⚑ 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 2004-10-06
INSTALLED APU INLET BARRIER FILTER AT 1794.0 ACFT HRS. (DW 4596) Original Location: AMCOM OLR/LM2 HAAF, GA 31409
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
2.0
DueCondComp install (hrs)2
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
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Part-Out Valuation
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Records Search
Semantic search across 794
maintenance records (182 faults, 612 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 3 open safety items requiring immediate attention before flight: restricted from known icing conditions due to main rotor blade deice failure, restricted from IMC/overwater operations, and restricted from CEFS use due to a capped fuel line.
Fault
2025-02-137,013.3 hrshigh
Aircraft restricted from known icing conditions due to main rotor blade deice failure, limiting operational envelope.
RESTRICTED FROM KNOWN ICING CONDITIONS DUE TO MR BLADE DEICE F AIL | status: open | recorded 2025-02-13 @ 7013.3h
Fault
2020-05-066,264.6 hrshigh
Aircraft restricted from CEFS use due to capped CEFS line at station 379, eliminating external fuel capability.
AIRCRAFT RESTRICTED FROM CEFS USE DUE TO CAPPED CEFS LINE AT S TA. 379 R/BL 34.5 | status: open | recorded 2020-05-06 @ 6264.6h
Fault
2021-04-126,429.9 hrshigh
ERFS auxiliary fuel control panel not installed, restricting aircraft from ERFS/ESSS mission requirements.
ERFS (ESSS) AUXILIARY FUEL CONTROL PANEL NOT INSTALLED. AIRCR AFT RESTRICTED FROM ERFS/ESSS MISSION REQUIREMENTS. | status: open | recorded 2021-04-12 @ 6429.9h
Fault
2024-09-036,953.2 hrsmedium
Pilot side number 1 engine top RPM light burnt out, affecting crew awareness of engine overspeed conditions.
PILOT SIDE #1 ENGINE TOP RPM LIGHT BURNT OUT | status: open | recorded 2024-09-03 @ 6953.2h
Fault
2025-06-027,020.8 hrshigh
Aircraft restricted from secure communications due to KY58 missing fills.
ACFT RESTRICTED FROM SECURE COMMS DUE TO KY58 MISSING FILLS | resolved: acft ransfered to USAR and no fills for the KY-58 availabl e at this time. when fills become available the KY-58's wi ll be tested for operational capabilities |…
The airframe has a history of significant repairs including oil cooler attachment hardware failure causing damage at station 379, multiple beam and skin repairs, and a repaired crack in the aft tail rotor pylon. These repairs are documented but indicate prior stress events.
Historical
2003-04-09high
Oil cooler attachment hardware vibrated loose causing oil cooler mounts to break and airframe damage with a crack at station 379 BL-0 beam, repaired under MEC.
OIL COOLER ATTACHMENT HDWRE VIBRATED LOOSE & OIL COOLER MOUNTS BROKE CAUSING AIRFRAME DAMAGE WITH A CRACK @ STA 379 BL 0 BEA M. (WS7954) Original Location: A CO 8-101 AVN REGT KUWAIT | at WH6BA0 Ft. Hood, TX | on 2003-04-09
Historical
2010-03-19high
Crack found on aft tail rotor pylon at station 677 WL 230, authorized repair applied.
LATE ENTRY: 19 JULY 2007 MEC# LE-BAL016-0029 CRACK FOUND ON AF T T/R PYLON @ STA 677 WL 230. AUTHORIZED REPAIR OF CRACK IAW DMWR 1-1520-237; REPAIR IAW WITH WP 0173, 0264 THROUGH 0266 AN | at WH6BA0 Ft. Hood, TX | on 2010-03-19
Historical
2012-02-24medium
Left hand beaded skin panel and both 34.5 tabs installed under MEC for repair.
LT HAND BEADED SKIN PANEL AND BOTH 34.5 INSTALLED IAW MEC#1398 48 AND DMWR 1-1520-237 WP 0333 AND 0335 Original Location: ALM D/DOL FORT BRAGG,NC | at WH6BA0 Ft. Hood, TX | on 2012-02-24
Historical
2017-01-23medium
Upper cabin plating at station 361 BL 16R WL 269 repaired under MEC.
UPPER CABIN PLATING, STA 361, BL 16R, WL 269 REPAIRED IAW MEC F319977A AT 5794.4 ACFT HRS. Original Location: LRC-A FT. HOOD , TX | at WH6BA0 Ft. Hood, TX | on 2017-01-23
Historical
2017-01-17medium
Right hand cabin splice strap at aft cargo door opening station 379 repaired under MEC.
R/H CABIN SPLICE STRAP AT AFT CARGO DOOR OPENING STA 379 REPAI RED IAW MEC F320109 AT 5794.4 ACFT HRS. Original Location: LRC -A FT. HOOD, TX | at WH6BA0 Ft. Hood, TX | on 2017-01-17
Historical
2021-05-05medium
Left hand main landing gear drag beam fitting lug bores repaired under MEC.
L/H MAIN LANDING GEAR DRAG BEAM FITTIND P/N 70219-02526-044 LU G BORES REPAIRED IAW MEC F381135A BY LRC-A FT HOOD, TX AT 6433 .9 ACFT HRS. | at WH6BA0 Ft. Hood, TX | on 2021-05-05
Historical
2020-05-05medium
Number one side upper door track repaired for damage under MEC.
MEC F367964C Number One Side Crack On Upper Door Track Complie d With At 6264.6 ACFT HRS. | at W0H95J Ft. Hood, TX | on 2020-05-05
Fault
2025-05-167,020.8 hrshigh
Yellow main rotor blade tip replaced due to damage in airframe, resolved with new tip cap installed.
YELLOW M/R BLADE TIP REQUIRES REPLACEMENT DUE TO CRACK IN AIRF RAME | resolved: REPLACED S/N:B84914244 WITH S/N: A84906349 | status: closed | recorded 2025-05-16 @ 7020.8h | closed 2025-05-20 @ 7020.8h
This aircraft has 4 open safety messages requiring compliance: H-60-26-SOF-02 (non-conforming primary main rotor servos), H-60-26-SOF-01 (non-conforming primary main rotor servos), H-60-25-ASAM-11 (main landing gear axle radial movement inspection), and H-60-25-ASAM-10 (pilot and copilot seat harness assembly replacement). Two seat harness assemblies were replaced in July 2025 but the ASAM remains open. Additionally, H-60-22-AMAM-08 (NAS1304 bolt inspection) and H-60-19-AMAM-03 (main rotor deice/chip detector harness chaffing) were not complied with prior to BEST induction.
Fault
2025-12-11361.5 hrshigh
H-60-26-SOF-02 non-conforming primary main rotor servos not complied with, open at 361.5 aircraft hours.
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
2025-12-114,780.6 hrshigh
H-60-26-SOF-02 non-conforming primary main rotor servos not complied with, open at 4780.6 aircraft hours.
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: 70410-02820-055…
Fault
2025-12-01361.5 hrshigh
H-60-26-SOF-01 non-conforming primary main rotor servos not complied with, open at 361.5 aircraft hours.
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
2025-12-014,780.6 hrshigh
H-60-26-SOF-01 non-conforming primary main rotor servos not complied with, open at 4780.6 aircraft hours.
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: 78286 PN: 70410-02820-055…
Fault
2025-08-157,022.6 hrshigh
H-60-25-ASAM-11 main landing gear axle radial movement inspection due at 7141.1 aircraft hours at next scheduled PMI.
COMPLY WITH H-60-25-ASAM-11, MAIN LANDING GEAR AXLE RADIAL MOV EMENT INSEPECITON, AT 7141.1 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
2025-07-087,022.6 hrshigh
H-60-25-ASAM-10 pilot and copilot seat harness assembly replacement due 22 July 2025, still open.
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…
Historical
2026-05-12high
H-60-19-AMAM-03 main rotor deice/chip detector harness chaffing and re-routing not complied with prior to BEST induction.
H-60-19-AMAM-03, M/R DE-ICE/CHIP DETECTOR HARNESS CHAFFING AND RE-ROUTING, NOT COMPLIED WITH | at W6TU14 | on 2026-05-12
Historical
2026-05-12high
H-60-25-ASAM-11 main landing gear axle radial movement inspection not complied with prior to BEST induction.
H-25-ASAM-11, MAIN LANDING GEAR AXLE RADIAL MOVEMENT INSPECTIO N, NOT COMPLIED WITH | at W6TU14 | on 2026-05-12
Historical
2026-05-12high
H-60-22-AMAM-08 NAS1304 bolt inspection not complied with prior to BEST induction, due by 14 July 2026.
H-60-22-AMAM-08, NAS1304 BOLT INPSECTION, NOT COMPLIED WITH | at W6TU14 | on 2026-05-12
Historical
2026-05-12medium
GEN-26-AMAM-01 ADS-B out inspection LCF update not complied with prior to BEST induction.
GEN-26-AMAM-01, ADS-B OUT INSPECTION LCF UPDATE, NOT COMLIED W ITH | at W6TU14 | on 2026-05-12
Historical
2026-05-12medium
H-60-17-AMAM-11 torque the inner and outer duplex bearing retaining ring bolts not complied with prior to BEST induction.
H-60-17-AMAM-11, TORQU THE INNER AND OUTER DUPLEX BEARING RETA INING RING BOLTS, NOT COMPLIED WITH | at W6TU14 | on 2026-05-12
Fault
2025-07-107,022.6 hrshigh
H-60-25-ASAM-10 pilot seat harness assembly replaced no later than 31 January 2026, resolved with compliance.
PILOT SEAT HARNESS ASSEMBLY REQUIRES REPLACEMENT PER H-60-25-A SAM-10 NO LATER THAN 31 JAN 26 | resolved: COMPLIED WITH H-60-25-ASAM-10 | status: closed | recorded 2025-07-10 @ 7022.6h | closed 2025-08-28 @ 7022.6h
Fault
2025-07-107,022.6 hrshigh
H-60-25-ASAM-10 copilot seat harness assembly replaced no later than 31 January 2026, resolved with compliance.
COPILOT SEAT HARNESS ASSEMBLY REQUIRES REPLACEMENT PER H-60-25 -ASAM-10 NO LATER THAN 31 JAN 26 | resolved: COMPLIED WITH H-60-25-ASAM-10 | status: closed | recorded 2025-07-10 @ 7022.6h | closed 2025-08-28 @ 7022.6h
Fault
2025-06-127,022.6 hrsmedium
H-60-25-ASAM-06 automatic dependent surveillance-broadcast (ADS-B out) inspection by 28 May 2025, resolved with compliance.
COMPLY WITH H-60-25-ASAM-06, AUTOMATIC DEPENDENT SURVEILLANCE- BROADCAST (OUT) (ADS-B(OUT)) INSPECTION BY 28 MAY 25. | resolved: ADS-B check complete. | status: closed | recorded 2025-06-12 @ 7022.6h | closed 2025-06-16 @ 7022.6h
The aircraft was inducted into the BEST program on 27 April 2026 at 7022.6 hours with no scheduled maintenance performed after that date. The main transmission filter impending bypass button has extended multiple times (most recently at 5506.7 hours), indicating filter loading and potential wear. Engines and APU have moderate time, and the receiving unit must torque duplex bearing retaining ring bolts at next PMI.
Fault
2026-04-277,022.6 hrshigh
Aircraft inducted into BEST program on 27 April 2026 at 7022.6 hours, no scheduled maintenance performed after this date.
Aircraft inducted into the BEST Program on 27-APR-2026. No DA 2408-18 scheduled maintenance performed after this date. | status: open | recorded 2026-04-27 @ 7022.6h
Historical
2015-01-06high
Main transmission filter impending bypass button extended at 5456.7 aircraft hours, oil inspection OK, indicating filter loading.
MAIN TRANSMISSION FILTER IMPENDING BYPASS BUTTON EXTENDED THIS DATE AT 5456.7 AIRCRAFT HOURS. OIL INSPECTION OK. Original L ocation: D CO 2-227 AVN REGT FORT HOOD TX, 76544 | at WH6BA0 Ft. Hood, TX | on 2015-01-06
Historical
2015-03-30high
Main transmission oil filter bowl impending bypass button extended at 5506.7 aircraft hours, oil inspection OK, filters replaced.
MAIN TRANSMISSION OIL FILTER BOWL IMPENDING BYPASS BUTTON EXTE NDED AT 5506.7 ACFT HOURS. OIL INSPECTION OK. FILTERS REPLAC ED AND BUTTON RESET. Original Location: D CO 2-227 AVN REGT FO | at WH6BA0 Ft. Hood, TX | on 2015-03-30
Fault
2025-05-147,020.8 hrsmedium
At next PMI the receiving unit will torque the inner and outer duplex bearing retaining ring bolts per work order.
At the next PMI, the receiving unit will torque the inner and outer duplex bearing retaining ring bolts IAW H-60-17-AMAM-11 (ESM2). | status: open | recorded 2025-05-14 @ 7020.8h
Fault
2024-08-026,935.5 hrsmedium
Monitor main transmission oil pressure for the next 120 flight hours, close status symbol at 7055.5 flight hours if no issues.
Monitor Main Transmission oil pressure for the next 120 Flight Hours, close status symbol at 7055.5 Flight Hours. If low oil pressure continues replace both pressure regulating valves pe r TM 1-1520-237-23&P, WP 0095, Fault Procedure 11. …
Historical
2026-05-14high
Engine 2 final reading at BEST induction: 364 hours, LCF1 215, LCF2 786, index 925.
ENG2 FINAL READING; SN: GEE903546, HIST REC SN: LMDH6096, LCF1 : 215, LCF2: 786, INDEX: 925, HOURS: 364 | at W6TU14 | on 2026-05-14
Historical
2026-05-14high
Engine 1 final reading at BEST induction: 373 hours, LCF1 204, LCF2 601, index 638.
ENG1 FINAL READING; SN: GEE767118C, HIST REC SN: LMDH4008, LCF 1: 204, LCF2: 601, INDEX: 638, HOURS: 373 | at W6TU14 | on 2026-05-14
Historical
2026-05-14high
APU final reading at BEST induction: 802.5 hours, 3875.0 events.
APU FINAL READING; SN: SPE112440, HRS: 802.5, EVENTS: 3875.0 | at W6TU14 | on 2026-05-14
Prior to delivery, the following items will be removed from the aircraft: GPS batteries, SATCOM wiring/antenna coaxes/HF switchbox, FM2 radio, ASE equipment, and cargo hook hardware. The buyer must be aware that these systems will not be functional and may require reinstallation or replacement.
Fault
2026-05-047,022.6 hrshigh
Notice to buyer: prior to delivery the following items will be removed from the aircraft per seller direction.
REMARK/NOTICE TO BUYER: Prior to delivery of the aircraft to the buyer the following items will be removed from the aircraf t at the direction of the US Government; to include but not li mited to: CMWS JUNCTION BOX; SA-26669/ALE-47 (V)…
Fault
2026-05-187,022.6 hrshigh
Notice to buyer: prior to delivery the following items will be removed from the aircraft at direction of U.S. government.
“REMARK/NOTICE TO BUYER: Prior to delivery of the aircraft to the buyer the following items will be removed from the aircra ft at the direction of the US Government; to include but not l imited to: CMWS JUNCTION BOX; SA-26669/ALE-47 (V)…
Fault
2026-05-127,022.6 hrsEntry errorhigh
Entry error notice to buyer: the following items have been removed from the aircraft at direction of U.S. government.
[ENTRY ERROR] 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…
Fault
2025-12-037,022.6 hrsmedium
Informational write-up: batteries removed due to aircraft being on ORF status, batteries will be reinstalled prior to transfer.
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…
Fault
2025-09-167,022.6 hrsmedium
GPS battery removed for storage, batteries removed per write-up dated 3 December 2025.
GPS BATTERY REMOVED FOR STORAGE | resolved: BATTERIES REMOVED; SEE WRITE UP DATED 3 DEC 2025, SEQ #1 | status: closed | recorded 2025-09-16 @ 7022.6h | closed 2025-12-03 @ 7022.6h
Fault
2025-04-247,017.8 hrshigh
FM2 inoperative, FM2 removed for divestment in the BEST program.
FM2 INOP | resolved: FM 2 removed for divestment in the BEST program. | status: closed | recorded 2025-04-24 @ 7017.8h | closed 2026-05-14 @ 7022.6h
Fault
2025-06-107,020.8 hrsmedium
Removal of ASE due to end of EUCOM rotation, ASE removed.
REMOVAL OF ASE DUE TO END OF EUCOM ROTATION | resolved: REMOVED ASE | status: closed | recorded 2025-06-10 @ 7020.8h | closed 2025-06-11 @ 7020.8h
Historical
2017-04-10medium
Single SATCOM wiring, antenna coaxes and HF/SATCOM switchbox removed permanently from aircraft per AMWO.
SINGLE SATCOM (AMWO 1-1520-237-SATCOM) WIRING, ANTENNA COAXES AND HF/SATCOM SWITCHBOX REMOVED PERMANENTLY FROM ACFT DURING I NSTALLATION OF AMWO 1-1520-237-ASC-15E (COMMUNICATION CENTRAL | at WH6BA0 Ft. Hood, TX | on 2017-04-10
Fault
2026-05-187,022.6 hrsmedium
Main rotor blade A00716223 (currently yellow) tip cap serial number verification required at next removal.
M/R Blade A00716223 (currently Yellow) tip cap S/N verificatio n required at next removal. | status: open | recorded 2026-05-18 @ 7022.6h
There are 2 entry errors in the maintenance records: one regarding APR-39 failure/degraded status during self-test, and one regarding logbook reconciliation. Additionally, the aircraft was administratively grounded on 17 June 2020 due to a missing flashlight on a different aircraft, later cleared. These data quality issues should be reviewed for accuracy.
Fault
2025-05-287,020.8 hrsEntry errorhigh
Entry error: APR-39 failure and APR-39 degraded populated during self-test, restricted for known hostile conditions due to entry error.
[ENTRY ERROR] APR-39 FAILURE AND APR-39 DEGRADED POPULATED DURING SELF TEST RESTRICTED FOR KNOWN HOSTILE CONDITIONS DUE TO APR-39 TEST FA ILURE | resolved: CLOSED IN ERROR BY Mcdougald, Zachary CW3 Entry mad e in error. | status: closed…
Fault
2025-06-247,022.6 hrsEntry errormedium
Entry error: inspection A801 logbook reconciliation for helicopter utility UH-60L was entered in error.
[ENTRY ERROR] INSP A801 LOGBOOK RECON FOR HELICPTR UTIL UH-60L CAGE: 78286 P N: UH-60L NSN: 1520012984532 SN: 9326510 IS DUE. STATUS WILL U PGRADE TO X ON: 25 JUN 2025 | resolved: CLOSED IN ERROR BY Loya, Joseph CIV Entry made in e…
Historical
2020-06-18medium
Aircraft 9326510 was administratively grounded on 17 June 2020 due to personal flashlight unaccounted for on different aircraft 9326525, flashlight later found and aircraft released.
17 JUNE 2020 ACFT 9326510 WAS ADMIN GROUNDED DUE TO A PERSONAL FLASHLIGHT UNACCOUNTED FOR ON ACFT 9326525. FLASHLIGHT WAS SE EN ONCE IN THE CABIN OF 525 AND LAST SEEN ON THE GROUND NEXT T | at WH6BA0 Ft. Hood, TX | on 2020-06-18
Historical
2007-12-05Entry errorlow
Entry error: entry 1 dated 4 November 2007 entered in error, corrected in records.
[ENTRY ERROR] ENTRY 1 DATED 4 NOV O7 ENTERED IN ERROR Original Location: D C O 4-3 AVN BIAP, IRAQ | at WH6BA0 Ft. Hood, TX | on 2007-12-05
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