⚑ Agent Identified Eitri-Agent-447APU Records Analysis
DA Form contained all necessary data to calculate APU times from the index-recorder
readings. No agent reconnaissance of significant history was required.
Date 2019-05-16
CAGE: 55820 PN: 116305-302 NSN: 2835013692818 SN: SPE122584 Nomen: AUXILIARY POWER UNIT Date: 2019-05-16 Remark: APU WAS OVERHAULED FOR NMP I/A/W DMWR 1-2835-209. CLEANED, INSPECTED, REPLACED ALL FUEL AND OIL FILTERS. REPLACED ROTOR ASSY, INLET, FUEL PUMP, EXCITER, AND WIRING HARNESS. APU TESTED/PASSED. OIL SAMPLE NORMAL. TBO FOR APU IS 6327 SSN/6327 METER EVENTS. TSN 51. ENTERED BY ERIC L COZINE CIV TI ESRA FTCKY LRC-A CAMPBELL. DSN 541-4659 Entered By: Cozine, Eric L UIC: W0H95C Location: Ft. Campbell, KY
APU Subcomponents
8 items
⚠APU calculations need index readings; information presented is APU information at install only.
AUXILIARY POWER UNIT
PN 116305-302APUHOURSCONDCond Hours
TSN (hrs) at install
51.0
DueCondComp install (hrs)51
Used:
—Remaining:
—⌛ needs recorder input
— % Life
PB $205,235 FN
PB $217,500 NE
PB $180,000 OH
PB $160,000 OR
PB $250,000 RP
PB $175,000 SV
SM $71,193 OH
SM $114,436 NE
AUXILIARY POWER UNIT
PN 116305-302APUSTARTSPASS6000.0 Starts
Component lifecycle analysis across airframe and engines
Engine
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Part-Out Valuation
Analyst-adjustable pricing breakdown — every component, source, and discount is tunable
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Records Search
Semantic search across 987
maintenance records (243 faults, 744 historical entries) for this airframe.
Type maintenance shorthand, part numbers, or plain English.
Risk Analysis
Pre-baked categorized risk review across the full corpus. Generated
2026-06-29
using claude-sonnet-4-5-20250929.
This aircraft has multiple open operational restrictions and deferred maintenance items that affect airworthiness. The aircraft is restricted to day VFR operations due to trim inoperative, requires daily visual inspections per AWR 744, and has several deferred inspections awaiting return to home station. Additionally, aft soundproofing is not installed.
Fault
2025-05-149,288.7 hrshigh
Aircraft restricted to day VFR operations due to trim inoperative and other AWR limitations requiring daily visual inspections.
OPERATE WITHIN THE LIMITATIONS PRESCRIBED IN THE ENCLOSED AWR’ S: AWR2294R3 DTD 28 OCT 24 (PPA); AWR 2277R2 DTD 27SEP24 (Geta c T800 Windows 10 Tablet); AWR 2261R3 DTD 5APR25 (EFB); AWR 2 190 R7 DTD 3FEB25 (HIGH FOM ANVIS) AWR 2122R8…
Fault
2025-06-309,310.7 hrshigh
Aft soundproofing not installed in aircraft, open discrepancy affecting cabin configuration.
Aft Soundproofing not installed in aircraft | status: open | recorded 2025-06-30 @ 9310.7h
Fault
2025-05-149,288.7 hrsmedium
Swashplate lubrication deferred until home station, affecting scheduled maintenance compliance.
DEFERED UNTIL HOME STATION (FORT CAVAZOS) INSP A299 LUBRICATE SWASHPLATE FOR HELICPTR UTIL UH-60L CAGE: 78286 PN: UH-60L NSN : 1520012984532 SN: 9226445 WAS DUE. STATUS UPGRADED TO X ON: 9622.9 AIRCRAFT HOURS OR 14 APR 2025 REFERENCE:…
Fault
2025-04-269,284.2 hrsmedium
Tail wheel bearing lubrication deferred until home station, affecting scheduled maintenance compliance.
DEFERED UNTIL HOME STATION (FORT CAVAZOS) INSP A298 LUBRICATE TAIL WHEEL BEARINGS FOR HELICPTR UTIL UH-60L CAGE: 78286 PN: U H-60L NSN: 1520012984532 SN: 9226445 WAS DUE. STATUS UPGRADED TO X ON: 14 APR 2025 OR 9622.9 AIRCRAFT HOURS …
Fault
2025-09-089,310.7 hrshigh
APU oil dipstick O-ring found broken during PMD, all parts recovered but requires replacement.
DURING PMD APU OIL DIPSTICK O-RING FOUND BROKEN, ALL PARTS REC OVERED NO FOD IN APU OR SURROUNDING AREA | status: open | recorded 2025-09-08 @ 9310.7h
The aircraft has a history of structural repairs including beaded panel repairs, channel repairs, and a floor repair requiring reinspection at the next 48-month inspection. These items have been addressed but require ongoing monitoring.
Fault
2024-04-109,140.8 hrshigh
Left-hand station 308 floor repair requires reinspection at next 48-month inspection or cabin floor removal to ensure correct repair procedures.
REINSPECTION OF L/H STA 308 FLOOR REPAIR AT NEXT 48 MONTH INS PECTION OR CABIN FLOOR REMOVAL TO ENSURE CORRECT REPAIR WAS DO NE. | status: open | recorded 2024-04-10 @ 9140.8h
Historical
2022-09-28high
Right-hand station 308 beam aft inboard tab cracked, repaired during PMI-2 at 8921.8 aircraft hours.
MEC F398034 PERFORMED FOR RIGHT HAND STA 308 BEAM AFT INBOARD TAB CRACKED. COMPLETED DURING PMI-2 @ 8921.8 AIRCRAFT HOURS BY LRC-A CAMPBELL | at WGLEA0 Ft. Campbell, KY | on 2022-09-28
Historical
2014-12-08medium
Right-hand tailcone access panel repaired at 7134.2 aircraft hours during reset.
MEC F188029 REPAIR RH TAILCONE ACCESS PANEL P/N 70210-05000-0 42 COMPLETED AT ACFT HRS 7134.2 Original Location: AFMA RASME L3 HAAF GA 31409 | at WGLEA0 Ft. Campbell, KY | on 2014-12-08
Historical
2014-12-08medium
Left-hand 308 beam gouge repaired at 7134.2 aircraft hours during reset.
MEC F190701 REPAIR LH 308 BEAM PN 70211-02107-014 GOUGE COMPLE TED AT ACFT HRS 7134.2 Original Location: AFMA RASME L3 HAAF G A 31409 | at WGLEA0 Ft. Campbell, KY | on 2014-12-08
Historical
2018-04-03medium
Left-hand inner and outer drag beam fuselage fitting repaired at 7563.4 aircraft hours.
MEC #F336800C, REPAIRED LEFT HAND INNER AND OUTER DRAG BEAM FU SELAGE FITTING AT 7563.4 AIRCRAFT HOURS. Original Location: DY NCORP INTERNATIONAL BAGRAM, AFGHANISTAN | at WGLEA0 Ft. Campbell, KY | on 2018-04-03
The aircraft has multiple open safety messages requiring compliance. Critical items include H-60-26-SOF-02 (non-conforming primary main rotor servos) due prior to next flight, H-60-25-ASAM-11 (main landing gear axle radial movement inspection) due at 9401.8 hours, and H-60-25-ASAM-10 (pilot and copilot seat harness assembly replacement) due by 31 Jan 26. Several other time-limited inspections and component replacements are pending.
Fault
2025-12-113,386.9 hrshigh
H-60-26-SOF-02 non-conforming primary main rotor servos compliance required prior to next flight but not to exceed 7 Dec 25.
SAFETY MESSAGE NUMBER: H-60-26-SOF-02 DESCRIPTION: COMPLY WITH H-60-26-SOF-02, NON-CONFORMING PRIMARY MAIN ROTOR SERVOS, PRI OR TO NEXT FLIGHT, BUT NOT TO EXCEED 17 DEC 2025. FOR SERVO, P RIMARY MAIN ROTOR CAGE: 82106 PN: 274000-1035 NSN:…
Fault
2025-12-113,243.9 hrshigh
H-60-26-SOF-02 non-conforming primary main rotor servos compliance required prior to next flight but not to exceed 7 Dec 25.
SAFETY MESSAGE NUMBER: H-60-26-SOF-02 DESCRIPTION: COMPLY WITH H-60-26-SOF-02, NON-CONFORMING PRIMARY MAIN ROTOR SERVOS, PRI OR TO NEXT FLIGHT, BUT NOT TO EXCEED 17 DEC 2025. FOR SERVO, P RIMARY MAIN ROTOR CAGE: 78286 PN: 70410-02820-054…
Fault
2025-12-112,153.9 hrshigh
H-60-26-SOF-02 non-conforming primary main rotor servos compliance required prior to next flight but not to exceed 7 Dec 25.
SAFETY MESSAGE NUMBER: H-60-26-SOF-02 DESCRIPTION: COMPLY WITH H-60-26-SOF-02, NON-CONFORMING PRIMARY MAIN ROTOR SERVOS, PRI OR TO NEXT FLIGHT, BUT NOT TO EXCEED 17 DEC 2025. FOR SERVO, P RIMARY MAIN ROTOR CAGE: 78286 PN: 70410-02820-054…
Fault
2025-12-013,386.9 hrshigh
H-60-26-SOF-01 non-conforming primary main rotor servos compliance required prior to next flight but not to exceed 7 Dec 25.
SAFETY MESSAGE NUMBER: H-60-26-SOF-01 DESCRIPTION: COMPLY WITH H-60-26-SOF-01, NON-CONFORMING PRIMARY MAIN ROTOR SERVOS, PRI OR TO NEXT FLIGHT, BUT NOT TO EXCEED 7 DEC 2025. FOR SERVO, PR IMARY MAIN ROTOR CAGE: 82106 PN: 274000-1035 NSN:…
Fault
2025-08-159,310.7 hrshigh
H-60-25-ASAM-11 main landing gear axle radial movement inspection due at 9401.8 aircraft hours at next scheduled PMI.
COMPLY WITH H-60-25-ASAM-11, MAIN LANDING GEAR AXLE RADIAL MOV EMENT INSEPECITON, AT 9401.8 ACFT HOURS AT THE NEXT SCHEDULED PREVENTIVE MAINTENANCE INSPECTION (PMI) BUT NOT TO EXCEED 14 A UG 2027. | status: open | recorded 2025-08-15 @…
Fault
2025-07-089,310.7 hrshigh
H-60-25-ASAM-10 pilot and copilot seat harness assembly replacement due by 22 Jul 25.
SAFETY MESSAGE NUMBER: H-60-25-ASAM-10 DESCRIPTION: PILOT AND COPILOT SEAT HARNESS ASSEMBLY REPLACEMENT. IS DUE: 22 JUL 202 5 CALENDAR | resolved: Inspected Pilot and Co-pilot seats; both seats are config 2. | status: closed | recorded…
Fault
2025-05-019,288.7 hrshigh
H-60-25-ASAM-07 reliability enhanced stabilator actuator inspection required prior to next flight but not to exceed 12 May 25.
COMPLY WITH H-60-25-ASAM-07, RELIABILITY ENHANCED STABILATOR A CTUATOR INSPECTION, PRIOR TO NEXT FLIGHT, BUT NOT TO EXCEED 1 MAY 25. | resolved: COMPLIED WITH H-60-25-ASAM-07, RELIABILITY ENHANCED STABIL ATOR ACTUATOR INSPECTION. | status:…
Fault
2025-05-019,288.7 hrshigh
H-60-25-ASAM-05 T700 series accessory module replacement required before 9298.7 aircraft hours but not later than 11 May 25.
COMPLY WITH H-60-25-ASAM-05, T700 SERIES ACCESSORY MODULE REPL ACEMENT, BEFORE 9298.7 AIRCRAFT HOURS, BUT NOT LATER THAN 11 M AY 25. | resolved: COMPLIED WITH H-60-25-ASAM-05, T700 SERIES ACCESSORY SECTI ON MODULE REPLACEMENT. | status:…
Fault
2025-05-019,288.7 hrshigh
H-60-25-ASAM-06 automatic dependent surveillance-broadcast inspection required by 28 May 25.
COMPLY WITH H-60-25-ASAM-06, AUTOMATIC DEPENDENT SURVEILLANCE- BROADCAST (OUT) (ADS-B(OUT)) INSPECTION BY 28 MAY 25. | resolved: completed and passed | status: closed | recorded 2025-05-01 @ 9288.7h | closed 2025-05-27 @ 9288.7h
Fault
2025-05-019,288.7 hrshigh
H-60-25-ASAM-04 main rotor blade inspection required by 11 May 25.
COMPLY WITH H-60-25-ASAM-04, MAIN ROTOR BLADE PN 70150-09100-0 43 INSPECTION, BY 11 MAY 25. | resolved: COMPLIED WITH H-60-25-ASAM-04, MAIN ROTOR BLADE PN 70150-0 9100-043 INSPECTION. ONE BLADE IS AFFECTED. THE FOLLOWING SN REQUIRES…
Fault
2025-05-019,288.7 hrshigh
H-60-25-ASAM-08 main generator lug terminal inspection required by 12 May 25.
COMPLY WITH H-60-25-ASAM-08, MAIN GENERATOR LUG TERMINAL INSPE CTION BY 12 MAY 25. | resolved: COMPLIED WITH H-60-25-ASAM-08, MAIN GENERATOR LUG TERMINAL INSPECTION. | status: closed | recorded 2025-05-01 @ 9288.7h | closed 2025-05-05 @…
SAFETY MESSAGE NUMBER: GEN-26-AMAM-01 DESCRIPTION: COMPLY WITH GEN-26-AMAM-01, RECURRING AUTOMATIC DEPENDENT SURVEILLANCE-BR OADCAST(OUT) [ADS-B(OUT)] INSPECTION LCF UPDATE. WAS DUE: 16 JAN 2026 CALENDAR | status: open | recorded…
The aircraft is at 9310.7 hours and has been inducted into the BEST program as of 23 Feb 2026. Multiple components are approaching or at end-of-life intervals, including batteries, filters, and scheduled inspections. A main rotor blade requires replacement at 9338.7 hours per safety message. The aircraft has not flown since induction and has accumulated numerous overdue periodic inspections.
Fault
2025-05-029,288.7 hrshigh
Main rotor blade requires replacement at 9338.7 aircraft hours, only 28 hours remaining before mandatory replacement.
MAIN ROTOR BLADE PN 70150-09100-043F, SN A007-04978 REQUIRES R EPLACEMENT PER H-60-25-ASAM-04 AT 9338.7 AIRCRAFT HOURS, BUT N OT TO EXCEED 3 JUN 25. | resolved: REPLACED WITH BLADE A007-19682 | status: closed | recorded 2025-05-02 @…
Fault
2026-04-239,310.7 hrshigh
Aircraft inducted into BEST program on 06 Apr 2026, no scheduled maintenance performed after this date.
Aircraft inducted into the BEST Program on 06-APR-2026. No DA 2408-18 scheduled maintenance performed after this date. | status: open | recorded 2026-04-23 @ 9310.7h
Historical
2026-02-23high
Aircraft transferred to BEST program on 23 Feb 2026 at 9310.7 aircraft hours for overhaul.
Aircraft transfered to BEST program on 23 February 2026 for AR MY / BEST program by ASF HOOD (W6TU14) @ 9310.7 acft hrs. Data Plate remains installed | at W6TU14 | on 2026-02-23
Fault
2026-02-099,310.7 hrsmedium
IVHMU lithium battery replacement due, component nearing end of service life.
INSP E550 REPLACE IVHMU AA LITHIUM BATTERY FOR HELICPTR UTIL U H-60L CAGE: 78286 PN: UH-60L NSN: 1520012984532 SN: 9226445 IS DUE. STATUS WILL UPGRADE TO X ON: 10 APR 2026 REFERENCE: AWR 1346/AWR 1823 | resolved: IVHMU REMOVED FOR…
Fault
2025-10-059,310.7 hrsmedium
ASN 128D Doppler GPS battery replacement due, component nearing end of service life.
INSP E015 ASN 128D DOPPLER GPS BATTERY REPLACEMENT FOR HELICPT R UTIL UH-60L CAGE: 78286 PN: UH-60L NSN: 1520012984532 SN: 92 26445 IS DUE. STATUS WILL UPGRADE TO X ON: 10 NOV 2025 REF ERENCE: MWO 1-1520-237-50-92 | resolved: STATUS…
Fault
2025-08-109,310.7 hrsmedium
APX-123 transponder battery replacement due, component nearing end of service life.
INSP E357 REPLACE APX-123 TRANSPONDER SAFT BATTERY FOR HELICPT R UTIL UH-60L CAGE: 78286 PN: UH-60L NSN: 1520012984532 SN: 92 26445 IS DUE. STATUS WILL UPGRADE TO X ON: 09 OCT 2025 REF ERENCE: GEN-16-AMAM-04 | resolved: REPLACED…
Fault
2025-07-109,310.7 hrsmedium
Tail rotor spring capsule assembly replacement due, component nearing end of service life.
INSP A648 REPLACE T/R SPRING CAPSULE ASSY FOR HELICPTR UTIL UH -60L CAGE: 78286 PN: UH-60L NSN: 1520012984532 SN: 9226445 WAS DUE. STATUS UPGRADED TO X ON: 09 JUL 2025 REFERENCE: TM 1 -1520-237-20P | status: open | recorded 2025-07-10…
Fault
2026-03-319,310.7 hrsmedium
Cargo hook cartridge thruster replacement due, component nearing end of service life.
INSP A662 REPLACE CARGO HOOK CARTRIDGE THRUSTER, MJ20 FOR HELI CPTR UTIL UH-60L CAGE: 78286 PN: UH-60L NSN: 1520012984532 SN: 9226445 IS DUE. STATUS WILL UPGRADE TO X ON: 30 MAY 2026 REFERENCE: TB 9-1300-385 | status: open | recorded…
The seller has flagged that FM radios, CMWS equipment, ASE equipment, and SINCGARS batteries have been removed from the aircraft. Additionally, batteries were removed due to ORF status. The buyer should verify the complete list of removed items and plan for reinstallation or replacement as needed.
Fault
2026-04-179,310.7 hrshigh
Notice to buyer: multiple items removed from aircraft at direction of U.S. Government including radios, ASE, and other equipment.
NOTICE TO BUYER: The following items have been removed from th e aircraft at the direction of the U.S. Government; to include but not limited to: CMWS JUNCTION BOC; SA-26669/ALE-47 (V) CM WS SEQUENCER; SENSOR ELECTRO-OPTIC MISSLE…
Fault
2024-08-309,211.0 hrshigh
FM radios removed due to induction into BEST program.
FM2 INOP | resolved: FM RADIOS REMOVED DUE TO INDUCTION INTO BEST. | status: closed | recorded 2024-08-30 @ 9211h | closed 2026-02-26 @ 9310.7h
Fault
2025-06-119,305.2 hrshigh
ASE equipment removed due to end of EUCOM rotation.
ASE REMOVAL DUE TO END OF EUCOM ROTATION | resolved: REMOVED ASE | status: closed | recorded 2025-06-11 @ 9305.2h | closed 2025-06-11 @ 9305.2h
Fault
2025-05-079,288.7 hrshigh
CMWS equipment removed due to end of UCOM mission.
REMOVAL OF CMWS REQUIRED DUE TO END OF UCOM | resolved: REMOVED ALL CMWS EQUIPMENT | status: closed | recorded 2025-05-07 @ 9288.7h | closed 2025-05-08 @ 9288.7h
Fault
2025-09-169,310.7 hrshigh
SINCGARS batteries removed for storage.
SINCGARS BATTERIES REMOVED FOR STORAGE | resolved: SEE FAULT DATED 4 DEC 2025, SEQ #1 | status: closed | recorded 2025-09-16 @ 9310.7h | closed 2025-12-04 @ 9310.7h
Fault
2025-12-049,310.7 hrsmedium
Informational write-up: batteries removed due to aircraft on ORF status, will be reinstalled prior to flight.
INFORMATIONAL WRITE-UP: THE FOLLOWING BATTERIES WERE REMOVED D UE TO ACFT BEING ON ORF STATUS. THE BATTERIES WILL BE REINSTAL LED IF THE AIRCRAFT RETURNS TO A FLYABLE STATUS: GMR BATTERY, KGV BATTERY, KY-58 BATTERIES (2 EA), DOPPLER GPS…
The aircraft records contain several entry errors that have been closed or corrected. These administrative discrepancies do not affect airworthiness but indicate data quality issues in the maintenance tracking system. Buyers should verify all open inspections and component times independently.
Fault
2025-06-109,305.2 hrsEntry errorhigh
Entry error: PMD required before next flight entry made in error and closed.
[ENTRY ERROR] PMD REQUIRED BEFORE NEXT FLIGHT | resolved: CLOSED IN ERROR BY Loya, Joseph CIV Entry made in e rror. | status: closed | recorded 2025-06-10 @ 9305.2h | closed 2025-06-24
Fault
2025-06-239,310.7 hrsEntry errorhigh
Entry error: engine history recorder readings inspection entry made in error.
[ENTRY ERROR] INSP A100 LH/RH ENGINE HISTORY RECORDER READINGS DUE FOR HELIC PTR UTIL UH-60L CAGE: 78286 PN: UH-60L NSN: 1520012984532 SN: 9226445 WAS DUE. STATUS UPGRADED TO X ON: 18 JUN 2025 REFE RENCE: TB 55-2840-248-20-16 |…
Fault
2025-06-109,301.1 hrsEntry errorhigh
Entry error: torque check remark entered in error for pitch change rod jamnuts.
[ENTRY ERROR] 9-11HR TQ CHECKS REQUIRED ON RED PC ROD JAMNUTS AT 9310.1-9312 .1 | resolved: REMARK ENTERED IN ERROR | status: closed | recorded 2025-06-10 @ 9301.1h | closed 2025-06-10 @ 9301.1h
Fault
2025-06-109,301.1 hrsEntry errorhigh
Entry error: torque check remark entered in error for all pitch change rod jamnuts.
[ENTRY ERROR] 9-11HR TQ CHECKS REQUIRED ON ALL PC ROD JAMNUTS AT 9310.1-9312 .1 | resolved: REMARK ENTERED IN ERROR | status: closed | recorded 2025-06-10 @ 9301.1h | closed 2025-06-11 @ 9305.2h
Fault
2025-06-059,298.1 hrsEntry errormedium
Entry error: track and balance requirement written in error.
[ENTRY ERROR] TRACK & BALLANCE REQ DUE TO BLUE MAIN ROTOR BLADE REPLACEMENT | resolved: WRITTEN IN ERROR | status: closed | recorded 2025-06-05 @ 9298.1h | closed 2025-06-05 @ 9298.1h
Fault
2025-06-239,310.7 hrsEntry errormedium
Entry error: logbook reconciliation inspection entry made in error.
[ENTRY ERROR] INSP A801 LOGBOOK RECON FOR HELICPTR UTIL UH-60L CAGE: 78286 P N: UH-60L NSN: 1520012984532 SN: 9226445 WAS DUE. STATUS UPGRA DED TO X ON: 16 JUN 2025 | resolved: CLOSED IN ERROR BY Loya, Joseph CIV Entry made in e rror. |…
Custom Analysis
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