06-Oct-2000 1

GROTON, CT. 06340

quality.control

CT AVCRADCH-47-00-ASAM-08 (TB 1-1520-240-20-128) INSPFWD YOKE SHAFT @ 1100.0 A/C HRS (SR0934)

13-Oct-2000 1

GROTON, CT. 06340

quality.control

CT AVCRADCH-47-01-ASAM-01 (TB 1-1520-240-20-127)INSPECT FOR MA-16 INERTIA REELS P/N 015-87045-3-16 @ 1100. ACFT HRS. (SR0934)

13-Oct-2000 2

GROTON, CT. 06340

quality.control

CT AVCRADCH-47-01-ASAM-02 (TB 1-1520-240-20-130)INSPECT FOR UNTESTED FSP 114R3650-6 & 11BOLTS FWD SPEED TRIM & STRAIN LINK TOSWASHPLATE & FWD & AFT DRIVE ARMCENTER FOR APPROVED CAGE CODES,TECHNOLOGIES INC 56878, AVIBANK MFG84256 @ 1100 ACFT HRS (SR0934)

31-Oct-2000 1

GROTON, CT. 06340

quality.control

CT AVCRADSOF CH-47-00-07 (TB 1-1520-240-20-129)INSPECT COMBINING XMSN COOLING FANDRIVE SHAFT @ 1100.0 A/C HRS. (SR0934)

16-Nov-2000 1

GROTON, CT. 06340

quality.control

CT AVCRADCH-47-01-ASAM-05 (TB 1-1520-240-20-132)INSPECT DROOP STOP BOLTS FOR PROPERLENGTH @ 1100.0 A/C HRS. (SR0934)

29-Dec-2000 1

GROTON, CT. 06340

quality.control

CT AVCRADCH-47-01-ASAM-06 (TB 1-1520-240-20-133)REVISION TO CH-47-01-ASAM-04 TIEBAR PINSFOR ACCEPTABLE CAGE CODES @ 1100ACFT HRS (SR0934)

02-Jan-2001 1

GROTON, CT. 06340

quality.control

CT AVCRADSOF CH-47-01-01 (TB 1-1520-240-20-134)ONETIME INSPECTION OF AFT ROTOR HEADASSY'S & ENGINE CROSS SHAFT ADAPTERASSY'S TO IDENTIFY REDUCTION IN LIFELIMIT PARTS @ 1100 ACFT HRS (SR0934)

02-Jan-2001 2

GROTON, CT. 06340

quality.control

CT AVCRADCH-47-01-ASAM-04 (TB 1-1520-240-20-133)INSPECT UNTESTED FSP P/N 114R2168-3 & 4TIE BAR PIN ASSY'S @ 1100.0 A/C HRS.(SR0934)

11-Jan-2001 1

GROTON, CT. 06340

quality.control

CT AVCRADACFT. HYD. SYSTEMS PURIFICATIONPERFORMED @ 1100.0 A/C HRS. PAL S/N A032START TIME 158.0, END TIME 186.6 AGPU S/NID P1003 START TIME 64.8 END TIME 93.4(SR0934)

13-Jan-2001 1

GROTON, CT. 06340

quality.control

CT AVCRADCH-47-01-ASAM-03 (TB 1-1520-240-20-131)INSPECT FWD & AFT ROTOR HUBLIGHTENING HOLES(EDDY CURRENT) @1100.0 A/C HRS. (SR0934)

01-Feb-2001 1

GROTON, CT. 06340

quality.control

CT AVCRADPHASE #1 COMPLETED @ 1100.0 A/C HRS.NEXT PHASE #2 DUE @ 1300.0 ACFT HRS.(SR0934)

01-Feb-2001 2

GROTON, CT. 06340

quality.control

CT AVCRADSOF CH-47-01-02 (TB 1-1520-240-20-136)INSPECT DROOP STOPS FOR CHAMFERLOCATION @ 1100.0 A/C HRS. (SR0934)

04-Feb-2001 1

GROTON, CT. 06340

quality.control

AASF-FTIGCH47-01-ASAM-07, TB1-1520-240-20-135,INSPECT 12 EA P/C/L BOLTS FOR UNTESTEDP/N: 114R3650-13 & -15 DUE BY 1 MAR 2002.(RB9919)

12-Feb-2001 1

ANNVILLE, PA

quality.control


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 8 of 20

AASF-FTIGAIRFRAME #1 & #2 ENGINE MOUNTSTRUCTURE NDI COMPLETED AT 1109.0 ACFTHRS. (GM0923)

13-Feb-2001 1


quality.control

AASF-FTIGSOF-CH47-01-03, TB1-1520-240-20-137 FIXEDDROOP UNGROUNDING REQUIREMENTS FORACFT GROUNDED BY SOF-01-02. (RB9919)

20-Feb-2001 1

ANNVILLE PA 17003

quality.control

AASF-FTIGGEN-01-ASAM-03 021315MAY01 REVISION TOGEN-00-ASAM-01 NVG STANDARDIZATIONAND UPGRADE REF TM11-5855-263-10 /23&23P / 300-10 / 23&P / 264-14 / 299-12(GM0923)

02-May-2001 1


quality.control

AASF-FTIGEMC/EMI FLIGHT TEST COMPLETED,AIRCRAFT AUTHORIZED TO OPERATE WITHCOMMUNICATION EAR PLUGS (CEP) IAW AWRDTD 14 JUL 99. (GM0923)

20-May-2001 1


quality.control

AASF-FTIGAIRCRAFT MODIFIED WITH MWO1-1520-240-50-83 DTD 01 MAY 2000. INSTALLATION OF FULLAUTHORITY DIGITAL ENGINE CONTROLS(FADEC) AND AUTHORIZED FOR FLIGHT I/A/WAWR DTD 21 MAR2001 R4. (GM0923)

21-May-2001 1


quality.control

AASF-FTIGCH47-01-ASAM-08 TB1-1520-240-20-138INSPECTION OF FLIGHT AND UTILITYHYDRAULIC CONTROL MODULES TO ENSURESHUT-OFF DIAPHRAGM HARDWARE ISINSTALLED (GM0923)

09-Aug-2001 1


quality.control

AASF-FTIGCH47-01-ASAM-09 TB1-1520-240-20-139UNTESTED FLT SAFETY PART BOLTS.114R3650-9 & BACB30ST10-40 INSPECT FWD &AFT DRIVE ARM TO DRIVE COLLAR ANDSTRAIN LINK LOWER BOLTS FORACCEPTABLE CAGE CODES NEXT PHASE BUTNLT 30 SEP 2002 (GM0923)

06-Sep-2001 1


quality.control

AASF #1 FT. IG.CH47-02-ASAM-01, TB1-1520-240-20-142, INSPOF TUNNEL COVERS STRUT ASSY'S**STAKED PIN** FOR SECURITY DUE NLT 18OCT 01. (RB9919)

04-Oct-2001 1

ANNVILLE PA 17003

quality.control

AASF-FTIGMAINTENANCE ADVISORY MESSAGE MAM-02-001 M130 FLARE DISPENSER1095-036-6886TM9-1095-206-30&P SEQUENCER PLATE ASSY5998-01-057-0042 P/N 9311488 INSP IAWPARA'S 2C & 3 FOR SERVICABILITY CHAFINGAND WIRE ROUTING (GM0923)

10-Oct-2001 1


quality.control

AASF-FTIGCH47-MIM-2002-01 171401ZOCT01 FIELDINSTRUCTIONS FOR TRACKING T55-GA-714ATURBINE ENGINE AND SUBASSEMBLIES, ANDCOMPLETING AMSAM-MMC FORM 721(ENGINE POWER ASSURANCE TEST RECORD). (GM0923)

22-Oct-2001 1


quality.control

AASF #1 FT. IG.CH47-02-ASAM-02, TB1-1520-240-20-143EXTENSION OF ASAM-00-08 FWD XMSN YOKEBOLT REPLACEMENT LIFE MUST BECOMPLIED WITH BY 31 DEC 01. (RB9919)

27-Dec-2001 1


quality.control

LM2ACE COMPLETED AT 1250 ACFT HRS BY ACETEAM MEMBER JJ, AMCOM OLR/MWOBRANCH.. (CC2212)

09-Jan-2002 1

FTIG, ANNVILLE, PA.

quality.control


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 9 of 20

AASF-FTIGSOF CH-47-02-01, TB1-1520-240-20-144INSPECTION OF SWASHPLATE'S LOWERSEAL RETAINING LOCK NUTS FOR PROPERTHREAD PROTRUSION. (RB9919)

25-Jan-2002 1

ANNVILLE PA 17003

quality.control

AASF-FTIGSOF-CH-47-02-02, TB1-1520-240-20-141INSPECTION OF ROTOR HEAD TIE-BARSHISTORICAL RECORDS FOR REDUCTION OFSERVICE LIFE AND ROTOR TACH.LIMITATIONS. (RB9919)

25-Jan-2002 2

ANNVILLE PA 17003

quality.control

AASF-FTIGSOF CH47-02-03 TB1-1520-240-20-141REVISION TO SOF CH47-02-02 TIE BAR LIFEREDUCTION AND TACH LIMITS. (RB9919)

26-Jan-2002 1

ANNVILLE PA 17003

quality.control

AASF-FTIGSOF MSG CH47-02-04 TB1-1520-240-20-145INSPECT FORWARD PIVOTING ACTUATOR TOSWASHPLATE ATTACH BOLT BEARING FORPROPER INTERNAL DIAMETER. CORRECT P/N145HS001-1 ID 0.5000 +.000/-.0005 (GM0923)

07-Feb-2002 1


quality.control

AASF-FTIGGEN-02-ASAM-02 NIGHT VISION GOGGLEINFORMATION UPDATE, REVISION TO GEN-01-ASAM-03 (GM0923)

21-Feb-2002 1


quality.control

AASF-FTIGSOF CH47-02-05 TB1-1520-240-20-146REVISION TO 02-03 TB-20-141 INSPECTROTORHEAD TIEBAR ASSY'S IAW TASK 5-23.1.1 NEXT PHASE BUT NLT25JAN04.COMPLETED @ PHASE 2 1300.0 ACFTHRS (GM0923)

25-Mar-2002 1


quality.control

AASF-FTIGPHASE#2 COMPLETED @ 1300.0 ACFT HRS.NEXT PHASE #3 DUE @ 1500.0 ACFT HRS.(GM0923)

06-May-2002 1


quality.control

AASF-FTIGCH47-02-ASAM-03 TB1-1520-240-147 INSPECTFUEL PUMP CONTROL BOXES FOR PROPERWIRING, REPORTED FAULT WIRES INSTALLEDON RELAY SCREWS WITHOUT CONNECTORS(GM0923)

14-Jun-2002 1


quality.control

AASF-FTIGSOF CH47-02-06 TB1-1520-240-20-148 INSPECTC-XMSN RECORD FOR CCAD OVERHAULBETWEEN 28JUN00 & 17JUN02 AND S/N'SLISTED IN PARA 8B. REMOVE FROM SERVICEDUE TO PLASTIC MEDIA USED FOR CLEANING(GM0923)

19-Jun-2002 1


quality.control

AASF-FTIGCH47-02-ASAM-04 TB1-1520-240-20-149INSPECT FOR UNTESTED AFT YOKE SUPPORTBOLT P/N 114C3044-2 EXCEPTABLE CAGECODES 77272 BOEING, 7D072 TURA MACHINECO, 07952 RUSCOMB TOOL & MACHINE(GM0923)

25-Jul-2002 1


quality.control

LMLMACE COMPLETED AT 1356 ACFT HRS BY ACEMEMBER L AMCOM OLR/MWO BRANCH(EH9090)

18-Sep-2002 1

ANNVILLE,PA

quality.control

AASF-FTIGSOF CH47-03-01 DETERMINE SERVICABILITYOF FWD AND AFT SWASHPLATES BY PURGELUBE AND SUBMIT AOAP GREASE SAMPLEEVERY 50 HRS. PERFORM VISUALINSPECTION OF BEARING BY REMOVINGSEAL PLATE EVERY 100 HR (GM0923)

07-Oct-2002 1


quality.control


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 10 of 20

AASF-FTIGGEN-MIM-03-001 IDENTIFY & REPLACESTANDISH WITH ADS ARC-220/VRC-100DISPLAYES. IDENTIFIED BY COLOR VARIANTIN UPPER LEFT FOR STANDISH & UPPERRIGHT FOR ADS DUE TO PIXEL FAILURES INHF CONTROL PANEL (GM0923)

26-Nov-2002 1


quality.control

AASF-FTIGGEN 03-ASAM-01 REISSUED FROM PREVIOUSMSG GPM 2002-004 INSP SINCGAR ARC-201BATTERY BOXES, BATTERY CLIP RETAININGRIVETS FOR CLEARANCE BETWEEN RIVETSAND BATTERIES (GM0923)

17-Dec-2002 1


quality.control

AASF-FTIGGEN 03-ASAM-01 CORRECTED COPY INSPSINCGAR ARC-201& HF CY-8515 BATTERYBOXES, BATTERY CLIP RETAINING RIVETSFOR CLEARANCE BETWWEEN RIVETS ANDBATTERIES (GM0923)

30-Dec-2002 1


quality.control

G CO 104TH AVN10 FEB 03 ACFT MOBILIZED FOR ENDURINGFREEDOM AND DEPLOYED OCONUSSOUTHWEST ASIA 20 MAR 03 THRU SAVANAHGA. ACFT HRS 1426.1 - MARITIME SHIPMENT.(MM9560)

27-Jun-2003 1

KANDAHARAFGHANISTAN

quality.control

G CO 104TH AVNMSG 1313132 MAR 03 GEN-03-ASAM-02INFORMATIONAL M18/M19 TEMPORARYLANDING/HELICOPTER PADS OPERATIONALBRIEFS AND SECURITY REQUIRED REF FM 5-430-00-02 (MM9560)

27-Jun-2003 2

KANDAHARAFGHANISTAN

quality.control

G CO 104TH AVN2513312 MAR 03 CH47-03-ASAM-01 TB 1-1520-240-20 EXTENSION OF LIFE LIMIT FROM 2000TO 6000 HRS ON CERTAIN ENG DRIVE SHAFTSP/N 114D3504-2 (MM9560)

27-Jun-2003 3

KANDAHARAFGHANISTAN

quality.control

G CO 104TH AVNALQ-156 COUNTER MEASURE LAMPS ONMASTER CAUTION ADVISORY PANEL WIREDINCORRECTLY. CORRECTED AS PERAMCOMS MATT WESSELSCHMITT 28 MAR 03BY REPINNED PIN N & L IN CONNECTOR 232P1(MM9560)

27-Jun-2003 4

KANDAHARAFGHANISTAN

quality.control

G CO 104TH AVNTB 1-1615-351-23 ROTOR BLADE TAPEAPPLIED BY OLR AT SAVANAH GA. (MM9560)

27-Jun-2003 5

KANDAHARAFGHANISTAN

quality.control

G CO 104TH AVNACFT DISASSEMBLED AND RE-ASSEMBLEDFOR AIR CARGO SHIPMENT TO KANDAHARAFGHANISTAN FOR TF SABER AT 1426.1 ACFTHRS (MM9560)

27-Jun-2003 6

KANDAHARAFGHANISTAN

quality.control

CO G 104TH AVNAWR BLUE FORCE TRACKING ENHANCEDINFORMATION SYST DTD 06 MAR 03 R2INSTALLED MWO1-1520-240-50 DRAFT(GM0923)

01-Jul-2003 1

KANDAHAR,AFGHANISTAN

quality.control

G CO 104TH AVNPHASE #3 COMPLETED @ 1489.0 ACFT HRS.NEXT PHASE IS #4 DUE @ 1689.0 ACFT HRS.(GM0923)

21-Jul-2003 1


quality.control

G CO 104TH AVNINSTALLED MWO55-1520-H47-50-097 FLIGHTCREW SEAT(SIMULA) FOR MH47D 160THSPECIAL OPERATIONS DTD 07 JUN 2001AUTHORIZED BY AWR DTD 03 JUN 2002(GM0923)

24-Jul-2003 1


quality.control


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 11 of 20

G CO 104TH AVNPHASE #4 COMPLETED AT 1675.0 ACFT HRS,NEXT PHASE IS #1 DUE AT 1875.0 ACFT HRS.PLACARD MEASUREMENTS REESTABLISHED:FWD 13 7/16, LAT 15 3/8. (EM6678)

12-Jan-2004 1


quality.control

G CO 104TH AVNREGIMENT APOAE09355

CH-47-04-ASAM-01 MSG DTD 031845ZFEB04ALL H47 SERIES ACFT-INSPECTION ANDCORRECTION OF AFT FUSELAGE BELLCRANKHARDWARE AT STA 445.5 (EM6678)

04-Feb-2004 1


quality.control

G CO 104TH AVNSOF CH47-04-01 052030ZFEB04 FWD & AFTSWASHPLATELUBRICATION/PURGE INSPECTGREASE LOCALLY & RETAIN SAMPLE UNTILNEXT 50 HR SCHEDULE INSPECTION (GM0923)

06-Feb-2004 1


quality.control

CO F-131ST AVNINSTALLED MWO1-1540-240-55-12 AN/ALE-47COUNTER-MEASUREE DISPENCER SYSTEM.(DW4576)

01-Mar-2004 1

KANDAHARAFGHANISTAN

quality.control

DOL AVIM, FT. DRUM,NY 13602

INSTALLATION OF AN/PRC-117F SATCOMRADIO COMPLETED I/A/W AWR DATED09FEB04 AT 1711.6 ACFT HRS (LB2031)

03-Mar-2004 1

KAF AFGHANISTAN

quality.control

G CO 104TH AVNCH47-MIM-2004-001 INSPECTION ANDREPLACEMENT OF APU START MODULESHOUSING P/N 145H1651-1 IF S/N IS 121 ORLOWER BY NEXT PHASE (GM0923)

31-Mar-2004 1


quality.control

COMPANY F 131 AVNAIRCRAFT S/N 92-00307 ACCEPTED BY CO F131 AVN @ 1768.5 ACFT HOURS, 10 APR 2004EL4622 (EL4622)

10-Apr-2004 1


quality.control

CO F 131 AVNCH-47-04-ASAM-02 TRANSIENT AND AVOIDBANDS ON THE CRUISE GUIDE INDICATORCOMPLIED WITH 01 MAY 04 AT 1791.8 ACFTHRS. (AE1051)

01-May-2004 1


quality.control

F CO 131 AVN REGTTB 1-1520-240-20-155 COMPLIED WITH AT1868.6 ACFT HOURS (GS0789)

13-Jun-2004 1

KANDAHARAFGHANISTAN

quality.control

CO F 131 AVNPHASE #1 COMPLETED @ 1868.6 ACFT HRSNEXT PHASE DUE @ 2068.6. (DW4576)

14-Jun-2004 1


quality.control

CO F 131 AVN REGTCOMBAT PHASE COMPLETED AT 2038.9 ACFTHOURS NEXT PHASE IS #2 DUE AT 2238.9ACFT HOURS (AE1051)

03-Oct-2004 1

KANDAHARAFGHANISTAN

quality.control

CO F 131ST AVN REGTCH-47-05-ASAM-01 CH-47 AIRCRAFT, AFTCRITICAL DYNAMIC COMPONENTS COMPLIEDWITH AT 2055.6 ACFT HRS. (AE1051)

16-Oct-2004 1

KANDAHARAFGHANISTAN

quality.control

CO F 131 AVN REGTPHASE #2 COMPLETED AT 2237.5 ACFT HRS.NEXT PHASE # 3 DUE AT 2437.5 (AE1051)

01-Jan-2005 1

KAF KANDAHARAFGHANISTAN

quality.control

AASF # 2TB 1-1500-200-20-31 COMPLIED WITH AT2380.1 A/C HRS. (AE1051)

07-Jul-2005 1

B'HAM AL.

quality.control


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 12 of 20

AASF# 3 LSI RESET#1 ENGINE FORWARD MOUNT LUGS, DRAGLINK, AFT MOUNT LINK, AND RELATED PARTSINSPECTED AND NDI COMPLETE AT 2399.6ACFT HRS (DH5576)

16-Jan-2006 1

DAVENPORT, IA 52806

quality.control

AASF# 3 LSI RESET#2 ENGINE FORWARD MOUNT LUGS, DRAGLINK, AFT MOUNT LINK, AND RELATED PARTSINSPECTED AND NDI COMPLETE AT 2399.6ACFT HRS (DH5576)

16-Jan-2006 2

DAVENPORT, IA 52806

quality.control

AASF# 3 LSI RESETRESET INSPECTION COMPLETEDINACCORDANCE WITH TB 1-1520-240-30-02 0N16 JAN 06 AT 2399.6 ACFT HOURS. ACFTENTERED INTO THE MODULAR PMD AND 400FLIGHT CYCLE SERVICE PLAN IAW AMCOMAWR FOR IMPLEMENTATION OF ALTERNATEMAINTENANCE CHECK-LISTS FOR SELECTEDCH-47D ACFT DTD 27 AUG 04 (DH5576)

16-Jan-2006 3

DAVENPORT, IA 52806

quality.control

AASF#3 LSI RESETPHASE 1-4 COMPLETED @ 2399.6 ACFT HRS.NEXT PHASE DUE @ 2799.6 ACFT HRS(DH5576)

16-Jan-2006 4

DAVENPORT, IA 52860

quality.control

AASF # 2ERROR 17-Jan-2006 1

BRIMINGHAM, AL

quality.control

AASF # 2CH-47-06-SOF-01 COMPLIED AS PER PARA7.1.2 OF SOF (GUN MOUNTS NOT INSTALLEDON ACFT) (ES3687)

27-Jan-2006 1

BRIMINGHAM, AL

quality.control

AASF # 2CH-47-06-SOF-02 COMPLIED WITH SOF PERPARA. 7.3 @ 2414.1 ACFT HRS (APU) (ES3687)

08-Mar-2006 1

BIRMINGHAM, AL

quality.control

AASF # 2CH47-06-ASAM-02 COMPLIED WITH PER PARA7.1.2 & 7.2.1 @ 2423.7 ACFT HRS(ACFT DOESNOT HAVE M240 H GUN MOUNTS) (ES3687)

09-Mar-2006 1

BIRMINGHAM, AL

quality.control

AASSF #2CH47-06-SOF-03 COMPLIED WITH PER PARA7.1, 7.3, 7.4 @ 2423.4 ACFT HRS. (ES3687)

10-Mar-2006 1

BIRMINGHAM, AL

quality.control

AASF # 2CH-47-ASAM-03 (AFT LCT INSP LOWER RODFITTING) COMPLIED WITH AT 2436.1 ACFTHRS.

12-May-2006 1

BIRMINGHAM, AL

edward.d.simmons

AASF #2CH-47-06-SOF-04 SUSPECT AFT ROTORBLADES COMPLIED WITH @ 2449.9 AFT HRS.

31-May-2006 1

BIRMINGHAM AL

amon.l.emerson

DYNCORP PROJECTOLR

OCM/ACE PERFORMED AT 2470 AIRCRAFTHOURS BY TEAM MEMBER UU AMCOMPROJECT OLR

29-Jun-2006 1

FT. CAMPBELL, KY

george.d.brengelman

DYNCORP PROJECTOLR

OCM/ACE PERFORMED AT 2470 AIRCRAFTHOURS BY TEAM MEMBER UU AMCOMPROJECT OLR

30-Jun-2006 1

FT. CAMPBELL, KY

george.d.brengelman

AASF #2CH-47-06-SOF-05 (FWD ROTOR BLADES)COMPLIED WITH AT 2509.5 ACFT HOURS

23-Aug-2006 1

BIRMINGHAM , AL

amon.l.emerson

AASF # 2CH-47-07-SOF-01 (SWASHPLATE ROTATINGRING) COMPLIED WITH AT 2550.1 ACFT HRS.

24-Oct-2006 1

BIRMINGHAM, AL

amon.l.emerson

AASF #2CH-47-07-ASAM-01 (ARC 220/ KY-100 START-UP PROCEDURES) COMPLIED WITH AT 2598.7ACFT HRS.

17-Jan-2007 1

BIRMINGHAM,AL

amon.l.emerson


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 13 of 20

DYNCORP PROJECTOLR

AIRWORTHINESS RELEASE (AWR) FOR CH-47D HELICOPTERS WITH THE AN/AAR-57(V) 5COMMON MISSLE WARNINGSYSTEM/IMPROVED COUNTERMEASURESDISPENSER (CMWS/ICMD) INSTALLED(TTS#25459)

23-Jan-2007 1

BIRMINGHAM,AL

joseph.stevens

DYNCORP PROJECTOLR

AIRWORTHINESS RELEASE(AWR) FOR CH-47DHELICOPTERS WITH FLUX VALVERELOCATEDDATED 6 SEPT 2005.

23-Jan-2007 2

BIRMINGHAM, AL

joseph.stevens

DYNCORP PROJECTOLR

AIRWORTHINESS RELEASE(AWR) FOR CH-47DHELICOPTERS WITH THE ADVANCED HEADS-UP DISPLAY(HUD) SYSTEM SIGNAL DATACONVERTER (SDC) PART NUMBER 125110-007INSTALLED.DATED 20 MAY 04 REV.3

23-Jan-2007 3

BIRMINGHAM,AL

joseph.stevens

DYNCORP PROJECTOLR

AIRWORTHINESS RELEASE (AWR) FORINSTALLATION AND OPERATION OFEXTENDED LENGTH FLARE DISPENSERCABLE ON CH-47D HELICOPTERS.DATED: 26NOV 2003

23-Jan-2007 4

BIRMINGHAM, AL

joseph.stevens

AASF # 2CH-47-07-SOF-02 (SUSPECT ROTOR BLADES)COMPLIED WITH @2598.7 ACFT HRS

23-Jan-2007 5

BIRMINGHAM, AL

edward.d.simmons

DYNORP PROJECT OLRAWR TTS 39147. BLUE FORCE TRACKING(REVISION 3)

08-Feb-2007 1

BIRMINGHAM, AL

joseph.stevens

DYNCORP PROJECTOLR

AWR,(TTS# 39748) INSTALLATION OF THEELECTRICALLY POWERED HYDRAULICACCUMULATOR PUMP.

08-Feb-2007 2

BIRMINGHAM, AL

joseph.stevens

DYNCORP PROJECTOLR

MEC# F58218 INSTALLATION OF ACCESPANELS FOR ACCESS TO AFT PYLON MOUNTBOLTS. L/H AND R/H SIDE DUE TOINSTALLATION OF CMWS.

09-Feb-2007 1

BIRMINGHAM, AL

joseph.stevens

AASF #2CH-47-07-ASAM-02 ( AIRCRAFT RIGIDCONNECTING LINKS) COMPLIED [email protected] AIRCRAFT HOURS

06-Mar-2007 1

BIRMINGHAM, AL

amon.l.emerson

DYNCORP PROJECTOLR

MWO 1-1520-240-50-99, AWR -TTS 36919B.VERIFICATION OF INSTALLATION OF THELEFT HAND CRASHWORTHY CREW SEAT.AWR DATE 26 FEB 2007.

13-Mar-2007 1

BIRMINGHAM, AL

joseph.stevens

DYNCORP PROJECTOLR

MWO 1-1520-240-50-111, INSTALLATION OFTHE R/H AFT PYLON HYD ACCESS DOORCREW STEP DOUBLER. AWR -TTS36951ADATED 11 DEC 2006

13-Mar-2007 2

BIRMINGHAM, AL

joseph.stevens

DYNCORP PROJECTOLR

APX-118 MODE S TRANSPONDER OCTALCODE (53407511)

20-Mar-2007 1

BIRMINGHAM, AL

joseph.stevens

L3/VERTEXAEROSPACE CFS

200 HOUR CSP COMPLETED @ 2598.7 ACFTHRS. - 400 HOUR CSP DUE AT 2798.7 ACFTHRS.

26-Apr-2007 1

BIRMINGHAM ,AL 35217

george.d.brengelman

AASF #2AWR (TTS 41283) INSTALLATION OFMODERNIZED SIGNAL PROCESSING UNIT(MSPU) EQUIPMENT( DATED 06 APR 2007)

16-May-2007 1

BIRMINGHAM , AL

amon.l.emerson


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 14 of 20

DYNCORP PROJECTOLR

AIRWORTHINESS RELEASE (AWR) FOROPERATION OF SPECIFIED CH-47DHELICOPTERS WITH THE COMMON MISSILEWARNING SYSTEM (CMWS), IMPROVEDCOUNTERMEASURES DISENCER (ICMD), ANDTHE CMWS P3I UPGRADE TO THEMISCELLANEOUS CONTROL PANELINSTALLED. (TTS 48244)

18-Sep-2007 1

BIRMINGHAM AL

timothy.d.vieyra

DYNCORP PROJECTOLR

OCM/ACE COMPLETED AT 2670 ACFT HRS. BYTEAM MEMBER UU AMCOM PROJECT OLR

05-Dec-2007 1

FT CAMPBELL, KY42223

HM309565

DYNCORP PROJECTOLR

INSTALLATION OF CMWS 5TH EOMS IAWDRAFT MWO 1-1520-240-50-120 AND AWRTTS52976 DATED 28 JAN 08

01-Feb-2008 1

FT. CAMPBELL, KY42223

DL886920

AASF # 2H-47-08-AMAM-03 AN/ASN-128B/D DOPPLERGPS NAVIGATION SET (DGNS) COMPLIEDWITH @ 2753.2 ACFT HRS (ES563687)

29-Mar-2008 1

BIRMINGHAM, AL

edward.d.simmons

DYNCORPINTERNATIONAL

OCM/ACE PERFORMED AT 2799 ACFT HRS BYTEAM MEMBERS R & J AMCOM RASM-E

17-Oct-2008 1

FT. CAMPBELL, KY.42223

tim.b.stegman

L3/VERTEXAEROSPACE CFS

400 HOUR CSP INSPECTION COMPLETED AT2798.7 AIRCRAFT HOURS. NEXT 200 HOURCSP INSPECTION DUE AT 2998.7 AIRCRAFTHOURS

30-Oct-2008 1

BIRMINGHAM, AL

george.d.brengelman

AASF #1, PAACFT TRANSFERED TO CO. B/2-104 GSAB 05DEC 2008. PA-ARNG (FORT INDIANTOWN GAPPA)

05-Dec-2008 1

BLDG 19-101 ANNVILLE,PA 17003

RB509919

AASF-FTIGH-47-09-SOF-02 ALL H-47 SERIES ENGINEDRIVE SHAFT AND INBD AND OTBDADAPTERS FOR EXCEEDING RC

17-Dec-2008 1


GM360923

B CO 2/104THAIRCRAFT DEPLOYED TO CAMP BUEHRING INSUPPORT OF OIF

22-Apr-2009 1

CAMP BUEHRING, APOAE 09330

lisa.m.shafer

D CO. 2/104THAIRCRAFT MODED WITH BALLISTICPROTECTION SYSTEM AND IR ANTI-COLLISION LIGHT I/A/W/ AWR'S TTS 11693AND TN 10705 BY L3 CONTRACTORS @ 2850.0AIRCRAFT HRS.

24-Apr-2009 1

CAMP BUEHRING, APOAE 09330

MM589560

D 2-104TH GSAB2408-17 DATA CORRUPTED IN ULLS-A/E.REPAIRED DATA BASE. LAST INSPECTIONRE-ENTERED INTO DATA BASE.

04-Jul-2009 1

LSA ADDER, IRAQ APO09331

jorge.l.alvarez

D 2-104TH GSABH-47-09-AMAM-02 ALL H-47 SERIESAIRCRAFT, AFT SLIDER SHAFT ASSEMBLYRETIREMENT LIFE COMPLIED WITH

17-Jul-2009 1


kenneth.r.butler

D CO. 2-104 GSABH-47-AMAM-09 HAND HELD FIREEXTINGUISHER ONE TIME INSPECTION FORREPLACEMENT IS COMPLIED WITH

15-Sep-2009 1


MM589560


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 15 of 20

D CO. 2-104 GSABH-47-AMAM-09-03 HAND HELD FIREEXTINGUISHER ONE TIME INSPECTION FORREPLACEMENT IS COMPLIED WITH

15-Sep-2009 2


MM589560

D CO. 2/104TH GSAB200 HR. CSP INSPECTION COMPLETED AT2999.0 ACFT. HRS. NEXT 400 HR. CSP DUE AT3199.0 ACFT. HRS.

09-Oct-2009 1


MM589560

D CO. 2/104TH AVNH-47-10-ASAM-02 COMPLIED WITH. NODEFICIENCIES NOTED. AMTRACKS ALSOCOMPLIED WITH.

18-Dec-2009 1


MM589560

D CO. 2/104THACFT. BLADES REMOVED FOR SHIPMENT TOCONUS

04-Jan-2010 1


MM589560

AASF#1ACFT RETURNED TO AASF #1, PA AFTERBEING DEPLOYED IN IRAQ FOR ONE YEAR.

28-Feb-2010 1


RB509919

AASF #1, PACH47-10-AMAM-03, FWD ROTOR HUBRETIREMENT LIFE REDUCTION FOR SELECTP/N HUBS. COMPLIED WITH.

16-Mar-2010 1


RB509919

AASF #1, PACH47-10-AMAM-04, AFT SLIDER SHAFTRETIREMENT LIFE TRACKINGREQUIREMENTS. ( COMPLIED WITH)

05-Apr-2010 1


RB509919

AFMA RASM-E/CSCLINE REAMED BORE OF O/B LUG ON LEFTHAND AFT CONTROLS BELLCRANK SUPPORTATTACHMENT ASSY P/N: 114S4824-3 ANDFABRICATED OVERSIZED BUSHING ASAUTORIZED BY MEC # F111779 AT 3167.2ACFT HRS

13-Jul-2010 1

HAAF GA 31409

darrel.e.dust

AFMA RASM-E/CSCREPAIRED PILOTS SIDE PEDAL BOX ASSYYAW BELLCRANK LOWER MOUNT BUSHINGBORE P/N: 114C1103-1 BY OVERSIZING BOREAND MANUFACTURING OVERSIZED BUSHINGAS AUTHORIZED BY MEC # F111781 AT 3167.2ACFT HRS.

13-Jul-2010 2

HAAF GA 31409

darrel.e.dust

OLR/ RASM EASTACE EVALUATION PERFORMED BY TEAMMEMBERS AA AND WW AT 3167.2 AIRCRAFTHOURS AT HAAF SAVANNAH, GA.

15-Jul-2010 1

HAAF/SAVANNAH, GA

joseph.j.brichacek

AFMA RASM-E/CSCREPAIRED #1 ENGINE MOUNT LUG "A" P/N:114S3819-55 FOLLOWING PROCEDURESGIVEN IN MEC # F112695 AT 3167.2 ACFT HRS.

02-Aug-2010 1

HAAF GA 31409

darrel.e.dust

AFMA RASM-E/CSCREPAIRED #2 ENGINE MOUNT LUG "G" P/N:114S3819-55 FOLLOWING PROCEDURESGIVEN IN MEC # F112697A AT 3167.2 ACFTHRS.

02-Aug-2010 2

HAAF GA 31409

darrel.e.dust

AFMA RASM-E/CSCREPAIRED #1 ENGINE MOUNT LUG "G" P/N:114S3819-55 FOLLOWING PROCEDURESGIVEN IN MEC # F112697A AT 3167.2 ACFTHRS.

02-Aug-2010 3

HAAF GA 31409

darrel.e.dust

AFMA RASM-E/CSC#2 ENG MOUNTS NDI COMPLETED AT 3167.2ACFT HRS. NEXT INSP DUE AT 3767.2 ACFTHRS.

23-Sep-2010 1

HAAF GA

james.barnes


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 16 of 20

AFMA RASM-E/CSC#1 ENG MOUNTS NDI COMPLETED AT 3167.2ACFT HRS. NEXT INSP DUE AT 3767.2 ACFTHRS.

23-Sep-2010 2

HAAF GA 31409

james.barnes

AFMA RASM-E/CSCAIRCRAFT FUEL TANK INSPECTIONCOMPLETED AT 3167.2 ACFT HRS. NEXT TANKINSP DUE AT 4367.2 ACFT HRS.

23-Sep-2010 3

HAAF GA 31409

james.barnes

AFMA RASM-E/CSCMODULAR PMD AND 400 FLIGHT HOUR CYCLESERVICE INSPECTION COMPLETED AT 3167.2ACFT HRS. NEXT SCHEDULED INSPECTION ISA 50 HR INSP DUE AT 3217.2 ACFT HRS.

23-Sep-2010 4

HAAF GA 31409

james.barnes

AFMA RASM-E/CSCTB 11-1500-361-24 AIRCRAFT SURVIVABILITYEQUIPMENT (ASE) & COMMUNICATION ANDNAVIGATION CLEANING REQUIREMENTSCOMPLIED WITH AT 3167.2 ACFT HRS.

23-Sep-2010 5

HAAF GA 31409

james.barnes

AFMA RASM-E/CSCTB 1-1520-240-30-02 CH-47D AIRCRAFTDESERT OPERATIONS SPECIAL INSPECTIONAND CLEANING COMPLIED WITH AT 3167.2ACFT HRS.

23-Sep-2010 6

HAAF GA 31409

james.barnes

AFMA RASM-E/CSCTB 1-1500-200-20-31 AIRCRAFT DESERTOPERATIONS CLEANING REQUIREMENTSCOMPLIED WITH AT 3167.2 ACFT HRS.

23-Sep-2010 7

HAAF GA 31409

james.barnes

AFMA RASM-E/CSC#1 & #2 FLIGHT HYDRAULIC AND UTILITYHYDRAULIC SYSTEM PURIFICATIONCOMPLETED THIS DATE AT 3167.2 ACFT HRSUSING AGPU SN: 0013 (AG02) AND PALLPURIFIER SN: A103

23-Sep-2010 8

HAAF GA 31409

james.barnes

AFMA RASM-E/CSCOPERATE WITHIN LIMITS AND RESTRICTIONSSPECIFIED IN THE ENCLOSED AWR TTS 70944(P3 DRAIN)

23-Sep-2010 9

HAAF GA 31409

james.barnes

AFMA RASAM EASTAWR TTS#70944, INSTALLATION OF P3 CHECKVALVE DRAIN LINE, ENTERED AT 3167.2 ACFTHRS

23-Sep-2010 10

HAAF, GA. 31409

paul.guyette

AFMA RASM EASTAWR TTS#54785, INSTALLATION OF AVIATIONVIBRATION ANLYZER (AVA) SINGLE CAMERATRACKER BRACKET. ENTERED AT 3167.2ACFT HRS.

23-Sep-2010 11

HAAF, GA. 31409

paul.guyette

AFMA RASM-E/ CSC(LATE ENTRY) H-47-10-AMAM-02 ULLS-A(E)LCF CHANGE 60B COMPLIED WITH

27-Sep-2010 1

HAAF GA 31409

darrel.e.dust

AFMA RASM-E/ CSC(LATE ENTRY)GEN-09-AMAM-03 ULLS-A LCFCHANGE 60 COMPLIED WITH

27-Sep-2010 2

HAAF GA 31409

darrel.e.dust

AFMA RASM-E/CSCREPLACED PILOTS SIDE PEDAL BOX YAWPEDAL SUPPORTS P/N'S: 114C1110-4,114C1111-1, & 114C1110-2 DUE TO SEVERECORROSION AS AUTHORIZED BY MEC #F115644

28-Sep-2010 1

HAAF, GA 31409

darrel.e.dust

AFMA RASM-E/CSCCOMPLIED WITH H-47-10-ASAM-07 (5000POUND TIE DOWN ADAPTER RINGINSPECTION) THIS DATE AT 3173.6 ACFT HRS

12-Oct-2010 1

HAAF GA 31409

darrel.e.dust

AFMA RASM-E/CSCCOMPLIED WITH H-47-11-ASAM-01 (ALUMINUMWASHERS AN960-1016) THIS DATE AT 3173.6ACFT HRS

13-Oct-2010 1

HAAF GA 31409

darrel.e.dust


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 17 of 20

1/111TH FLARNG VQQACFT TRANSFERED TO FLARNG FROMPAARNG

10-Nov-2010 1

JACKSONVILLE, FL

robert.l.wilson

AASF#1 FLARNGH-47-AMAM-02) ALL MH-47G SERIES ACFT,AFT PITCH VARYING HOUSING RETIREMENTLIFE, FOR CHRONOGICAL ORDER ONLY

01-Dec-2010 1

JACKSONVILLE, FL

ivan.v.moon

AASF#1 FLARNGH-47-11-AMAM-01)ULLS-A( E ) INTERGRATEDMATERIAL MANAGEMENT CENTERLEGITIMATE CODE FILE CHANGE 61REQUIREMENTS COMPLIED WITH.

04-Jan-2011 1

JACKSONVILLE, FL

john.a.emery

AASF#1 FLARNGH-47-11-ASAM-03) ALL H-47 SERIESAIRCRAFT, CORRODED CONNECTING LINKSCOMPLIED WITH @ 3235.4 ACFT HRS.

07-Apr-2011 1

JACKSONVILLE, FL

john.a.emery

CSCACE COMPLETED AT 3237 A/C HOURS BYTEAM MEMBER AA & O. AFMA,RASM-E,AMCOM

13-Apr-2011 1

JACKSONVILLE, FL

DC0722

AASF #1 FLARNGH-47-11-ASAM-04 ALL 47 SERIES ACFT, BLADELAG DAMPER ROD END BEARING C/W @3237.5 AIRCRAFT HOURS

19-Apr-2011 1

JACKSONVILLE, FL

darryl.e.roberts

1108TH TASMGR/H AFT LANDING GEAR TRUNNION P/N114S3849-2 REPLACED AT 1108TH TASMG IAWMEC# 125499B AT 3240.7 ACFT HRS T.I.JS191142 DSN 293-1335

10-Jun-2011 1

GULFPORT, MS

joey.sharplin

AASF #1 FLARNGBLUE FORCE TRACKER REVISION VERSIONTRANSCEIVER 6.5 ROUTER 3.0 @ ACFT. HRS.3251.9

29-Jun-2011 1

JACKSONVILLE, FL.32221

darryl.e.roberts

1-111TH AVN GSABAIRCRAFT RELOCATED TO FT HOOD TX FORPREPARATION OF OPERATION NEW DAWN @3291.6 ACFT.HRS

01-Sep-2011 1

LONGHORN AAF NORTHFT HOOD TX.

darryl.e.roberts

CO D, 111TH AVN (QC)COMPLIED WITH H-47-11-AMAM-04. ASN-128BSUITE "D" SOFTWARE UPDATE NOTINSTALLED @ 3298.0

24-Sep-2011 1

LONGHORN AAF, N FTHOOD TX.

christopher.sanchez

AASF #1 OKARNGAIRCRAFT RECIEVED AT HOME STATION(HMY) FROM FT HOOD TX 26OCT11 AND 3303.8HOURS.

26-Oct-2011 1

LEXINGTON, OK 73051-9549

JH543815

AASF #1 OKARNGCOMPLIED WITH H-47-11-AMAM-03. ULLS-A (E)LCF CHANGE 62 REQUIREMENTS 26 OCT 2011@ 3303.8 ACFT HRS

26-Oct-2011 2


karem.a.alarafi

AASF #1 OKARNGCOMPLIED WITH H-47-12-SOF-01, 29 NOV 11 @3329.8 ACFT HRS. ON DIGITAL ELETRONICCONTROL UNITS.

01-Dec-2011 1


karem.a.alarafi

MO-TASMG400 HR CSP COMPLETED 28 FEB 2012 @3329.8 ACFT HRS. 200 HR CSP NEXT DUE @3529.8 ACFT HRS. AIRCRAFT RELEASED FORMTF.

28-Feb-2012 1


JH543815

AASF #1 OKARNGCOMPLIED WITH REQUIREMENTS OF H-47-11-AMAM-04 ON AN/ASN 128D DOPPLERSOFTWARE UPGRADE ON 7 MAR 2012 @3330.0 ACFT HRS.

08-Mar-2012 1


karem.a.alarafi


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 18 of 20

AASF #1 OKARNGCOMPLIED WITH H-47-12-AMAM-02TRANMISSION OIL SAMPLE INTERVALCHANGE @ 3367.3 ACFT HRS

02-Jun-2012 1


karem.a.alarafi

AASF #1 OKARNGCOMPLIED WITH REQUIREMENTS OF H-47-12-ASAM-01 ON THIS DATE @ 3466.5 ACFT HRS.ON YAW INTERGRATED LOWER CONTROLACTUATOR INPUT CONTROL HARDWARE /HYDRAULIC PRESSURE TUBE CLEARANCE.

14-Aug-2012 1


karem.a.alarafi

AASF #1 OKARNGCOMPLIED WITH H-47-12-AMAM-04 ON FULLATHORITY DIGITAL ENGINE CONTROLS(FADEC) 14 SEP 12 @ 3474.6 ACFT HRS

14-Sep-2012 1


karem.a.alarafi

FT HOOD AFMADYNCORP INTL

AIRWORTHINESS RELEASE (AWR) FORINSTALLATION OF MODIFICATION WORKORDER (MWO) 1-1520-240-50-119,MODIFICATION INSTRUCTIONS FOR THEINSTALLATION OF INFRARED SUPPRESSIONSYSTEM (IRSS) ON THE CH-47D AIRCRAFT,FLIGHT OPERATION WITH A-KIT ONLY AWRTTS 103236A DTD 25 APR 2012 REV 1.APPLIED AT 3474.6 ACFT HRS.

27-Sep-2012 1

KILLEEN TX 76543

bruce.m.sowa

B CO. 3-126 AVNCOMPLIED WITH INITIAL COMPLIANCE H-47-13-ASAM-01 BOTH LINKS FAIL PN145C3340-7

22-Oct-2012 1

KANDAHAR, AFG

m.aquilina

AECOMPMS2 INSPECTION COMPLETED AT 3529.7AIRCRAFT HOURS. NEXT PMS3 INSPECTIONDUE AT 3729.7 AIRCRAFT HOURS

25-Nov-2012 1

KANDAHAR, AFG

damian.m.goldsmith

D CO 3-25 AVN RGTCOMPLIED WITH H-47-13-AMAM-02; ULLS-A(E)LCF CHANGE 63 REQUIREMENTS

02-Dec-2012 1

KANDAHAR, AFG

david.c.fisher

D CO 2-3ASAM H-47-13-ASAM-02 " MID-CABIN HATCHCARGO HOOK" COMPLIED WITH. 13-1ENTRIES COMPLETED.

15-Dec-2012 1

KANDAHAR, AFG

billy.r.anderson

D C0 2-3MAINTANCE ENGINEERING ORDER NO #A6278 CH-47 WINDSHIELD/WINDSCREENDAMAGE IN SOUTHWEST ASIA . INSPECTWINDSHIELD BEFORE AND AFTER AVERYFLIGHT. POC NICK HURTA, LE TEAM DSN #861-2551

17-Dec-2012 1

KAF

billy.r.anderson

D CO 2-3COMPLY WITH ASAM H-47-13-ASAM-03 "INFRARED SUPPRESSOR SYSTEM" ACFTFINAL COMPLIANCE 16 JUN 13.

17-Dec-2012 2

KAF

billy.r.anderson

D C0 2-3H-47-13-ASAM-03 N/A IRSS NOT INSTALLED 08-Jan-2013 1

KAF

billy.r.anderson

D CO 2-3COMPLIED WITH AMAM " GEN-13-AMAM-02"CMWS/ATIRCM COMPONENT TRACKINGSYTEM

04-Feb-2013 1

KAF

billy.r.anderson

AECOMIN COMPLIANCE WITH H-47-13-ASAM-01,REPLACE RIGID CONNECTING LINK 2EA,PN/145C3340-7 IAW H-47-13-ASAM-01 NLT 30NOV 2013. THESE LINKS REQUIRESREPLACEMENT.

11-Mar-2013 1

KAF

roger.g.williams

AECOMPMS-3/ 400 HR PHASE COMPLETED AT3707.1ACFT HRS, NEXT PHASE DUE PMS-2/200HRS AT 3907.1 ACFT HRS.

18-Mar-2013 1

KAF

roger.g.williams


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 19 of 20

AECOMACFT. UTILITY HYD SYSTEM AND FLIGHT HYDSYSTEM BLEED AND PURIFICATIONCOMPLETED AT 3707.1 ACFT HRS.

18-Mar-2013 2

KAF

roger.g.williams

B CO 3-126 GSABACFT CONFIGURED FOR C-17 TRANSPORTFROM KAF AFG TO ROC NY @ 3746 ACFT HRS

11-Apr-2013 1

KAF

dennis.a.whewell

B CO 2/238TH GSABACFT DAMAGED BY SEVERE HAIL STORMCAUSING DAMAGE TO ALL 6 ROTOR BLADES,TUNNEL COVERS, COCKPIT GLASS, BUBBLEWINDOWS, AND ALONG CABIN CEILINGSHEET METAL. ROTOR BLADES, COCKPITGLASS, AND BUBBLE WINDOWS WEREREPLACED.

23-Apr-2013 1

KANDAHAR

B CO 238THRIGHT YAW/ROLL STOP STUD IN STALLEDFROM CRASHED ACFT AFTER NDI INSP BYDH942067

15-May-2013 1

KANDAHAR, AF

layton.c.elkin

B CO 2/238COMPLIED WITH THE REQUIREMENTS OF H-47-13-SOF-02

15-Jun-2013 1

KANDAHAR, AF

layton.c.elkin

B CO 2-238TH GSABCOMPLIED WITH THE REQUIREMENTS OF H-47-13-AMAM-04

24-Jul-2013 1

KANDAHAR, AF

john.f.burckhard

B CO 2-238TH GSABCOMPLIED WITH REQUIREMENTS OF H-47-13-ASAM-06 (INSTALLED FASTENERS LOCATEDON AFT PIVOTING SERVOCYLINDER RIGHTSUPPORT FITTING).

24-Aug-2013 1

KANDAHAR, AF

john.f.burckhard

AECOMMEC # F171775 DURING 200 HRS PHASE INSPSTATION 420 P/N # 414S24111 FLOOR BEAMSPT AFT CARGO HOOK AFT BEAM HAS 3INTERGRANULAR CORROSION MEASURING 6X 4.250 , 9 X 3.50 AND 6 X 3.750 2 FRONT SIDEVIOD HAD 7.00 SEPARATION. FRONT SIDEVIOD OF 6 X .250 SEPARATED BY 3 .250 INFROM AFT SIDE VOID 9 X3.5 VOID MEA 6 X.750 OVER LAPS THE AFT SIDE VOID ALLDAMAGE IS RT CENTER LINE OF REPAIRAREARECOVER MIN OF A 20 X5 INCH OFAREA LARGE REPAIR AUTH GRANTED FORTASMG (KAF) REPAIR STA 420 FLOORFORMER P/N 414S2414-11 FOR CH-47D ACFT92-00307 IAW DMWER 1-1520-240 WP 0083 00COMPLETED @ 3907.1 ACFT HRS .

21-Sep-2013 1

KAF

james.cloud

AECOMACFT FLIGHT HYD & UTILITY HYD SYSTEMSBLEED AND PURIFICATION COMPLETED AT3907.1: AGPU S/N B292, PALL S/N A254

28-Sep-2013 1

KAF

paul.j.vincek

AECOMNEUTRAL RIG CHECK COMPLETED 29 SEPT2013 @3907.1 ACFT HRS STICK POSTION FWDAND AFT (13 5/16) LAT( 14 7/8 )

29-Sep-2013 1

KAF

james.cloud

AECOMPMS2/200 COMPLETED @ 3970.1 ACFT HRSNEXT PHASE DUE PMS 3 /400 HRS @ 4107.1ACFT HRS

09-Oct-2013 1

KAF

james.cloud

AASF#3ACFT TRANSFERRED TO AASF#3, PEORIA, IL,15-NOV-2013; REMAINS UNDER UIC: WNH8G2

15-Nov-2013 1

PEORIA, IL. 61607-1497

B CO. 2-238TH GSABAIRCRAFT CONFIGURED FOR C5/C17LOADOUT FOR SHIPPING TO CONUS.

18-Nov-2013 1

KAF, AFGHANISTAN

john.f.burckhard


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 20 of 20

AASF#3ACFT RECONFIGURED FOR FLIGHTFOLLOWING C17 TEARDOWN, MOC'SBEGINNING 18 MAR 14

18-Mar-2014 1

PEORIA, IL. 61607-1497

AASF #3COMPLIED WITH THE REQUIREMENTS OF H-47-14-AMAM-02. (ULLS-A (E) CHANGE 65)

08-May-2014 1

PEORIA, IL. 61607-1497

AASF #3COMPLIED WITH THE REQUIREMENTS OF H-47-14-AMAM-03 (ULLS-A (E) AMCOM CHANGE 66).

18-Sep-2014 1

PEORIA, IL. 61607-1497

AASF #3PMS-3 COMPLETED AT 4107.1 ACFT HRS ON25-SEP-2014. NEXT PHASE DUE: PMS-2 AT4301.7 ACFT HRS.

25-Sep-2014 1

PEORIA, IL. 61607-1497

AASF #3#1 & #2 ECU -21 SOFTWARE UPGRADECOMPLETE I/A/W MWO 1-2995-200-20-1 ANDAWR: TN 64589K DTD 18MAR14.

23-Oct-2014 1

PEORIA, IL. 61607-1497

AASF #3CBOX MSPU ACCELEROMETER INSERTSREPLACED BY MO TASMG.

28-Jan-2015 1

PEORIA, IL. 61607-1497

AASF #3COMPLIED WITH THE REQUIREMENTS OF H-47-15-AMAM-01 (ENGINE CHIP DETECTORS).

03-Feb-2015 1

PEORIA, IL. 61607-1497

AASF #3COMPLIED WITH REQUIREMENTS OF H-47-15-AMAM-02 (ASE)

10-Feb-2015 1

PEORIA, IL. 61607-1497

robert.d.childers

AASF #3COMPLIED WITH REQUIREMENTS OF H-47-15-SOF-01 (TUNNEL COVER H/W)

01-Apr-2015 1

PEORIA, IL. 61607-1497

robert.d.childers

AASF #3COMPLIED WITH REQUIREMENTS OF H-47-15-SOF-02 (XMSNS S/N)

12-Jun-2015 1

PEORIA, IL. 61607-1497

robert.d.childers

AASF #3AWR HISTORICAL RECORDS REVIEWCOMPLETE; ALL APPLICABLE QUALITATIVEEMC CHECKS HAVE BEEN COMPLETED WITHNO FAULTS OR INTERFERENCE NOTED FORALL PAST AND PRESENT CH-47D AWR'S ASOF 30-JUN-2015 PER AASF #3 QC.

30-Jun-2015 1

PEORIA, IL. 61607-1497

robert.d.childers

AASF#3COMPLIED WITH REQUIREMENTS OF H-47-15-SOF-03 ( 5 AND 10K TIE DOWN RINGS).

02-Sep-2015 1

PEORIA, IL. 61607-1497

robert.d.childers

AASF#3COMPLIED WITH REQUIREMENTS OF H-47-16-ASAM-01 (ECU)

29-Oct-2015 1

PEORIA, IL. 61607-1497

robert.d.childers

AASF #3PMS-2 COMPLETED AT 4307.1 ACFT HRS ON22-JULY-2016. NEXT PHASE DUE: PMS-3 AT4507.1 ACFT HRS

22-Jul-2016 1

PEORIA, IL. 61607-1497

robert.d.childers

AASF #3COMPLIED WITH REQUIREMENTS OF H-47-16-AMAM-02 (ULLS-A(E) PHASE LCF UPDATES)

24-Aug-2016 1

PEORIA, IL. 61607-1497

william.r.fargher

AASF #3COMPLIED WITH REQUIREMENTS OF H-47-16-AMAM-01 (ULLS-A(E) COMPONENTSDUPLICATION)

26-Aug-2016 1

PEORIA, IL. 61607-1497

william.r.fargher

AASF #3COMPLIED WITH REQUIREMENTS OF H-47-17-AMAM-01 (LEGITIMATE CODE FILE (LCF)CHANGE 68)

14-Dec-2016 1

PEORIA, IL. 61607-1497

robert.d.childers


DATE AC HRS SHAFT VERTICAL REASON FOR VIBRATION CHECKLONGITUDINALLATERALIPS READINGS4.

9200307HELICOPTER, CARGOCH-47D

3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Page 1 of 12

a b c d e f g

PHASE #220-Sep-1996 ENG CROSS 0.130.300.05550.0

PHASE #220-Sep-1996 SYNCHRONIZ

0.050.160.12550.0

PHASE #220-Sep-1996 C-XMSN FAN 0.190.080.10550.0

PHASE #220-Sep-1996 AFT XMSN F 0.310.000.34550.0

50HR INSP.16-Mar-1997 ENG CROSS 0.000.160.08599.1

50HR INSP.16-Mar-1997 SYNCHRONIZ

0.000.180.27599.1

50HR INSP.16-Mar-1997 C-XMSN FAN 0.000.150.14599.1

50HR INSP.16-Mar-1997 AFT XMSN F 0.280.000.39599.1

100 HR INSP / MWO08-Jul-1997 ENG CROSS 0.000.180.04648.4

100 HR INSP / MWO08-Jul-1997 SYNCHRONIZ

0.000.030.17648.4

100 HR INSP / MWO08-Jul-1997 C-XMSN FAN 0.000.110.13648.4

100 HR INSP / MWO08-Jul-1997 AFT XMSN F 0.260.000.31648.4

PHASE #4 G MOORE 092330-Jul-1999 ENG CROSS 0.000.310.14950.0

PHASE #4 G MOORE 092330-Jul-1999 SYNCHRONIZ

0.000.080.30950.0

PHASE #4 G MOORE 092330-Jul-1999 C-XMSN FAN 0.000.130.13950.0

PHASE #4 G MOORE 092330-Jul-1999 AFT XMSN F 0.300.000.29950.0

50 HR GMO92325-Feb-2000 ENG CROSS 0.000.380.06998.5

50 HR GMO92325-Feb-2000 SYNCHRONIZ

0.000.220.35998.5

50 HR GMO92325-Feb-2000 C-XMSN FAN 0.000.080.13998.5

50 HR GMO92325-Feb-2000 AFT XMSN F 0.390.000.48998.5

100 HR GM092330-Jun-2000 ENG CROSS 0.000.210.061,049.5

100 HR GM092330-Jun-2000 SYNCHRONIZ

0.000.020.211,049.5

100 HR GM092330-Jun-2000 C-XMSN FAN 0.000.090.091,049.5

100 HR GM092330-Jun-2000 AFT XMSN F 0.430.000.471,049.5

PHASE #1 CT AVCRAD GM092307-Feb-2001 ENG CROSS 0.000.150.081,100.0

PHASE #1 CT AVCRAD GM092307-Feb-2001 SYNCHRONIZ

0.000.180.341,100.0


DA FORM 2408-15-2, OCT 1991 AIRCRAFT VIBRATION RECORD




Page 2 of 12

a b c d e f g

PHASE #1 CT AVCRAD GM092307-Feb-2001 C-XMSN FAN 0.000.080.091,100.0

PHASE #1 CT AVCRAD GM092307-Feb-2001 AFT XMSN F 0.020.000.061,100.0

50 HR INSP GM092320-Jun-2001 ENG CROSS 0.000.130.101,149.3

50 HR INSP GM092320-Jun-2001 SYNCHRONIZ

0.000.040.231,149.3

50 HR INSP GM092320-Jun-2001 C-XMSN FAN 0.000.300.301,149.3

50 HR INSP GM092320-Jun-2001 AFT XMSN F 0.030.000.071,149.3

100 HR GM092317-Aug-2001 ENG CROSS 0.000.080.121,201.1

100 HR GM092317-Aug-2001 SYNCHRONIZ

0.050.080.171,201.1

100 HR GM092317-Aug-2001 C-XMSN FAN 0.000.080.071,201.1

100 HR GM092317-Aug-2001 AFT XMSN F 0.020.000.031,201.1

50 HR INSP GM092308-Jan-2002 ENG CROSS 0.000.280.131,250.2

50 HR INSP GM092308-Jan-2002 SYNCHRONIZ

0.000.120.341,250.2

50 HR INSP GM092308-Jan-2002 C-XMSN FAN 0.000.110.061,250.2

50 HR INSP GM092308-Jan-2002 AFT XMSN F 0.030.000.081,250.2

PHASE #2 GM092307-Jun-2002 ENG CROSS 0.000.070.051,300.0

PHASE #2 GM092307-Jun-2002 SYNCHRONIZ

0.000.090.141,300.0

PHASE #2 GM092307-Jun-2002 C-XMSN FAN 0.000.150.111,300.0

PHASE #2 GM092307-Jun-2002 AFT XMSN F 0.050.000.051,300.0

50 HR GM092307-Sep-2002 ENG CROSS 0.000.070.131,351.3

50 HR GM092307-Sep-2002 SYNCHRONIZ

0.000.130.201,351.3

50 HR GM092307-Sep-2002 C-XMSN FAN 0.000.130.111,351.3

50 HR GM092307-Sep-2002 AFT XMSN F 0.050.000.041,351.3

100 HR GW585911-Jan-2003 ENG CROSS 0.000.060.091,398.0

100 HR GW585911-Jan-2003 SYNCHRONIZ

0.000.090.181,398.0

100 HR GW585911-Jan-2003 C-XMSN FAN 0.000.070.081,398.0

100 HR GW585911-Jan-2003 AFT XMSN F 0.060.000.041,398.0






Page 3 of 12

a b c d e f g

50 HR RN142327-Jun-2003 ENG CROSS 0.000.150.251,449.4

50 HR RN142327-Jun-2003 SYNCHRONIZ

0.000.250.431,449.4

50 HR RN142327-Jun-2003 C-XMSN FAN 0.000.140.071,449.4

50 HR RN142327-Jun-2003 AFT XMSN F 0.000.000.031,449.4

PHASE #3 RN142303-Aug-2003 ENG CROSS 0.000.200.121,489.0

PHASE #3 RN142303-Aug-2003 SYNCHRONIZ

0.000.200.381,489.0

PHASE #3 RN142303-Aug-2003 C-XMSN FAN 0.000.060.111,489.0

PHASE #3 RN142303-Aug-2003 AFT XMSN F 0.000.000.101,489.0

50 HR GM092301-Oct-2003 ENG CROSS 0.000.300.051,536.9

50 HR GM092301-Oct-2003 SYNCHRONIZ

0.000.120.321,536.9

50 HR GM092301-Oct-2003 C-XMSN FAN 0.000.030.071,536.9

50 HR GM092301-Oct-2003 AFT XMSN F 0.040.000.141,536.9

100 HR GM092329-Oct-2003 ENG CROSS 0.000.250.131,585.5

100 HR GM092329-Oct-2003 SYNCHRONIZ

0.000.120.321,585.5

100 HR GM092329-Oct-2003 C-XMSN FAN 0.000.030.071,585.5

100 HR GM092329-Oct-2003 AFT XMSN F 0.040.000.141,585.5

50 HR GM092329-Nov-2003 ENG CROSS 0.000.250.161,636.5

50 HR GM092329-Nov-2003 SYNCHRONIZ

0.000.120.281,636.5

50 HR GM092329-Nov-2003 C-XMSN FAN 0.000.120.091,636.5

50 HR GM092329-Nov-2003 AFT XMSN F 0.060.000.141,636.5

PHASE #4 EM667810-Jan-2004 ENG CROSS 0.000.340.151,675.0

PHASE #4 EM667810-Jan-2004 SYNCHRONIZ

0.000.180.311,675.0

PHASE #4 EM667810-Jan-2004 AFT XMSN F 0.130.000.171,675.0

PHASE #4 EM667810-Jan-2004 C-XMSN FAN 0.000.120.101,675.0

100. HOUR13-Apr-2004 ENG CROSS 0.000.070.291,772.5

100. HOUR13-Apr-2004 SYNC SHAFT 0.000.120.151,772.5






Page 4 of 12

a b c d e f g

100. HOUR13-Apr-2004 AFT XMSN F 0.130.000.181,772.5

100. HOUR13-Apr-2004 C-XMSN FAN 0.000.100.091,772.5

#1 ENG XMSN CROSS SHAFT04-May-2004 AFT XMSN F 0.000.000.001,806.7

#1 ENG XMSN CROSS SHAFT04-May-2004 SYNC SHAFT 0.000.110.121,806.7

#1 ENG XMSN CROSS SHAFT04-May-2004 C-XMSN FAN 0.000.120.141,806.7

#1 ENG XMSN CROSS SHAFT04-May-2004 CROSSSHAF

0.000.110.051,806.7

50 HR11-May-2004 AFT XMSN F 0.170.000.171,826.3

50 HR11-May-2004 SYNC SHAFT 0.000.230.301,826.3

50 HR11-May-2004 C-XMSN FAN 0.000.120.151,826.3

50 HR11-May-2004 CROSSSHAF

0.000.340.141,826.3

PHASE COMPLETED18-Jun-2004 CROSSSHAF

0.000.460.291,868.6

PHASE COMPLETED18-Jun-2004 SYNC SHAFT 0.000.310.671,868.6

PHASE COMPLETED18-Jun-2004 CXMSN BOX 0.000.090.041,868.6

PHASE COMPLETED18-Jun-2004 AFT XMSN 0.050.000.041,868.6

ROUTINE19-Jul-2004 ENGINE CRO 0.000.410.331,914.3

ROUTINE19-Jul-2004 SYNC SHAFT 0.000.260.681,914.3

ROUTINE19-Jul-2004 CBOX FAN 0.000.070.051,914.3

ROUTINE19-Jul-2004 AFT XMSN 0.030.000.041,914.3

100 HOUR12-Aug-2004 ENGINE CRO 0.000.170.111,967.3

100 HOUR12-Aug-2004 SYNC SHAFT 0.000.420.581,967.3

100 HOUR12-Aug-2004 CBOX FAN 0.000.080.101,967.3

100 HOUR12-Aug-2004 AFT XMSN 0.070.000.041,967.3

#2 ENG INSTALL04-Sep-2004 ENG CROSS 0.000.130.212,008.4

#2 ENG INSTALL04-Sep-2004 SYNC SHAFT 0.000.170.512,008.4

#2 ENG INSTALL04-Sep-2004 CBOX FAN 0.000.070.092,008.4

#2 ENG INSTALL04-Sep-2004 AFT XMSN F 0.050.000.022,008.4






Page 5 of 12

a b c d e f g

C-BOX REPLACEMENT07-Sep-2004 ENG CROSS 0.000.410.552,013.8

C-BOX REPLACEMENT07-Sep-2004 SYNC SHAFT 0.000.530.122,013.8

C-BOX REPLACEMENT07-Sep-2004 C BOX FAN 0.000.180.192,013.8

C-BOX REPLACEMENT07-Sep-2004 AFT XMSN F 0.000.000.002,013.8

50 HOUR10-Sep-2004 ENG CROSS 0.000.520.432,020.4

50 HOUR10-Sep-2004 SYNC SHAFT 0.000.460.572,020.4

50 HOUR10-Sep-2004 C BOX FAN 0.000.180.172,020.4

50 HOUR10-Sep-2004 AFT XMSN F 0.050.000.022,020.4

POST PHASE01-Oct-2004 ENG CROSS 0.000.170.142,038.9

POST PHASE01-Oct-2004 SYNC SHAFT 0.000.090.142,038.9

POST PHASE01-Oct-2004 C BOX FAN 0.000.140.132,038.9

POST PHASE01-Oct-2004 AFT XMSN F 0.160.000.212,038.9

50 HOUR05-Nov-2004 ENG CROSS 0.000.120.422,087.2

50 HOUR05-Nov-2004 SYNC SHAFT 0.000.290.512,087.2

50 HOUR05-Nov-2004 C BOX FAN 0.000.150.172,087.2

50 HOUR05-Nov-2004 AFT XMSN F 0.060.000.202,087.2

100 HOUR08-Dec-2004 ENG CROSS 0.000.320.482,136.5

100 HOUR08-Dec-2004 SYNC SHAFT 0.000.050.412,136.5

100 HOUR08-Dec-2004 C BOX FAN 0.000.130.062,136.5

100 HOUR08-Dec-2004 AFT XMSN 0.060.000.212,136.5

50 HOUR03-Jan-2005 ENG CROSS 0.000.230.512,187.5

50 HOUR03-Jan-2005 SYNC SHAFT 0.000.100.292,187.5

50 HOUR03-Jan-2005 C BOX FAN 0.000.080.032,187.5

50 HOUR03-Jan-2005 AFT XMSN F 0.160.000.182,187.5

PHASE/COMBAT28-Jan-2005 ENG CROSS 0.000.170.222,237.5

PHASE/COMBAT28-Jan-2005 SYNC SHAFT 0.000.060.172,237.5






Page 6 of 12

a b c d e f g

PHASE/COMBAT28-Jan-2005 C BOX FAN 0.000.020.042,237.5

PHASE/COMBAT28-Jan-2005 AFT XMSN F 0.100.000.212,237.5

100 HOUR08-Mar-2005 ENG CROSS 0.000.260.092,336.6

100 HOUR08-Mar-2005 SYNC SHAFT 0.000.300.252,336.6

100 HOUR08-Mar-2005 C BOX 0.000.010.032,336.6

100 HOUR08-Mar-2005 AFT XMSN 0.190.000.292,336.6

REASSEMBLY FOR TRANSPORT01-Apr-2005 ENG CROSS 0.000.050.252,327.9

REASSEMBLY FOR TRANSPORT01-Apr-2005 SYNC SHAFT 0.000.100.402,327.9

REASSEMBLY FOR TRANSPORT01-Apr-2005 C BOX FAN 0.000.060.052,327.9

REASSEMBLY FOR TRANSPORT01-Apr-2005 AFT XMSN 0.270.000.152,327.9

50 HOUR02-Aug-2005 ENG CROSS 0.000.100.272,389.1


50 HOUR02-Aug-2005 C BOX FAN 0.000.060.042,389.1

50 HOUR02-Aug-2005 AFT XMSN 0.240.000.162,389.1

RESET COMPLETION OF PHASE30-Jan-2006 ENG CROSS 0.000.580.312,399.6

RESET COMPLETION OF PHASE30-Jan-2006 SYNC SHAFT 0.000.370.582,399.6

RESET COMPLETION OF PHASE30-Jan-2006 C BOX FAN 0.000.030.052,399.6

RESET COMPLETION OF PHASE30-Jan-2006 AFT XMSN 0.190.000.152,399.6

50 HOUR23-May-2006 ENG CROSS 0.000.600.352,449.9

50 HOUR23-May-2006 SYNC SHAFT 0.000.020.502,449.9

50 HOUR23-May-2006 C BOX FAN 0.000.020.062,449.9

50 HOUR23-May-2006 AFT XMSN 0.250.000.232,449.9

REPLACEMENT OF XMSN14-Jul-2006 AFT XMSN 0.120.000.102,475.8

100 HOUR08-Aug-2006 CROSSSHAF

0.000.600.332,500.1


100 HOUR08-Aug-2006 CBOX FAN 0.000.070.082,500.1






Page 7 of 12

a b c d e f g

100 HOUR08-Aug-2006 AFT XMSN 0.100.000.112,500.1

50 HOUR19-Oct-2006 CROSS 0.000.700.272,548.1

50 HOUR19-Oct-2006 SYNC SHAFT 0.000.220.382,548.1

50 HOUR19-Oct-2006 C BOX FAN 0.000.090.082,548.1

50 HOUR19-Oct-2006 AFT XMSN 0.090.000.092,548.1

200 HOUR-(VMEP)21-Jun-2007 AFT FAN 0.180.000.242,598.7

200 HOUR-(VMEP)21-Jun-2007 C BOX FAN 0.000.150.092,598.7

200 HOUR- (VMEP)21-Jun-2007 CROSSSHAF

0.000.140.082,598.7

200 HOUR- (VMEP)21-Jun-2007 SYNC SHAFT 0.000.170.402,598.7

50 HOUR-(VMEP)19-Oct-2007 SYNC SHAFT 0.000.190.342,649.1

50 HOUR-(VMEP)19-Oct-2007 CROSSSHAF

0.000.220.042,649.1

50 HOUR-(VMEP)19-Oct-2007 AFT FAN 0.180.000.232,649.1

50 HOUR-(VMEP)19-Oct-2007 C BOX FAN 0.000.120.092,649.1

100 HOUR17-Jan-2008 AFT FAN 0.190.000.242,699.9

100 HOUR17-Jan-2008 C BOX FAN 0.000.120.102,699.9

100 HOUR17-Jan-2008 CROSSSHAF

0.000.230.052,699.9

100 HOUR17-Jan-2008 SYNC 0.000.200.352,699.9

50 HR-(VEMP)21-Mar-2008 CROSSSHAF

0.000.380.352,750.8

50HR-(VEMP)21-Mar-2008 SYNC SHAF 0.000.150.192,750.8

50HR-(VEMP)21-Mar-2008 CBOX FAN 0.000.080.032,750.8

50HR-(VEMP)21-Mar-2008 AFT XMSN 0.180.000.252,750.8

200 HR-(VMEP)05-Nov-2008 AFT XMSN 0.230.000.292,802.2

200 HR-(VMEP)05-Nov-2008 CBOX FAN 0.000.070.042,802.2

200 HR-(VMEP)05-Nov-2008 CROSSSHAF

0.000.670.482,802.2

200 HR-(VMEP)05-Nov-2008 SYNC SHAF 0.000.260.462,802.2

50 HR.05-Mar-2009 AFT XMSN 0.230.000.272,845.0






Page 8 of 12

a b c d e f g

50 HR.05-Mar-2009 CBOX FAN 0.000.070.022,845.0

50 HR.05-Mar-2009 CROSSSHAF

0.000.600.392,845.0

50 HR.05-Mar-2009 SYNC SHAF 0.000.090.112,845.0

100 HR.17-Jul-2009 AFT XMSN 0.250.000.102,900.0

100 HR.17-Jul-2009 CBOX FAN 0.000.090.042,900.0

100 HR.17-Jul-2009 CROSSSHAF

0.000.840.492,900.0

100 HR.17-Jul-2009 SYNC SHAF 0.000.250.442,900.0

50 HR.18-Aug-2009 AFT XMSN 0.220.000.272,948.0

50 HR.18-Aug-2009 CBOX FAN 0.000.070.052,948.0

50 HR.18-Aug-2009 CROSSSHAF

0.000.480.522,948.0

50 HR.18-Aug-2009 SYNC SHAF 0.000.320.382,948.0

200 HR.18-Oct-2009 AFT XMSN 0.230.000.292,999.0

200 HR.18-Oct-2009 CBOX FAN 0.000.080.072,999.0

200 HR.18-Oct-2009 CROSSSHAF

0.000.190.192,999.0

200 HR.18-Oct-2009 SYNC SHAF 0.000.360.682,999.0

50 HR.24-Nov-2009 AFT XMSN 0.230.000.293,047.0

50 HR.24-Nov-2009 CBOX FAN 0.000.010.073,047.0

50 HR.24-Nov-2009 CROSSSHAF

0.000.110.213,047.0

50 HR.24-Nov-2009 SYNC SHAF 0.000.520.803,047.0

POST RESET04-Oct-2010 AFT XMSN 0.210.000.403,167.2

POST RESET04-Oct-2010 CBOX FAN 0.000.080.133,167.2

POST RESET04-Oct-2010 CROSS SHFT 0.000.330.143,167.2

POST RESET04-Oct-2010 SYNC SHAFT 0.000.040.523,167.2

50 HR27-Jan-2011 AFT XSMN 0.170.000.223,212.2

50 HR27-Jan-2011 SYNC SHAFT 0.000.220.913,212.2

50 HR27-Jan-2011 CBOX FAN 0.000.080.133,212.2






Page 9 of 12

a b c d e f g

50 HR27-Jan-2011 CROSS SHFT 0.000.090.313,212.2

50 HR18-Jul-2011 AFT XSMN 0.170.000.223,264.8

50 HR18-Jul-2011 SYNC SHAFT 0.000.070.423,264.8

50 HR18-Jul-2011 CBOX FAN 0.000.080.103,264.8

50 HR18-Jul-2011 CROSS SHFT 0.000.140.053,264.8

PRE PHASE21-Oct-2011 CROSS SHFT 0.000.050.033,329.8

PRE PHASE21-Nov-2011 AFT FAN 0.160.000.223,329.8

PRE PHASE21-Nov-2011 C-BOX 0.000.090.093,329.8

PRE PHASE21-Nov-2011 SYNC SHAFT 0.000.080.293,329.8

PRE PHASE21-Nov-2011 CROSS SHFT 0.000.050.033,329.8

PRE PHASE21-Nov-2011 CROSS SHFT 0.000.050.033,329.8

POST PHASE28-Feb-2012 AFT FAN 0.150.000.203,329.8

POST PHASE28-Feb-2012 C-BOX 0.000.070.033,329.8

POST PHASE28-Feb-2012 CROSS SHFT 0.000.290.163,329.8

POST PHASE28-Feb-2012 SYNC SHFT 0.000.210.263,329.8

POST BUILD UP27-Oct-2012 AFT FAN 0.160.000.203,484.7

POST BUILD UP27-Oct-2012 C-BOX 0.000.020.023,484.7

POST BUILD UP27-Oct-2012 CROSS 0.000.430.353,484.7

POST BUILD UP27-Oct-2012 SYNC 0.000.230.133,484.7

POST PHASE29-Nov-2012 AFT FAN 0.150.000.193,535.3

POST PHASE29-Nov-2012 SYNCH 0.000.290.653,535.3

POST PHASE29-Nov-2012 C-BOX 0.000.040.063,535.3

POST PHASE29-Nov-2012 CROSS 0.000.480.433,535.3

#1 ENG REPLACEMENT05-Dec-2012 AFT FAN 0.160.000.193,538.7

#1 ENG REPLACEMENT05-Dec-2012 SYNC SHAFT 0.000.310.633,538.7

#1 ENG REPLACEMENT05-Dec-2012 C-BOX 0.000.050.043,538.7






Page 10 of 12

a b c d e f g

#1 ENG REPLACEMENT05-Dec-2012 CROSS 0.000.410.313,538.7

50 HR27-Feb-2013 AFT FAN 0.160.000.173,677.6

50 HR27-Feb-2013 SYNC 0.000.230.523,677.6

50 HR27-Feb-2013 C-BOX 0.000.050.023,677.6

50HR27-Feb-2013 CROSS 0.000.750.493,677.6

50 HR07-Jun-2013 AFT FAN 0.140.000.153,756.4

50 HR07-Jun-2013 SYNC 0.000.230.463,756.4

50 HR07-Jun-2013 C-BOX 0.000.060.043,756.4

50 HR07-Jun-2013 CROSS 0.000.300.073,756.4

50 HR13-Aug-2013 AFT FAN 0.130.000.143,854.6

50 HR13-Aug-2013 SYNC SHAFT 0.000.260.223,854.6

50 HR13-Aug-2013 CBOX 0.000.140.053,854.6

50 HR13-Aug-2013 CROSS 0.000.140.023,854.6

POST PHASE06-Oct-2013 AFT FAN 0.160.000.193,907.1

POST PHASE06-Oct-2013 C-BOX 0.000.120.093,907.1

POST PHASE06-Oct-2013 CROSS 0.000.660.343,907.1

POST PHASE06-Oct-2013 SYNC SHAFT 0.000.140.223,907.1

50 HR22-Oct-2013 AFT FAN 0.160.000.193,953.0

50 HR22-Oct-2013 CBOX 0.000.120.103,953.0

50 HR22-Oct-2013 CROSS 0.000.520.323,953.0

50 HR22-Oct-2013 SYNC SHAFT 0.000.120.263,953.0

C-17 BUILD UP27-Mar-2014 AFT FAN 0.170.000.224,003.5

C-17 BUILD UP27-Mar-2014 CBOX 0.000.070.094,003.5

C-17 BUILD UP27-Mar-2014 CROSS 0.000.320.134,003.5

C-17 BUILD UP27-Mar-2014 SYNC SHAFT 0.000.170.144,003.5

50 HOUR09-Apr-2014 AFT FAN 0.170.000.224,007.4






Page 11 of 12

a b c d e f g

50 HOUR09-Apr-2014 C-BOX 0.000.060.094,007.4

50 HOUR09-Apr-2014 CROSS 0.000.220.084,007.4

09-Apr-2014 SYNC SHAFT 0.000.170.224,007.4

50 HOUR22-Jul-2014 AFT FAN 0.220.000.274,057.0

50 HR22-Jul-2014 CBOX 0.000.030.094,057.0

50HR22-Jul-2014 CROSS 0.000.270.164,057.0

50HR22-Jul-2014 SYNC SHAFT 0.000.280.284,057.0

50 HOUR26-Sep-2014 CBOX 0.000.130.114,107.1

50 HOUR26-Sep-2014 CROSS 0.000.450.344,107.1

50 HOUR26-Sep-2014 SYNC SHAFT 0.000.340.534,107.1

50 HOUR26-Sep-2014 AFT FAN 0.180.000.204,107.1

50 HR17-Jun-2015 AFT FAN 0.160.000.194,155.7

50 HR17-Jun-2015 CBOX 0.000.140.094,155.7

50 HR17-Jun-2015 CROSS 0.000.330.224,155.7

50 HR17-Jun-2015 SYNC 0.000.350.544,155.7

50 HR01-Dec-2015 AFT FAN 0.170.000.194,206.5

50 HR01-Dec-2015 CBOX 0.000.140.134,206.5

50 HR01-Dec-2015 CROSS 0.000.170.194,206.5

50 HR01-Dec-2015 SYNC 0.000.320.424,206.5

50 HR06-May-2016 AFT FAN 0.170.000.174,269.7

50 HR06-May-2016 CBOX 0.000.120.074,269.7

50 HR06-May-2016 CROSS 0.000.290.174,269.7

50 HR06-May-2016 SYNC 0.000.320.524,269.7

5. REMARKS






Page 12 of 12

a b c d e f g



(ACFT HRS)

ji kgfdcba

RMVL HRSRMVL HRSCOMPO/HNOMENWUC O/HLOCATIONNSN

AND he SINCELIFE

PREVSER NO.ANDNOMENCLATURE P/N TIMEINST HRS MENT DUEREPLACINST HRSNO.COMPONENT

NOMEN REPLACE -O/H ORCOMP6.

1615013914398HEAD ASSY ROT WING FWD 145R2003-10 A4480 05A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 53

2887 6272

1615011994145 FWD05A01A

5225936HUB ROTARY WING FWD M20091192114R2050-35 RCRC

4800 8221

1615007406480 FWD05A01H

4865936TIE BAR ASSY 2006A10850114R2155-1 RCRC

4800 7424

1615007406480 FWD05A01H


4800 8434

1615007406480 FWD05A01H


COND COND

3040014107183 FWD05A01I

1455936PITCH HOUSING FWD GA3921145R2075-15 CCCC

COND COND

3040014107183 FWD05A01I

1455936PITCH HOUSING FWD NP6015145R2075-15 CCCC

COND COND

3040014107183 FWD05A01I

1455936PITCH HOUSING FWD NP6027145R2075-15 CCCC

2700 6112

3110008387064 FWD05A01I02A

4955936PITCH BEARING AZN1591114R2131-1 RCRC

2700 6085

3110008387064 FWD05A01I02A


2700 6085

3110008387064 FWD05A01I02A


2700 5565

3110009545730 FWD05A01I02B

10425936PITCH BEARING A5250114R2130-2 RCRC

2700 5654

3110009545730 FWD05A01I02B

9535936PITCH BEARING N16594114R2130-2 RCRC

2700 5474

3110009545730 FWD05A01I02B

11335936PITCH BEARING N49149114R2130-2 RCRC

COND COND

1615012053921 FWD05A01I05

1455936PITCH SHAFT FWD LK2008A1189234R2088-1 CCCC

COND COND

1615012053921 FWD05A01I05

30375936PITCH SHAFT FWD ZR2915234R2088-1 CCCC

COND COND

1615012053921 FWD05A01I05

22485936PITCH SHAFT FWD ZR4602234R2088-1 CCCC

1200 4845

3110004556179 FWD05A01O01

2625936BEARING, VERT PIN 201001771114RS214-6 RCRC

1200 4845

3110004556179 FWD05A01O01


1200 4845

3110004556179 FWD05A01O01


2400 5307

3110004556188 R05A01O02

12006136BEARING, VERT PIN (LOWER) AZN1833114RS214-5 RCRC

1200 4962

3110004556188 FWD05A01O02

1455936BEARING, VERT PIN (LOWER) AZN693114RS214-5 RCRC

APD LC v2.00EDITION MAY 1967 IS OBSOLETE For use of this form, see DA PAM 738-751; the proponet agency is DCSLOG

AIRCRAFT COMPONENT HISTORICAL RECORDDA FORM 2408-16, OCT 1991

(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615013914398HEAD ASSY ROT WING FWD 145R2003-10 A4480 05A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 2 of 53

2400 5150

3110004556188 FWD05A01O02

11575936BEARING, VERT PIN (LOWER) BDH181114RS214-5 RCRC

2400 6307

531501295700805A01P

52736203PIN HORIZONTAL HINGE VM4564114R2197-7 2674

2400 6307

531501295700805A01P

38816203PIN HORIZONTAL HINGE VM4795114R2197-7 2674

2400 6162

531501295700805A01P

4126203PIN HORIZONTAL HINGE FM1890114R2197-7 00

1200 4962

3110013110024 FWD05A01Q01

1455936HORZ PIN BEARING AZN1007114RS225-1 RCRC

1200 4796

3110013110024 FWD05A01Q01


1200 4796

3110013110024 FWD05A01Q01


1200 4962

3110013102258 FWD05A01Q02

1455936HORZ PIN BEARING 201200126114RS226-1 RCRC

1200 4962

3110013102258 FWD05A01Q02

1455936HORZ PIN BEARING A705114RS226-1 RCRC

1200 4962

3110013102258 FWD05A01Q02




COMPO/H OR REPLACE -

NOMENCOMPONENT NO. INST HRS

REPLAC MENT DUEINST HRS TIMEP/NNOMENCLATURE

AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND

NSN LOCATION O/HWUC NOMEN O/H COMPRMVL HRS RMVL HRS

a b c d f g ki j

Page 3 of 53

7. SIGNIFICANT HISTORICAL DATA

13-Jul-2012 1 CCAD RECAPPED, TSN:5791, TSO:0, O/H: 5. THE RETIRMENT INTERVALS OF THESE PARTS MAY BEEXTENDED 100% PROVIDED THEY ARE ROTATED 180 DEG AT 1200 HOURS.

*THESE HORZONTIAL PINS AND BEARINGS MUST BE ROTATED AT M/R HEAD TOTAL TIME: 6991 HOURS.S/N: FM1890, VM4795, VM4564, AZN1007, AZN2441, A705, 201200126, AZN693

*BEARINGS MUST BE ROTATED AT M/R HEAD TOTAL TIME: 6825 HOURS. S/N AZN1331, AZN1069

*BEARINGS MUST BE ROTATED AT M/R HEAD TOTAL TIME: 6874 HOURS. S/N 201001771, 201001881,201001776

*BEARINGS MUST BE ROTATED AT M/R HEAD TOTAL TIME: 6198 HOURS. S/N AZN1833

** THESE BEARINGS HAVE BEEN ROTATED AND MUST BE REPLACED AT M/R HEAD TOTAL TIME: 6991.S/N BDH181.

CS0131 CCAD CCAD

APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991

(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011457109BLADE ASSY ROT WING FWD 114R1702-37 A1756E 05A024. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 4 of 53






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 5 of 53


14-Feb-2013 1 SERVICEABILITY INSP C/W PER HT-445330, ENG. DRWG. 114R1702 & DOC D210-13745-1 TEETERBALANCED & TRACKED @ 3933 HRS. TRIM TAB SET 5 DEGREES UP. BOEING HELICOPTERS PHILA, PA.GM2510

GM2510 BOEING HELI PHILA, PA.


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




Page 6 of 53






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 7 of 53


13-Feb-2013 1 SERVICEABILITY INSP C/W PER HT-441185, ENG. DRWG. 114R1702 & DOC D210-13745-1 TEEETERBALANCED & TRACKED @ 3219 HRS. TRIM TAB SET 3 DEGREES UP. BOEING HELICOPTERS PHILA, PA.GM2510

GM2510 BOEING HELI PHILA, PA


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




Page 8 of 53






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 9 of 53


02-May-2013 1 SERVICEABILITY INSP. C/W PER HT-444377 ENG. DRWG. 114R1702&DOC. D210-13745-1 TEETERBALANCED & TRACKED @ 1109 HRS. TRIM TAB SET 6 DEGREES UP. BOEING HELICOPTERS PHILA, PA.GM2510

layton.c.elkin B CO 238TH KAF


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615013950006SWASHPLATE ASSY 145R3551-17 2007A9586 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 10 of 53

COND COND

161501115362405A03A01

2882510STATIONARY RING, FWD BCW906145R3351-1 CCCC

COND COND

161501114612505A03A02

0510ROTATING RING ASSY GA0748114R3464-9 CCCC

1200 4730

311001356048905A03A04

0510SWASHPLATE BEARING BDH20115351114RS308-2 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 11 of 53


26-Mar-2012 1 26 MAR 2012-CCAD-TSN: 510. TSO: 0. # O/H: 1. RECAPPED IAW AED-T3317 AND AED-T3726.

CS8562 CCAD CORPC, TX


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615013914399HEAD ASSY ROT WING AFT 145R2004-20 2009A5582 05B014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 12 of 53

1995 5632

161501198755305B01A

00HUB ROTARY WING AFT M2009-249114R2050-36 RCRC

4800 8437

161500740648005B01E


4800 8437

161500740648005B01E


4800 8437

161500740648005B01E


8200 11837

304001407729805B01F

00PITCH HOUSING AFT B00877145R2075-16 RCRC

8200 11837

304001407729805B01F


8200 11837

304001407729805B01F


2700 6337

311000838706405B01G01

00PITCH BEARING BDH457114R2131-1 RCRC

2700 6337

311000838706405B01G01


2700 6337

311000838706405B01G01


2700 6337

311000954573005B01G02

00PITCH BEARING ANZ2731114R2130-2 RCRC

2700 6337

311000954573005B01G02


2700 6337

311000954573005B01G02


COND COND

304001206392505B01H

00PITCH SHAFT AFT LK2008A1163234R2088-2 CCCC

COND COND

3040012063925 green05B01H


COND COND

3040012063925 red05B01H


1200 4837

3110004556179 aft red05B01J01

00BEARING, VERT PIN BDH1975114RS214-6 RCRC

1200 4837

3110004556179 aft yellow05B01J01


1200 4837

3110004556179 aft green05B01J01


1200 4837

3110004556188 aft red05B01J02


1200 4837

3110004556188 aft yellow05B01J02




(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615013914399HEAD ASSY ROT WING AFT 145R2004-20 2009A5582 05B014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 13 of 53

1200 4837

3110004556188 aft green05B01J02


1200 5059

531501295700805B01K

0222PIN HORIZONTAL HINGE FM3736114R2197-7 00

1200 4837

3110013110024 aft red05B01L01


1200 4837

3110013110024 aft red05B01L01


1200 4837

3110013110024 green05B01L01


1200 5059

3110013102258 aft red05B01L02

0222HORZ PIN BEARING N42792114RS226-1 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 14 of 53


25-Sep-2012 1 25SEP2009 BOEING HELICOPTERS,PHILADELPHIA,PENNSYLVANIA. CONTRACT # DAAH23-02-D-0307.THIS ROTORHEAD IS NEW AND WAS MANUFACTURED IAW THE ABOVE CONTRACT, ENGR. DWG.145R2004 REV. "T", PL. REV. "CB", AND NOTES. * TO REACH FULL RETIREMENT LIFE IT IS MANDATORYTHAT BEARINGS/PINS BE ROTATED 180 DEGREES AT 1200 HOURS. BEARINGS/PINS ARE TO BEROTATED ONLY ONCE TO THEIR UNLOADED SIDE, REGARDLESS OF TIME REMAINING WHENBEARINGS/PINS WERE ROTATED. AT NO TIME WILL "TIME SINCE NEW" IN BLOCK "H" OF ROTORHEADCOMPONENTS/PARTS, DA FORM 2408-16, EXCEED 2400 HOURS.TSN=0, TSO=0, NUMBER OF O/H'S=0. WY8177 610-591-1613

dennis.a.whewell 3/126 GSAB FOB WOLVERINE

23-Oct-2013 1 200 HR END CAP INSPECTION COMPLETED AT 347.3 HRS COMPONENT TIME

RN564555 LOCKHEED MARTIN FT CAMPBELL, KY





AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 15 of 53

07-Jul-2015 1 ALL HISTORICAL REMARKS HAVE BEEN REVIEWED, UPDATED, AND CORRECTED

AS FOLLOWS:

* DENOTES BEARINGS/PINS REQUIRE ROTATION AT 1200HRS IN ORDER TOREACHFULL RETIREMENT LIFE.

** DENOTES BEARINGS/PINS HAVE BEEN ROTATED ONCE TO THEIR UNLOADED

SIDE AND MUST BE REPLACED UPON REACHING 2400HRS.BEARINGS/PINS THATINCLUDE ** WILL HAVE AT LEAST 1200 HOURS TIMESINCE NEW IN BLOCK "H"OF THE ROTOR HEAD 2408-16.

--NOTE: TBO TIMES FOR BEARINGS/PINS THATHAVE NOT BEEN ROTATEDAND HAVE LESS THAN 1200 HRS HAVE BEEN CHANGEDWITHIN THEPARTS LCF OF ULLS-A(E) TO REFLECT TBO TIMES INDEPENDANTLYBY S/N.UPON REACHING 1200 HRS, THESE BEARINGS NEED TO BE ROTATED AND

UPDATED TO SHOW 2400 HRS TBO BY SELECTING THE "TBO DEPENDENT"OPTIONWITHIN THE PARTS LCF IN ULLS-A(E) AND UPDATING EACH S/N.

THE FOLLOWING PARTS REQUIRE ROTATION AT 1200 HEAD ASSY HRS:

BEARING PN: 114RS214-5, S/N: BDH11562, BDH11563, BDH11564

BEARING PN: 114RS214-6, S/N: BDH1975, BDH1976, BDH1977

BEARING PN: 114RS225-1, S/N: 200900984, 200900986, 200900990

BEARING PN: 114RS226-1, S/N: 200901090, 200901108

PIN HORIZ PN: 114R2197-7, S/N: M2009-238, M2009-300

THE FOLLOWING PARTS REQUIRE ROTATION AT 978 HEAD ASSY HRS:BEARING PN: 114RS226-1, S/N: N42792PIN HORIZ PN: 114R2197-7, S/N: FM3736

AASF #3 PEORIA, IL


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011457110BLADE ASSY ROT WING AFT 114R1702-38 A21250 05B024. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 16 of 53






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 17 of 53



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011457110BLADE ASSY ROT WING AFT 114R1702-38 A21810 05B024. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 18 of 53






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 19 of 53



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011457110BLADE ASSY ROT WING AFT 114R1702-38 A2226E 05B024. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 20 of 53






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 21 of 53



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615013950007SWASHPLATE ASSY 145R3551-18 A841161 05B03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 22 of 53

COND COND

1615012023322 AFT05B03A01

22755821STATIONARY RING, AFT GA0669145R3352-2 CCCC

1200 4907

3110013560489 AFT05B03A04

05821SWASHPLATE BEARING BDH201111089114RS308-2 RCRC

COND COND

1615011146125 AFT05B03A05

05821ROTATING RING ASSY GA0669114R3464-9 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 23 of 53



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615013176446FORWARD TRANSMISSION 145D1300-9 2008A13875MG 06B4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 24 of 53

6218 10325

1615011125879 F06B01

0338SHAFT ASSY, FWD M2352145D1301-3 RCRC

COND COND

3110013317702 F06B03

0338BEARING, ROLLER CYLINDE GG3529145DS016-2 CCCC

COND COND

3110013317703 F06B03

0338BEARING, BALL DUPLEX GG1907145DS017-3 CCCC

COND COND

3110014426174 F06B03


COND COND

3110011146331 F06B03


COND COND

3110011146324 F06B03

0338BEARING, BALL ANNULAR 2008000325145DS020-2 CCCC

COND COND

3110013576501 F06B03

0338BEARING, BALL ANNULAR GG3200145DS034-5 CCCC

COND COND

3110011146337 F06B03

0338BEARING, ROLLER TAPERED GP0821145DS100-4 CCCC

COND COND

3110011146337 F06B03

0338BEARING, ROLLER TAPERED GP0830145DS100-4 CCCC

COND COND

3110013537369 F06B04

0338GEAR/BEARING, ASSY GG3888MG145DS010-6 CCCC

COND COND

3110013537369 F06B04


COND COND

3110013537369 F06B04


COND COND

311001353736906B04


COND COND

3110013537369 F06B04


COND COND

3110013537369 F06B04


COND COND

3110013503674 F06B04


COND COND

3110013503674 F06B04


COND COND

3110013503674 F06B04


COND COND

3110013503674 F06B04


COND COND

3020011149716 F06B05

0338STATIONARY RING GEAR M3247145D0105-2 CCCC

COND COND

3020012281685 F06B06

0338SUN GEAR M3599145D0103-3 CCCC



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615013176446FORWARD TRANSMISSION 145D1300-9 2008A13875MG 06B4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 25 of 53

COND COND

1615011122995 F06B07

0338CARRIER FIRST STAGE 2008N1749145D0104-3 CCCC

COND COND

3040012281728 F06B08

0338PINION GEAR, BEVEL (FWD) M2145145D1306-3 CCCC

COND COND

3040012281731 F06B09

0338S.B. GEAR M2289145D1305-3 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 26 of 53



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615013154071AFT TRANSMISSION 145D2300-7 A9-612 06C4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 27 of 53

COND COND

414001287243206C01J

02833FAN ASSY, AFT XMSN 2006C0215145DS210-4 CCCC

COND COND

311001115946306C02

00BEARING, ROLLER CYLINDR GG260145DS016-1 CCCC

COND COND

311001331770306C02

00BEARING, BALL DUPLEX GG537145DS017-2 CCCC

COND COND

311001442617406C02

00BEARING, ROLLER CYLINDR VB107L145DS018-1 CCCC

COND COND

311001114633106C02


COND COND

311001114632406C02

00BEARING, BALL ANNULAR VB203L145DS020-1 CCCC

COND COND

311001357650106C02

00BEARING, BALL ANNULAR GG264145DS034-1 CCCC

COND COND

311001331770106C02

00BEARING, BALL ANNULAR WY336145DS200-1 CCCC

COND COND

311001353736906C03

00GEAR/BEARING, ASSY VB858L145DS010-5 CCCC

COND COND

311001353736906C03


COND COND

311001353736906C03


COND COND

311001353736906C03


COND COND

311001353736906C03


COND COND

311001353736906C03


COND COND

311001232770806C03


COND COND

311001232770806C03


COND COND

311001232770806C03


COND COND

311001232770806C03


COND COND

302001114971606C04

00STATIONARY RING GEAR M2432145D0105-2 CCCC

COND COND

302001228168506C05

00SUN GEAR M2395145D0103-3 CCCC

COND COND

161501112299506C06A

00CARRIER FIRST STAGE M2350145D0104-3 CCCC



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615013154071AFT TRANSMISSION 145D2300-7 A9-612 06C4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 28 of 53

COND COND

284001113023406C06B

00CARRIER SECOND STAGE M1430145D2302-2 CCCC

COND COND

304001228172906C07

00PINION GEAR M1462145D2306-3 CCCC

COND COND

304001228173206C08

00S.B. GEAR (AFT XMSN) M1532145D2305-3 CCCC

COND COND

304001114976206C09

00ACCESSORY GEAR SHAFT M1171145D2311-2 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 29 of 53


13-Jan-1992 1 WUC: 06C PN: 145D2300-7 PSN: A9-612 XMSN ASSEMBLY AFT 1/13/92 BOEING HELICOPTERS PHILA., PA. CONTRACT #DAAJO9-89-C-A010 TT: NEW

quality.control BOEING HELICOPTERS PHILA., PA.

18-May-1998 1 WUC: 06C PN: 145D2300-7 PSN: A9-612 XMSN ASSEMBLY AFT 18 MAY 98, CH-47-98-ASAM-04, ONE TIME SERIAL NUMBER INSP FOR IMPROPERLY SHIMMED INPUT PINION GEAR ASSY COMPLIED WITH 18 MAY 98 K. SUITOR TI

quality.control (NO ORGANIZATION) (NO LOCATION)

27-Aug-1999 1 WUC: 06C PN: 145D2300-7 PSN: A9-612 XMSN ASSEMBLY AFT 27 AUG 99 SOF CH-47-99-04 C/W ALL TRANSMISSION GEAR/BEARING ASSEMBLIES IDENTIFIED BY S/N PREFIX "VB" PER BILL OLSON DSN 879- 3379 ALL GEAR/BEARING ASSEMBLIES FOR AFT TRANSMISSION DOES HAVE S/N PREFIX "VB" PETE LAQUERS AMCOM PROJECT OLR HAAF, GA. 31409

quality.control AMCOM PROJECT OLR HAAF, GA. 31409


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615014643974COMBINING TRANSMISSION 145D5300-20 2010A9091 06D4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 30 of 53

COND COND

311001114632506D02

00BEARING, BALL ANNULAR ZV278145DS500-2 CCCC

COND COND

311001325496406D02

00BEARING, ROLLER CYLINDE 2010002358145DS501-4 CCCC

COND COND

311001340992806D02


COND COND

311001330655006D02


COND COND

311001464556506D02


COND COND

311001464556506D02


COND COND

311001445435806D02


COND COND

311001445435806D02


COND COND

311001445435906D02


COND COND

311001445435906D02


COND COND

304001114945706D03

00GEARSHAFT, SPUR 2009N5777145D5313-2 CCCC

COND COND

304001232777706D04

00GEARSHAFT, BEVEL M2729145D5305-3 CCCC

COND COND

304001228173006D05

00GEARSHAFT, BEVEL 2010N1524145D5306-3 CCCC

COND COND

304001228173006D05

00GEARSHAFT, BEVEL 2010N2771145D5306-3 CCCC

COND COND

414001311690106D07

00FAN ASSY, COMB XMSN 2011B0076145DS518-6 CCCC

COND COND

304001310497706D08

00FAN DRIVESHAFT 2011A2771145D5319-5 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 31 of 53


22-Sep-2013 1 29 AUG 2011 BOEING HEILCOPTERS ,PHILADELPHIA PENNSYLVANIA, CONTRACT # DAAH23-02-D=0307.THIS TRANSMISSION IS NEW MANUFACTURED I/A/W THE ABOVE CONTRACT . ENGR DWG 145D5300 REVG , AND NOTES . TSN=0 JC5297 610- 591-5112

JC5297 BOEING HELICOPTERS PHILADELPHIA PENNSYLVANIA


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615014647113XMSN ASSY ENGINE MECH 145D6300-14 2006A12041 06E4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 32 of 53

COND COND

3110012024072 #206E03

00BEARING, ROLLER, CYLIND ZV1222114DS664-4 CCCC

COND COND

3110014632983 #106E03

00BEARING, ROLLER, CYLIND GG311114DS665-6 CCCC

COND COND

3110010515811 #106E03

00BEARING, BALL, ANNULAR GG4185114DS668-3 CCCC

COND COND

3110012026680 #106E03

00BEARING, BALL, ANNULAR BCX1302114DS669-5 CCCC

COND COND

3110012024073 #106E03

00BEARING, ROLLER, CYLIND BCX627114DS670-5 CCCC

COND COND

3110011146336 #106E03

00BEARING, ROLLER, TAPE GP0910145DS600-7 CCCC

COND COND

3110013537293 #106E03


COND COND

3040011149452 #106E04


COND COND

1615012198665 #106E05

00CLUTCH ASSEMBLY XBW2131114DS672-1 CCCC

COND COND

3040011130438 #106E05A

00SHAFT, SHOULDERED M3546145D6305-3 CCCC

COND COND

3040011149453 #106E06







AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 33 of 53


27-Aug-2007 1 CONTRACT #DAAH23-03-G-0012. THIS TRANSMISSIONIS NEW AND WAS MANUFACTURED IAW THEABOVE CONTRACT, ENGR. DWG. 145D6300 REV. "AG", PL.REV."B", AND NOTES. TSN=0 610-591-1613

WY8177 BOEING HELICOPTERS PHILADELPHIA PENNSYLVANIA


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615014645563XMSN ASSY ENGINE MECH 145D6300-15 A11-460DRGI 06E4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 34 of 53

COND COND

3110012024072 206E03

12853866BEARING, ROLLER, CYLIND VB348G114DS664-2 CCCC

COND COND

3110014632983 206E03

03866BEARING, ROLLER, CYLIND ZV304114DS665-7 CCCC

COND COND

3110010515811 206E03

24073866BEARING, BALL, ANNULAR 02174114DS668-3 CCCC

COND COND

3110012026680 206E03

03866BEARING, BALL, ANNULAR 38589-89114DS669-5 CCCC

COND COND

3110012024073 206E03

12733866BEARING, ROLLER, CYLIND 0010114DS670-3 CCCC

COND COND

3110011146336 206E03

03866BEARING, ROLLER, TAPE GP0672145DS600-7 CCCC

COND COND

3110013537293 206E03


COND COND

3040011149452 206E04

28063866GEARSHAFT, BEVEL M728DRGI145D6301-2 CCCC

COND COND

3040011130438 206E05A

31933866SHAFT, SHOULDERED P248145D6305-3 CCCC

COND COND

3040011149453 206E06

41073866GEARSHAFT, BEVEL M431DRGI145D6302-2 CCCC

COND COND

1615013064353 206E08

03866CLUTCH ASSEMBLY XN30967CL40093-7-23 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 35 of 53


14-May-2007 1 CCAD OVERHAULED. TSN: 3866, TSO: 0, CNTRL #: DLMD-153349. RECAPPED IAW DMWR 55-1615-323,CHANGE 12.S/ PHYLLIS SUMMERFIELD, A/C DATA TECH, CCAD, CORPC, TX. 78419-5260.

CCAD CORP C TX 78419-5260

10-Apr-2012 1 RESET INSPECTION COMPLETED IAW TB 1-1520-240-30-02 @ 5610 COMPONENT HOURS.

chris.poyner AMCOM AFMA/URS JBLM, WA 98433


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1680013201191SHAFT ASSY, AFT VERTICAL 145D3300-6 A508 06H024. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 36 of 53

7024 11331

304001338627806H02J

03753AFT SLIDER SHAFT ASSY UT3251114R3053-10 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 37 of 53



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011130248SEC 1 DRIVE SHAFT ASSY 145D3400-23 2005A3744 06H06A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 38 of 53

COND COND

3110010965634 106H06A01

00BEARING, SHAFT ASSY SYN GG12593145DS301-3 CCCC

COND COND

161501140097206H06A02

02400 DRIVE SHAFT ADAPTER A-27996145D3407-10 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 39 of 53


11-Oct-2005 1 WUC: 06H06A PN: 145D3400-23 PSN: 2005A3744 SEC 1 D/S ASSEMBLYOCT 11 2005 BOEING HELICOPTER PHILA, PA TT: 0.0 TM2234 (610)591-2720

quality.control BOEING HELICOPTER PHILA, PA


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011125897DRIVESHAFT ASSY, SEC 2-6 145D3400-31 A-2923 06H104. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 40 of 53

COND COND

3110010965634 #506H10A


COND COND

1615011400972 #506H10B

57325732 DRIVE SHAFT ADAPTER A-1826145D3407-10 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 41 of 53



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011125897DRIVESHAFT ASSY, SEC 2-6 145D3400-31 A8628 06H104. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 42 of 53

COND COND

3110010965634 406H10A


COND COND

1615011400972 406H10B

21202336 DRIVE SHAFT ADAPTER A7264145D3407-10 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 43 of 53



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011125897DRIVESHAFT ASSY, SEC 2-6 145D3400-31 NC771 06H104. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 44 of 53

COND COND

3110010965634 # 606H10A

02846BEARING, SHAFT ASSY SYN AAAB6E145DS301-1 CCCC

COND COND

NSN PENDING # 606H10B

02846D/S ADAPTER ASSY NC930145D3400-36 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 45 of 53



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011125897DRIVESHAFT ASSY, SEC 2-6 145D3400-32 2008A13806 06H104. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 46 of 53

COND COND

3110010965634 306H10A

25780BEARING, SHAFT ASSY SYN VB568J145DS301-2 CCCC

COND COND

1615011400972 306H10B

00 DRIVE SHAFT ADAPTER 200813398145D3407-10 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 47 of 53



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011125897DRIVESHAFT ASSY, SEC 2-6 145D3400-32 2009A6789 06H104. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 48 of 53

COND COND

3110010965634 206H10A


COND COND

1615011400972 206H10B

880880 DRIVE SHAFT ADAPTER 2009A6149145D3407-10 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 49 of 53



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011130292AFT SEC 1 D/S ASSY 145D3400-25 A1695 06H13A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 50 of 53

COND COND

3110010965634 # 806H13A01

7683170BEARING, SHAFT ASSY SYN ZV1102145DS301-1 CCCC

COND COND

1615011400972 # 806H13A02

21693170 DRIVE SHAFT ADAPTER A29743145D3407-10 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 51 of 53



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1680011185607ACTUATOR ASSY DASH 145CS100-5 893 11D034. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 52 of 53

COND COND

168001118560611D03A

52960ACT ELECTRO-MECH, UPPER 893145CS100-6 CCCC

COND COND

168001118560511D03B

52960ACT ELECTRO-MECH, LOWE 893145CS100-7 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 53 of 53



STARTS/HOURS

LIFE

STARTS/RMVL

HOURS

COMP

STARTS/INST

HOURS

SINCEO/H

STARTS/RMVL

HOURS

NHA

HOURSSTARTS/

O/H

7k.REPLACE

DUE

7j.O/H OR

REPLACE7i.

7h.COMP

7g.STARTS/HOURS

7f.

7e.NHAINST

7d.NO.

PREV

7c.COMPONENT

SERIAL NUMBER

7b.PART NUMBER

AND NSNAND WUCNOMENCLATURE

7a.

7. REPLACEMENT DUE STARTS/HOURS FOR THE APU AND SUB-COMPONENTS

6d. APU HISTORICAL STARTS/HOURS

1. MODEL

3. SERIAL NUMBER

2. NOMENCLATURE

4. PART NUMBER 5. NHA S/N

6. LINE NUMBER 6a. STARTS LAST O/H 6b. STARTS 6c. OPERATING HOURS

METER READING AT APU INSTALL

3

2-

TOTAL METER COUNTS SINCE INSTALL LINE 3 MINUS LINE 2

PREVIOUS STARTS/HOURS

4=

1+

TOTAL STARTS/HOURS LINE 4 PLUS LINE 1

METER READING AT APU REMOVAL

5=

6

20

11860

20

2907

1

877509

APU

160150-10A 9200307

3 6160150-10A 877509AUXILIARY POWER UNIT 11860

15B 2835014693420

60146000

starts

RC RC4503999 V36HB437WHEEL, TURBINE (APU) 11854 0

15B02A 2835014623974

60146000

starts

RC RC4503340 2J5COMPRESSOR ROTOR 11854 0

15B02B 2835014623375

60146000

starts


23-Oct-2009 1 9196 THIS DATE, RECEIVED APU S/N: 877509 FOR OVERHAUL(ED). METER READINGS: HRS: 1284; STS:4613; TSN: 2906; SSN: 11854. INITIATED NEW FORM. 9296 THIS DATE, OVERHAUL(ED) APU S/N: 877509.OVERHAUL PROCESSED IN ACCORDANCE WITH DMWR 55-2835-205 AS SUPPLEMENTED BYNAVAIRDEPOT MCAS CHPT LES CP23-0-LL-173, REV B AND IS SERVICEABLE FOR INSTALLATION ANDCONTINUED SEVICE. WORK PERFORMED IS AS FOLLOWS:INSTALLED: NEW C/W; NEW T/W. NEWMETERS INSTALLED AT TSN:2906 AND SSN: 11854. METER READING AT INSTALL: HOURS: 0000 ANDSTARTS: 0000. START METER ADVANCED 14 STARTS DURING OP CHECK. METER READINGS: HRS: 1;STS: 20; TSN: 2907; SSN: 11860 GP8475 DSN 451-7874 FRC EAST CHERRY POINT

GP8475 CHERRY POINT MCAS CHERRY POINT NC

For use of this form, see DA PAM 738-751; the proponent agency is DCS G-4

APD LC v1.00AUXILIARY POWER UNIT AND COMPONENT RECORDDA FORM 2408-16-2, MAR 2014

(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1520010883669HELICOPTER, CARGO CH-47D 9200307 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Condition Change Components Page 1 of 4

COND COND

1560011171084 NOSE02A16

46443530VIBRATION ABSORBER BF479234N0003-1 CCCC

COND COND

1560011171084 PILOT02A17

03530VIBRATION ABSORBER 0142-0412234N0003-1 CCCC

COND COND

1560011171084 C0-PILOT02A18

44983530VIBRATION ABSORBER BF379234N0003-1 CCCC

COND COND

2915014686108 104A06A

10704441DIGITAL ELECT CONTROL 1159900020104SC110710-08A1 CCCC

COND COND

2915014686108 204A06A

2334441DIGITAL ELECT CONTROL 1159901280740SC110710-08A1 CCCC

COND COND

168001227174804A07E

2463330N1 QUADRANT CONTROL 807145ES010-6 CCCC

COND COND

1615011457109 FWD YELLOW05A02

39333747BLADE ASSY ROT WING FWD A1756E114R1702-37 CCCC

COND COND

1615011457109 FWD RED05A02


COND COND

1615011457109 FWD GREEN05A02


COND COND

1560013267231 F05A03B

02400DRIVE ARM ASSY NP-0060114R3434-9 CCCC

COND COND

1615011457110 AFT YELLOW05B02

62563747BLADE ASSY ROT WING AFT A21250114R1702-38 CCCC

COND COND

1615011457110 AFT GREEN05B02

43553747BLADE ASSY ROT WING AFT A21810114R1702-38 CCCC

COND COND

1615011457110 AFT RED05B02

47133747BLADE ASSY ROT WING AFT A2226E114R1702-38 CCCC

COND COND

1560013267231 A05B03E

01675DRIVE ARM ASSY TS-864114R3434-9 CCCC

COND COND

1615013176446 F06B

3384107FORWARD TRANSMISSION 2008A13875MG145D1300-9 CCCC

COND COND

161501315407106C

21732476AFT TRANSMISSION A9-612145D2300-7 CCCC

COND COND

161501464397406D

03907COMBINING TRANSMISSION 2010A9091145D5300-20 CCCC

COND COND

1615014647113 #106E

03167XMSN ASSY ENGINE MECH 2006A12041145D6300-14 CCCC

COND COND

1615014645563 206E

65784377XMSN ASSY ENGINE MECH A11-460DRGI145D6300-15 CCCC

COND COND

161501113024906H06B

40152400FWD XMSN D/S ADAPTER AS A-651145D3407-6 CCCC

COND COND

161501140670306H12B

0163FWD C-BOX ADAPTER A-36569145D3407-7 CCCC



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




Condition Change Components Page 2 of 4

COND COND

161501119336006H13B

21792599COMB XMSN AFT ADAPTER A-3695145D3407-8 CCCC

COND COND

161501114084506H14B

0163AFT XMSN ADAPTER ASSY A-3283145D3407-9 CCCC

COND COND

1650013020076 F07A37

03907CYLINDER ACT SWIVEL FWD UR1878A145H6700-19 CCCC

COND COND

165001304901607A38

03126CYLINDER ASSY PIVOT FWD 2008AA198145H6600-19 CCCC

COND COND

165001303789807A39

44863530CYLINDER ACT SWIVEL AFT UR590BANS145H6700-18 CCCC

COND COND

165001303789707A40

04307CYLINDER ASSY PIVOT AFT UR1985AS145H6600-20 CCCC

COND COND

168001118560711D03

9603933ACTUATOR ASSY DASH 893145CS100-5 CCCC

COND COND

299501169529115A04

32572570ENGINE SEQUENCING UNIT 75842173163290-100 CCCC

COND COND

599601415867319D01A

46443530AMPLIFIER, RADIO FREQUEN 1224822-0787-001 CCCC

COND COND

582101413423419D02

16434057CONTROL, HF RADIO SET 1896AA822-0786-001 CCCC

COND COND

5841014214162 PILOT19E05A

03907RECEIVER-TRANSMITTER, R 1216AAHG7209AD01 CCCC

COND COND

5841012459093 CO PILOT19E05C

03825INDICATOR,HEIGHT 0508FFA3060591 CCCC

COND COND

5841012459093 LOAD MASTER19E05C

03825INDICATOR,HEIGHT 0873FFA3060591 CCCC

COND COND

581001376138019H

25163176TSEC/KY-100 PROCESSOR 75230N616736-1 CCCC

COND COND

581001376138119H02

7483176TSEC/AVH RCU 24720N616779-1 CCCC

COND COND

589501395744776A03

53444270COMPARATOR/PROCESSOR L02390035A3214085 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 3 of 4Condition Change Components


24-Sep-2009 3 LOCATED LOWER RED FWD HEAD

24-Sep-2009 4 LOCATION GREEN LOWER

24-Sep-2009 5 LOCATION FWD RED LOWER

11-Jan-2001 6 ROT WING FWD. 11JAN01 REPLACED LOWER LIGHTENING JUMPER DOUBLERS,LIGHTENING JUMPER WIRE (ROOT END), PAINTED AND BALANCED BLADES S/N:A1421E @ 2081 HRS. IAW AVION S/N: AV-96007 CHORD=8.46, SPAN=183.55,WGT=356.06, SM=65354 CM=3010 WITH 10 EA PLARES INST. ENTERED BY MARKPRANTER T.I. MO-AVCRAD, QC000000 AVCRAD MO

23-Jan-2007 7 COMPLETED REQUIREMENTS OF CH-47-07-SOF-02, CE705006, DALLAS AASF,GRAND PRAIRIE, TX 75051

29-Dec-2011 8 PMI COMPLETED, REPAIRED, AND BALANCED MAIN ROTOR BLADE S/N: A1-1030@ 2583 HRS BLADE TSN. USING AVION BALANCER S/N: AV96005. SM=65367,SCG=183.29, W=356.62 LB, CM=2947, CCG=8.265 ( 9 WEIGHT PLATES.) RIBCLOSURE REPAIRED. ANTI STATIC MEGGAR TEST COMPLETED O.K. REPAIREDVOID TOP SIDE STA. 116. ROOT END SOCKET LINER REPLACED AUTH SRAAX211211. ENTERED BY L. BLYSTONE , LB5035 T.I. MO-AVCRAD, SPRINGFIELD,MO. 417-874-8400 (EXT) 5305.

25-Oct-2011 9 PMI COMPLETED, REPAIRED, AND BALANCED MAIN ROTOR BLADE S/N: A1-1030@ 2583 HRS BLADE TSN. USING AVION BALANCER S/N: AV96005. SM=65382,SCG=183.08, W=357.12 LB, CM=2988, CCG=8.366 ( 9 WEIGHT PLATES.) RIBCLOSURE REPAIRED. ROOT END SOCKET LINER REPLACED AUTH SRAAX211211. REPAIRED VOID TOP SIDE STA'S 265, 248, 143. ENTERED BY L.BLYSTONE , LB5035 T.I. MO-AVCRAD, SPRINGFIELD, MO. 417-874-8400 (EXT) 5305.

25-Oct-2011 10 PMI COMPLETED, REPAIRED, AND BALANCED MAIN ROTOR BLADE S/N: A1-827E@ 4214 HRS BLADE TSN. USING AVION BALANCER S/N: AV96005. SM=65382,SCG=183.08, W=357.12 LB, CM=2988, CCG=8.366 ( 9 WEIGHT PLATES.) RIBCLOSURE REPAIRED. ROOT END SOCKET LINER REPLACED AUTH SRAAX211211. REPAIRED VOID TOP SIDE STA'S 265, 248, 143. ENTERED BY L.BLYSTONE , LB5035 T.I. MO-AVCRAD, SPRINGFIELD, MO. 417-874-8400 (EXT) 5305.

30-Dec-2011 11 REPAIRED, AND BALANCED MAIN ROTOR BLADE S/N: A2-2668 @ 3167 HRSBLADE TSN. USING AVION BALANCER S/N: AV96005. SM=65366, SCG=184.87,W=353.58 LB, CM=22928, CCG=8.280 ( 9 WEIGHT PLATES.) RIB CLOSUREREPAIRED. UPPER SHOCK ABSORBER BUSHING REPLACED WITH #6OVERSIZED. ENTERED BY L. BLYSTONE , LB5035 T.I. MO-AVCRAD, SPRINGFIELD,MO. 417-874-8400 (EXT) 5305.





AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 4 of 4Condition Change Components

29-Dec-2011 12 REPAIRED, AND BALANCED MAIN ROTOR BLADE S/N: A2-187E @ 2985 HRSBLADE TSN. USING AVION BALANCER S/N: AV96005. SM=65351, SCG=183.55,W=356.04 LB, CM=2958, CCG=8.308 ( 10 WEIGHT PLATES.)ENTERED BY L.BLYSTONE , LB5035 T.I. MO-AVCRAD, SPRINGFIELD, MO. 417-874-8400 (EXT) 5305.

29-Dec-2011 13 29-DEC 2011 REPAIRED, AND BALANCED MAIN ROTOR BLADE S/N: A2-1203 @4783 HRS BLADE TSN. USING AVION BALANCER S/N: AV96005. SM=65385,SCG=184.40, W=354.58 LB, CM=2945, CCG=8.305 ( 10 WEIGHT PLATES.) RIBCLOSURE REPAIRED. VOID REPAIRED STA. 151 TO 144 TOP SIDE. ENTERED BY L.BLYSTONE , LB5035 T.I. MO-AVCRAD, SPRINGFIELD, MO. 417-874-8400 (EXT) 5305.


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




Time Change Components Page 1 of 4

2800 4065

2840014585361 104A

12651265ENGINE ASSY TURBINE GA751892-001-020-39 02

2800 4453

2840014585361 204A

30583058ENGINE ASSY TURBINE GA752132-001-020-39 14051

2400 6162

1615013914398 FWD05A01

59363907HEAD ASSY ROT WING FWD A4480145R2003-10 1455

1200 4730

161501395000605A03A

5103530SWASHPLATE ASSY 2007A9586145R3551-17 01

7523 10690

1615000031146 FWD05A03L

03167BOLT ASSY, ROTARY WING H 07917-3114R3650-3 RCRC

7523 11230

1615000031146 F PIV UP05A03N

03707BOLT ASSY, ROTARY WING H 07843-3114R3650-3 RCRC

4000 7530

5306013017793 FWD YELLOW05A03Q

03530BOLT, PITCH LINK UPPER 19570-16114R3650-16 RCRC

4000 7167

5306013017793 GREEN05A03Q


4000 7167

5306013017793 RED05A03Q


4000 7167

5306013017794 GREEN05A03R

03167BOLT, PITCH LINK LOWER 21146-17114R3650-17 RCRC

4000 7167

5306013017794 YELLOW05A03R


4000 7167

5306013017794 RED05A03R


2400 6037

1615013914399 aft05B01

7444381HEAD ASSY ROT WING AFT 2009A5582145R2004-20 00

1200 4907

1615013950007 AFT05B03A

58213707SWASHPLATE ASSY A841161145R3551-18 07

4000 7167

1615011153609 UPPER05B03J

03167BOLT ASSEMBLY 000666145R3650-1 RCRC

7757 10924

5306000085025 LOWER05B03K

03167BOLT, SELF RETAINING 0583BACB30ST8-31 RCRC

4000 7167

1615011153609 Upper05B03L

12124379BOLT ASSEMBLY 08282-1B145R3650-1 RCRC

4000 7167

5306013017793 GREEN05B03N

03167BOLT, PITCH LINK UPPER 05U29114R3650-16 RCRC

4000 7167

5306013017793 RED05B03N

03167BOLT, PITCH LINK UPPER 07B69114R3650-16 RCRC

4000 7530

5306013017793 AFT YELLOW05B03N


4000 7167

5306013017794 RED05B03P




(ACFT HRS)

ji kgfdcba


AND he SINCELIFE





4000 7167

5306013017794 YELLOW05B03P


4000 7707

5306013017794 GREEN05B03P


7757 10924

5306000085025 AFT05B03Q

03167BOLT, SELF RETAINING 03286BACB30ST8-31 RCRC

4797 5351

168001320119106H02

26133167SHAFT ASSY, AFT VERTICAL A508145D3300-6 RCRC

6000 6163

1615013162661 #2 ENGINE06H04

0163SHAFT ASSY, ENG DRIVEN A-2100145D3504-2 RCRC

6000 6163

1615013162661 #1 ENGINE06H04

0163SHAFT ASSY, ENG DRIVEN A-2101145D3504-2 RCRC

4581 6067

1615013195092 #1 ENG06H04A

01486ADAPTER ASSY ENG D/S INB A-7809145D3500-17 RCRC

4581 8064

1615013195092 2INBD06H04A

03483ADAPTER ASSY ENG D/S INB NP-5546145D3500-17 RCRC

4581 5278

1615013195091 1 O/B06H04B

26333330ADAPTER ASSY ENG D/S OU A4701145D3500-16 RCRC

4581 8859

1615013195091 206H04B

994377ADAPTER ASSY ENG D/S OU NP-6886145D3500-16 RCRC

10061 12461

1615011130248 106H06A

02400SEC 1 DRIVE SHAFT ASSY 2005A3744145D3400-23 RCRC

10061 7496

1615011125897 #506H10

57323167DRIVESHAFT ASSY, SEC 2-6 A-2923145D3400-31 RCRC

10061 10552

1615011125897 406H10

23362827DRIVESHAFT ASSY, SEC 2-6 A8628145D3400-31 RCRC

10061 10922

1615011125897 # 606H10

28463707DRIVESHAFT ASSY, SEC 2-6 NC771145D3400-31 RCRC

10061 13258

1615011125897 306H10

03197DRIVESHAFT ASSY, SEC 2-6 2008A13806145D3400-32 RCRC

10061 12888

1615011125897 206H10

8803707DRIVESHAFT ASSY, SEC 2-6 2009A6789145D3400-32 RCRC

10061 11930

161501112589506H12A

01869SEC 7 DRIVE SHAFT ASSY A-13288145D3400-24 RCRC

9426 9963

1615011130292 # 806H13A

31703707AFT SEC 1 D/S ASSY A1695145D3400-25 RCRC

9426 11826

1615011193359 #906H14A

02400AFT SEC 2 D/S ASSY A16017145D3400-26 RCRC

6948 9806

3120001108542 AFT FIXED11G01

3093167BEARING, ROD END YD1437114CS123-1 RCRC



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE





6948 10115

312000110854211G02

03167BEARING, ROD END 4844114CS123-1 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 4 of 4Time Change Components


30-Oct-2004 1 WUC: 06H14A PN: 145D3400-26 PSN: A16017 AFT SEC 2D/S ASSYOCT 30 2004 BOEING HELICOPTER PHILA. PA. T.T. 00:00 TM2234

30-Oct-2004 2 WUC: 06H14A PN: 145D3400-26 PSN: A16017 AFT SEC 2 D/S ASSYOCT 30 2004 BOEING HELICOPTER PHILA. PA. T.T. 00:00 TM2234


of 19SERIAL NUMBER MODEL AREA NAME

9200307 CH-47D_BASELINE SECTION A - COCKPIT AREACH-47D

NAME OR PIDNUMBER DATE

db c

DATE NUMBER RANKRANK NAME OR PID

CHECK CHECK

ba ad

5. VERIFICATION

c

brett.brazell1 SPC 30-May-2013

jeffrey.a.mctea2 MSG 29-May-2014

b. LOCATION/REMARKSCHECK NO.

6. LOCATION OR REMARKS

a. ITEM NUMBER

Nomenclature

AN/APX-100RECEIVER/TRANSMITTER (IF

INSTALLED)1 NOT INSTALLED13

C-10131/ALQ-156COUNTERMEASURES

CONTROL UNIT1 NOT INSTALLED18

CMWS MISC CONTROL PANELP3I

1 NOT INSTALLED19

C-12293/AVS-7 CONVERTERCONTROL UNIT (HUD)

2 THEATER PROVIDED EQUIPMENT21

CV-3338A/ASN-128D GPS SDC(AVX CLOSET)

1 HAS BEEN REPLACED WITH THE ASN-128D41

CV-3338A/ASN-128D GPS SDC(AVX CLOSET)

2 HAS BEEN REPLACED WITH THE ASN-128D41

MSPU STACK UP1NO LONGER INSTALLED, HAS BEEN REPLACED BY THE

APX-118 SYSTEM43

MSPU STACK UP2 43

MSPU QAR1 NO LONGER INSTALLED45

MSPU QAR2 NO LONGER INSTALLED45

REVERSE OF DA FORM 2408-17, NOV 1991




db c


CHECK CHECK

ba ad

5. VERIFICATION

c



C-12510/AAR-57(V) CMWS ECU(AVX CLOSET)


SU-202/AAR-57(V) EOMS (EXT.L&R SIDE, FWD PYLON)


GPS DTM RECEPTACLE1 INSTALLED FOR THE CURRENT MISSION SET61

DELETED1 INSTALLED FOR CURRENT MISSION SET64

DELETED1 INSTALLED67




KIT-1C IFF COMPUTER (IFINSTALLED)

1NO LONGER INSTALLED, HAS BEEN REPLACED BY THE

APX-11878

RT-1220B/ ALQ-156RECEIVER/TRANSMITTER (IF

INSTALLED)1 NO LONGER INSTALLED80

RT-1220B/ ALQ-156





db c


CHECK CHECK

ba ad

5. VERIFICATION

c



RECEIVER/TRANSMITTER (IFINSTALLED)

2 NO LONGER INSTALLED80

DOPPLER NAVIGATION SYSTEMCV-3338/ASN-128

1 HAS BEEN REPLACED BY THE CV-3338B/ASN-128D93

DOPPLER NAVIGATION SYSTEMCV-3338/ASN-128

2 HAS BEEN REPLACED BY THE CV-3338B/ASN-128D93



9200307 CH-47D_BASELINE SECTION B - CABIN AREACH-47D


db c


CHECK CHECK

ba ad

5. VERIFICATION

c





a. ITEM NUMBER

Nomenclature

FOOT SWITCHES WITH CABLE,GUNNER

1 PART NOT LONGER BEING USED5

FOOT SWITCHES WITH CABLE,GUNNER

2 NO LONGER BEING USED5

TROOP SEAT (1 MAN)1ONLY TWO 1-MAN SEATS ARE INSTALLED, THRID ONE IS

NOT USED9

SU-202/AAR-57(V) 5TH EOMS(EXT. BOTTOM, FWD OF RAMP)


CMWS SEQUENCER R/H (#2) SN_________________


IVHMS IVHMU P/N 30279-0202(OR 30279-0402)

1 NOT USED73

TRANSMITTER, INFRARED T-1678/ALQ-212(V) ATIRCM (MBL)


LASER, DIRECTIONAL ASSY, SU-241/ALQ-212(V) ATIRCM (IRJH)


CONTROL TRANSMITTER,COUNTERMEASURE C-

12794/ALQ-212(V) ATIRCM(JHCU)


OPTICAL ASSY, LASER, ATIRCM(COUPLER)




9200307 CH-47D_BASELINE SECTION B - CABIN AREACH-47D


db c


CHECK CHECK

ba ad

5. VERIFICATION

c





9200307 CH-47D_BASELINE SECTION C - RAMP AREACH-47D


db c


CHECK CHECK

ba ad

5. VERIFICATION

c





a. ITEM NUMBER

Nomenclature

9311431 M-130 ELECTRONICMODULE (IF INSTALLED)

1 NOT INSTALLED2

9311434 M-130 DISPENSERASSEMBLY (IF INSTALLED)

1 NOT INSTALLED3

9311451 M-130 PAYLOADMODULE (IF INSTALLED)

1 NOT INSTALLED4

EMERGENCY EXIT LIGHT1 INSTALLED13

PROBE POLE, CARGO LOADING1 INSTALLED14

CD-45(V)/ALE-47(V)PROGRAMMER (IF INSTALLED)

1 INSTALLED15

114ES290-1REMOTE FIRINGSWITCH, 14 FT (IF INSTALLE

1 INSTALLED16

SA-2669/ALE-47(V)SEQUENCERS (IF INSTALLED)

1 INSTALLED18

SA-2669/ALE-47(V)SEQUENCERS (IF INSTALLED)


D-61/ALQ-212(V) AN/AAR-57(V)DISPENSER ASSY CMWS (IF

INSTALLED1 INSTALLED19





db c


CHECK CHECK

ba ad

5. VERIFICATION

c



D-61/ALQ-212(V) AN/AAR-57(V)DISPENSER ASSY CMWS (IF

INSTALLED2 THEATER PROVIDED EQUIPMENT19

196405-001 AN/AAR-57(V)PAYLOAD MODULE CMWS (IF

INSTALLED)1 INSTALLED20

196405-001 AN/AAR-57(V)PAYLOAD MODULE CMWS (IF

INSTALLED)2 THEATER PROVIDED EQUIPMENT20

AS-3149/ALQ-156COUNTERMEASURES ANTENNA

1 INSTALLED21

AS-3149/ALQ-156COUNTERMEASURES ANTENNA


AS-2890/APR-39 BLADEANTENNA

1 INSTALLED22

AS-2890/APR-39 BLADEANTENNA


COVER, OIL COOLER INLET,145G0001-1

1 COVERED IN SECTION B23

COVER ENGINE AIR OUTLET,114G1323-2


COVER ENGINE INLET WITHSCREEN, 219G1001-1


COVER ENGINE INLET WITH





db c


CHECK CHECK

ba ad

5. VERIFICATION

c


jeffrey.a.mctea2 MSG 29-May-2014COVER ENGINE INLET WITH

WITHOUT SCREENS1 COVERED IN SECTION B26

COVER, OIL COOLER EXHAUST,145G0002-5


COVER PITOT TUBE, 114E5040-33


COVER, OIL COOLER EXHAUST,145G0002-6


COVER, COCKPIT ENCLOSURE,145G0006-1


COVER HYDRAULIC COOLEXHAUST, 145G0004-1


COVER ROTOR HUB FWD &AFT, 114G1023-25


COVER HEATER, 114G1024-11 COVERED IN SECTION B33

COVER HEATER EXHAUST,114G1025-1


COVER APU EXHAUST,145G0005-1


COVER, AW INLET, 14560003-11 COVERED IN SECTION B36





db c


CHECK CHECK

ba ad

5. VERIFICATION

c



RAMP EXTENSION, 1560CH-47-398-1

1 Remarks38

BLADE ANCHOR1 COVERED IN SECTION B39

TIEDOWN CHAINS TYPE MB-11 COVERED IN SECTION B40

TIEDOWN STRAPS TYPECGU1/B


SPACER SET RIGGING(ACTUATOR BLOCK), 114E5900-


PIN, GROUND SAFETY BLADEBLOCKING, 114E5897-13


ATTACHMENT FITTINGS,TRANSPORT WITH BOLT

114G1049-1 COVERED IN SECTION B44

INTERCOM CORD, 50 FT1 COVERED IN SECTION B45

WINCH/HOIST OPERATORINTERCOM CORD


AIR DAT TRANSDUCER1 COVERED IN SECTION B47





db c


CHECK CHECK

ba ad

5. VERIFICATION

c



INCLINOMETER (HUD)1 Remarks48

CONVERTER CONTROL1 COVERED IN SECTION B49



9200307 CH-47D_BASELINE SECTION D - ENGINE AND AFT PYLONCH-47D


db c


CHECK CHECK

ba ad

5. VERIFICATION

c





a. ITEM NUMBER

Nomenclature

R-2218/APR-39A(V) RADARRECEIVER (IN AFT PYLON)


SU-202/AAR-57(V) EOMS (EXT.L&R SIDE, AFT PYLON)


TYPE AERONAUTIC FIRST AIDKIT

1 COVERED IN PREVIOUS SECTIONS5

LIGHT ASSEMBLY 114ES247-11 COVERED IN PREVIOUS SECTIONS6

INTERPHONE CONTROL C-65331 COVERED IN PREVIOUS SECTIONS7

MARKER BEACON ANTENNA AT-640/ARN

1 INSTALLED9

TROOP SEAT TYPE 3 MAN1 COVERED IN PREVIOUS SECTIONS10

TROOP SEAT TYPE 1 MAN1 COVERED IN PREVIOUS SECTIONS11

BELT SAFETY TROOP1 COVERED IN PREVIOUS SECTIONS12

TIEDOWN FITTINGS 10,000LB1 COVERED IN PREVIOUS SECTIONS13





db c


CHECK CHECK

ba ad

5. VERIFICATION

c



PROBE POLE, CARGO HOOK UP1 COVERED IN PREVIOUS SECTIONS14

WINCH CONTROL GRIP ANDCORD ASSEMBLY


CRANK ASSY. EMERGENCYRAMP & RESCUE


ANTENNA AS-2595/APN-194 (V)1 COVERED IN PREVIOUS SECTIONS17

145G0006-1 COVER, COCKPITENCLOSURE


114G1025-1 COVER HEATEREXHAUST


COVER HEATER 114G1024-11 COVERED IN PREVIOUS SECTIONS20

COVER PITOT TUBE (114E5040-33)


145G0001-1 FWD. PYLONINTAKE COVER


114G1323-1 COVER ENGINEOUTLET


219G1001-1 COVER ENGINE





db c


CHECK CHECK

ba ad

5. VERIFICATION

c


jeffrey.a.mctea2 MSG 29-May-2014219G1001-1 COVER ENGINE

INLET1 COVERED IN PREVIOUS SECTIONS24

PROTECTIVE RING ASSY.ENGINE INLET-114G1206


145G0004-1 COVER AFT. PYLONEXHAUST


145G0002-5 COVER FWD.PYLON EXHAUST


145G0002-6 COVER FWD.PYLON


145G0003-1 COVER AFT. PYLON1 COVERED IN PREVIOUS SECTIONS29

145G0005-1 COVER APUEXHAUST


BLADE ANCHOR 114E5060-11 COVERED IN PREVIOUS SECTIONS31

114G1023-25 ROTOR HUBCOVERS


TIEDOWN CHAINS TYPE MB-11 COVERED IN PREVIOUS SECTIONS33

TIEDOWN STRAPS TYPECGU1/B






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



RAMP EXTENSION 114S6003-211 COVERED IN PREVIOUS SECTIONS35

RAMP EXTENSION 1560CH47-400-1


GUNNER CABLE ASSY.1 COVERED IN PREVIOUS SECTIONS38

VHF-AM/FM ANTENNA S65-8280-30


ANTENNA, ADF LOOP1 COVERED IN PREVIOUS SECTIONS40

ANTENNA, SENSE AS-1869/ARN1 COVERED IN PREVIOUS SECTIONS41

UHF-AM ANTENNA AT-256( )ARC


ANTENNA AS-1922( )/ARC1 COVERED IN PREVIOUS SECTIONS43

IGNITION KEYS1 COVERED IN PREVIOUS SECTIONS44

BRACKET & PADLOCK1 COVERED IN PREVIOUS SECTIONS45





db c


CHECK CHECK

ba ad

5. VERIFICATION

c



ANTENNA ADF AS-2108/ARN-89(LOOP)


(BFT) FWD PALLET XCVR ASSY(STA. 320)


(BFT) XCVR MOUNT (STA. 320)1 COVERED IN PREVIOUS SECTIONS52

(BFT) KGV-72 (STA. 360)1 COVERED IN PREVIOUS SECTIONS53

SINCGARS ANTENNAS AS3939/ARC (TOP)


SINCGARS ANTENNAS AS3939/ARC (BOTTOM)


SLAB BATTERY; PN D8565/11-11 COVERED IN PREVIOUS SECTIONS56

FLUX VALVE (CN-405/ASN)1 INSTALLED57

(CMWS) SMART DISPENSER LHS/N: __________


(CMWS) SMART DISPENSER LHS/N: __________


(CMWS) SMART DISPENSER RHS/N: __________






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



(CMWS) SMART DISPENSER RHS/N: __________


(CMWS) PAYLOAD MODULE LHS/N: __________


(CMWS) PAYLOAD MODULE LHS/N: __________


(CMWS) PAYLOAD MODULE RHS/N: __________


(CMWS) PAYLOAD MODULE RHS/N: __________




9200307 CH-47D_BASELINE UNIT UNIQUE INVENTORY ITEMSCH-47D


db c


CHECK CHECK

ba ad

5. VERIFICATION

c





a. ITEM NUMBER

Nomenclature

BLANK1 NOT IN INSTALLED1

ERFS FUEL SAMPLING PUMPKIT 1680-01-474-3324

1 NOT IN INSTALLED2

ERFS FUEL SAMPLING PUMPKIT 1680-01-474-3324

2 NOT INSTALLED2

CAVITY DRAIN HOSE 4720-01-424-5554

1 NOT IN INSTALLED3

CAVITY DRAIN HOSE 4720-01-424-5554

2 NOT INSTALLED3

GROUNDING CABLE 6150-01-398-4389

2 NOT INSTALLED4

HARNESS TANK POWER 645-01-380-2981

1 NOT IN INSTALLED5

HARNESS TANK POWER 645-01-380-2981

2 NOT INSTALLED5

FUEL HOSE SINGLE POINTPRESSURE REFUELING 4720-01

-425-12151 NOT IN INSTALLED6

FUEL HOSE SINGLE POINTPRESSURE REFUELING 4720-01

-425-12152 NOT INSTALLED6





db c


CHECK CHECK

ba ad

5. VERIFICATION

c



VENT HOSE ASSY 4720-01-471-6739

1 NOT IN INSTALLED7

VENT HOSE ASSY 4720-01-471-6739

2 NOT INSTALLED7

FUEL HOSE, TANK-TO -ACFTRANGE EXT 4720-01-424-5558

1 NOT IN INSTALLED8

FUEL HOSE, TANK-TO -ACFTRANGE EXT 4720-01-424-5558

2 NOT INSTALLED8

FUEL PROBE ELECTRICALCABLE 6150-01-475-7634

1 NOT IN INSTALLED9

FUEL PROBE ELECTRICALCABLE 6150-01-475-7634

2 NOT INSTALLED9

CH-47 ERFS II FUEL CONTROLPANEL P/N HM022-123-51

1 NOT IN INSTALLED10

CH-47 ERFS II FUEL CONTROLPANEL P/N HM022-123-51

2 NOT INSTALLED10

CH-47 ERFS II ROLLER ASSYKIT P/N WOH93JCH-47-T-F-K


CH-47 ERFS II ROLLER ASSYKIT P/N WOH93JCH-47-T-F-K

2 NOT INSTALLED11

EFRS TANK COVER P/N IT765-





db c


CHECK CHECK

ba ad

5. VERIFICATION

c


jeffrey.a.mctea2 MSG 29-May-2014EFRS TANK COVER P/N IT765-

HMO22-T17-111 NOT IN INSTALLED12

EFRS TANK COVER P/N IT765-HMO22-T17-11

2 NOT INSTALLED12

AN/PRC- 117F SATCOMMANPACK RADIO


SATCOM RF POWERAMPLIFIER/PREAMLIFIER

(SATCOM PALLET)1 NOT IN INSTALLED15

SATCOM RF POWERAMPLIFIER/PREAMLIFIER

(SATCOM PALLET)2 THEATER PROVIDED EQUIPMENT15

PLATE ASSY, BLANKING,ATIRCM COOLING FAN R/H

UPPER (OVAL)1 NOT IN INSTALLED49

LOWER FAN SUPPORT ASSY,R/H, ATIRCM PN: 0056A3009-20


DUCT, LOWER FAN, R/H,ATIRCM PN: 0056A4043-02


ACCESS PANEL, R/H, PN:114S5931-1, INTERCOSTALAREA AFT OF AUX TANK



SECTION A - COCKPIT AREACH-47D_BASELINE

4. EQUIPMENT CHECKLIST

9200307 CH-47D

3. AREA NAME 2. MODEL 1. SERIAL NUMBER

Page 1 of 39

1FIRE EXTINGUISHER, CF3BR,10501725

U UUUUUUUU UU 11

1

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER

QTY REQNOMENCLATURE:ITEM NO.

1FIRE EXTINGUISHER, CF3BR,10501725

U UUUUUUUU UU1

1

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


3C-6533()/ARC ICS PANELS

U UUUUUUUU UU3

2

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 33

2

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1476()/ARC-201 RECEIVER/TRANSMITTER (SINCGARS)

U UUUUUUUU UU 11

3

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1476()/ARC-201 RECEIVER/TRANSMITTER (SINCGARS)

U UUUUUUUU UU1

3

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1Z-AHP VOICE SECURITY CONTROL (Z-AHP/KY58)

U UUUUUUUU UU1

4

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1Z-AHP VOICE SECURITY CONTROL (Z-AHP/KY58)

U UUUUUUUU UU 11

4

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1518C/ARC-164 RECEIVER/TRANSMITTER (UHF)

U UUUUUUUU UU 11

5

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1518C/ARC-164 RECEIVER/TRANSMITTER (UHF)

U UUUUUUUU UU1

5

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1354B/ARC-186 RECEIVER/TRANSMITTER (VHF)

U UUUUUUUU UU1

6

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1354B/ARC-186 RECEIVER/TRANSMITTER (VHF)

U UUUUUUUU UU 11

6

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1C-12436/URC, HF CONTROL DISPLAY UNIT

U UUUUUUUU UU 11

7

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1C-12436/URC, HF CONTROL DISPLAY UNIT

U UUUUUUUU UU1

7

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ON616650 TSEC/KY-100 REMOTE CONTROL UNIT

U UUUUUUUU UU1

8

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


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

AIRCRAFT INVENTORY RECORDDA FORM 2408-17, NOV 1991



9200307 CH-47D


Page 2 of 39

1ON616650 TSEC/KY-100 REMOTE CONTROL UNIT

U UUUUUUUU UU 11

8

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1C-7392A/ARN-89 ADF CONTROL

U UUUUUUUU UU 11

9

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU1

9

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1C-10048C/ARN-123(V) VOR CONTROL

U UUUUUUUU UU1

10

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1C-10048C/ARN-123(V) VOR CONTROL

U UUUUUUUU UU 11

10

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CP-1252C/ASN-128D COMPUTER DISPLAY UNIT (GPS)

U UUUUUUUU UU 11

11

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CP-1252C/ASN-128D COMPUTER DISPLAY UNIT (GPS)

U UUUUUUUU UU1

11

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1C-12664/APX-118 REMOTE CONTORL UNIT (TRANSPONDER)

U UUUUUUUU UU1

12

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1C-12664/APX-118 REMOTE CONTORL UNIT (TRANSPONDER)

U UUUUUUUU UU 11

12

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0AN/APX-100 RECEIVER/TRANSMITTER (IF INSTALLED)

U UUUUUUUU UU 00

13

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1115()/APN-209(V) RECVR/TRANS (PILOTS RADAR ALT)

U UUUUUUUU UU 11

14

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1115()/APN-209(V) RECVR/TRANS (PILOTS RADAR ALT)

U UUUUUUUU UU1

14

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ID-1917()/APN-209(V) REM. IND. (COPILOTS RADAR ALT)

U UUUUUUUU UU1

15

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ID-1917()/APN-209(V) REM. IND. (COPILOTS RADAR ALT)

U UUUUUUUU UU 11

15

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1C-11308/APR-39A(V) RADAR CONTROL UNIT

U UUUUUUUU UU 11

16

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 3 of 39

1C-11308/APR-39A(V) RADAR CONTROL UNIT

U UUUUUUUU UU1

16

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1IP-1150A/APR-39(V) RADAR INDICATOR (DIGITAL)

U UUUUUUUU UU1

17

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1IP-1150A/APR-39(V) RADAR INDICATOR (DIGITAL)

U UUUUUUUU UU 11

17

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0C-10131/ALQ-156 COUNTERMEASURES CONTROL UNIT

U UUUUUUUU UU 00

18

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CMWS MISC CONTROL PANEL P3I

U UUUUUUUU UU 10

19

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CMWS MISC CONTROL PANEL P3I

U UUUUUUUU UU1

19

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CMWS DIGITAL CONTROL DISPLAY UNIT (DCDU)

U UUUUUUUU UU 11

20

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1C-12293/AVS-7 CONVERTER CONTROL UNIT (HUD)

U UUUUUUUU UU 01

21

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1C-12293/AVS-7 CONVERTER CONTROL UNIT (HUD)

U UUUUUUUU UU1

21

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SIDE ARMOR PANEL,1560-CH47-267-103 (COPILOTS LWR LEG)

U UUUUUUUU UU1

22

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SIDE ARMOR PANEL,1560-CH47-267-103 (COPILOTS LWR LEG)

U UUUUUUUU UU 11

22

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SIDE ARMOR PANEL, 1560-CH47-267-104 (PILOTS LWR LEG)

U UUUUUUUU UU 11

23

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SIDE ARMOR PANEL, 1560-CH47-267-104 (PILOTS LWR LEG)

U UUUUUUUU UU1

23

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SHOULDER ARMOR PANEL, 1560-CH47-277-103 (COPILOTS)

U UUUUUUUU UU1

24

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SHOULDER ARMOR PANEL, 1560-CH47-277-103 (COPILOTS)

U UUUUUUUU UU 11

24

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 4 of 39

1SHOULDER ARMOR PANEL, 1560-CH47-277-104 (PILOTS)

U UUUUUUUU UU 11

25

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SHOULDER ARMOR PANEL, 1560-CH47-277-104 (PILOTS)

U UUUUUUUU UU1

25

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2BOTTOM ARMOR PANEL, 1560-CH47-301-1 (LARGE PANELS)

U UUUUUUUU UU2

26

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2BOTTOM ARMOR PANEL, 1560-CH47-301-1 (LARGE PANELS)

U UUUUUUUU UU 22

26

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2BOTTOM ARMOR PANEL, 1560-CH47-302-1 (SMALL PANELS)

U UUUUUUUU UU 22

27

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2BOTTOM ARMOR PANEL, 1560-CH47-302-1 (SMALL PANELS)

U UUUUUUUU UU2

27

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2BACK ARMOR PANEL, 1560-CH47-303-1

U UUUUUUUU UU2

28

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2BACK ARMOR PANEL, 1560-CH47-303-1

U UUUUUUUU UU 22

28

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2SU-180/AVS-7 DISPLAY UNIT(EYE OPTIC)

U UUUUUUUU UU 22

29

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2SU-180/AVS-7 DISPLAY UNIT(EYE OPTIC)

U UUUUUUUU UU2

29

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRST AID KIT, AERONAUTIC

U UUUUUUUU UU1

30

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

30

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP COMMANDER SEAT, 114ES011-3

U UUUUUUUU UU 11

31

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP COMMANDER SEAT, 114ES011-3

U UUUUUUUU UU1

31

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP COMMANDER SEAT CUSHION, 114E4088

U UUUUUUUU UU1

32

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 5 of 39

1TROOP COMMANDER SEAT CUSHION, 114E4088

U UUUUUUUU UU 11

32

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP COMMANDER SEAT BELT, 9841781-3

U UUUUUUUU UU 11

33

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP COMMANDER SEAT BELT, 9841781-3

U UUUUUUUU UU1

33

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AM-7189A/ARC IFM AMPLIFIER (AVX CLOSET)

U UUUUUUUU UU1

34

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AM-7189A/ARC IFM AMPLIFIER (AVX CLOSET)

U UUUUUUUU UU 11

34

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1TSEC/KY-58 VOICE SECURITY PROCESSOR (AVX CLOSET)

U UUUUUUUU UU 11

35

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1TSEC/KY-58 VOICE SECURITY PROCESSOR (AVX CLOSET)

U UUUUUUUU UU1

35

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1749/URC RECEIVER/TRANSMITTER (AVX CLOSET)

U UUUUUUUU UU1

36

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1749/URC RECEIVER/TRANSMITTER (AVX CLOSET)

U UUUUUUUU UU 11

36

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AM-7531/URC POWER AMPLIFIER COUPLER (AVX CLOSET)

U UUUUUUUU UU 11

37

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AM-7531/URC POWER AMPLIFIER COUPLER (AVX CLOSET)

U UUUUUUUU UU1

37

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ON616604 TSEC/KY-100 PROCESSOR (AVX CLOSET)

U UUUUUUUU UU1

38

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ON616604 TSEC/KY-100 PROCESSOR (AVX CLOSET)

U UUUUUUUU UU 11

38

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1R-1496A/ARN-89 ADF RECEIVER (AVX CLOSET)

U UUUUUUUU UU 11

39

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1R-1496A/ARN-89 ADF RECEIVER (AVX CLOSET)

U UUUUUUUU UU1

39

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 6 of 39

1AN/ARN-123 VOR/ILS RECEIVER (AVX CLOSET)

U UUUUUUUU UU1

40

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AN/ARN-123 VOR/ILS RECEIVER (AVX CLOSET)

U UUUUUUUU UU 11

40

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CV-3338A/ASN-128D GPS SDC (AVX CLOSET)

U UUUUUUUU UU 00

41

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CV-3338A/ASN-128D GPS SDC (AVX CLOSET)

U UUUUUUUU UU1

41

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1836/APX-118(V) RECVR/TRANS (IFF,AVX CLOSET)

U UUUUUUUU UU1

42

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1836/APX-118(V) RECVR/TRANS (IFF,AVX CLOSET)

U UUUUUUUU UU 11

42

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1MSPU STACK UP

U UUUUUUUU UU 10

43

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1MSPU STACK UP

U UUUUUUUU UU1

43

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CP-1597A/APR-39A(V) DIGITAL PROCESSOR (AVX CLOSET)

U UUUUUUUU UU1

44

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CP-1597A/APR-39A(V) DIGITAL PROCESSOR (AVX CLOSET)

U UUUUUUUU UU 11

44

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1MSPU QAR

U UUUUUUUU UU 00

45

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1MSPU QAR

U UUUUUUUU UU1

45

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1C-12510/AAR-57(V) CMWS ECU (AVX CLOSET)

U UUUUUUUU UU 01

46

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CV-4229(V)7/AVS-7 HUD SDC (AVX CLOSET)

U UUUUUUUU UU 11

47

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CV-4229(V)7/AVS-7 HUD SDC (AVX CLOSET)

U UUUUUUUU UU1

47

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 7 of 39

2TACKLE BLOCK, 114E0658-23

U UUUUUUUU UU2

48

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2TACKLE BLOCK, 114E0658-23

U UUUUUUUU UU 21

48

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1HOOK AND CABLE ASSEMBLY, 114E6042-15

U UUUUUUUU UU 12

49

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1HOOK AND CABLE ASSEMBLY, 114E6042-15

U UUUUUUUU UU1

49

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RESCUE BLOCK, 114E6050-39

U UUUUUUUU UU1

50

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RESCUE BLOCK, 114E6050-39

U UUUUUUUU UU 11

50

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1HOIST OPERATORS HARNESS

U UUUUUUUU UU 11

51

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1HOIST OPERATORS HARNESS

U UUUUUUUU UU1

51

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1GUARD ASSEMBLY

U UUUUUUUU UU1

52

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1GUARD ASSEMBLY

U UUUUUUUU UU 11

52

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-2218/APR-39A(V) RADAR RECVR (NOSE COMPARTMENT)

U UUUUUUUU UU 11

53

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-2218/APR-39A(V) RADAR RECVR (NOSE COMPARTMENT)

U UUUUUUUU UU1

53

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3549A/APR-39 L/H SPIRAL ANT. (EXT. NOSE AREA)

U UUUUUUUU UU1

54

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3549A/APR-39 L/H SPIRAL ANT. (EXT. NOSE AREA)

U UUUUUUUU UU 11

54

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3548A/APR-39 R/H SPIRAL ANT. (EXT. NOSE AREA)

U UUUUUUUU UU 11

55

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 8 of 39

1AS-3548A/APR-39 R/H SPIRAL ANT. (EXT. NOSE AREA)

U UUUUUUUU UU1

55

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2SU-202/AAR-57(V) EOMS (EXT. L&R SIDE, FWD PYLON)

U UUUUUUUU UU 02

56

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1NCS MAGNUS TABLET COMPUTER LOGBOOK

U UUUUUUUU UU 11

57

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPUTER LOGBOOK

U UUUUUUUU UU1

57

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT 1193A/ASN-128D (ANT)

U UUUUUUUU UU1

58

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT 1193A/ASN-128D (ANT)

U UUUUUUUU UU 11

58

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ELT EBC-406HM (OUTBOARD SIDE OF AVIONICS CLOSET)

U UUUUUUUU UU 11

59

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ELT EBC-406HM (OUTBOARD SIDE OF AVIONICS CLOSET)

U UUUUUUUU UU1

59

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SINCGARS ANTENNAS 3939/ARC (BOTTOM)

U UUUUUUUU UU1

60

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SINCGARS ANTENNAS 3939/ARC (BOTTOM)

U UUUUUUUU UU 11

60

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS DTM RECEPTACLE

U UUUUUUUU UU 11

61

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS DTM RECEPTACLE

U UUUUUUUU UU1

61

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0DELETED

U UUUUUUUU UU 00

62

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0DELETED

U UUUUUUUU UU 00

63

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0DELETED

U UUUUUUUU UU 01

64

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 9 of 39

0DELETED

U UUUUUUUU UU 01

65

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0DELETED

U UUUUUUUU UU 00

66

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0DELETED

U UUUUUUUU UU 01

67

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0DELETED

U UUUUUUUU UU 01

68

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0DELETED

U UUUUUUUU UU 01

69

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0DELETED

U UUUUUUUU UU 01

70

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0DELETED

U UUUUUUUU UU 01

71

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0DELETED

U UUUUUUUU UU 01

72

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AIR DATA TRANSDUCER (HUD) (AVIONICS CLOSET BELOW SHELF 3)

U UUUUUUUU UU 11

73

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AIR DATA TRANSDUCER (HUD) (AVIONICS CLOSET BELOW SHELF 3)

U UUUUUUUU UU1

73

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AM-7189A/ARC IFM AMPLIFIER

U UUUUUUUU UU 12

74

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1TSEC/KY-58 VOICE SECURITY PROCESSOR

U UUUUUUUU UU 11

75

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1R-1496A/ARN-89 ADF RECEIVER

U UUUUUUUU UU 11

76

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AN/ARN-123 VOR/ILS RECEIVER

U UUUUUUUU UU 11

77

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0KIT-1C IFF COMPUTER (IF INSTALLED)

U UUUUUUUU UU 00

78

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 10 of 39

1CP-1597A/APR-39A (V) DIGITAL PROCESSOR (IF INSTALLED)

U UUUUUUUU UU 11

79

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1220B/ ALQ-156 RECEIVER/TRANSMITTER (IF INSTALLED)

U UUUUUUUU UU 00

80

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1R-2218/ APR-39A (V) RADAR RECEIVER (IF INSTALLED)

U UUUUUUUU UU 11

81

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3549A/ APR-39 L/H SPIRAL ANTENNA (IF INSTALLED)

U UUUUUUUU UU 21

82

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3548A/ APR-39 R/H SPIRAL ANTENNA (IF INSTALLED)

U UUUUUUUU UU 21

83

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0SU-202/ AAR-57 (V) ELECT OPTIC MSL SENSOR (IF INSTALLED)

U UUUUUUUU UU 02

84

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1NCS MAGNUS TABLET COMPUTER LOGBOOK

U UUUUUUUU UU 11

85

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1Z-AHP VOICE SECURITY CONTROL (KY-58)

U UUUUUUUU UU 11

86

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1518C/ARC-164 RECEIVER TRANSMITTER

U UUUUUUUU UU 11

87

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT-1354B/ARC-186 RECEIVER TRANSMITTER

U UUUUUUUU UU 11

88

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1C-12436/URC,HF CONTROL DISPLAY UNIT

U UUUUUUUU UU 11

89

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2ANTENNA AS-2595/APN-194

U UUUUUUUU UU 22

90

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2ANTENNA AS-2595/APN-194

U UUUUUUUU UU2

90

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA AS-1922/ARC

U UUUUUUUU UU1

91

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA AS-1922/ARC

U UUUUUUUU UU 11

91

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 11 of 39

1ANTENNA AS-2890/APR-39

U UUUUUUUU UU 11

92

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA AS-2890/APR-39

U UUUUUUUU UU1

92

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1DOPPLER NAVIGATION SYSTEM CV-3338/ASN-128

U UUUUUUUU UU 00

93

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CP-1252C/ASN-128D COMPUTER DISPLAY UNIT

U UUUUUUUU UU 11

94

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT 1193A/ASN-128D

U UUUUUUUU UU 11

95

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

96

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CV-3338A/ASN-128D SIGNAL DATA CONVERTER

U UUUUUUUU UU 11

97

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER




SECTION B - CABIN AREACH-47D_BASELINE


9200307 CH-47D


Page 12 of 39

1FIRE EXTINGUISHER, CF3BR, 10501725

U UUUUUUUU UU 11

1

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU1

1

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1DOOR AND EXIT LOCKS (SET)

U UUUUUUUU UU1

2

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1DOOR AND EXIT LOCKS (SET)

U UUUUUUUU UU 11

2

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2EMERGENCY EXIT LIGHTS

U UUUUUUUU UU 22

3

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2EMERGENCY EXIT LIGHTS

U UUUUUUUU UU2

3

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANCHOR LINE ASSY, 114E5139-6

U UUUUUUUU UU1

4

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANCHOR LINE ASSY, 114E5139-6

U UUUUUUUU UU 11

4

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2FOOT SWITCHES WITH CABLE, GUNNER

U UUUUUUUU UU 00

5

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2FOOT SWITCHES WITH CABLE, GUNNER

U UUUUUUUU UU2

5

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU2

6

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 22

6

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 66

7

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU6

7

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


10TROOP SEAT (3 MAN)

U UUUUUUUU UU10

8

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 13 of 39

10TROOP SEAT (3 MAN)

U UUUUUUUU UU 1010

8

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2TROOP SEAT (1 MAN)

U UUUUUUUU UU 22

9

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2TROOP SEAT (1 MAN)

U UUUUUUUU UU2

9

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


32BELT TROOP SAFETY

U UUUUUUUU UU32

10

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


32BELT TROOP SAFETY

U UUUUUUUU UU 3233

10

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AXE, EMERGENCY ESCAPE

U UUUUUUUU UU 11

11

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AXE, EMERGENCY ESCAPE

U UUUUUUUU UU1

11

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1WINCH CONTROL GRIP AND CORD ASSEMBLY

U UUUUUUUU UU1

12

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

12

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRANK ASSY. EMERGENCY RAMP & RESCUE

U UUUUUUUU UU 11

13

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU1

13

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1PROBE POLE, CARGO LOADING

U UUUUUUUU UU1

14

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

14

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1EAWIS IAIU (STA. 168)

U UUUUUUUU UU 11

15

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1EAWIS IAIU (STA. 168)

U UUUUUUUU UU1

15

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 14 of 39

3114ES290-1REMOTE FIRING SWITCH, 14 FT (IF INSTALLED)

U UUUUUUUU UU3

16

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


3114ES290-1REMOTE FIRING SWITCH, 14 FT (IF INSTALLED)

U UUUUUUUU UU 33

16

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1PIF01249-1REMOTE FIRING SWITCH, 22 FT (IF INSTALLED)

U UUUUUUUU UU 11

17

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1PIF01249-1REMOTE FIRING SWITCH, 22 FT (IF INSTALLED)

U UUUUUUUU UU1

17

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2SA-2669/ALE-47(V) SEQUENCERS(L/H STA 430 & R/H STA 411)

U UUUUUUUU UU 22

18

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


4D-61/ALQ-212(V) AN/AAR-57(V) DISP. ASSY (EXT. L&R STA 400)

U UUUUUUUU UU 44

19

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


4196405-001 AN/AAR-57(V) PAYLOAD MOD. (EXT. L&R STA 400)

U UUUUUUUU UU 44

20

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ID-1917 ()/APN-209(V) REM. IND. (LOADMASTER)

U UUUUUUUU UU 12

21

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ID-1917 ()/APN-209(V) REM. IND. (LOADMASTER)

U UUUUUUUU UU1

21

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-2890/APR-39 BLADE ANTENNA (EXT. BOTTOM STA 99)

U UUUUUUUU UU1

22

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-2890/APR-39 BLADE ANTENNA (EXT. BOTTOM STA 99)

U UUUUUUUU UU 11

22

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER, OIL COOLER INLET, 145G0001-1 (FWD PYLON, TOP)

U UUUUUUUU UU 11

23

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER, OIL COOLER INLET, 145G0001-1 (FWD PYLON, TOP)

U UUUUUUUU UU1

23

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER ENGINE AIR OUTLET, 114G1323-1 (TAILCONE COVER)

U UUUUUUUU UU2

24

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER ENGINE AIR OUTLET, 114G1323-1 (TAILCONE COVER)

U UUUUUUUU UU 22

24

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 15 of 39

2COVER ENGINE INLET, 219G1001-1 (FOD SCREEN COVERS)

U UUUUUUUU UU 22

25

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER ENGINE INLET, 219G1001-1 (FOD SCREEN COVERS)

U UUUUUUUU UU2

25

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER ENGINE INLET, 114G1206-1 (DOUGHNUTS)

U UUUUUUUU UU2

26

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER ENGINE INLET, 114G1206-1 (DOUGHNUTS)

U UUUUUUUU UU 22

26

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER, OIL COOLER EXHAUST, 145G0002-5 (FWD PYLON, L/H SIDE)

U UUUUUUUU UU 11

27

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER PITOT TUBE, 114E5040-33

U UUUUUUUU UU 22

28

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU2

28

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER, OIL COOLER EXHAUST, 145G0002-6 (FWD PYLON, R/H SIDE)

U UUUUUUUU UU 11

29

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER, COCKPIT ENCLOSURE, 145G0006-1

U UUUUUUUU UU 11

30

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU1

30

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER HYDRAULIC COOL EXHAUST, 145G0004-1 (AFT PYLON, TOP)

U UUUUUUUU UU1

31

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER HYDRAULIC COOL EXHAUST, 145G0004-1 (AFT PYLON, TOP)

U UUUUUUUU UU 11

31

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER ROTOR HUB FWD & AFT, 114G1023-25

U UUUUUUUU UU 22

32

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU2

32

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER HEATER, 114G1024-1 (INTAKE)

U UUUUUUUU UU1

33

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 16 of 39

1COVER HEATER, 114G1024-1 (INTAKE)

U UUUUUUUU UU 11

33

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER HEATER EXHAUST, 114G1025-1

U UUUUUUUU UU 11

34

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU1

34

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER APU EXHAUST, 145G0005-1

U UUUUUUUU UU1

35

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

35

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER, AIR INLET, 145G0003-1 (CLAMSHELL DOOR COVER)

U UUUUUUUU UU 11

36

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER, AIR INLET, 145G0003-1 (CLAMSHELL DOOR COVER)

U UUUUUUUU UU1

36

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0RAMP EXTENSION, 1560CH-47-4000-1

U UUUUUUUU UU 22

37

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RAMP SUPPORT, 1560CH-47-398-1

U UUUUUUUU UU 11

38

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RAMP SUPPORT, 1560CH-47-398-1

U UUUUUUUU UU1

38

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


6BLADE ANCHOR (ROPES)

U UUUUUUUU UU6

39

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


6BLADE ANCHOR (ROPES)

U UUUUUUUU UU 66

39

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


8TIEDOWN CHAINS TYPE MB-1

U UUUUUUUU UU 88

40

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU8

40

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


32TIEDOWN STRAPS TYPE CGU1/B

U UUUUUUUU UU32

41

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 17 of 39


U UUUUUUUU UU 3232

41

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


4SPACER SET RIGGING (ACTUATOR BLOCK), 114E5900-17

U UUUUUUUU UU 44

42

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU4

42

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


6PIN, GROUND SAFETY BLADE, 114E5897-13 (LOCKOUT PINS)

U UUUUUUUU UU6

43

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


6PIN, GROUND SAFETY BLADE, 114E5897-13 (LOCKOUT PINS)

U UUUUUUUU UU 66

43

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2ATTACHMENT FITTINGS, TRANS. W/ BOLT, 65-SSMAC-C-0095

U UUUUUUUU UU 22

44

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2ATTACHMENT FITTINGS, TRANS. W/ BOLT, 65-SSMAC-C-0095

U UUUUUUUU UU2

44

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1INTERCOM CORD, 50 FT

U UUUUUUUU UU1

45

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

45

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1WINCH/HOIST OPERATOR INTERCOM CORD

U UUUUUUUU UU 11

46

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS ANTENNA

U UUUUUUUU UU 11

47

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS ANTENNA

U UUUUUUUU UU1

47

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SU-202/AAR-57(V) 5TH EOMS (EXT. BOTTOM, FWD OF RAMP)

U UUUUUUUU UU 01

48

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2CONVERTER CONTROL

U UUUUUUUU UU 22

49

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


3BASE SHROUD (145R2215-4)

U UUUUUUUU UU 31

50

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 18 of 39

3BASE SHROUD (145R2215-4)

U UUUUUUUU UU3

50

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


3SHROUD ASSY DROOP (145R2215-11)

U UUUUUUUU UU3

51

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


3SHROUD ASSY DROOP (145R2215-11)

U UUUUUUUU UU 31

51

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRASH WORTHY CREW CHIEF SEAT (CCCS) 349D790-1

U UUUUUUUU UU 11

52

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRASH WORTHY CREW CHIEF SEAT (CCCS) 349D790-1

U UUUUUUUU UU1

52

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1M-24 LEFT MOUNT ASSY P/N 11699655

U UUUUUUUU UU1

53

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1M-24 LEFT MOUNT ASSY P/N 11699655

U UUUUUUUU UU 11

53

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1M-24 RIGHT MOUNT ASSY P/N 11699658

U UUUUUUUU UU 11

54

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1M-24 RIGHT MOUNT ASSY P/N 11699658

U UUUUUUUU UU1

54

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1M-41 REAR RAMP MOUNT ASSY P/N 8436675

U UUUUUUUU UU1

55

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1M-41 REAR RAMP MOUNT ASSY P/N 8436675

U UUUUUUUU UU 11

55

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


5AIR WARRIOR B-KIT (MICROCLIMATE)

U UUUUUUUU UU 00

56

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


5AIR WARRIOR B-KIT (MICROCLIMATE)

U UUUUUUUU UU5

56

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0AS-3149/ ALQ-156 COUNTERMEASURES ANTENNA

U UUUUUUUU UU 02

57

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-2890/ APR-39 BLADE ANTENNA

U UUUUUUUU UU 11

58

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 19 of 39

0SPACER SET RIGGING (ACTUATOR BLOCK) 114E5900-17

U UUUUUUUU UU 01

59

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0PIN, GROUND SAFETY BLADE BLOCKING, 114E5897-13

U UUUUUUUU UU 06

60

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0ATTACHMENT FITTINGS, TRANSPORT WITH BOLT

U UUUUUUUU UU 22

61

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

62

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU1

62

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1WINCH/ HOIST OPERATOR INTERCOM CORD

U UUUUUUUU UU1

63

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1WINCH/ HOIST OPERATOR INTERCOM CORD

U UUUUUUUU UU 11

63

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0COVER ENGINE INLET RING TYPE 114G1206-1

U UUUUUUUU UU 00

64

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0COVER ENGINE INLET WITHOUT SCREENS

U UUUUUUUU UU 02

65

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SLAB BATTERY PN D856511-1

U UUUUUUUU UU 11

66

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SLAB BATTERY PN D856511-1

U UUUUUUUU UU1

66

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRASH WORTHY CREW CHIEF SEAT (CCCS) 349D790-1 (LEFT SIDE)

U UUUUUUUU UU1

67

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRASH WORTHY CREW CHIEF SEAT (CCCS) 349D790-1 (LEFT SIDE)

U UUUUUUUU UU 12

67

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1DROOP STOP SHROUD ASSEMBLY STORAGE BAG 145E5001-10

U UUUUUUUU UU 11

68

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU1

68

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 20 of 39

1GPS ANTENNA 22433-40 GPS-128B

U UUUUUUUU UU 11

69

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SINCGARS ANTENNAS AS 3939/ARC (TOP)

U UUUUUUUU UU 11

70

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0BLANK

U UUUUUUUU UU 00

71

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CMWS SEQUENCER R/H (#2) SN _________________

U UUUUUUUU UU 01

72

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1IVHMS IVHMU P/N 30279-0202 (OR 30279-0402)

U UUUUUUUU UU 10

73

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2TRANSMITTER, INFRARED T-1678/ALQ-212(V) ATIRCM (MBL)

U UUUUUUUU UU 02

74

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2LASER, DIRECTIONAL ASSY, SU-241/ALQ-212(V) ATIRCM (IRJH)

U UUUUUUUU UU 02

75

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2CONTROL TRANSMITTER, COUNTERMEASURE C-12794/ALQ-212(V)ATIRCM (JHCU)

U UUUUUUUU UU 02

76

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2OPTICAL ASSY, LASER, ATIRCM (COUPLER)

U UUUUUUUU UU 02

77

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER




SECTION C - RAMP AREACH-47D_BASELINE


9200307 CH-47D


Page 21 of 39


U UUUUUUUU UU 11

1

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU1

1

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


09311431 M-130 ELECTRONIC MODULE (IF INSTALLED)

U UUUUUUUU UU 00

2

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


09311434 M-130 DISPENSER ASSEMBLY (IF INSTALLED)

U UUUUUUUU UU 00

3

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


09311451 M-130 PAYLOAD MODULE (IF INSTALLED)

U UUUUUUUU UU 00

4

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0186220-001 AN/ALE-47 DISPENSER ASSY (IF INSTALLED)

U UUUUUUUU UU 04

5

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0185470-0001/0002 AN/ALE-47 PAYLOAD MOD (IF INSTALLED

U UUUUUUUU UU 02

6

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2SA-2669/ALE-47(V) SEQUENCERS (USED W/CMWS, L&R SIDE STA 544)

U UUUUUUUU UU 22

7

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SA-2671/ALE-47(V) SAFETY SWITCH (USED W/CMWS)

U UUUUUUUU UU 11

8

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SA-2671/ALE-47(V) SAFETY SWITCH (USED W/CMWS)

U UUUUUUUU UU1

8

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1135947-0001 AN/ALE-47(V) SAFETY FLAG (USED W/CMWS)

U UUUUUUUU UU1

9

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1135947-0001 AN/ALE-47(V) SAFETY FLAG (USED W/CMWS)

U UUUUUUUU UU 11

9

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


4D-61/ALQ-212(V) AN/AAR-57(V) DISP. ASSY (EXT. L&R SIDE RAMP)

U UUUUUUUU UU 44

10

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


4196405-001 AN/AAR-57(V) PAYLOAD MOD (EXT. L&R SIDE RAMP)

U UUUUUUUU UU 44

11

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

12

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 22 of 39


U UUUUUUUU UU1

12

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1EMERGENCY EXIT LIGHT

U UUUUUUUU UU1

13

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1EMERGENCY EXIT LIGHT

U UUUUUUUU UU 11

13

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

14

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CD-45(V)/ALE-47(V) PROGRAMMER (IF INSTALLED)

U UUUUUUUU UU 11

15

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


3114ES290-1REMOTE FIRING SWITCH, 14 FT (IF INSTALLE

U UUUUUUUU UU 33

16

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1PIF01249-1REMOTE FIRING SWITCH, 22 FT (IF INSTALLE

U UUUUUUUU UU 12

17

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2SA-2669/ALE-47(V) SEQUENCERS (IF INSTALLED)

U UUUUUUUU UU 02

18

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


4D-61/ALQ-212(V) AN/AAR-57(V) DISPENSER ASSY CMWS (IFINSTALLED

U UUUUUUUU UU 04

19

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


4196405-001 AN/AAR-57(V) PAYLOAD MODULE CMWS (IF INSTALLED)

U UUUUUUUU UU 04

20

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2AS-3149/ALQ-156 COUNTERMEASURES ANTENNA

U UUUUUUUU UU 02

21

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-2890/APR-39 BLADE ANTENNA

U UUUUUUUU UU 01

22

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER, OIL COOLER INLET, 145G0001-1

U UUUUUUUU UU 11

23

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER ENGINE AIR OUTLET, 114G1323-2

U UUUUUUUU UU 21

24

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER ENGINE INLET WITH SCREEN, 219G1001-1

U UUUUUUUU UU 21

25

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 23 of 39

2COVER ENGINE INLET WITH WITHOUT SCREENS

U UUUUUUUU UU 21

26

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER, OIL COOLER EXHAUST, 145G0002-5

U UUUUUUUU UU 11

27

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 21

28

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER, OIL COOLER EXHAUST, 145G0002-6

U UUUUUUUU UU 11

29

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

30

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER HYDRAULIC COOL EXHAUST, 145G0004-1

U UUUUUUUU UU 11

31

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 21

32

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER HEATER, 114G1024-1

U UUUUUUUU UU 11

33

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

34

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

35

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER, AW INLET, 14560003-1

U UUUUUUUU UU 11

36

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 23

37

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

38

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


6BLADE ANCHOR

U UUUUUUUU UU 61

39

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 81

40

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 24 of 39


U UUUUUUUU UU 321

41

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 41

42

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


6PIN, GROUND SAFETY BLADE BLOCKING, 114E5897-13

U UUUUUUUU UU 61

43

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2ATTACHMENT FITTINGS, TRANSPORT WITH BOLT 114G1049-

U UUUUUUUU UU 21

44

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

45

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1WINCH/HOIST OPERATOR INTERCOM CORD

U UUUUUUUU UU 11

46

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AIR DAT TRANSDUCER

U UUUUUUUU UU 11

47

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1INCLINOMETER (HUD)

U UUUUUUUU UU 11

48

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2CONVERTER CONTROL

U UUUUUUUU UU 21

49

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1INTERCOM CORD, 50 FT (FE)

U UUUUUUUU UU 11

50

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1INTERCOM CORD, 50 FT (FE)

U UUUUUUUU UU1

50

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2FIRE EXTINGUISH SYSTEM BOTTLES 114PS203-3

U UUUUUUUU UU2

51

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2FIRE EXTINGUISH SYSTEM BOTTLES 114PS203-3

U UUUUUUUU UU 22

51

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


3RAMP EXTENSION 1560CH-47-4000-1

U UUUUUUUU UU 33

52

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


3RAMP EXTENSION 1560CH-47-4000-1

U UUUUUUUU UU3

52

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER




SECTION D - ENGINE AND AFT PYLONAASF #3 PIA IL


9200307 CH-47D


Page 25 of 39

1R-2218/APR-39A(V) RADAR RECEIVER (IN AFT PYLON)

U UUUUUUUU UU1

1

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1R-2218/APR-39A(V) RADAR RECEIVER (IN AFT PYLON)

U UUUUUUUU UU 11

1

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3549A/APR-39 L/H SPIRAL ANTENNA (EXT. AFT PYLON)

U UUUUUUUU UU 11

2

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3549A/APR-39 L/H SPIRAL ANTENNA (EXT. AFT PYLON)

U UUUUUUUU UU1

2

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3548A/APR-39 R/H SPIRAL ANTENNA (EXT. AFT PYLON)

U UUUUUUUU UU1

3

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3548A/APR-39 R/H SPIRAL ANTENNA (EXT. AFT PYLON)

U UUUUUUUU UU 11

3

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2SU-202/AAR-57(V) EOMS (EXT. L&R SIDE, AFT PYLON)

U UUUUUUUU UU 02

4

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


6TYPE AERONAUTIC FIRST AID KIT

U UUUUUUUU UU 61

5

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


3LIGHT ASSEMBLY 114ES247-1

U UUUUUUUU UU 31

6

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2INTERPHONE CONTROL C-6533

U UUUUUUUU UU 21

7

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1BATTERY 145E2089, BB-432B/A (NICAD)

U UUUUUUUU UU 10

8

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1MARKER BEACON ANTENNA AT-640/ARN

U UUUUUUUU UU 11

9

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1MARKER BEACON ANTENNA AT-640/ARN

U UUUUUUUU UU1

9

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


10TROOP SEAT TYPE 3 MAN

U UUUUUUUU UU 101

10

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


3TROOP SEAT TYPE 1 MAN

U UUUUUUUU UU 31

11

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


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33BELT SAFETY TROOP

U UUUUUUUU UU 331

12

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


8TIEDOWN FITTINGS 10,000LB

U UUUUUUUU UU 81

13

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


8TIEDOWN FITTINGS 10,000LB

U UUUUUUUU UU8

13

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1PROBE POLE, CARGO HOOK UP

U UUUUUUUU UU 11

14

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

15

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

16

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2ANTENNA AS-2595/APN-194 (V)

U UUUUUUUU UU 21

17

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1145G0006-1 COVER, COCKPIT ENCLOSURE

U UUUUUUUU UU 11

18

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1114G1025-1 COVER HEATER EXHAUST

U UUUUUUUU UU 11

19

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER HEATER 114G1024-1

U UUUUUUUU UU 11

20

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER PITOT TUBE (114E5040-33)

U UUUUUUUU UU 21

21

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1145G0001-1 FWD. PYLON INTAKE COVER

U UUUUUUUU UU 11

22

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2114G1323-1 COVER ENGINE OUTLET

U UUUUUUUU UU 21

23

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2219G1001-1 COVER ENGINE INLET

U UUUUUUUU UU 21

24

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2PROTECTIVE RING ASSY. ENGINE INLET-114G1206

U UUUUUUUU UU 21

25

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


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1145G0004-1 COVER AFT. PYLON EXHAUST

U UUUUUUUU UU 11

26

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1145G0002-5 COVER FWD. PYLON EXHAUST

U UUUUUUUU UU 11

27

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1145G0002-6 COVER FWD. PYLON

U UUUUUUUU UU 11

28

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1145G0003-1 COVER AFT. PYLON

U UUUUUUUU UU 11

29

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1145G0005-1 COVER APU EXHAUST

U UUUUUUUU UU 11

30

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


6BLADE ANCHOR 114E5060-1

U UUUUUUUU UU 61

31

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2114G1023-25 ROTOR HUB COVERS

U UUUUUUUU UU 21

32

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 81

33

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 321

34

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RAMP EXTENSION 114S6003-21

U UUUUUUUU UU 11

35

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2RAMP EXTENSION 1560CH47-400-1

U UUUUUUUU UU 21

36

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2GUNNER FOOTSWITCHES

U UUUUUUUU UU 00

37

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2GUNNER CABLE ASSY.

U UUUUUUUU UU 21

38

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2VHF-AM/FM ANTENNA S65-8280-30

U UUUUUUUU UU 21

39

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA, ADF LOOP

U UUUUUUUU UU 11

40

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


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1ANTENNA, SENSE AS-1869/ARN

U UUUUUUUU UU 11

41

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA, SENSE AS-1869/ARN

U UUUUUUUU UU1

41

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF-AM ANTENNA AT-256( )ARC

U UUUUUUUU UU1

42

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF-AM ANTENNA AT-256( )ARC

U UUUUUUUU UU 11

42

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA AS-1922( )/ARC

U UUUUUUUU UU 11

43

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2IGNITION KEYS

U UUUUUUUU UU 21

44

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2IGNITION KEYS

U UUUUUUUU UU2

44

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1BRACKET & PADLOCK

U UUUUUUUU UU 11

45

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


3DROOP STOP SHROUDS

U UUUUUUUU UU 30

46

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 10

47

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


3DROOP STOP SHIELD 114R2215-11

U UUUUUUUU UU 30

48

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


3DROOP STOP BASE 114R2215-4

U UUUUUUUU UU 30

49

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA ADF AS-2108/ARN-89(LOOP)

U UUUUUUUU UU 11

50

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) FWD PALLET XCVR ASSY(STA. 320)

U UUUUUUUU UU 11

51

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) FWD PALLET XCVR ASSY(STA. 320)

U UUUUUUUU UU1

51

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


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1(BFT) XCVR MOUNT (STA. 320)

U UUUUUUUU UU 11

52

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) KGV-72 (STA. 360)

U UUUUUUUU UU 11

53

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU 11

54

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER



U UUUUUUUU UU1

54

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SINCGARS ANTENNAS AS 3939/ARC (BOTTOM)

U UUUUUUUU UU 11

55

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SLAB BATTERY; PN D8565/11-1

U UUUUUUUU UU 11

56

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1FLUX VALVE (CN-405/ASN)

U UUUUUUUU UU 11

57

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1FLUX VALVE (CN-405/ASN)

U UUUUUUUU UU1

57

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) ANT EIS S/N: ____________

U UUUUUUUU UU1

58

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) ANT EIS S/N: ____________

U UUUUUUUU UU 11

58

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) ANT GPS S/N: ____________

U UUUUUUUU UU 11

59

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) ANT GPS S/N: ____________

U UUUUUUUU UU1

59

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) LOW NOISE AMP (STA. 372)

U UUUUUUUU UU1

60

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) LOW NOISE AMP (STA. 372)

U UUUUUUUU UU 11

60

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) DC/DC CONVERTER (STA. 210)

U UUUUUUUU UU 11

61

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


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1(BFT) DC/DC CONVERTER (STA. 210)

U UUUUUUUU UU1

61

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) PALLET S/N: ____________

U UUUUUUUU UU1

62

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) PALLET S/N: ____________

U UUUUUUUU UU 11

62

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) ROUTER S/N: ________

U UUUUUUUU UU 11

63

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) ROUTER S/N: ________

U UUUUUUUU UU1

63

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) DAGGER S/N: __________

U UUUUUUUU UU1

64

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(BFT) DAGGER S/N: __________

U UUUUUUUU UU 11

64

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(CMWS) SMART DISPENSER LH S/N: __________

U UUUUUUUU UU 01

65

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(CMWS) SMART DISPENSER LH S/N: __________

U UUUUUUUU UU 01

66

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(CMWS) SMART DISPENSER RH S/N: __________

U UUUUUUUU UU 01

67

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(CMWS) SMART DISPENSER RH S/N: __________

U UUUUUUUU UU 01

68

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(CMWS) PAYLOAD MODULE LH S/N: __________

U UUUUUUUU UU 01

69

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(CMWS) PAYLOAD MODULE LH S/N: __________

U UUUUUUUU UU 01

70

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(CMWS) PAYLOAD MODULE RH S/N: __________

U UUUUUUUU UU 01

71

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1(CMWS) PAYLOAD MODULE RH S/N: __________

U UUUUUUUU UU 01

72

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






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0(CMWS) EOMS LH S/N: __________

U UUUUUUUU UU 01

73

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0(CMWS) EOMS RH S/N: __________

U UUUUUUUU UU 01

74

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0(CMWS) SEQUENCERS LH S/N: __________

U UUUUUUUU UU 01

75

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


0(CMWS) SEQUENCERS RH S/N: __________

U UUUUUUUU UU 01

76

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3549A/APR-39 L/H SPIRAL ANTENNA

U UUUUUUUU UU 11

77

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3549A/APR-39 R/H SPIRAL ANTENNA

U UUUUUUUU UU 11

78

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1TRANSMITTER REMOTE COMPASS WITH COMPNS CN-405()/A

U UUUUUUUU UU 11

79

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1TRANSMITTER REMOTE COMPASS WITH COMPNS CN-405()/A

U UUUUUUUU UU 11

80

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2SU-202/AAR-57(V) EOMS (AFT PYLON)

U UUUUUUUU UU 22

81

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER




UNIT UNIQUE INVENTORY ITEMSCH-47D_BASELINE


9200307 CH-47D


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0BLANK

U UUUUUUUU UU 00

1

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ERFS FUEL SAMPLING PUMP KIT 1680-01-474-3324

U UUUUUUUU UU 00

2

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CAVITY DRAIN HOSE 4720-01-424-5554

U UUUUUUUU UU 00

3

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1GROUNDING CABLE 6150-01-398-4389

U UUUUUUUU UU 01

4

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1HARNESS TANK POWER 645-01-380-2981

U UUUUUUUU UU 00

5

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1FUEL HOSE SINGLE POINT PRESSURE REFUELING 4720-01-425-1215

U UUUUUUUU UU 00

6

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1VENT HOSE ASSY 4720-01-471-6739

U UUUUUUUU UU 00

7

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1FUEL HOSE, TANK-TO -ACFT RANGE EXT 4720-01-424-5558

U UUUUUUUU UU 00

8

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1FUEL PROBE ELECTRICAL CABLE 6150-01-475-7634

U UUUUUUUU UU 00

9

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CH-47 ERFS II FUEL CONTROL PANEL P/N HM022-123-51

U UUUUUUUU UU 00

10

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CH-47 ERFS II ROLLER ASSY KIT P/N WOH93JCH-47-T-F-K

U UUUUUUUU UU 00

11

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1EFRS TANK COVER P/N IT765-HMO22-T17-11

U UUUUUUUU UU 00

12

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


4 SURVIVAL KIT READY ACCESS MODULAR (SKRAM) STA. 280 & 400(L/H & R/H)

U UUUUUUUU UU 42

13

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


4 SURVIVAL KIT READY ACCESS MODULAR (SKRAM) STA. 280 & 400(L/H & R/H)

U UUUUUUUU UU4

13

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AN/PRC- 117F SATCOM MANPACK RADIO

U UUUUUUUU UU 01

14

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






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1SATCOM RF POWER AMPLIFIER/PREAMLIFIER (SATCOM PALLET)

U UUUUUUUU UU 00

15

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SATCOM POWER SWITCH (SATCOM PALLET)

U UUUUUUUU UU 11

16

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SATCOM POWER SWITCH (SATCOM PALLET)

U UUUUUUUU UU1

16

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SATCOM AUDIO INTERFACE UNIT (SATCOM PALLET)

U UUUUUUUU UU1

17

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SATCOM AUDIO INTERFACE UNIT (SATCOM PALLET)

U UUUUUUUU UU 11

17

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF/SATCOM SWITCH (AVIONICS CLOSET)

U UUUUUUUU UU 11

18

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF/SATCOM SWITCH (AVIONICS CLOSET)

U UUUUUUUU UU1

18

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SATCOM ANTENNA CHELTON 19-430-10P4 (# 3 TUNNEL COVER)

U UUUUUUUU UU1

19

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1SATCOM ANTENNA CHELTON 19-430-10P4 (# 3 TUNNEL COVER)

U UUUUUUUU UU 11

19

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RAD WARN ANT/DETECT [AFT] [LH] AS-3548A/APR-39A(V)

U UUUUUUUU UU 11

20

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1RAD WARN ANT/DETECT [AFT] [RH] AS-3549A/APR-39A(V)

U UUUUUUUU UU 11

21

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CMWS EOMS SENSOR [AFT] [LH] SU-202/AAR-57(V)

U UUUUUUUU UU 11

22

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1CMWS EOMS SENSOR [AFT] [RH] SU-202/AAR-57(V)

U UUUUUUUU UU 11

23

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1C-11308/APR-39A (V) RADAR CONTROL UNIT

U UUUUUUUU UU 11

40

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1IP-1150A/APR-39 (V) RADAR INDICATOR (DIGITAL)

U UUUUUUUU UU 11

41

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


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1Z-AHP VOICE SECURITY CONTROL

U UUUUUUUU UU 11

42

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1C-10131/ALQ-156 COUNTER MEASURES CONTROL UNIT

U UUUUUUUU UU 11

43

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1BLUE FORCE TRACKING-AVN

U UUUUUUUU UU 11

44

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1TSEC/KY-100 REMOTE CONTROL UNIT ON616650

U UUUUUUUU UU 11

45

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


5PLATE ASSY, BLANKING, CMWS EOM PN: LSF00884-001

U UUUUUUUU UU 51

46

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


5PLATE ASSY, BLANKING, CMWS EOM PN: LSF00884-001

U UUUUUUUU UU5

46

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1PLATE ASSY, BLANKING, ATIRCM COOLING FAN L/H UPPER (OVAL)

U UUUUUUUU UU1

47

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1PLATE ASSY, BLANKING, ATIRCM COOLING FAN L/H UPPER (OVAL)

U UUUUUUUU UU 11

47

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1PLATE ASSY, BLANKING, ATIRCM COOLING FAN L/H LOWER(SQUARE)

U UUUUUUUU UU 11

48

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1PLATE ASSY, BLANKING, ATIRCM COOLING FAN L/H LOWER(SQUARE)

U UUUUUUUU UU1

48

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1PLATE ASSY, BLANKING, ATIRCM COOLING FAN R/H UPPER (OVAL)

U UUUUUUUU UU1

49

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1PLATE ASSY, BLANKING, ATIRCM COOLING FAN R/H UPPER (OVAL)

U UUUUUUUU UU 10

49

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1PLATE ASSY, BLANKING, ATIRCM COOLING FAN R/H LOWER(SQUARE)

U UUUUUUUU UU 11

50

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1PLATE ASSY, BLANKING, ATIRCM COOLING FAN R/H LOWER(SQUARE)

U UUUUUUUU UU1

50

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 35 of 39

1FAIRING ASSY, IRJH, ATIRCM L/H UPPER PN: 0056A4022-02

U UUUUUUUU UU1

51

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1FAIRING ASSY, IRJH, ATIRCM L/H UPPER PN: 0056A4022-02

U UUUUUUUU UU 11

51

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1FAIRING ASSY, IRJH, ATIRCM L/H LOWER PN: 0056A4039-01

U UUUUUUUU UU 11

52

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1FAIRING ASSY, IRJH, ATIRCM L/H LOWER PN: 0056A4039-01

U UUUUUUUU UU1

52

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1FAIRING ASSY, IRJH, ATIRCM R/H UPPER PN: 0056A4022-02

U UUUUUUUU UU1

53

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1FAIRING ASSY, IRJH, ATIRCM R/H UPPER PN: 0056A4022-02

U UUUUUUUU UU 11

53

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1FAIRING ASSY, IRJH, ATIRCM R/H LOWER PN: 0056A4039-02

U UUUUUUUU UU 11

54

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1FAIRING ASSY, IRJH, ATIRCM R/H LOWER PN: 0056A4039-02

U UUUUUUUU UU1

54

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1UPPER FAN SUPPORT ASSY, L/H, ATIRCM PN: 0056A3008-10

U UUUUUUUU UU1

55

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1UPPER FAN SUPPORT ASSY, L/H, ATIRCM PN: 0056A3008-10

U UUUUUUUU UU 11

55

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1LOWER FAN SUPPORT ASSY, L/H, ATIRCM PN: 0056A3009-10

U UUUUUUUU UU 11

56

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1LOWER FAN SUPPORT ASSY, L/H, ATIRCM PN: 0056A3009-10

U UUUUUUUU UU1

56

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2DUCT, LOWER FAN, L/H, ATIRCM PN: 0056A4043-01

U UUUUUUUU UU2

57

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2DUCT, LOWER FAN, L/H, ATIRCM PN: 0056A4043-01

U UUUUUUUU UU 22

57

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1UPPER FAN SUPPORT ASSY, R/H, ATIRCM PN: 0056A3008-10

U UUUUUUUU UU 11

58

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 36 of 39

1UPPER FAN SUPPORT ASSY, R/H, ATIRCM PN: 0056A3008-10

U UUUUUUUU UU1

58

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1LOWER FAN SUPPORT ASSY, R/H, ATIRCM PN: 0056A3009-20

U UUUUUUUU UU1

59

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1LOWER FAN SUPPORT ASSY, R/H, ATIRCM PN: 0056A3009-20

U UUUUUUUU UU 10

59

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1DUCT, LOWER FAN, R/H, ATIRCM PN: 0056A4043-02

U UUUUUUUU UU 10

60

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1DUCT, LOWER FAN, R/H, ATIRCM PN: 0056A4043-02

U UUUUUUUU UU1

60

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ACCESS PANEL, R/H, PN: 114S5931-1, INTERCOSTAL AREA AFT OFAUX TANK

U UUUUUUUU UU1

61

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ACCESS PANEL, R/H, PN: 114S5931-1, INTERCOSTAL AREA AFT OFAUX TANK

U UUUUUUUU UU 10

61

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ACCESS PANEL, L/H, PN: 114S5931-2, INTERCOSTAL AREA AFT OFAUX TANK

U UUUUUUUU UU 14

62

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1ACCESS PANEL, L/H, PN: 114S5931-2, INTERCOSTAL AREA AFT OFAUX TANK

U UUUUUUUU UU1

62

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1R-2218/APR-39A(V) RADAR RECEIVER AFT PYLON (IF INSTALLED)

U UUUUUUUU UU 11

63

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3549A/APR-39 L/H SPIRAL ANTENNA (IF INSTALLED)

U UUUUUUUU UU 11

64

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1BOX, OIL STORAGE, RED

U UUUUUUUU UU 11

65

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1BOX, OIL STORAGE, RED

U UUUUUUUU UU1

65

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1STEP LADDER, FIBERGLASS (STA 470)

U UUUUUUUU UU1

66

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER






9200307 CH-47D


Page 37 of 39

1STEP LADDER, FIBERGLASS (STA 470)

U UUUUUUUU UU 11

66

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COCKPIT COVER (BRUCE AIRCRAFT COVERS) W/BAG

U UUUUUUUU UU 11

67

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1BROOM, CORN, FLOOR SWEEPING

U UUUUUUUU UU 11

68

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1BROOM, CORN, FLOOR SWEEPING

U UUUUUUUU UU1

68

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1BLUE FORCE TRACKER L BAND TRANSCEIVER 050280-1

U UUUUUUUU UU 11

69

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1BLUE FORCE TRACKER MICROROUTER 6137658-100

U UUUUUUUU UU 11

70

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER




SECTION ACH-47D_BASELINE


9200307 CH-47D


Page 38 of 39

1DOOR & EXIT LOCKS SET

U UUUUUUUU UU 11

1

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1OIL COOLER INLET COVER

U UUUUUUUU UU 11

2

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2ENG AIR OUTLET COVER

U UUUUUUUU UU 22

3

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2ENG INLET COVER [W/ SCREENS]

U UUUUUUUU UU 22

4

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2ENG INLET COVER [W/O SCREENS]

U UUUUUUUU UU 22

5

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1OIL COOLER EXHAUST COVER

U UUUUUUUU UU 11

6

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2PITOT TUBE COVER

U UUUUUUUU UU 22

7

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1OIL COOLER EXHAUST COVER

U UUUUUUUU UU 11

8

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1COCKPIT ENCLOSURE COVER

U UUUUUUUU UU 11

9

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1HYD COOLER EXHAUST COVER

U UUUUUUUU UU 11

10

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2ROTOR HUB COVER

U UUUUUUUU UU 22

11

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1HEATER INLET COVER

U UUUUUUUU UU 11

12

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1HEATER EXHAUST COVER

U UUUUUUUU UU 11

13

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1APU EXHAUST COVER

U UUUUUUUU UU 11

14

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


1APU INLET COVER

U UUUUUUUU UU 11

15

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER




SECTION ACH-47D_BASELINE


9200307 CH-47D


Page 39 of 39

6BLADE ANCHOR

U UUUUUUUU UU 66

16

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


8TIE DOWN CHAIN [MB1]

U UUUUUUUU UU 88

17

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


32TIE DOWN STRAP [CGU1/B]

U UUUUUUUU UU 3232

18

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


4RIGGING (ACTUATOR BLOCKS) SPACER SET

U UUUUUUUU UU 44

19

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


6BLADE LOCKING PIN

U UUUUUUUU UU 66

20

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2TRANSPORT ATTACHMENT FITTING [W/ BOLT]

U UUUUUUUU UU 22

21

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER


2ENG INLET COVER [W/ EAPS]

U UUUUUUUU UU 22

22

12.11.10.9.8.7.6.5.4.3.2.1.CHECK NUMBER




of 5

9200307HELICOPTER, CARGO CH-47D

7. FREQUENCY 4. 5. ITEM TO BE INSPECTED

2. MODEL 3. SERIAL NUMBER 1. NOMENCLATURE

8.DUE

NEXT 6. REFERENCE 9. COMPLETED ATINSP NO.

A002 29 May 201714TM 1-1520-240-PMS1PREVENTIVE MAINTENANCEDAILY

15 May 2017D

A014 29 May 201714TM 1-1520-240-23 P14 DAY ENGINE RUN REQUIRED 15 May 2017D

A040 4468.525TM 1-1520-240-23 PVISUAL INSPECT OUTBOARDDRIVE SHAFT LUGS ADAPTER

4443.5H

A070 4456.350TB 43-0211#1 ENGINE OIL SAMPLE 4406.3H

A071 4456.350TB 43-0211#2 ENGINE OIL SAMPLE 4406.3H

A072 4507.1400H-47-12-AMAM-02AFT XMSN OIL SAMPLE DUE 4107.1H

A073 4507.1400H-47-12-AMAM-02FWD XMSN OIL SAMPLE DUE 4107.1H

A074 4507.1400H-47-12-AMAM-02#2 ENGINE MECHANICAL XMSNOIL SAMPLE DUE

4107.1H

A075 4507.1400H-47-12-AMAM-02ENGINE COMBINING XMSN OILSAMPLE DUE

4107.1H

A081 4507.1400H-47-12-AMAM-02#1 ENGINE MECHANICAL XMSNOIL SAMPLE DUE

4107.1H

A088 4457.150TM 1-1520-240-23 PPERFORM LUBRICATION IAWLUBRICATION CHARTS

4407.1H

A092 31 May 201730TM 11-6140-203-23 P30 DAY SLAB BATTERYINSPECTION (M8565/11-1)

01 May 2017D

A103 28 May 201730TM 1-1500-344-23AIRCRAFT WASH DUE 28 Apr 2017D

A115 4457.150TM 1-1520-240-23 PPERFORM ENGINE WATERWASH IAW IETM

4407.1H

A128 4468.525TM 1-1520-240-23 P#1 ENGINE DUAL CHIPDETECTOR FOR CONTINUITY

4443.5H

A129 4468.525TM 1-1520-240-23 P#2 ENGINE DUAL CHIPDETECTOR FOR CONTINUITY

4443.5H

A131 4457.150TM 1-1520-240-23 PCOMBINING XMSN COOLER FANVIBRATION TEST

4407.1H

A133 4457.150TM 1-1520-240-23 PAFT XMSN COOLER FANVIBRATION TEST

4407.1H

A145 4454.150TM 55-1520-240-23-1PERFORM 50 HR DATADOWNLOAD ON IVHMS SYSTEM

4404.1H

A155 31 May 201790TM 1-1520-240-PMS4CORROSION CONTROLINSPECTION, ABBREVIATED,MILD

02 Mar 2017D

A170 09 Aug 201790TTS 56578A AWR FORELT

90 DAY/100 HOUR ELT SELF-TEST INSPECTION

11 May 2017D

A170 4539.5100TTS 56578A AWR FORELT

90 DAY/100 HOUR ELT SELF-TEST INSPECTION

4439.5H

A177 13 Jun 201790AR 95-190 DAY REVIEW/UPDATE OF 365-4 ENTRIES

15 Mar 2017D

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, OCT 1997 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

of 5




8.DUE


A180 4506.3100TM 1-1520-240-23 PPERFORM LUBRICATIONREQUIREMENTS IAW LUBECHARTS

4406.3H

A182 4506.3100TM 1-1520-240-23 PINSP FWD AFT SWASHPLATEBEARING IAW SOF CH-47-04-01

4406.3H

A190 4507.1200TM 1-1520-240-23 PINSPECT FWD AFTSWASHPLATE ROTATING RINGCH-47-07-SOF-

4307.1H

A191 4507.1200H47-10-ASAM-075000LB TIE DOWN ADAPTERRINGS INSP

4307.1H

A196 4506.3100TM 1-1520-240-23 P#1 #2 ENGINE XMSN FAIRING 4406.3H

A202 4507.1100TM 1-1520-240-23 PTORQUE CHECK FWD PITCHLINK BOLTS

4407.1H

A204 4506.3100TM 1-1520-240-23 PTORQUE CHECK AFT PITCH LINKBOLTS

4406.3H

A210 4493.550TM 1-1520-240-23 PPERFORM 50 HR ENGINE DECUDOWNLOAD

4443.5H

A216 4506.3100TM 1-1520-240-23 PINSPECT THE COMBINING XMSNCOOLING FAN SHAFT PER TASK

4406.3H

A217 4506.3100TM 1-1520-240-23 PCHECK COMBINING XMSCOOLING FAN SHAFT OUTPUTGEAR SPLIN

4406.3H

A262 4507.1200TM 1-1520-240-23 PINSPECTION OF AFTCONNECTING LINK (TASK 4-37)

4307.1H

A264 4507.1200TM 1-1520-240-23 PPERFORM LUBRICATIONREQUIREMENTS IAW LUBECHARTS

4307.1H

A280 4707.1400TM 1-1520-240-PMS2PERFORM PMS2 CYCLEINSPECTION

4307.1H

A365 25 Jul 201824TM 1-1520-240-23 PINSP HORIZONTAL HINGE PINBEARING (AFT HEAD)

25 Jul 2016M

A366 25 Jul 201824TM 1-1520-240-23 PINSP HORIZONTAL HINGE PINBEARING (FWD HEAD)

25 Jul 2016M

A370 4507.1400TM 1-1520-240-23 PPERFORM LUBRICATIONREQUIREMENT IAW LUBECHART

4107.1H

A380 4507.1400TM 1-1520-240-PMS3PERFORM PMS3 CYCLEINSPECTION

4107.1H

A390 4570.1600TM 1-1520-240-23PEDDY CURRENT NO. 1 FWDMOUNT

3970.1H

A391 4570.1600TM 1-1520-240-23PEDDY CURRENT NO.2 FWDMOUNT

3970.1H

A460 4529.81200TM 1-1520-240-23 PINSPECT FUEL TANKASSEMBLIES

3329.8H

A478 4529.81200TM 1-1520-240-23 PINSPECT FUEL BOOST PUMPPOWER WIRE HARNESS

3329.8H

A496 29 Aug 2017180TM 1-1500-204-23-1CF3BR FIRE EXTINGUISHERWEIGHT TEST & INSPECTION

02 Mar 2017D




of 5




8.DUE


A500 12 Sep 2017180TM 1-1520-240-PMS4CORROSION CONTROLINSPECTION, IN-DEPTH, MILD

16 Mar 2017D

A505 12 Jul 2017360TM 1-1680-377-13 PAMSS SURVIVAL KITINSPECTION

17 Jul 2016D

A520 09 Feb 201812TTS 56578A AWR FORELT

ANNUAL G-SWITCH ELTINSPECTION

09 Feb 2017M

A530 29 May 201712TM 1-1520-240-23 PAIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

29 May 2016M

A532 02 Mar 201812TM 1-1500-204-23-4COMPASS SWING 02 Mar 2017M

A534 02 Nov 201712TM 1-1500-204-23-1FIRST AID KIT INSPECTION 02 Nov 2016M

A553 02 Apr 201812AR 95-1AIRCRAFT WEIGHINGINVENTORY (365-1)

02 Apr 2017M

A558 02 Mar 201812TM 1-1500-204-23-4HSI/RMI FOR CORRECTREADINGS

02 Mar 2017M

A563 24 Sep 201712TM 1-1520-240-23 PENGINE FIRE EXTINGUISHERSYSTEM INSPECTION

24 Sep 2016M

A564 18 Sep 201712TM 1-1520-240-23PENGINE FIRE BOTTLE FORWEIGHT

18 Sep 2016M

A580 01 Feb 201824TM 11-6140-203-23PRETURN SLAB TO AVIM FORCAPACITY CHECK

01 Feb 2016M

A649 02 Apr 202036AR 95-1AIRCRAFT WEIGHING CLASS 1 02 Apr 2017M

A660 05 Jan 201936TM 11-6140-203-23PREPLACEMENT OF BATTERY(SLAB M8565/11-1)

05 Jan 2016M

A670 30 Jun 201960TTS 56578A AWR FORELT

REPLACE ELT BATTERY GS-46 30 Jun 2014M

A690 31 Jul 2026114TB 9-1300-385ENGINE FIRE EXTINGUISHER (#1AFT) MH-92

31 Jan 2017M

A699 31 Jul 2026114TB 9-1300-385ENGINE FIRE EXTINGUISHER (#2AFT) MH-92

31 Jan 2017M

A700 31 Jul 2026114TB 9-1300-385ENGINE FIRE EXTINGUISHER (#1FWD), MH-92

31 Jan 2017M

A710 31 Jul 2026114TB 9-1300-385ENGINE FIRE EXTINGUISHER (#2FWD) MH-92

31 Jan 2017M

A806 62722887TM 1-1520-240-23 O/H& RET. SCHED.

REPLACE FWD ROTARY WINGHUB ASSY (PN 114R2050-35)

3385H

A820 48451200TM 1-1520-240-23&PFWD ROTOR HEAD VERTICALHINGE PIN UPPER BEARINGROTATION DUE

3645H

A821 49621200TM 1-1520-240-23&PFWD ROTOR HEAD VERTICALHINGE PIN LOWER BEARINGROTATION DUE

3762H

A822 60452400TM 1-1520-240-23&PFWD ROTOR HEAD VERTICALHINGE PIN UPPER BEARINGREPLACEMENT DUE

3645H




of 5




8.DUE


A823 51502400TM 1-1520-240-23&PFWD ROTOR HEAD VERTICALHINGE PIN LOWER BEARINGREPLACEMENT DUE

2750H

A825 51071200TM 1-1520-240-23&PFWD ROTOR HEAD HORIZONTALHINGE PIN BEARING ROTATIONDUE

3907H

A826 63072400TM 1-1520-240-23&PFWD ROTOR HEAD HORIZONTALHINGE PIN BEARINGREPLACEMENT DUE

3907H

A829 49621200TM 1-1520-240-23&PFWD ROTOR HEAD HORIZONTALHINGE PIN ROTATION DUE

3762H

A830 63072400TM 1-1520-24-23&PFWD ROTOR HEAD HORIZONTALHINGE PIN REPLACEMENT DUE

3907H

A831 54742700TM 1-1520-24-23&PFWD ROTOR HEAD PITCHBEARING REPLACEMENT DUE

2774H

A832 74244800TM 1-1520-240-23&PFWD ROTOR HEAD TIE BARASSEMBLY REPLACEMENT DUE.

2624H

A833 4837.31200TM 1-1520-240-23&PAFT ROTOR HEAD VERTICALHINGE PIN UPPER BEARINGROTATION DUE

3637.3H

A834 52041200TM 1-1520-240-23&PAFT ROTOR HEAD VERTICALHINGE PIN LOWER BEARINGROTATION DUE

4004H

A835 56132400TM 1-1520-240-23&PAFT ROTOR HEAD VERTICALHINGE PIN UPPER BEARINGREPLACEMENT DUE

3213H

A836 64042400TM 1-1520-240-23&PAFT ROTOR HEAD VERTICALHINGE PIN LOWER BEARINGREPLACEMENT DUE

4004H

A837 52041200TM 1-1520-240-23&PAFT ROTOR HEAD HORIZONTALHINGE PIN BEARING ROTATIONDUE

4004H

A838 64042400TM 1-1520-240-23&PAFT ROTOR HEAD HORIZONTALHINGE PIN BEARINGREPLACEMENT DUE

4004H

A839 59991995TM 1-1520-240-23&PAFT ROTOR HEAD HUBREPLACEMENT DUE

4004H

A840 52041200TM 1-1520-240-23&PAFT ROTOR HEAD HORIZONTALHINGE PIN ROTATION DUE

4004H

A841 64042400TM 1-1520-240-23&PAFT ROTOR HEAD HORIZONTALHINGE PIN REPLACEMENT DUE

4004H

A842 50162700TM 1-1520-240-23&PAFT ROTOR HEAD PITCHBEARING REPLACEMENT DUE

2316H

A843 68254800TM 1-1520-240-23&PAFT ROTOR HEAD TIE BARASSEMBLY REPLACEMENT DUE

2025H

A851 47301200TM 1-1520-240-23&POH&RET SCHED

FWD SWASHPLATE BEARING(P/N 114RS308-2) REPLACEMENTDUE

3530H




of 5




8.DUE


A852 49071200TM 1-1520-240-23&PAFT SWASHPLATE BEARING(P/N 114RS308-2) REPLACEMENTDUE

3707H

E230 09 Aug 201790AED ELT MEMO 24NOV 2002

INSPECT ELT BATTERY 11 May 2017D

E351 21 Sep 20176TM 11-5895-1841-13PREPLACE APX-118TRANSPONDER BATTERY

21 Mar 2017M

E801 21 Sep 20176ETMREPLACE 128D GPS BATTERY 21 Mar 2017M




2-121-090-79 28400147956831365103554 9200307 DISK ASSY, 1ST 1ST 30-Nov-200191547

5. NSN 8. ACCEPT. DATE2. SN 7. STAGE6. CAGE NO.4. NOMENCLATURE3. ACFT1. PART NO

Report Date: Page 1 of 118-May-2017

WHEEL WITH BLADES

(1) b (2)(1)BEFORE GRIND

b (2)

WHEEL WITH BLADESDATE AFTER GRIND

aBEFORE GRINDTIMEDATEAFTER GRINDTIME

WHEEL WHEEL c

WHEEL DIAMETRICAL MEASUREMENTS

a

c

9.

1345 14.586 14.50629-Jan-2009

ABNORMAL TEMPERATURE AND/OR OVERSPEED DATA10.

TEMPERATUREENGINE TimeWHEELREMARKSTIMEDATE TIME Over Limit(Degrees C) SPEED

a b f gc d e

REMOVEDSN

INSTALLATION DATAINSTALLED

DATEc

11.

MODELENGINE

ENG TIME

ACTIVITY

d REASON FOR

(2)W/T

bENG TIME

a (1) (2)

DATE

(1)

REMOVAL

(1) e f(2)

T55GA714AWOMUAA 1653 1345GA75213 23-Feb-2009

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

AIRCRAFT ENGINE TURBINE WHEEL HISTORICAL RECORDDA FORM 2408-19-E, NOV 91

2-121-110-35 284001479568181365101304 9200307 DISK ASSY, 2N 2ND 29-Jan-200991547

5. NSN 8. ACCEPT. DATE2. SN 7. STAGE6. CAGE NO.4. NOMENCLATURE3. ACFT1. PART NO


WHEEL WITH BLADES

(1) b (2)(1)BEFORE GRIND

b (2)

WHEEL WITH BLADESDATE AFTER GRIND

aBEFORE GRINDTIMEDATEAFTER GRINDTIME

WHEEL WHEEL c

WHEEL DIAMETRICAL MEASUREMENTS

a

c

9.

14.918 14.91429-Jan-2009

ABNORMAL TEMPERATURE AND/OR OVERSPEED DATA10.

TEMPERATUREENGINE TimeWHEELREMARKSTIMEDATE TIME Over Limit(Degrees C) SPEED

a b f gc d e

REMOVEDSN

INSTALLATION DATAINSTALLED

DATEc

11.

MODELENGINE

ENG TIME

ACTIVITY

d REASON FOR

(2)W/T

bENG TIME

a (1) (2)

DATE

(1)

REMOVAL

(1) e f(2)

T55GA714AW0MUAA 1653GA75213 23-Feb-2009

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

AIRCRAFT ENGINE TURBINE WHEEL HISTORICAL RECORDDA FORM 2408-19-E, NOV 91

T55-GA-714AENGINE ASSY TURBINE GA75189

ACT/REQALTTSONUMBER °C ACT/REQACT/REQPRESS N1 %ENGSERIAL OAT EGT/TOTTORQUE

10.9.6. AIRCRAFT 7. 8. 13. REMARKS4. DATE 5. BASETORQ

12.11.

3. ENGINE SERIAL NUMBER2. ENGINE MODEL 1. NOMENCLATURE

Page 1 of 1

/ / /


T53/55 TURBINE ENGINE ANALYSIS CHECK RECORDDA FORM 2408-19-1, NOV 1991

T55-GA-714AENGINE ASSY TURBINE GA75213

ACT/REQALTTSONUMBER °C ACT/REQACT/REQPRESS N1 %ENGSERIAL OAT EGT/TOTTORQUE

10.9.6. AIRCRAFT 7. 8. 13. REMARKS4. DATE 5. BASETORQ

12.11.

3. ENGINE SERIAL NUMBER2. ENGINE MODEL 1. NOMENCLATURE

Page 1 of 1

/ / /


T53/55 TURBINE ENGINE ANALYSIS CHECK RECORDDA FORM 2408-19-1, NOV 1991

Report Date: 1/118-May-2017

9200307GA75189T55-GA-714A

MARGIN VALUE FLOWMAX / ACT ALT °C MAX / ACT MIN / ACT

6. PRESS 9. N1 %

3. AIRCRAFT SERIAL NUMBER

7. OAT 8. PTIT 10. TORQUE4. DATE 5. ENGINE TSO

12. REMARKS / TEMP11. FUEL

2. ENGINE SERIAL NUMBER1. ENGINE MODEL

770/806 / TRGR : 17; ADJ PATN: 24;CW3 GROVE

1700909010010214500005-Dec-2012 /

780/806 / TRIGGER = 21150074.274.2101.5101.534500016-May-2013 /

735/806 / POST C-17 BUILD UP.REMOVED IRSSTAILCONES & INSTALLEDSTANDARD CANTED. TV =14

18009898100.5104102000173702-Apr-2014 /

773/806 / TRIGGER : 21 POST PMS-3400HR INSP, UPGRADEDTO -21.

170093.293.399.4103.5183209182026-Sep-2014 /

ENGINE POWER ASSURANCE TEST RECORD DA FORM 2408-19-4, MAR 2014For use of this form, see DA PAM 738-751; the proponent agency is DCS G-4

Report Date: 1/118-May-2017

9200307GA75213T55-GA-714A

MARGIN VALUE FLOWMAX / ACT ALT °C MAX / ACT MIN / ACT

6. PRESS 9. N1 %

3. AIRCRAFT SERIAL NUMBER

7. OAT 8. PTIT 10. TORQUE4. DATE 5. ENGINE TSO

12. REMARKS / TEMP11. FUEL

2. ENGINE SERIAL NUMBER1. ENGINE MODEL

790/806 / NEW TRIGGER VALUE = 1516408787102.3103.7107000190907-Dec-2010 /

785/806 / POST PHASE 200 HR, TV =22, TQ ACT = 73

1400858510111128700028-Aug-2010 /

795/806 / TRIGGER VALUE: 241850101101101.5104103000221119-Jun-2012 /

770/806 / NEW TRIGGER VALUE 17185010510510110410120080827-Oct-2011 /

800/806 / PAC DUE TO IRSSINSTALL. TV=23

19009898103.5104103000225030-Nov-2012 /

780/806 / POST C-17 BUILD UP.REMOVED IRSSTAILCONES & INSTALLEDSTANDARD CANTED. TV =18

1825109.1108.9102.8104.202250264809-May-2014 /

763.9/806 / TRIGGER : 19 ECU'SUPGRADED TO -21'S.

177591.291.7101.4103.5193626274230-Sep-2014 /

773.5/806 / PRE-PMS-2 LMTF PAC.TRIGGER: 19

1850109.1109.3102.9104.9-103752279605-Mar-2015 /

ENGINE POWER ASSURANCE TEST RECORD DA FORM 2408-19-4, MAR 2014For use of this form, see DA PAM 738-751; the proponent agency is DCS G-4

0

50

4354.1

9200307 0 1265

e. ACFT HRS INSTALLEDc. TIME SINCE NEW OR OVERHAULc. SERIAL NUMBER

CH-47D GA75189 Days

b. MAKE OR TYPE d. ACFT HRS LAST OIL CHANGEb. SERIAL NUMBER

HELICOPTER, CARGO ENGINE ASSY TURBINE Hrs

a. NOMENCLATURE AND TYPEa. NOMENCLATUREFREQUENCY

COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 1 of 10

a b

SUBMITTED

c a b

SAMPLE DATE PIDSAMPLELAST OILEND ITEM

RESULTSDATE RESULTS RECEIVED7. 8.6. REASON FORHOURS5.4.

COMPONENTCHANGE

randy.c.clements21-Dec-2012NORMALBASELINE1.01265353905-Dec-2012

miranda.m.mooreROUTINE40.01315357818-Dec-2012

guillermo.munoz25-Jan-2013NORMALROUTINE93.01360363123-Jan-2013

guillermo.munoz28-Feb-2013NORMALROUTINE140.01410367828-Feb-2013

randy.c.clements11-Mar-2013NORMALROUTINE169.01439370709-Mar-2013

ryan.m.elkins08-Jun-2013NORMALROUTINE218.01488375607-Jun-2013

ryan.m.elkins23-Jul-2013NORMALROUTINE267.01537380516-Jul-2013

ryan.m.elkins14-Aug-2013NORMALROUTINE317.01587385513-Aug-2013

ryan.m.elkins05-Sep-2013NORMALROUTINE368.01638390602-Sep-2013

montrell.l.hill25-Oct-2013NORMALROUTINE417.01687395522-Oct-2013

jeffrey.a.mcteague30-Jul-2014NORMALROUTINE521.04059405922-Jul-2014

robert.d.childers10-Sep-2014NORMALROUTINE569.14107.14107.126-Aug-2014

robert.d.childers06-Jul-2015NORMALROUTINE48.64155.74155.718-Jun-2015

robert.d.childers07-Dec-2015NORMALROUTINE50.84206.54206.530-Nov-2015

robert.d.childers16-May-2016NORMALROUTINE48.64255.14255.110-May-2016

robert.d.childers12-Jul-2016NORMAL200 HOUR52.04307.14307.106-Jul-2016

robert.d.childers09-Dec-2016NORMALROUTINE47.04354.14354.106-Dec-2016

robert.d.childers03-Apr-2017NORMALROUTINE52.24406.34406.324-Mar-2017

9. REMARKS:

For use of this form, see DA PAM 738-751; the proponent agency is DCSLOGDA FORM 2408-20, DEC 91, MAY BE USED

OIL ANALYSIS LOGDA FORM 2408-20, OCT 1997

0

50

8548.4

9200307 1405 3058


CH-47D GA75213 Days




COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 2 of 10

a b

SUBMITTED

c a b



COMPONENTCHANGE

ML51903017-Jul-2010NORMALROUTINE8710.08710871013-Jul-2010

ML51903031-Aug-2010NORMALROUTINE7110.08763876328-Aug-2010

ML51903012-Sep-2010NORMALROUTINE7154.08858880710-Sep-2010

alexander.k.branan09-Oct-2010NORMALROUTINE7254.08958890704-Oct-2010

alexander.k.branan11-Jan-2011NORMALROUTINE7351.01959900407-Jan-2011

JS79582927-Jan-2011NORMALROUTINE7401.02009905420-Jan-2011

alexander.k.branan28-Feb-2011NORMALROUTINE7453.02057910626-Feb-2011

alexander.k.branan02-Apr-2011NORMALROUTINE404.02057913729-Mar-2011

alexander.k.branan13-May-2011NORMALROUTINE451.02107918405-May-2011

kayrene.r.middleton15-Dec-2011NORMALROUTINE500.02172923314-Dec-2011

chris.poyner29-Feb-2012NORMALPRE RESET537.02211927028-Feb-2012

chris.poyner15-Jun-2012NORMALPOST RESET0.02211927014-Jun-2012

john.c.zimmerman09-Oct-2012NORMALBASELINE17.02230928701-Oct-2012

ryan.m.elkins15-Jan-2013NORMALROUTINE50.02265932014-Jan-2013

ryan.m.elkins29-Apr-2013NORMALROUTINE99.02314936923-Apr-2013

ryan.m.elkins03-Jun-2013NORMALROUTINE146.02361941631-May-2013

ryan.m.elkins11-Jun-2013NORMALSPECIAL158.02373942808-Jun-2013

ryan.m.elkins21-Jun-2013NORMALROUTINE191.02406946118-Jun-2013



montrell.l.hill21-Sep-2013NORMALROUTINE338.02553960817-Sep-2013

jack.dailey17-Oct-2013NORMALROUTINE391.02606966115-Oct-2013

jeffrey.a.mcteague26-Mar-2014NORMALOTHER437.723489707.726-Mar-2014

jeffrey.a.mcteague16-Jun-2014NORMALROUTINE489.69759.69759.612-Jun-2014

14-Oct-2014NORMALROUTINE48.69808.29808.230-Sep-2014

robert.d.childers20-May-2015NORMALROUTINE52.89861986105-Mar-2015

robert.d.childers15-Jun-2015NORMALROUTINE49.99910.99910.912-Jun-2015

robert.d.childers03-Aug-2015NORMALROUTINE47.79958.69958.631-Jul-2015

robert.d.childers18-Aug-2015NORMALSPECIAL0.09958.69958.618-Aug-2015

robert.d.childers08-Dec-2015NORMALROUTINE-1657.78300.98300.902-Dec-2015

robert.d.childers16-Mar-2016NORMALROUTINE48.98349.88349.803-Mar-2016

robert.d.childers26-Apr-2016NORMALROUTINE75.48425.28425.226-Apr-2016

robert.d.childers03-Jun-2016NORMAL400 HOUR20.68445.88445.803-Jun-2016

robert.d.childers13-Jun-2016ABNORMAL400 HOUR3.58449.38449.308-Jun-2016

robert.d.childers07-Jul-2016NORMAL400 HOUR3.58452.88452.807-Jul-2016

robert.d.childers02-Dec-2016NORMALROUTINE44.18496.98496.917-Nov-2016

robert.d.childers14-Feb-2017NORMALROUTINE51.58548.48548.414-Feb-2017

robert.d.childers03-Apr-2017NORMALROUTINE70.531724406.324-Mar-2017



0

50

8548.4

9200307 1405 3058


CH-47D GA75213 Days




COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 3 of 10

9. REMARKS:



0

400

4110.1

9200307 CC 4107


CH-47D 2008A13875MG Days


HELICOPTER, CARGO FORWARD TRANSMISSION Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 4 of 10

a b

SUBMITTED

c a b



COMPONENTCHANGE


06-Oct-2014NORMALBASELINE0.0341.14110.102-Oct-2014

9. REMARKS:



0

400

4122

9200307 CC 2476


CH-47D A9-612 Days


HELICOPTER, CARGO AFT TRANSMISSION Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 5 of 10

a b

SUBMITTED

c a b



COMPONENTCHANGE

edward.d.simmons20-Mar-2006ABNORMALROUTINE0.02148293415-Mar-2006

edward.d.simmons20-Mar-2006NORMALROUTINE1.02149293517-Mar-2006

edward.d.simmons09-Aug-2006NORMALROUTINE24.02197250004-Aug-2006

amon.l.emerson25-Oct-2006NORMALROUTINE71.02244254713-Oct-2006

amon.l.emerson20-Jun-2007NORMALROUTINE123.02296259915-Jun-2007

amon.l.emerson18-Oct-2007ABNORMALROUTINE173.02346264916-Oct-2007

amon.l.emerson31-Oct-2007NORMALSPECIAL179.02352265526-Oct-2007

amon.l.emerson17-Jan-2008NORMALROUTINE224.02397270015-Jan-2008

edward.d.simmons27-Mar-2008ABNORMALROUTINE275.02448275121-Mar-2008

m.walker21-Apr-2008NORMALSPECIAL280.02453275617-Apr-2008

m.walker01-Jul-2008NORMALROUTINE323.02496279927-Jun-2008

jorge.l.alvarez13-Mar-2009NORMALROUTINE369.02542284504-Mar-2009

jennifer.s.gerondale20-Jun-2009NORMALROUTINE424.02597290016-Jun-2009

jennifer.s.gerondale21-Aug-2009NORMALROUTINE472.02645294818-Aug-2009

MM58956019-Sep-2009NORMALROUTINE523.02696299917-Sep-2009

MM58956027-Nov-2009NORMALROUTINE571.02744304724-Nov-2009

miranda.m.mooreROUTINE621.02794309722-Dec-2009

DK70887812-May-2010EXCESS PARROUTINE672.02845314806-May-2010

charles.j.bass23-Jun-2010NORMALPRE RESET691.02864316721-Jun-2010

charles.j.bass07-Oct-2010NORMALPOST RESET0.02864316704-Oct-2010

darryl.e.roberts14-Dec-2010NORMALBASELINE40.02904320710-Dec-2010

darryl.e.roberts28-Jan-2011NORMALROUTINE45.02909321227-Jan-2011

john.a.emery20-Jul-2011NORMALROUTINE98.02962326519-Jul-2011

JH54381513-Nov-2011NORMALROUTINE151.03015331809-Nov-2011

JH54381517-Nov-2011NORMAL50 HOUR163.03027333017-Nov-2011

CH78031329-Oct-2012NORMAL400 HOUR317.03181348426-Oct-2012

michael.d.smith11-Mar-2013ABNORMALROUTINE540.03404370709-Mar-2013

guillermo.munoz27-Mar-2013NORMALLAB REQUES543.03407371025-Mar-2013

jeffrey.a.mcteague22-Apr-2014ABNORMALROUTINE840.43704.44004.502-Apr-2014

jeffrey.a.mcteague24-Apr-2014NORMALLAB REQUES850.23714.24017.224-Apr-2014

robert.d.childers22-Sep-2014ABNORMALROUTINE940.13804.14107.125-Aug-2014

robert.d.childers28-Oct-2014NORMALSPECIAL3.03807.14110.114-Oct-2014

robert.d.childers26-Mar-2015ABNORMALLAB REQUES11.93819412226-Mar-2015

robert.d.childers29-Jun-2015NORMALSPECIAL31.23850.24153.215-Jun-2015

9. REMARKS:



0

400

0

9200307 CC 3907


CH-47D 2010A9091 Days


HELICOPTER, CARGO COMBINING TRANSMISSION Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 6 of 10

a b

SUBMITTED

c a b



COMPONENTCHANGE

jeffrey.a.mcteague22-Apr-2014ABNORMALROUTINE4007.4100.44004.402-Apr-2014

jeffrey.a.mcteague24-Apr-2014ABNORMALLAB REQUES4017.2110.24017.224-Apr-2014



9. REMARKS:



0

400

3167

9200307 CC 3167


CH-47D 2006A12041 Days


HELICOPTER, CARGO XMSN ASSY ENGINE MECH Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 7 of 10

a b

SUBMITTED

c a b



COMPONENTCHANGE

charles.j.bass07-Oct-2010NORMALPOST RESET0.0316704-Oct-2010


darryl.e.roberts28-Jan-2011NORMALROUTINE45.045321227-Jan-2011

john.a.emery20-Jul-2011NORMALROUTINE98.098326519-Jul-2011

robert.t.calvert13-Nov-2011NORMALROUTINE151.0151331809-Nov-2011

JH54381517-Nov-2011NORMAL50 HOUR163.0163333017-Nov-2011

CH78031329-Oct-2012ABNORMAL400 HOUR317.0317348426-Oct-2012

david.c.fisher02-Nov-2012NORMALLAB REQ318.0318348531-Oct-2012

michael.d.smith11-Mar-2013ABNORMALROUTINE540.0540370709-Mar-2013

guillermo.munoz27-Mar-2013NORMALLAB REQUES543.0543371025-Mar-2013

jeffrey.a.mcteague22-Apr-2014NORMALROUTINE840.4840.44004.502-Apr-2014


9. REMARKS:



0

400

8445.8

9200307 CC 4377


CH-47D A11-460DRGI Days




COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 8 of 10

a b

SUBMITTED

c a b



COMPONENTCHANGE

karen.l.hall29-Jun-2007NORMALINITIAL0.03866752624-Jun-2007

john.g.morris03-Jul-2007NORMALROUTINE5.03871753130-Jun-2007

john.g.morris23-Jul-2007NORMALSPECIAL23.03889754916-Jul-2007

karen.l.hall15-Aug-2007NORMALROUTINE54.03920758010-Aug-2007

john.g.morris23-Aug-2007NORMALSPECIAL76.03942760218-Aug-2007

john.g.morris11-Sep-2007NORMALROUTINE89.03955761505-Sep-2007

karen.l.hall29-Oct-2007NORMALROUTINE139.04005766518-Oct-2007

karen.l.hall15-Nov-2007NORMALROUTINE185.04051771104-Nov-2007

karen.l.hall24-Nov-2007ABNORMALSPECIAL226.04092775219-Nov-2007

karen.l.hall06-Dec-2007NORMALROUTINE237.04103776322-Nov-2007

karen.l.hall06-Dec-2007NORMALLAB REQUES242.04108776826-Nov-2007

karen.l.hall06-Dec-2007NORMALBASELINE4.04112777227-Nov-2007

karen.l.hall19-Dec-2007NORMALROUTINE46.04154781413-Dec-2007

karen.l.hall27-Jan-2008NORMALSPECIAL79.04187784714-Jan-2008

karen.l.hall27-Jan-2008NORMALROUTINE96.04204786420-Jan-2008

karen.l.hall26-Feb-2008NORMALROUTINE147.04255791522-Feb-2008

karen.l.hall29-Mar-2008NORMALROUTINE195.04303796311-Mar-2008

karen.l.hall29-Mar-2008NORMALSPECIAL230.04338799825-Mar-2008

karen.l.hall13-Apr-2008NORMALROUTINE246.04354801428-Mar-2008

karen.l.hall30-May-2008NORMALROUTINE298.04406806620-May-2008

karen.l.hall14-Jun-2008ABNORMALSPECIAL323.04431809129-May-2008

karen.l.hall18-Jun-2008NORMALROUTINE348.04456811611-Jun-2008

karen.l.hall18-Jun-2008NORMALLAB REQUES361.04469812915-Jun-2008

karen.l.hall09-Jul-2008NORMALROUTINE399.04507816728-Jun-2008

karen.l.hall12-Jul-2008NORMALROUTINE426.04534819406-Jul-2008

darrel.e.dust01-Aug-2008NORMALRESET429.04537819725-Jul-2008

karen.l.hall11-Dec-2008NORMALBASELINE0.04537819723-Oct-2008

sidney.j.cowan22-Jan-2009NORMALROUTINE46.04583824315-Jan-2009

sidney.j.cowan19-Feb-2009NORMALROUTINE97.046348293.611-Feb-2009

casey.j.haugen10-Apr-2009NORMALROUTINE151.08347834802-Apr-2009

casey.j.haugen28-Apr-2009NORMALPRE-PHASE185.04722838222-Apr-2009

jeremy.a.connors25-Jun-2009NORMALROUTINE186.04723838317-Jun-2009

stanford.s.horne18-Sep-2009NORMALROUTINE241.04778843809-Sep-2009

casey.j.haugen14-Dec-2009NORMALROUTINE287.04824848408-Dec-2009

casey.j.haugen22-May-2010NORMALROUTINE371.04908856816-May-2010

ML51903002-Jun-2010NORMALROUTINE414.04951861101-Jun-2010

ML51903016-Jun-2010NORMALROUTINE462.04999865913-Jun-2010

ML51903017-Jul-2010NORMALROUTINE513.05089874913-Jul-2010

timothy.d.carroll31-Aug-2010NORMALROUTINE566.05103876328-Aug-2010

ML51903012-Sep-2010NORMALROUTINE610.05147880710-Sep-2010

alexander.k.branan30-Sep-2010NORMALROUTINE661.05198885825-Sep-2010

alexander.k.branan09-Oct-2010NORMALROUTINE710.05247890704-Oct-2010

alexander.k.branan11-Jan-2011NORMALROUTINE807.05344900407-Jan-2011

JS79582927-Jan-2011NORMALROUTINE857.05394905420-Jan-2011



0

400

8445.8

9200307 CC 4377


CH-47D A11-460DRGI Days




COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 9 of 10

alexander.k.branan28-Feb-2011NORMALROUTINE909.05446910626-Feb-2011

alexander.k.branan02-Apr-2011NORMALROUTINE940.05477913729-Mar-2011

alexander.k.branan13-May-2011NORMALROUTINE987.05524918405-May-2011

kayrene.r.middleton15-Dec-2011NORMALROUTINE1036.05573923314-Dec-2011

chris.poyner29-Feb-2012NORMALPRE RESET1073.05610927028-Feb-2012

chris.poyner15-Jun-2012NORMALPOST RESET0.05610927014-Jun-2012

john.c.zimmerman09-Oct-2012NORMALBASELINE17.05627928701-Oct-2012

ryan.m.elkins18-Jul-2013NORMALSPECIAL221.05831949117-Jul-2013

jack.dailey17-Oct-2013NORMALROUTINE391.06001966115-Oct-2013

jeffrey.a.mcteague22-Apr-2014NORMALROUTINE448.56058.59718.504-Apr-2014


robert.d.childers12-Aug-2015ABNORMALSPECIAL224.56298.69958.631-Jul-2015

robert.d.childers20-Oct-2015ABNORMALSPECIAL12.26310.89970.814-Oct-2015

robert.d.childers10-Nov-2015NORMALBASELINE2.86313.69973.603-Nov-2015

robert.d.childers10-Jun-2016ABNORMAL400 HOUR7.56475.88445.803-Jun-2016

robert.d.childers13-Jun-2016NORMAL400 HOUR3.56479.38449.308-Jun-2016

9. REMARKS:



90

100

3167

9200307 0


CH-47D 877509 Days


HELICOPTER, CARGO AUXILIARY POWER UNIT Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 10 of 10

a b

SUBMITTED

c a b



COMPONENTCHANGE



FE2, AL1, MG2, PB1, SN4,"A"

9. REMARKS:



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REMOVAL

f

NSTALL

ji kgdcbaCYC/HRS

COMPO/H

NOMEN

WUC

Hours/Cycles)

O/H

LOCATIONNSNAND

heSINCE

LIFE

(EnginePREV

SER NO.AND

NOMENCLATURE PN

TIME CYC/HRS

DUEREPLACE

NO.

COMPONENTNOMEN

REP.O/H ORCOMP

6.

04A

5. WUC4. SERIAL NUMBER3. PART NUMBER OR MODEL2. NSN1. NOMENCLATURE

ENGINE ASSY TURBINE 2840014585361 2-001-020-39 GA75189


1NSN PENDING04A01C

1265CCCOMPRESSOR ROTOR ASSY 2-101-600-57 31365100934 CC 1402 COND COND

1284001458998404A02A

1265CCLINER ASSY, COMBUSTION 2-131-110-76 72463718918 CC 1367 COND COND

Cycles1284001465893404A02B12

238RCSEALING PLATE, 1ST GP 2-121-075-36 61365105366 RC 238 20990 20990

Cycles1536501467909504A02B13

228RCSPACER, TURBINE GAS 2-121-071-42 71365101240 RC 228 8300 8300

1284001461468504A02C

1265CCNOZZLE ASSY 1ST TURBINE 2-121-430-25 6P32155 CC 1573 COND COND

Cycles1284001479568304A03A

190RCDISK ASSY, 1ST TURBINE 2-121-090-79 71365101105 RC 190 10400 10400

1284001478534604A03B

1265CCCYLINDER 1ST TURBINE 2-121-470-49 1499500494 CC 1273 COND COND

1283501453789004A03D

1265CCNOZZLE ASSY, 2ND TURBINE 2-121-100-79 42490605144 CC 1228 COND COND

1284001483025404A03E

1265CCTURBINE ROTOR 2-141-140-45 5P25109 CC 666 COND COND

Hours1291501371930504A05A

18720HYDROMECHANICAL ASSY 110700-02D6 1159901370739 0 607 2800 4065

PART 2 - 714A ENGINE/COMPONENT REPORT APPROVED BY DA G4

CYC/HRS

NSTALL

REMOVAL

CYC/HRS

REMOVAL

f

NSTALL

ji kgdcbaCYC/HRS

COMPO/H

NOMEN

WUC

Hours/Cycles)

O/H

LOCATIONNSNAND

heSINCE

LIFE

(EnginePREV

SER NO.AND

NOMENCLATURE PN

TIME CYC/HRS

DUEREPLACE

NO.

COMPONENTNOMEN

REP.O/H ORCOMP

6.

04A






LIN

E

3=

00

00

3rd

CO

MP

a

1-

2.

E

NG

S/N

T-5

5-G

A-7

14

A

3. N

OM

EN

CL

AT

UR

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31

36

51

00

93

4

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OD

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2

6. H

IST

OR

ICA

L C

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NT

S O

N E

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PA

RT

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71

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GIN

E /

CO

MP

ON

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T R

EP

OR

T A

PP

RO

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D B

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4

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MP

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SS

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f

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GP

SP

AC

ER

4. P

/N

00

GA

75

18

9

11

59

90

00

20

10

4

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G O

P H

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CC

AC

FT

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GP

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TU

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TU

RB

bc

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TU

RB

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tal C

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nts

RE

AD

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AT

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NO

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AU

LS

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ING

AT

Co

un

ts s

ince

inst

all

LIN

E 2

MIN

US

LIN

E 1

= T

ota

l

INS

TA

LL

AT

ION

CYC/HRS

NSTALL

REMOVAL

CYC/HRS

REMOVAL

f

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ji kgdcbaCYC/HRS

COMPO/H

NOMEN

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Hours/Cycles)

O/H

LOCATIONNSNAND

heSINCE

LIFE

(EnginePREV

SER NO.AND

NOMENCLATURE PN

TIME CYC/HRS

DUEREPLACE

NO.

COMPONENTNOMEN

REP.O/H ORCOMP

6.

04A01C


COMPRESSOR ROTORASSY

NSN PENDING 2-101-600-57 31365100934


Cycles1284001391725704A01C01

1402RCCOMPRESSOR SHAFT 2-101-238-09 82517400510 RC 57 15000 16345

Cycles1284001478361704A01C09A

1402RC1 COMPRESSOR DISK 2-101-331-09 31365101737 RC 424 15000 15978

Cycles1284001475927304A01C09B


Cycles1284001475926304A01C09C


Cycles1284001475927204A01C09D


Cycles1284001475088604A01C09E


Cycles1284001475089704A01C09F


Cycles1284001475927004A01C09G


Cycles1284001195689604A01C09H

1402RCSPACER 1ST COMPRESSOR 2-103-024-04 972512304425 RC 2139 15000 14263

Cycles1536501214592804A01C09J

1402RCSPACER 2ND COMPRESSOR 2-100-047-09 61686801248 RC 478 15000 15924


CYC/HRS

NSTALL

REMOVAL

CYC/HRS

REMOVAL

f

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ji kgdcbaCYC/HRS

COMPO/H

NOMEN

WUC

Hours/Cycles)

O/H

LOCATIONNSNAND

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LIFE

(EnginePREV

SER NO.AND

NOMENCLATURE PN

TIME CYC/HRS

DUEREPLACE

NO.

COMPONENTNOMEN

REP.O/H ORCOMP

6.

04A01C



NSN PENDING 2-101-600-57 31365100934


Cycles1536501492695804A01C09K

1402RCSPACER 3,4,5 COMPRESSOR 2-100-048-14 32512390854 RC 424 15000 15978

Cycles1536501492695804A01C09K


Cycles1536501492695804A01C09K


Cycles1284001475923804A01C09L

1402RCSPACER 6TH COMPRESSOR 2-100-052-33 1903302561 RC 560 15000 15842



LIN

E

3=

00

00

3rd

CO

MP

a

1-

2.

E

NG

S/N

T-5

5-G

A-7

14

A

3. N

OM

EN

CL

AT

UR

E

5P

25

10

9

1. M

OD

EL

2

6. H

IST

OR

ICA

L C

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NT

S O

N E

NG

INE

PA

RT

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71

4A

EN

GIN

E /

CO

MP

ON

EN

T R

EP

OR

T A

PP

RO

VE

D B

Y H

Q D

A G

4

TU

RB

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RO

TO

R

f

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-14

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5

g

GP

SP

AC

ER

4. P

/N

00

GA

75

18

9

11

59

90

00

20

10

4

EN

G O

P H

RS

CC

AC

FT

h

1st

GP

5A

. D

EC

U S

/N

5. S

/N

3rd

TU

RB

ed

00

4th

TU

RB

bc

1st

TU

RB

2n

d T

UR

B

EN

GIN

E =

To

tal C

ou

nts

RE

AD

ING

AT

RE

MO

VA

L O

F

7.

NO

. O

F O

VE

RH

AU

LS

RE

AD

ING

AT

Co

un

ts s

ince

inst

all

LIN

E 2

MIN

US

LIN

E 1

= T

ota

l

INS

TA

LL

AT

ION

CYC/HRS

NSTALL

REMOVAL

CYC/HRS

REMOVAL

f

NSTALL

ji kgdcbaCYC/HRS

COMPO/H

NOMEN

WUC

Hours/Cycles)

O/H

LOCATIONNSNAND

heSINCE

LIFE

(EnginePREV

SER NO.AND

NOMENCLATURE PN

TIME CYC/HRS

DUEREPLACE

NO.

COMPONENTNOMEN

REP.O/H ORCOMP

6.

04A03E


TURBINE ROTOR 2840014830254 2-141-140-45 5P25109


Cycles1282501205076904A03E02

503RCDISK ASSY 4TH TURBINE 2-141-170-22 41365108704 RC 503 10960 10960

Cycles1284001474862004A03F

527RCSHAFT ASSY, INTEGRAL 2-141-350-10 51365100819 RC 527 13200 13200



LIN

E

3=

53

82

56

85

74

51

8

3rd

CO

MP

a

1-

2.

E

NG

S/N

T-5

5-G

A-7

14

A

3. N

OM

EN

CL

AT

UR

E

GA

75

21

3

1. M

OD

EL

2

6. H

IST

OR

ICA

L C

OU

NT

S O

N E

NG

INE

PA

RT

1 -

71

4A

EN

GIN

E /

CO

MP

ON

EN

T R

EP

OR

T A

PP

RO

VE

D B

Y H

Q D

A G

4

EN

GIN

E A

SS

Y T

UR

BIN

E

f

2-0

01

-02

0-3

9

g

GP

SP

AC

ER

4. P

/N

13

45

13

45

92

00

30

7

11

59

90

12

80

74

0

EN

G O

P H

RS

1

AC

FT

h

1st

GP

5A

. D

EC

U S

/N

5. S

/N

3rd

TU

RB

ed

13

45

30

58

4th

TU

RB

bc

1st

TU

RB

2n

d T

UR

B

EN

GIN

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tal C

ou

nts

RE

AD

ING

AT

RE

MO

VA

L O

F

7.

NO

. O

F O

VE

RH

AU

LS

RE

AD

ING

AT

Co

un

ts s

ince

inst

all

LIN

E 2

MIN

US

LIN

E 1

= T

ota

l

INS

TA

LL

AT

ION

CYC/HRS

NSTALL

REMOVAL

CYC/HRS

REMOVAL

f

NSTALL

ji kgdcbaCYC/HRS

COMPO/H

NOMEN

WUC

Hours/Cycles)

O/H

LOCATIONNSNAND

heSINCE

LIFE

(EnginePREV

SER NO.AND

NOMENCLATURE PN

TIME CYC/HRS

DUEREPLACE

NO.

COMPONENTNOMEN

REP.O/H ORCOMP

6.

04A




2NSN PENDING04A01C

1653CCCOMPRESSOR ROTOR ASSY 2-101-600-57 31365100919 CC 1393 COND COND

2284001458998404A02A

1653CCLINER ASSY, COMBUSTION 2-131-110-76 52463717637 CC 765 COND COND

Cycles2284001465893404A02B12

1345RCSEALING PLATE, 1ST GP 2-121-075-36 1365102174 RC 1345 20990 20990

Cycles2536501467909504A02B13

1345RCSPACER, TURBINE GAS 2-121-071-42 1365103072 RC 1345 8300 8300

2284001461468504A02C

1653CCNOZZLE ASSY 1ST TURBINE 2-121-430-25 5P13885 CC 660 COND COND

Cycles2284001479568304A03A

1345RCDISK ASSY, 1ST TURBINE 2-121-090-79 1365103554 RC 1345 10400 10400

Cycles284001479568104A03C

9959RCDISK ASSY, 2ND TURBINE 2-121-110-35 81365101304 RC 518 3300 12741

2284001483025404A03E

1653CCTURBINE ROTOR 2-141-140-45 361145 CC 1695 COND COND

Hours2291501371930504A05A

16530HYDROMECHANICAL ASSY 2-170-580-02 99AJW310 0 1338 2800 3115


CYC/HRS

NSTALL

REMOVAL

CYC/HRS

REMOVAL

f

NSTALL

ji kgdcbaCYC/HRS

COMPO/H

NOMEN

WUC

Hours/Cycles)

O/H

LOCATIONNSNAND

heSINCE

LIFE

(EnginePREV

SER NO.AND

NOMENCLATURE PN

TIME CYC/HRS

DUEREPLACE

NO.

COMPONENTNOMEN

REP.O/H ORCOMP

6.

04A





24-Feb-2009 1 1 ENGINE RECAPPED (OVERHAUL) 23 FEB 09 IAW MEO P5092B DTD 12JUL05, RH3098

RH3098 CCAD CORPUS CHRISTI, TX 78419

03-May-2012 1 2ND TURBINE NOZZLE (SN 2490601965) INSTALLED DURING RESET. THIS 2ND STAGE NOZZLE HAS ANMEC AUTHORIZING STOP DRILLING OF CRACKS BY CCAD. MEC# P96561 B.

chris.poyner AMCOM AFMA/URS JBLM, WA


LIN

E

3=

00

00

3rd

CO

MP

a

1-

2.

E

NG

S/N

T-5

5-G

A-7

14

A

3. N

OM

EN

CL

AT

UR

E

31

36

51

00

91

9

1. M

OD

EL

2

6. H

IST

OR

ICA

L C

OU

NT

S O

N E

NG

INE

PA

RT

1 -

71

4A

EN

GIN

E /

CO

MP

ON

EN

T R

EP

OR

T A

PP

RO

VE

D B

Y H

Q D

A G

4

CO

MP

RE

SS

OR

RO

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R A

SS

Y

f

2-1

01

-60

0-5

7

g

GP

SP

AC

ER

4. P

/N

00

GA

75

21

3

11

59

90

12

80

74

0

EN

G O

P H

RS

CC

AC

FT

h

1st

GP

5A

. D

EC

U S

/N

5. S

/N

3rd

TU

RB

ed

00

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RB

bc

1st

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NO

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F O

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RH

AU

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AT

Co

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ts s

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LIN

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US

LIN

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l

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TA

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AT

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CYC/HRS

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REMOVAL

CYC/HRS

REMOVAL

f

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COMPO/H

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LOCATIONNSNAND

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LIFE

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SER NO.AND

NOMENCLATURE PN

TIME CYC/HRS

DUEREPLACE

NO.

COMPONENTNOMEN

REP.O/H ORCOMP

6.

04A01C



NSN PENDING 2-101-600-57 31365100919


Cycles2284001391725704A01C01

574RCCOMPRESSOR SHAFT 2-101-238-09 22517400011 RC 729 15000 14845

Cycles2284001478361704A01C09A


Cycles2284001475927304A01C09B


Cycles2284001475926304A01C09C


Cycles2284001475927204A01C09D


Cycles2284001475088604A01C09E


Cycles2284001475089704A01C09F


Cycles2284001475927004A01C09G


Cycles2536501492695804A01C09K


Cycles2536501492695804A01C09K



CYC/HRS

NSTALL

REMOVAL

CYC/HRS

REMOVAL

f

NSTALL

ji kgdcbaCYC/HRS

COMPO/H

NOMEN

WUC

Hours/Cycles)

O/H

LOCATIONNSNAND

heSINCE

LIFE

(EnginePREV

SER NO.AND

NOMENCLATURE PN

TIME CYC/HRS

DUEREPLACE

NO.

COMPONENTNOMEN

REP.O/H ORCOMP

6.

04A01C



NSN PENDING 2-101-600-57 31365100919


Cycles2536501492695804A01C09K


Cycles284001128658204A01D

574RCCENTRIFUGAL IMPELLER 2-100-180-17 51365106606 RC 1063 15000 14511


24-Feb-2009 1 24FEB09, ENGINE RECAPPED (OVERHAUL) 23 FEB 09 IAW MEO P5092B DTD 12JUL05. RH3098, CCAD,CORPUS CHRISTI, TX 78419-5260

RH3098 CCAD CORPUS CHRISTI, TX 78419-5260


LIN

E

3=

00

00

3rd

CO

MP

a

1-

2.

E

NG

S/N

T-5

5-G

A-7

14

A

3. N

OM

EN

CL

AT

UR

E

36

11

45

1. M

OD

EL

2

6. H

IST

OR

ICA

L C

OU

NT

S O

N E

NG

INE

PA

RT

1 -

71

4A

EN

GIN

E /

CO

MP

ON

EN

T R

EP

OR

T A

PP

RO

VE

D B

Y H

Q D

A G

4

TU

RB

INE

RO

TO

R

f

2-1

41

-14

0-4

5

g

GP

SP

AC

ER

4. P

/N

00

GA

75

21

3

11

59

90

12

80

74

0

EN

G O

P H

RS

CC

AC

FT

h

1st

GP

5A

. D

EC

U S

/N

5. S

/N

3rd

TU

RB

ed

00

4th

TU

RB

bc

1st

TU

RB

2n

d T

UR

B

EN

GIN

E =

To

tal C

ou

nts

RE

AD

ING

AT

RE

MO

VA

L O

F

7.

NO

. O

F O

VE

RH

AU

LS

RE

AD

ING

AT

Co

un

ts s

ince

inst

all

LIN

E 2

MIN

US

LIN

E 1

= T

ota

l

INS

TA

LL

AT

ION

CYC/HRS

NSTALL

REMOVAL

CYC/HRS

REMOVAL

f

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ji kgdcbaCYC/HRS

COMPO/H

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LOCATIONNSNAND

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LIFE

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SER NO.AND

NOMENCLATURE PN

TIME CYC/HRS

DUEREPLACE

NO.

COMPONENTNOMEN

REP.O/H ORCOMP

6.

04A03E


TURBINE ROTOR 2840014830254 2-141-140-45 361145


Cycles2282501205076904A03E02

2568RCDISK ASSY 4TH TURBINE 2-141-170-22 E510 RC 2568 10960 10960

Cycles2284001474862004A03F

538RCSHAFT ASSY, INTEGRAL 2-141-350-10 11365106296 RC 538 13200 13200



Swung: By: david.j.king05-Nov-2008

PILOT'S COMPASS CORRECTION CARD

H.S.I.Compass:

270

180

090

000

W 270

DD Form 1613

Fly To Steer Fly To Steer

345

330

315

300

285

255

225

240

195

210

S 180

165

150

135

120

045

075

105

E 090

060

030

015

N 000

270

180

090

000

W 270

DD Form 1613


345

330

315

300

285

255

225

240

195

210

S 180

165

150

135

120

045

075

105

E 090

060

030

015

N 000

COMPASS

DATE

COMPENSATED AND SWUNG BY

For Compensation procedure, refer to Specification AN-C 106.

MAGNETIC

05-Nov-2008

david.j.king


AIRCRAFT

9200307

DD Form 1613 E, JUL 67 REPLACES AFTO FORM 76, MAY 56 WHICH IS OBSOLETE

Swung: By: richard.ballar22-Oct-2009


H.S.I.Compass:

314

268

224

178

133

088

044

358

W 270

DD Form 1613


345

330

315

300

285

255

225

240

195

210

S 180

165

150

135

120

045

075

105

E 090

060

030

015

N 000

315

269

224

178

134

088

045

001

W 270

DD Form 1613


345

330

315

300

285

255

225

240

195

210

S 180

165

150

135

120

045

075

105

E 090

060

030

015

N 000

COMPASS

DATE



MAGNETIC

22-Oct-2009

richard.ballard


AIRCRAFT

9200307


Swung: By: lucas.d.bohm01-Apr-2016


COPILOT HSICompass:

315

270

225

180

135

090

045

360

W 270

DD Form 1613


345

330

315

300

285

255

225

240

195

210

S 180

165

150

135

120

045

075

105

E 090

060

030

015

N 000

318

269

223

181

135

090

048

001

W 270

DD Form 1613


345

330

315

300

285

255

225

240

195

210

S 180

165

150

135

120

045

075

105

E 090

060

030

015

N 000

COMPASS

DATE



MAGNETIC

01-Apr-2016

lucas.d.bohm


AIRCRAFT

9200307


Swung: By: lucas.d.bohm01-Apr-2016


PILOT HSICompass:

316

270

226

181

137

093

045

360

W 270

DD Form 1613


345

330

315

300

285

255

225

240

195

210

S 180

165

150

135

120

045

075

105

E 090

060

030

015

N 000

COMPASS

DATE



PILOT HSI

01-Apr-2016

lucas.d.bohm


AIRCRAFT

9200307


No. of PagePage No.Engine Serial NumberEngine NumberA/C Serial NumberEngine Model

1/1 1

18-May-2017

Date

Engine Installed At ______________________________ A/C Hours: __________________________________________ Engine Hours

TGTLimit

TorqueAir Speed

ºCºC

ºC

ºCLimit

ATFETF

TGTMargin

Ind. TGT(1)

Table TGT(2)

PAFATA/C HoursDateTGT

MarginInd. TGT

(1)Table TGT

(2)PAFAT

A/C HoursDate

DA FORM 2408-16

1. NOMENCLATURE

HEAD ASSY ROT WING AFT

2. NSN

1615013914399

3. PN NUMBER OR MODEL

145R2004-20

4. SERIAL NUMBER

2009A5582

5. WUC

05B01

COUNT /

DATE

6. NOMECLATURE AND WUC

a

P

O

S

P/N

AND

NSN

b

COMPONENT

SE NO.

LOCATION

c

NO.

PREV

O/H

d

NOMEN

ISNT HRS

e

NOMEN

RMVL

HRS

f

TIME

SINCE

O/H

g

COMP

ISNT HRS

h

COMP

RMVL

HRS

i

O/H OR

REPLAC

LIFE

j

REPLAC-

MENT

DUE

(ACFT

HRS

k

Page 1 of 5

1615011987553

1 of 1

28-Sep-09

HUB ROTARY WING AFT

05B01A

2114R2050-36 M2009249

0 0 0 0

1615007406480

1 of 3

28-Sep-09

AFT TIE BAR ASSY

05B01E

1114R2155-1 2009A6541

0 0 0 0

1615007406480

2 of 3

28-Sep-09

AFT TIE BAR ASSY

05B01E

2114R2155-1 2009A6543

0 0 0 0

1615007406480

3 of 3

28-Sep-09

AFT TIE BAR ASSY

05B01E

3114R2155-1 2009A6544

0 0 0 0

3040014077298

1 of 3

28-Sep-09

PITCH HOUSING

05B01F

1145R2075-16 B00877

0 0 0 0

3040014077298

2 of 3

28-Sep-09

PITCH HOUSING

05B01F

3145R2075-16 B00955

0 0 0 0

3040014077298

3 of 3

28-Sep-09

PITCH HOUSING

05B01F

2145R2075-16 B00956

0 0 0 0

3110008387064

1 of 3

28-Sep-09

AFT PITCH BEARING O/B

05B01G01

1114R2131-1 BDH457

0 0 0 0

3110008387064

2 of 3

28-Sep-09


05B01G01

2114R2131-1 BDH461

0 0 0 0

DA FORM 2408-16, OCT 91

EDITION OF MAY 67 IS OBSOLETE

AIRCRAFT COMPONENT HISTORICAL RECORD

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

DA FORM 2408-16

1. NOMENCLATURE


2. NSN

1615013914399


145R2004-20

4. SERIAL NUMBER

2009A5582

5. WUC

05B01

COUNT /

DATE


a

P

O

S

P/N

AND

NSN

b

COMPONENT

SE NO.

LOCATION

c

NO.

PREV

O/H

d

NOMEN

ISNT HRS

e

NOMEN

RMVL

HRS

f

TIME

SINCE

O/H

g

COMP

ISNT HRS

h

COMP

RMVL

HRS

i

O/H OR

REPLAC

LIFE

j

REPLAC-

MENT

DUE

(ACFT

HRS

k

Page 2 of 5

3110008387064

3 of 3

28-Sep-09


05B01G01

3114R2131-1 BDH463

0 0 0 0

3110009545730

1 of 3

28-Sep-09

AFT PITCH BEARING I/B

05B01G02

1114R2130-2 AZN2731

0 0 0 0

3110009545730

2 of 3

28-Sep-09


05B01G02

2114R2130-2 AZN2738

0 0 0 0

3110009545730

3 of 3

28-Sep-09


05B01G02

3114R2130-2 AZN2756

0 0 0 0

3040012063925

1 of 3

28-Sep-09

PITCH SHAFT AFT

05B01H

2234R2088-2 LK2008A1163

0 0 0 0 COND

3040012063925

2 of 3

28-Sep-09

PITCH SHAFT AFT

05B01H

3234R2088-2 LK2008A1165

0 0 0 0 COND

3040012063925

3 of 3

28-Sep-09

PITCH SHAFT AFT

05B01H

1234R2088-2 LK2008A1166

0 0 0 0 COND

3110004556179

1 of 3

28-Sep-09

AFT VERT PIN BRG, UPPER

05B01J01

1114RS214-6 BDH1975

0 0 0 0

3110004556179

2 of 3

28-Sep-09


05B01J01

2114RS214-6 BDH1976

0 0 0 0

DA FORM 2408-16, OCT 91




DA FORM 2408-16

1. NOMENCLATURE


2. NSN

1615013914399


145R2004-20

4. SERIAL NUMBER

2009A5582

5. WUC

05B01

COUNT /

DATE


a

P

O

S

P/N

AND

NSN

b

COMPONENT

SE NO.

LOCATION

c

NO.

PREV

O/H

d

NOMEN

ISNT HRS

e

NOMEN

RMVL

HRS

f

TIME

SINCE

O/H

g

COMP

ISNT HRS

h

COMP

RMVL

HRS

i

O/H OR

REPLAC

LIFE

j

REPLAC-

MENT

DUE

(ACFT

HRS

k

Page 3 of 5

3110004556179

3 of 3

28-Sep-09


05B01J01

3114RS214-6 BDH1977

0 0 0 0

3110004556188

1 of 3

28-Sep-09

AFT VERT PIN BRG, LOWER

05B01J02

1114RS214-5 BDH11562

0 0 0 0

3110004556188

2 of 3

28-Sep-09


05B01J02

2114RS214-5 BDH11563

0 0 0 0

3110004556188

3 of 3

28-Sep-09


05B01J02

3114RS214-5 BDH11564

0 0 0 0

5315012957008

1 of 3

28-Jan-13

PIN HORIZONTAL HINGE (AFT)

05B01K

114R2197-7 FM3736 0 222 0 0 2400

5315012957008

2 of 3

28-Sep-09


05B01K

3114R2197-7 M2009238

0 0 0 0 2400

5315012957008

3 of 3

28-Sep-09


05B01K

2114R2197-7 M2009300

0 0 0 0 2400

3110013110024

1 of 3

28-Sep-09

AFT HORZ PIN BRG, LEAD

05B01L01

1114RS225-1 200900984

0 0 0 0

3110013110024

2 of 3

28-Sep-09


05B01L01

2114RS225-1 200900986

0 0 0 0

DA FORM 2408-16, OCT 91




DA FORM 2408-16

1. NOMENCLATURE


2. NSN

1615013914399


145R2004-20

4. SERIAL NUMBER

2009A5582

5. WUC

05B01

COUNT /

DATE


a

P

O

S

P/N

AND

NSN

b

COMPONENT

SE NO.

LOCATION

c

NO.

PREV

O/H

d

NOMEN

ISNT HRS

e

NOMEN

RMVL

HRS

f

TIME

SINCE

O/H

g

COMP

ISNT HRS

h

COMP

RMVL

HRS

i

O/H OR

REPLAC

LIFE

j

REPLAC-

MENT

DUE

(ACFT

HRS

k

Page 4 of 5

3110013110024

3 of 3

28-Sep-09


05B01L01

3114RS225-1 200900990

0 0 0 0

3110013102258

1 of 3

28-Jan-13

AFT HORZ PIN BRG, TRAIL

05B01L02

114RS226-1 N42792 0 222 0 0

3110013102258

2 of 3

28-Sep-09


05B01L02

2114RS226-1 200901090

0 0 0 0

3110013102258

3 of 3

28-Sep-09


05B01L02

3114RS226-1 200901108

0 0 0 0

DA FORM 2408-16, OCT 91




DA FORM 2408-16

1. NOMENCLATURE


2. NSN

1615013914399


145R2004-20

4. SERIAL NUMBER

2009A5582

5. WUC

05B01

COUNT /

DATE


a

P

O

S

P/N

AND

NSN

b

COMPONENT

SE NO.

LOCATION

c

NO.

PREV

O/H

d

NOMEN

ISNT HRS

e

NOMEN

RMVL

HRS

f

TIME

SINCE

O/H

g

COMP

ISNT HRS

h

COMP

RMVL

HRS

i

O/H OR

REPLAC

LIFE

j

REPLAC-

MENT

DUE

(ACFT

HRS

k

Page 5 of 5

REMARKS

28SEPTEMBER2009

BOEING HELICOPTERS, PHILADELPHIA, PENNSYLVANIA. CONTRACT # DAAH23-02-D-0307. THIS

ROTORHEAD IS NEW AND WAS MANUFACTURED IAW THE ABOVE CONTRACT, ENGR. DWG.

145R2004 REV."T", PL. REV."CB", AND NOTES. * TO REACH FULL RETIREMENT LIFE IT IS MANDATORY THAT ALL VERT. & HORIZ. PIN BEARINGS BE ROTATED 180

DEGREES AT 1200 HOURS. BEARINGS ARE TO BE ROTATED ONLY ONCE TO THEIR UNLOADED SIDE, REGARDLESS OF TIME REMAINING WHEN BEARINGS WERE

ROTATED. AT NO TIME WILL "TIME SINCE NEW" IN BLOCK "H" OF ROTORHEAD COMPONENTS/PARTS, DA FORM 2408-16, EXCEED 2400 HOURS.

TSN=0, TSO=0, NUMBER OF O/HS=0 WY8177 610-591-1613

DA FORM 2408-16, OCT 91




CH-47D K6U6669200307

1DATE _________________ NUMBERS OF PAGES IN FLIGHT PACK

2627

2525

2625

2724

2525

02 May 2017

09 May 2017

11 May 2017

15 May 2017

21 May 2017

4507.1

4450.5

100.61344419.7

12. LOCAL USE

56.6

c. NEXT PHASE/SCHEDULED INSP DUE ATPID

115 May 2017LAST GENERATION PHASE/SCHEDULED

OPERATION SINCE DATE COMPLETED

PMD DUEe.b. NEXT PHASE/SCHEDULED INSP (NO.)a. HOURS OF d. HOURS OF

SCHEDULED INSPECTION INFORMATION11.

TOTALOTHER

ELEC TODAY

ARM 001CURRENT

VHOURS

ACFTCYCLES

AUTOROTATIONSSTD

LANDINGSHSF/AIRCRAFT

FLIGHT DATASYSTEM STATUS 10.9.

TOTAL

TODAY

CURRENT

DATE STARTSHOURSNO. 2NO. 1 HR METER NUMBER 2NUMBER 1

ENGINE HIT READINGS APU HISTORY6. 7. 8. ENGINE STARTS

MIDDLETOWN, DELAWARE

1.AIRCRAFT SERIAL NUMBER 2. MODEL 4. STATION 5. NAME OF CE/MECH3. UIC

HOVER TOUCHDOWN

OPERATION TO NEXT

INSPECTION

EDITION OF OCT 91 IS OBSOLETE For use of this form, see DA PAM 738-751; the proponent agency is DCS, G-4

AIRCRAFT STATUS INFORMATION RECORDDA FORM 2408-13, MAR 2014


9200307 CH-47D



4. PAGE3. DATE

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 14359.8 X

00

AFT 3MAN TRROP SEAT LATCH POST ON 2ND 3MAN SEAT ONL/H SIDE BROKE AIRCRAFT RESTRICTED TO 29 PASSENGERS

PID

SYS DATE ACFT HRSNO

V WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 1 02:57:00

HRS

joshua.r.childers10-Dec-2016

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 14022.2 K

00

OPERATE WITHIN LIMITATIONS AND RESTRICTIONS SPECIFIEDIN THE ENCLOSED AIRWORTHINESS RELEASE DATED:30APR14 (HYDRO-MECH ASSY), 08APR14 R1 (TRACKINGWEDGES), 21JAN14 R3 (IPAD), 20MAR13 R4 (EMC-100 ECU),10DEC13 R16 (MSPU), 10JUL12 (IRSS), 10OCT13 (EAWIS),16MAY12 R1 (LOG BOOK LAPTOP), 02MAY12 (DUAL EMD)24OCT13 R2 (DGNS), 09MAY11 (RAMP GUNNER SEAT), 19JUL10-R1 (GARMIN 496), 12JAN10 (DGNS P31), 11JAN10 (ATIRCM),09NOV09 R2 (MILTOPE MSD), 25JUN09 (BFT/SINGLE EDM),10SEP09 (OREGON AERO), 25JUN09 (P3 CHECKVALVE&DECU),10APR09 (CMWS), 13FEB09-R1 (ELT EBC-406HM), 20NOV08 R4(SATCOM), 18JAN08 (ERFS II CONTROL), 16OCT07-R1 (EPUSHA), 18SEP08 (M240 CATCH BAG), 07FEB07 R7 (BFT), 01FEB07(HOVER POWER CHECKS), 17AUG06 (ADV HUD SDC), 31OCT05(UPPER CLAMSHELL DOOR LATCH), 30SEP05 (SPLIT RING),06SEP05 (FLUX VALVE RELOCATION), 29JUN05 (CREW CHIEFSEAT), 28NOV03-R1 (BUBBLE WINDOW LOCATION), 26NOV03(EXT. LENGTH FLARE CABLE). OPERATE AIRCRAFT ASPRESCRIBED IN THE ENCOLSED AIRWORTHINESS RELEASE

AWR WRITE UP WILL BE SIGNEDOFF AS NEW AWRS ARE RELEASEDOR AIRCRAFT HAS NEW AWRS

PID

SYS DATE ACFT HRSNO

V WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 6 02:07:00

HRS




9200307 CH-47D



4. PAGE3. DATE

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 23907.1 O

06

AIRCRAFT RESTRICTED TO FLIGHT OPERTION AT A MAXIMUMOF 100 PERCENT DUAL ENGINE TORQUE, FOR AIRCRAFT THATEXCEED THE 100 PERCENT TORQUE LIMIT CHANGE THESTATUS SYMBOL TO RED X . THE RED X ENTRY SHALL STATEAIRCRAFT SXCEEDED 100PERCENT DUAL ENGINE TORQUELIMIT ATION, REPLACE FWD AND AFT NMAIN TRANSMISSION INACCORDANCE WITH SAFETY OF FLIGHT CH-47-00-03AIRCRAFT WHICH EXCEED THIS LIMITATION AREAUUTHORIZED A ONE TIME FLIGHT TO THE NEARESTMAINTENANCE FACILITY(TRANSCRIBED FROM ULLS-A(E)

PID

SYS DATE ACFT HRSNO

V WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 100 12:36:00

HRS

james.cloud29-Sep-2013

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

O 14443.5 O

00

INSP A103 - AIRCRAFT WASH DUE. Due at: 28-May-2017.Upgrade to Red X Status on 01-Jun-2017

PID

SYS DATE ACFT HRSNO

- WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 1 08:20:32

HRS

COMGEN22-May-2017

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

O 14443.5 O

00

INSP A155 - CORROSION CONTROL INSPECTION,ABBREVIATED, MILD. Due at: 31-May-2017. Upgrade to Red XStatus on 10-Jun-2017

PID

SYS DATE ACFT HRSNO

- WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 2 08:20:32

HRS

COMGEN22-May-2017



9200307 CH-47D



4. PAGE3. DATE

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

O 14450.5 O

04A08

INSP A070 - #1 ENGINE OIL SAMPLE. Due at: 4456.3 Hours.Upgrade to Red X Status on 4461.4 Hours

PID

SYS DATE ACFT HRSNO

- WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 3 08:44:38

HRS

COMGEN22-May-2017

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

O 14450.5 O

04A08

INSP A071 - #2 ENGINE OIL SAMPLE. Due at: 4456.3 Hours.Upgrade to Red X Status on 4461.4 Hours

PID

SYS DATE ACFT HRSNO

- WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 4 08:44:38

HRS

COMGEN22-May-2017

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

O 14450.5 O

00

INSP A088 - PERFORM LUBRICATION IAW LUBRICATIONCHARTS. Due at: 4457.1 Hours. Upgrade to Red X Status on4462.2 Hours

PID

SYS DATE ACFT HRSNO

- WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 5 08:44:38

HRS

COMGEN22-May-2017



9200307 CH-47D



4. PAGE3. DATE

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

O 14450.5 O

04A

INSP A115 - PERFORM ENGINE WATER WASH IAW IETM. Due at:4457.1 Hours. Upgrade to Red X Status on 4462.2 Hours

PID

SYS DATE ACFT HRSNO

- WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 6 08:44:38

HRS

COMGEN22-May-2017

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

O 14450.5 O

06D07

INSP A131 - COMBINING XMSN COOLER FAN VIBRATION TEST.Due at: 4457.1 Hours. Upgrade to Red X Status on 4462.2 Hours

PID

SYS DATE ACFT HRSNO

- WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 7 08:44:38

HRS

COMGEN22-May-2017

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

O 14450.5 O

06C01J

INSP A133 - AFT XMSN COOLER FAN VIBRATION TEST. Due at:4457.1 Hours. Upgrade to Red X Status on 4462.2 Hours

PID

SYS DATE ACFT HRSNO

- WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 8 08:44:38

HRS

COMGEN22-May-2017



9200307 CH-47D



4. PAGE3. DATE

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

O 14450.5 O

00

INSP A145 - PERFORM 50 HR DATA DOWNLOAD ON IVHMSSYSTEM. Due at: 4454.1 Hours. Upgrade to Red X Status on4459.2 Hours

PID

SYS DATE ACFT HRSNO

- WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 9 08:44:38

HRS

COMGEN22-May-2017

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

O 14432.2 O

00


PID

SYS DATE ACFT HRSNO

- WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 1 07:22:00

HRS

COMGEN28-Apr-2017



9200307 CH-47D



4. PAGE3. DATE

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 14022.2 K

00

PERFORM DAILY VISUAL INSPECTIONS REQUIRED BY THEENCLOSED AIRWORTHINESS RELEASE DATED: 08APR14(TRACKING WEDGES), 10OCT13 (EAWIS), 02MAY12 (DUAL EDM),09MAY11 (RAMP GUNNER SEAT),25JUN09 (BFT/SINGLE EDM),13FEB09-R1 (ELT EBC-406HM), 18JAN08 (ERFS II CONTORL),16OCT07-R1 (EPUSHA), 18SEP08 (M240 CATCH BAG), 07FEB07R7 (BFT), 10APR09 (CMWS), 25JUN09 (P3 CHECKVALVE&DECU),20NOV08 (SATCOM), 31OCT05 (UPPER CLAMSHELL DOORLATCH), 06SEP05 (FLUX VALVE RELOCATION), 29 JUN05 (CREWCHIEF SEAT) IN CONJUNTION WITH PMD. PERFORM SPECIALINSPECTIONS REQUIRED BY THE ENCLOSED AIRWORTHINESSRELEASE DATED: 30SEP05 (SPLIT RING).

AWR WRITE UP WILL BE SIGNEDOFF AS NEW AWRS ARE RELEASEDOR AIRCRAFT HAS NEW AWRS

PID

SYS DATE ACFT HRSNO

- WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 7 02:09:00

HRS


DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 24432.2 V

09


PID

SYS DATE ACFT HRSNO

/ WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 2 07:05:00

HRS

joshua.a.biagioni27-Apr-2017



9200307 CH-47D



4. PAGE3. DATE

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 14415.8 X

04


PID

SYS DATE ACFT HRSNO

/ WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 1 09:20:00

HRS

vernon.r.jabson12-Apr-2017

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 24377.2 X

07

HYDRAULIC RETURN LINE AT STA 545 L/H SIDE OF RAMPCROWN SEEPING AT SWAGE

PID

SYS DATE ACFT HRSNO

/ WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 3 11:38:00

HRS

kyle.w.waller10-Feb-2017

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 24357.6 X

02

L/H UPPER C-BOX CLAM SHELL DOOR IRSS BRACKETCRACKED

PID

SYS DATE ACFT HRSNO

/ WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 3 10:24:00

HRS

david.d.shadowen09-Dec-2016



9200307 CH-47D



4. PAGE3. DATE

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT

G 24357.6 X

07


PID

SYS DATE ACFT HRSNO

/ WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

A 4 10:26:00

HRS

david.d.shadowen09-Dec-2016

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT PID

SYS DATE ACFT HRSNO

WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

HRS

DELAY WUC

ACFT HRS MAL EFF

TIPID TI MANHOURS

PID HRSPID HRS CAT

HOW RECWHEN DISC

CATCAT PID

SYS DATE ACFT HRSNO

WUC

FAULTS/REMARKS

ROUNDS ACTION CODE


ACTION

HRS


DATE _______________________________________ Page ___________

12. CAT 13. MMH8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID

7. FAULT

6. FAULT NUMBER5. FAULT DATE

2. SERIAL NUMBER 3. SYSTEM CODE1. STATUS 4. TIME

DA FORM 2408-13-2, NOV 91, MAY BE USED. For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

DA FORM 2408-13-2, OCT 1997 RELATED MAINTENANCE ACTIONS RECORD

Page ___________

Engine InformationEngine Serial #: GA75189 Downloaded on: 2017/05/22 12:50:44Controller Serial #: None Version: GSE 3.0Controller Type: DECU Data origin: GSE 3.0

Page 1

Engine HistoryEngine Hrs 2156.9Engine Starts 525Controller Hrs 7Utilization Hrs 0.0Mjr N1 Cycles 106Mnr N1 Cycles 418

Power Assurance Check

Record EngineHr T4.5°C (°F) T1°C (°F) P1

[psia]

Q [% of1300ft-

lbs]PACN Fuel Flow

[pph]T4.5 Mrg°C (°F)

T4.5 MrgAdj °C (°F)

N1 Mrg[% 18,720

rpm]

N1 Mrg Adj[% 18,720

rpm]

EngConfig



[psia]

Q [% of1300ft-

lbs]PACN Fuel Flow



N1 Mrg[% 18,720

rpm]

N1 Mrg Adj[% 18,720

rpm]

EngConfig

Baseline Power Assurance Test


[psia]

Q [% of1300ft-

lbs]PATN Fuel Flow

[pph]PAT

TriggerN1

[% 18,720 rpm]Eng

Config



[psia]

Q [% of1300ft-

lbs]PATN Fuel Flow

[pph]PAT

TriggerN1

[% 18,720 rpm]Eng

Config

Engine Health Trend (PAT Margin)

Insufficient points to plot.



Generated from C:\Users\wgatlin\Desktop\GA75189_None_20170522_125022_9200307_1.adf on 2017/05/22 12:54:12

T4.5 Exceedances> 866°C (1590°F) Part [mins] 1.0> 882°C (1620°F) Part [mins] 0.0> 918°C (1685°F) Part [mins] 0.0> 899°C (1650°F) Maint [mins] 0.0> 932°C (1710°F) Maint [secs] 0.0> 943°C (1730°F) Maint [secs] 0.0


Torque Exceedances> 123% (sec) 0.0> 128% (sec) 0.0> 154% (sec) 0.0


N2 Exceedances> 102% (sec) 14.4> 106% (sec) 0.0> 111.5% (sec) 0.0


Component Life Cycles Initial Calculated

3rd Compressor Disk 867 1142GP Sealing Plate 238 432GP Spacer 228 4091st Turbine Disk 1573 16902nd Turbine Disk 214 3723rd Turbine Disk 527 10544th Turbine Disk 503 1028



Page 2

Daily Power Assurance Test


[psia]

Q [% of1300ft-

lbs]PATN Fuel Flow

[pph]PAT

MarginN1

[% 18,720 rpm]Eng

Config



[psia]

Q [% of1300ft-

lbs]PATN Fuel Flow

[pph]PAT

MarginN1

[% 18,720 rpm]Eng

Config



Page 1

Engine HistoryEngine Hrs 3222.2Engine Starts 600Controller Hrs 7Utilization Hrs 0.0Mjr N1 Cycles 177Mnr N1 Cycles 489



[psia]

Q [% of1300ft-

lbs]PACN Fuel Flow



N1 Mrg[% 18,720

rpm]

N1 Mrg Adj[% 18,720

rpm]

EngConfig



[psia]

Q [% of1300ft-

lbs]PACN Fuel Flow



N1 Mrg[% 18,720

rpm]

N1 Mrg Adj[% 18,720

rpm]

EngConfig



[psia]

Q [% of1300ft-

lbs]PATN Fuel Flow

[pph]PAT

TriggerN1

[% 18,720 rpm]Eng

Config



[psia]

Q [% of1300ft-

lbs]PATN Fuel Flow

[pph]PAT

TriggerN1

[% 18,720 rpm]Eng

Config












Component Life Cycles Initial Calculated

3rd Compressor Disk 1005 1351GP Sealing Plate 1722 1988GP Spacer 1709 19611st Turbine Disk 1664 18522nd Turbine Disk 348 5773rd Turbine Disk 1183 17834th Turbine Disk 3213 3813



Page 2



[psia]

Q [% of1300ft-

lbs]PATN Fuel Flow

[pph]PAT

MarginN1

[% 18,720 rpm]Eng

Config



[psia]

Q [% of1300ft-

lbs]PATN Fuel Flow

[pph]PAT

MarginN1

[% 18,720 rpm]Eng

Config


INSP

NO WUC

LAST DONE

DATE ACFT HRS

NEXT DUE

DATE ACFT HRS FREQ DESCRIPTION

MDS: CH-47D SERIAL NO: 9200307

Report Date: AUTOMATED 2408-18 LAST/NEXT DUE 1/522-May-2017

00 PREVENTIVE MAINTENANCE DAILY15-May-2017 29-May-2017 14 DaysA002

04A 14 DAY ENGINE RUN REQUIRED15-May-2017 29-May-2017 14 DaysA014

06H04B VISUAL INSPECT OUTBOARD DRIVE SHAFTLUGS ADAPTER

4468.5 254443.5 HoursA040

04A08 #1 ENGINE OIL SAMPLE4456.3 504406.3 HoursA070

04A08 #2 ENGINE OIL SAMPLE4456.3 504406.3 HoursA071

06C01 AFT XMSN OIL SAMPLE DUE4507.1 4004107.1 HoursA072

06B02 FWD XMSN OIL SAMPLE DUE4507.1 4004107.1 HoursA073

06E01 #2 ENGINE MECHANICAL XMSN OIL SAMPLEDUE

4507.1 4004107.1 HoursA074

06D01 ENGINE COMBINING XMSN OIL SAMPLE DUE4507.1 4004107.1 HoursA075

06E01 #1 ENGINE MECHANICAL XMSN OIL SAMPLEDUE

4507.1 4004107.1 HoursA081

00 PERFORM LUBRICATION IAW LUBRICATIONCHARTS

4457.1 504407.1 HoursA088

09B01A 30 DAY SLAB BATTERY INSPECTION (M8565/11-1)

01-May-2017 31-May-2017 30 DaysA092

00 AIRCRAFT WASH DUE28-Apr-2017 28-May-2017 30 DaysA103

INSP

NO WUC

LAST DONE

DATE ACFT HRS

NEXT DUE




04A PERFORM ENGINE WATER WASH IAW IETM4457.1 504407.1 HoursA115

04A08E #1 ENGINE DUAL CHIP DETECTOR FORCONTINUITY

4468.5 254443.5 HoursA128

04A08E #2 ENGINE DUAL CHIP DETECTOR FORCONTINUITY

4468.5 254443.5 HoursA129

06D07 COMBINING XMSN COOLER FAN VIBRATIONTEST

4457.1 504407.1 HoursA131

06C01J AFT XMSN COOLER FAN VIBRATION TEST4457.1 504407.1 HoursA133

00 PERFORM 50 HR DATA DOWNLOAD ON IVHMSSYSTEM

4454.1 504404.1 HoursA145

00 CORROSION CONTROL INSPECTION,ABBREVIATED, MILD

02-Mar-2017 31-May-2017 90 DaysA155

19R 90 DAY/100 HOUR ELT SELF-TEST INSPECTION11-May-2017 09-Aug-2017 90 DaysA170

19R 90 DAY/100 HOUR ELT SELF-TEST INSPECTION4539.5 1004439.5 HoursA170

00 90 DAY REVIEW/UPDATE OF 365-4 ENTRIES15-Mar-2017 13-Jun-2017 90 DaysA177

00 PERFORM LUBRICATION REQUIREMENTS IAWLUBE CHARTS

4506.3 1004406.3 HoursA180

05 INSP FWD AFT SWASHPLATE BEARING IAWSOF CH-47-04-01

4506.3 1004406.3 HoursA182

05A03A02A INSPECT FWD AFT SWASHPLATE ROTATINGRING CH-47-07-SOF-

4507.1 2004307.1 HoursA190

02C11 5000LB TIE DOWN ADAPTER RINGS INSP4507.1 2004307.1 HoursA191

INSP

NO WUC

LAST DONE

DATE ACFT HRS

NEXT DUE




02C #1 #2 ENGINE XMSN FAIRING4506.3 1004406.3 HoursA196

05A03C TORQUE CHECK FWD PITCH LINK BOLTS4507.1 1004407.1 HoursA202

05B03B TORQUE CHECK AFT PITCH LINK BOLTS4506.3 1004406.3 HoursA204

04A06A PERFORM 50 HR ENGINE DECU DOWNLOAD4493.5 504443.5 HoursA210

06D01 INSPECT THE COMBINING XMSN COOLING FANSHAFT PER TASK

4506.3 1004406.3 HoursA216

06D01 CHECK COMBINING XMS COOLING FAN SHAFTOUTPUT GEAR SPLIN

4506.3 1004406.3 HoursA217

02C10B02 INSPECTION OF AFT CONNECTING LINK (TASK4-37)

4507.1 2004307.1 HoursA262

00 PERFORM LUBRICATION REQUIREMENTS IAWLUBE CHARTS

4507.1 2004307.1 HoursA264

00 PERFORM PMS2 CYCLE INSPECTION4707.1 4004307.1 HoursA280

05B01L INSP HORIZONTAL HINGE PIN BEARING (AFTHEAD)

25-Jul-2016 25-Jul-2018 24 MonthsA365

05A01Q INSP HORIZONTAL HINGE PIN BEARING (FWDHEAD)

25-Jul-2016 25-Jul-2018 24 MonthsA366

00 PERFORM LUBRICATION REQUIREMENT IAWLUBE CHART

4507.1 4004107.1 HoursA370

00 PERFORM PMS3 CYCLE INSPECTION4507.1 4004107.1 HoursA380

INSP

NO WUC

LAST DONE

DATE ACFT HRS

NEXT DUE




02C10A EDDY CURRENT NO. 1 FWD MOUNT4570.1 6003970.1 HoursA390

02C10A EDDY CURRENT NO.2 FWD MOUNT4570.1 6003970.1 HoursA391

10D INSPECT FUEL TANK ASSEMBLIES4529.8 12003329.8 HoursA460

10 INSPECT FUEL BOOST PUMP POWER WIREHARNESS

4529.8 12003329.8 HoursA478

17B CF3BR FIRE EXTINGUISHER WEIGHT TEST &INSPECTION

02-Mar-2017 29-Aug-2017 180 DaysA496

00 CORROSION CONTROL INSPECTION, IN-DEPTH, MILD

16-Mar-2017 12-Sep-2017 180 DaysA500

00 AMSS SURVIVAL KIT INSPECTION17-Jul-2016 12-Jul-2017 360 DaysA505

19R ANNUAL G-SWITCH ELT INSPECTION09-Feb-2017 09-Feb-2018 12 MonthsA520

00 AIRCRAFT EQUIPMENT INVENTORY (DA FORM2408-17)

29-May-2016 29-May-2017 12 MonthsA530

08A09 COMPASS SWING02-Mar-2017 02-Mar-2018 12 MonthsA532

17A FIRST AID KIT INSPECTION02-Nov-2016 02-Nov-2017 12 MonthsA534

00 AIRCRAFT WEIGHING INVENTORY (365-1)02-Apr-2017 02-Apr-2018 12 MonthsA553

08A07 HSI/RMI FOR CORRECT READINGS02-Mar-2017 02-Mar-2018 12 MonthsA558

12C ENGINE FIRE EXTINGUISHER SYSTEMINSPECTION

24-Sep-2016 24-Sep-2017 12 MonthsA563

INSP

NO WUC

LAST DONE

DATE ACFT HRS

NEXT DUE




12C01 ENGINE FIRE BOTTLE FOR WEIGHT18-Sep-2016 18-Sep-2017 12 MonthsA564

09B01A RETURN SLAB TO AVIM FOR CAPACITY CHECK01-Feb-2016 01-Feb-2018 24 MonthsA580

17A AIRCRAFT WEIGHING CLASS 102-Apr-2017 02-Apr-2020 36 MonthsA649

09B01A REPLACEMENT OF BATTERY (SLAB M8565/11-1)

05-Jan-2016 05-Jan-2019 36 MonthsA660

19R REPLACE ELT BATTERY GS-4630-Jun-2014 30-Jun-2019 60 MonthsA670

12C04 ENGINE FIRE EXTINGUISHER (#1 AFT) MH-9231-Jan-2017 31-Jul-2026 114 MonthsA690

12C04 ENGINE FIRE EXTINGUISHER (#2 AFT) MH-9231-Jan-2017 31-Jul-2026 114 MonthsA699

12C04 ENGINE FIRE EXTINGUISHER (# 1FWD), MH-9231-Jan-2017 31-Jul-2026 114 MonthsA700

12C04 ENGINE FIRE EXTINGUISHER (#2 FWD) MH-9231-Jan-2017 31-Jul-2026 114 MonthsA710

19R INSPECT ELT BATTERY11-May-2017 09-Aug-2017 90 DaysE230

19F02 REPLACE APX-118 TRANSPONDER BATTERY21-Mar-2017 21-Sep-2017 6 MonthsE351

Current Status A:

9200307CH-47D

K6U666FOR:

22-May-2017 To01-Jan-2010Selection Range :

V Current Status E: Current Status O: Current Status W:

NEXT PHASE: 4507.1 LAST MISSION: 21-May-2017

MODEL: SERIAL NUMBER: HOURS: 4450.5

OPEN FAULT REPORT

Report Date:

Page 1 of 7

22-May-2017

DELAY

0miranda.m.moore

TIPID MMH

0F062GO

WHEN HOW MAL MAINT DEFERRED

DISC REC EFF

WUC

TYPE DAYS

00

WUC

29-Sep-2013 29-Sep-201312:36 PM

FAULT CLOSED. TRANSCRIBED TO AIRCRAFT LOGBOOK BYULLSA PHASE CLOSEOUT. Oct 4 2013 4:59AM)

03907.1

AIRCRAFT RESTRICTED TO FLIGHT OPERTION AT A MAXIMUM OF100 PERCENT DUAL ENGINE TORQUE, FOR AIRCRAFT THATEXCEED THE 100 PERCENT TORQUE LIMIT CHANGE THE STATUSSYMBOL TO RED X . THE RED X ENTRY SHALL STATE AIRCRAFTSXCEEDED 100PERCENT DUAL ENGINE TORQUE LIMIT ATION,REPLACE FWD AND AFT NMAIN TRANSMISSION IN ACCORDANCEWITH SAFETY OF FLIGHT CH-47-00-03 AIRCRAFT WHICH EXCEEDTHIS LIMITATION ARE AUUTHORIZED A ONE TIME FLIGHT TO THENEAREST MAINTENANCE FACILITY(TRANSCRIBED FROM ULLS-A(E)PHASE: WJEQB03250002 ON Oct 4 2013 4:59AM)

3907.1james.cloud1005A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY

CODE DATE / TIME NO STATUS PID HOURS

FAULT WRITE-UP:

V

PID

0

TYPEMMH

AWR WRITE UP WILL BE SIGNED OFF AS NEW AWRS ARERELEASED OR AIRCRAFT HAS NEW AWRS ADDED

DELAY

0

TIPID MMH

0F001GK


DISC REC EFF

WUC

TYPE DAYS

WUC

07-May-2014 2:07 PM 00

OPERATE WITHIN LIMITATIONS AND RESTRICTIONS SPECIFIED INTHE ENCLOSED AIRWORTHINESS RELEASE DATED: 30APR14(HYDRO-MECH ASSY), 08APR14 R1 (TRACKING WEDGES), 21JAN14R3 (IPAD), 20MAR13 R4 (EMC-100 ECU), 10DEC13 R16 (MSPU),10JUL12 (IRSS), 10OCT13 (EAWIS), 16MAY12 R1 (LOG BOOKLAPTOP), 02MAY12 (DUAL EMD) 24OCT13 R2 (DGNS), 09MAY11(RAMP GUNNER SEAT), 19JUL10-R1 (GARMIN 496), 12JAN10 (DGNSP31), 11JAN10 (ATIRCM), 09NOV09 R2 (MILTOPE MSD), 25JUN09(BFT/SINGLE EDM), 10SEP09 (OREGON AERO), 25JUN09 (P3CHECKVALVE&DECU), 10APR09 (CMWS), 13FEB09-R1 (ELT EBC-406HM), 20NOV08 R4 (SATCOM), 18JAN08 (ERFS II CONTROL),16OCT07-R1 (EPUSHA), 18SEP08 (M240 CATCH BAG), 07FEB07 R7(BFT), 01FEB07 (HOVER POWER CHECKS), 17AUG06 (ADV HUDSDC), 31OCT05 (UPPER CLAMSHELL DOOR LATCH), 30SEP05(SPLIT RING), 06SEP05 (FLUX VALVE RELOCATION), 29JUN05(CREW CHIEF SEAT), 28NOV03-R1 (BUBBLE WINDOW LOCATION),26NOV03 (EXT. LENGTH FLARE CABLE). OPERATE AIRCRAFT ASPRESCRIBED IN THE ENCOLSED AIRWORTHINESS RELEASEDATED 26MAR08 (AVA SINGLE CAM. MOUNT).

4022.2robert.d.childers6A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

V

PID

0

TYPEMMH

Current Status A:

9200307CH-47D

K6U666FOR:





OPEN FAULT REPORT

Report Date:

Page 2 of 7

22-May-2017

DELAY

0

TIPID MMH

0F001GX


DISC REC EFF

WUC

TYPE DAYS

WUC

10-Dec-2016 2:57 PM 00

AFT 3MAN TRROP SEAT LATCH POST ON 2ND 3MAN SEAT ON L/HSIDE BROKE AIRCRAFT RESTRICTED TO 29 PASSENGERS

4359.8joshua.r.childers1A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

V

PID

0

TYPEMMH

AWR WRITE UP WILL BE SIGNED OFF AS NEW AWRS ARERELEASED OR AIRCRAFT HAS NEW AWRS ADDED

DELAY

0

TIPID MMH

0F001GK


DISC REC EFF

WUC

TYPE DAYS

WUC

07-May-2014 2:09 PM 00

PERFORM DAILY VISUAL INSPECTIONS REQUIRED BY THEENCLOSED AIRWORTHINESS RELEASE DATED: 08APR14(TRACKING WEDGES), 10OCT13 (EAWIS), 02MAY12 (DUAL EDM),09MAY11 (RAMP GUNNER SEAT),25JUN09 (BFT/SINGLE EDM),13FEB09-R1 (ELT EBC-406HM), 18JAN08 (ERFS II CONTORL),16OCT07-R1 (EPUSHA), 18SEP08 (M240 CATCH BAG), 07FEB07 R7(BFT), 10APR09 (CMWS), 25JUN09 (P3 CHECKVALVE&DECU),20NOV08 (SATCOM), 31OCT05 (UPPER CLAMSHELL DOOR LATCH),06SEP05 (FLUX VALVE RELOCATION), 29 JUN05 (CREW CHIEFSEAT) IN CONJUNTION WITH PMD. PERFORM SPECIALINSPECTIONS REQUIRED BY THE ENCLOSED AIRWORTHINESSRELEASE DATED: 30SEP05 (SPLIT RING).

4022.2robert.d.childers7A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

-

PID

0

TYPEMMH

DELAY

0

TIPID MMH

0F001OO


DISC REC EFF

WUC

TYPE DAYS

WUC

28-Apr-2017 7:22 AM 00


4432.21A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

-

PID

0

TYPEMMH

Current Status A:

9200307CH-47D

K6U666FOR:





OPEN FAULT REPORT

Report Date:

Page 3 of 7

22-May-2017

DELAY

0

TIPID MMH

0F001OO


DISC REC EFF

WUC

TYPE DAYS

WUC

22-May-2017 8:20 AM 00

INSP A103 - AIRCRAFT WASH DUE. Due at: 28-May-2017. Upgrade toRed X Status on 01-Jun-2017

4443.51A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

-

PID

0

TYPEMMH

DELAY

0

TIPID MMH

0F001OO


DISC REC EFF

WUC

TYPE DAYS

WUC

22-May-2017 8:20 AM 00

INSP A155 - CORROSION CONTROL INSPECTION, ABBREVIATED,MILD. Due at: 31-May-2017. Upgrade to Red X Status on 10-Jun-2017

4443.52A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

-

PID

0

TYPEMMH

DELAY

0

TIPID MMH

0F04A081OO


DISC REC EFF

WUC

TYPE DAYS

WUC

22-May-2017 8:44 AM 00

INSP A070 - #1 ENGINE OIL SAMPLE. Due at: 4456.3 Hours. Upgradeto Red X Status on 4461.4 Hours

4450.53A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

-

PID

0

TYPEMMH

Current Status A:

9200307CH-47D

K6U666FOR:





OPEN FAULT REPORT

Report Date:

Page 4 of 7

22-May-2017

DELAY

0

TIPID MMH

0F04A081OO


DISC REC EFF

WUC

TYPE DAYS

WUC

22-May-2017 8:44 AM 00

INSP A071 - #2 ENGINE OIL SAMPLE. Due at: 4456.3 Hours. Upgradeto Red X Status on 4461.4 Hours

4450.54A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

-

PID

0

TYPEMMH

DELAY

0

TIPID MMH

0F001OO


DISC REC EFF

WUC

TYPE DAYS

WUC

22-May-2017 8:44 AM 00

INSP A088 - PERFORM LUBRICATION IAW LUBRICATION CHARTS.Due at: 4457.1 Hours. Upgrade to Red X Status on 4462.2 Hours

4450.55A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

-

PID

0

TYPEMMH

DELAY

0

TIPID MMH

0F04A1OO


DISC REC EFF

WUC

TYPE DAYS

WUC

22-May-2017 8:44 AM 00

INSP A115 - PERFORM ENGINE WATER WASH IAW IETM. Due at:4457.1 Hours. Upgrade to Red X Status on 4462.2 Hours

4450.56A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

-

PID

0

TYPEMMH

Current Status A:

9200307CH-47D

K6U666FOR:





OPEN FAULT REPORT

Report Date:

Page 5 of 7

22-May-2017

DELAY

0

TIPID MMH

0F06D071OO


DISC REC EFF

WUC

TYPE DAYS

WUC

22-May-2017 8:44 AM 00

INSP A131 - COMBINING XMSN COOLER FAN VIBRATION TEST. Dueat: 4457.1 Hours. Upgrade to Red X Status on 4462.2 Hours

4450.57A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

-

PID

0

TYPEMMH

DELAY

0

TIPID MMH

0F06C01J1OO


DISC REC EFF

WUC

TYPE DAYS

WUC

22-May-2017 8:44 AM 00

INSP A133 - AFT XMSN COOLER FAN VIBRATION TEST. Due at:4457.1 Hours. Upgrade to Red X Status on 4462.2 Hours

4450.58A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

-

PID

0

TYPEMMH

DELAY

0

TIPID MMH

0F001OO


DISC REC EFF

WUC

TYPE DAYS

WUC

22-May-2017 8:44 AM 00

INSP A145 - PERFORM 50 HR DATA DOWNLOAD ON IVHMSSYSTEM. Due at: 4454.1 Hours. Upgrade to Red X Status on 4459.2Hours

4450.59A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

-

PID

0

TYPEMMH

Current Status A:

9200307CH-47D

K6U666FOR:





OPEN FAULT REPORT

Report Date:

Page 6 of 7

22-May-2017

DELAY

0

TIPID MMH

0F022GX


DISC REC EFF

WUC

TYPE DAYS

WUC

09-Dec-2016 10:24 AM 00

L/H UPPER C-BOX CLAM SHELL DOOR IRSS BRACKET CRACKED

4357.6david.d.shadowens3A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

/

PID

0

TYPEMMH

DELAY

0

TIPID MMH

0F072GX


DISC REC EFF

WUC

TYPE DAYS

WUC

09-Dec-2016 10:26 AM 00


4357.6david.d.shadowens4A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

/

PID

0

TYPEMMH

DELAY

0

TIPID MMH

0F072GX


DISC REC EFF

WUC

TYPE DAYS

WUC

10-Feb-2017 11:38 AM 00

HYDRAULIC RETURN LINE AT STA 545 L/H SIDE OF RAMP CROWNSEEPING AT SWAGE

4377.2kyle.w.waller3A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

/

PID

0

TYPEMMH

Current Status A:

9200307CH-47D

K6U666FOR:





OPEN FAULT REPORT

Report Date:

Page 7 of 7

22-May-2017

DELAY

0

TIPID MMH

0F041GX


DISC REC EFF

WUC

TYPE DAYS

WUC

12-Apr-2017 9:20 AM 00


4415.8vernon.r.jabson1A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

/

PID

0

TYPEMMH

DELAY

0

TIPID MMH

0F092GV


DISC REC EFF

WUC

TYPE DAYS

WUC

27-Apr-2017 7:05 PM 00


4432.2joshua.a.biagioni2A

ROUNDS ACTCODE

CORRECTION

DATE / TIME HOURS

ACTION TAKEN:

SYSTEMDISCOVERY


FAULT WRITE-UP:

/

PID

0

TYPEMMH

STATUS

VMDS

CH-47D

SER NO

9200307 4450.5

CURR HOURS CURR ROUND

0

LANDINGS

4598

APU STARTS

1344

CYCLES

0

APU HOURS

419.7

Report Date: SHORT LIFE REPORT (SLR) 1/422-May-2017

FREQInspection NarrativeInspec No. NEXT DUETILL DUETYPE

14PREVENTIVE MAINTENANCE DAILYA002 29-May-20177D

1414 DAY ENGINE RUN REQUIREDA014 29-May-20177D

25VISUAL INSPECT OUTBOARD DRIVE SHAFT LUGS ADAPTERA040 4468.518H

50#1 ENGINE OIL SAMPLEA070 4456.35.8H

50#2 ENGINE OIL SAMPLEA071 4456.35.8H

400AFT XMSN OIL SAMPLE DUEA072 4507.156.6H

400FWD XMSN OIL SAMPLE DUEA073 4507.156.6H

400#2 ENGINE MECHANICAL XMSN OIL SAMPLE DUEA074 4507.156.6H

400ENGINE COMBINING XMSN OIL SAMPLE DUEA075 4507.156.6H

400#1 ENGINE MECHANICAL XMSN OIL SAMPLE DUEA081 4507.156.6H

50PERFORM LUBRICATION IAW LUBRICATION CHARTSA088 4457.16.6H

3030 DAY SLAB BATTERY INSPECTION (M8565/11-1)A092 31-May-20179D

30AIRCRAFT WASH DUEA103 28-May-20176D

50PERFORM ENGINE WATER WASH IAW IETMA115 4457.16.6H

25#1 ENGINE DUAL CHIP DETECTOR FOR CONTINUITYA128 4468.518H

25#2 ENGINE DUAL CHIP DETECTOR FOR CONTINUITYA129 4468.518H

50COMBINING XMSN COOLER FAN VIBRATION TESTA131 4457.16.6H

50AFT XMSN COOLER FAN VIBRATION TESTA133 4457.16.6H

50PERFORM 50 HR DATA DOWNLOAD ON IVHMS SYSTEMA145 4454.13.6H

90CORROSION CONTROL INSPECTION, ABBREVIATED, MILDA155 31-May-20179D

9090 DAY/100 HOUR ELT SELF-TEST INSPECTIONA170 09-Aug-201779D

10090 DAY/100 HOUR ELT SELF-TEST INSPECTIONA170 4539.589H

9090 DAY REVIEW/UPDATE OF 365-4 ENTRIESA177 13-Jun-201722D

100PERFORM LUBRICATION REQUIREMENTS IAW LUBE CHARTSA180 4506.355.8H

100INSP FWD AFT SWASHPLATE BEARING IAW SOF CH-47-04-01A182 4506.355.8H

STATUS

VMDS

CH-47D

SER NO

9200307 4450.5


0

LANDINGS

4598

APU STARTS

1344

CYCLES

0

APU HOURS

419.7


200INSPECT FWD AFT SWASHPLATE ROTATING RING CH-47-07-

SOF-A190 4507.156.6H

2005000LB TIE DOWN ADAPTER RINGS INSPA191 4507.156.6H

100#1 #2 ENGINE XMSN FAIRINGA196 4506.355.8H

100TORQUE CHECK FWD PITCH LINK BOLTSA202 4507.156.6H

100TORQUE CHECK AFT PITCH LINK BOLTSA204 4506.355.8H

50PERFORM 50 HR ENGINE DECU DOWNLOADA210 4493.543H

100INSPECT THE COMBINING XMSN COOLING FAN SHAFT PER

TASKA216 4506.355.8H

100CHECK COMBINING XMS COOLING FAN SHAFT OUTPUT

GEAR SPLINA217 4506.355.8H

200INSPECTION OF AFT CONNECTING LINK (TASK 4-37)A262 4507.156.6H

200PERFORM LUBRICATION REQUIREMENTS IAW LUBE CHARTSA264 4507.156.6H

400PERFORM PMS2 CYCLE INSPECTIONA280 4707.1256.6H

400PERFORM LUBRICATION REQUIREMENT IAW LUBE CHARTA370 4507.156.6H

400PERFORM PMS3 CYCLE INSPECTIONA380 4507.156.6H

600EDDY CURRENT NO. 1 FWD MOUNTA390 4570.1119.6H

600EDDY CURRENT NO.2 FWD MOUNTA391 4570.1119.6H

1200INSPECT FUEL TANK ASSEMBLIESA460 4529.879.3H

1200INSPECT FUEL BOOST PUMP POWER WIRE HARNESSA478 4529.879.3H

180CF3BR FIRE EXTINGUISHER WEIGHT TEST & INSPECTIONA496 29-Aug-201799D

180CORROSION CONTROL INSPECTION, IN-DEPTH, MILDA500 12-Sep-2017113D

360AMSS SURVIVAL KIT INSPECTIONA505 12-Jul-201751D

12AIRCRAFT EQUIPMENT INVENTORY (DA FORM 2408-17)A530 29-May-20177M

12FIRST AID KIT INSPECTIONA534 02-Nov-2017164M

12ENGINE FIRE EXTINGUISHER SYSTEM INSPECTIONA563 24-Sep-2017125M

12ENGINE FIRE BOTTLE FOR WEIGHTA564 18-Sep-2017119M

90INSPECT ELT BATTERYE230 09-Aug-201779D

STATUS

VMDS

CH-47D

SER NO

9200307 4450.5


0

LANDINGS

4598

APU STARTS

1344

CYCLES

0

APU HOURS

419.7


6REPLACE APX-118 TRANSPONDER BATTERYE351 21-Sep-2017122M

Component Listing for 16 Items

PART NOMENCLATUREPART NOWUC

AIRCRAFTCURR DUE

HRS TOREPLACESERIAL NONSN

DISK ASSY, 2NDTURBINE

04A03C 2-121-110-35 4450.5 -1150.52840-01-479-5681 81365101304 3300

HYDROMECHANICALASSY

04A05A 110700-02D6 4450.5 -1650.52915-01-371-9305 1159901370739 2800

HYDROMECHANICALASSY

04A05A 2-170-580-02 4450.5 -1650.52915-01-371-9305 99AJW310 2800

BEARING, VERT PIN05A01O01 114RS214-6 4450.5 394.53110-00-455-6179 201001771 4845



BEARING, VERT PIN(LOWER)

05A01O02 114RS214-5 4450.5 856.53110-00-455-6188 AZN1833 5307


05A01O02 114RS214-5 4450.5 511.53110-00-455-6188 AZN693 4962


05A01O02 114RS214-5 4450.5 699.53110-00-455-6188 BDH181 5150

HORZ PIN BEARING05A01Q01 114RS225-1 4450.5 511.53110-01-311-0024 AZN1007 4962



HORZ PIN BEARING05A01Q02 114RS226-1 4450.5 511.53110-01-310-2258 201200126 4962

HORZ PIN BEARING05A01Q02 114RS226-1 4450.5 511.53110-01-310-2258 A705 4962


SWASHPLATE ASSY05A03A 145R3551-17 4450.5 279.51615-01-395-0006 2007A9586 4730

SWASHPLATE BEARING05A03A04 114RS308-2 4450.5 279.53110-01-356-0489 BDH20115351 4730

BEARING, VERT PIN05B01J01 114RS214-6 4450.5 386.53110-00-455-6179 BDH1975 4837




05B01J02 114RS214-5 4450.5 386.53110-00-455-6188 BDH11562 4837


05B01J02 114RS214-5 4450.5 386.53110-00-455-6188 BDH11563 4837


05B01J02 114RS214-5 4450.5 386.53110-00-455-6188 BDH11564 4837

PIN HORIZONTALHINGE

05B01K 114R2197-7 4450.5 608.55315-01-295-7008 FM3736 5059

HORZ PIN BEARING05B01L01 114RS225-1 4450.5 386.53110-01-311-0024 200900984 4837



HORZ PIN BEARING05B01L02 114RS226-1 4450.5 608.53110-01-310-2258 N42792 5059

SWASHPLATE ASSY05B03A 145R3551-18 4450.5 456.51615-01-395-0007 A841161 4907

STATUS

VMDS

CH-47D

SER NO

9200307 4450.5


0

LANDINGS

4598

APU STARTS

1344

CYCLES

0

APU HOURS

419.7


SWASHPLATE BEARING05B03A04 114RS308-2 4450.5 456.53110-01-356-0489 BDH201111089 4907

SHAFT ASSY, AFTVERTICAL

06H02 145D3300-6 4450.5 900.51680-01-320-1191 A508 5351

ADAPTER ASSY ENG D/SOUTB

06H04B 145D3500-16 4450.5 827.51615-01-319-5091 A4701 5278

PART NOWUC

Component Listing for 16-1 Items

PART NOMENCLATURE NSN SERIAL NO

HRS TOREPLACE

ENGINECURR DUE

PART NOWUC

Component Listing for 16-2 Items


STARTSTOREPLACE

APUCURR DUE

Component Listing for 76F01 Items

PART NOMENCLATUREPART NOWUC

METERCURR DUE

HRS TOREPLACESERIAL NONSN

PART NOWUC

Component Listing for 714 Engines


HRS TOREPLACE

ENGINECURR DUE

2-170-580-02 2604HYDROMECHANICALASSY

04A05A 99AJW310 2800 1962915-01-371-9305

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