⚑ 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 2026-05-14
APU FINAL READINGG; SN: SPE112488, HRS: 386, EVENTS: 1908
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
0.0
DueCondComp install (hrs)0
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
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Records Search
Semantic search across 793
maintenance records (195 faults, 598 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 restrictions that ground or limit flight operations. The buyer must address trim inoperative restrictions, moderate icing restrictions, and secure communications limitations before unrestricted flight.
Fault
2025-05-127,883.5 hrshigh
Aircraft restricted from moderate icing conditions due to de-ice system failure.
ACFT IS RESTRICTED FROM MODERATE ICING CONDITIONS DUE TO DE-IC E FAILING STEP 4 | resolved: COULD NOT DUPLICATE FAULT | status: closed | recorded 2025-05-12 @ 7883.5h | closed 2025-05-21 @ 7884.8h
Fault
2025-05-147,884.8 hrshigh
Aircraft restricted from secure communications due to missing KY58 fills.
ACFT RESTRICTED FROM SECURE COMS DUE TO KY58 MISSING FILLS | resolved: no fills available since unit is closing due to ATI requir ements. no fills will be available for the near future. sy stem will be checked again when fills are…
Fault
2025-05-147,884.8 hrshigh
Aircraft restricted from flight without O-6 approval due to transponder failure.
AIRCRAFT RSTRICTED FROM FLIGHT WITHOUT O-6 APPROVAL TRANSPONDE R ADSB OUT MUC:S CHANNEL B FAIL | resolved: Replaced NO.2 DATA BUS COUPLER | status: closed | recorded 2025-05-14 @ 7884.8h | closed 2025-05-22 @ 7884.8h
Fault
2025-08-087,912.8 hrshigh
Center windshield anti-ice bracket disbonded; aircraft restricted from known icing conditions.
Center windsheild anti-ice bracket disbonded from windsheild. acft rest from know icing conditions | status: open | recorded 2025-08-08 @ 7912.8h
Fault
2023-09-197,782.6 hrsmedium
Aircraft must operate within limitations and restrictions specified in AWR 2022 dated 15 FEB 20.
OPERATE WITHIN LIMITATIONS AND RESTRICTIONS SPECIFIED IN AWR 2 022, DATED 15 FEB 20. | status: open | recorded 2023-09-19 @ 7782.6h
Fault
2025-08-137,912.8 hrsmedium
Visual inspection required by AWR 744 R15 prior to first flight of the day.
PERFORM VISUAL INSP AS REQUIRED BY THE FOLLOWING AWRS PRIOR TO 1ST FLIGHT OF THE DAY: 744 R15 DTD 13JUN23 (PILOT STEP TOW PL ATE); 1054 R25 DTD 07DEC23 (BAMBI); 1309 R15 DTD 31AUG23 (OREG ON AERO SEAT CUSHIONS); 1120 R15 DTD 30NOV23…
Fault
2024-02-077,782.6 hrshigh
APR-39 display failure restricts aircraft from flying in hostile environments.
APR-39 DISPLAY FAILURE. AIRCRAFT RESTRICTED FROM FLYING IN HOS TILE ENVIRONMENTS | resolved: REMOVED FOR UNIT TRANSFER | status: closed | recorded 2024-02-07 @ 7782.6h | closed 2025-06-16 @ 7907.8h
Fault
2024-08-067,830.2 hrshigh
Aircraft restricted from flights into known hostile environments due to laser failure of the APR39.
Aircraft restricted from flights into known hostile environmen ts due to laser failure of the APR39 | resolved: REMOVED FOR UNIT TRANSFER | status: closed | recorded 2024-08-06 @ 7830.2h | closed 2025-06-16 @ 7907.8h
This aircraft has a history of engine cowling damage and windshield bracket disbonding. The buyer should verify all repairs are complete and inspect for recurring issues in these areas.
Fault
2025-01-217,872.2 hrshigh
No. 1 and No. 2 engine aft cowling cracked from previous repair; open status.
NO 1,NO 2 ENGINE AFT COWLING CRACKED FROM PREVIOUS REPAIR | status: open | recorded 2025-01-21 @ 7872.2h
Fault
2025-02-207,876.5 hrsmedium
BFT antenna cracked; equipment removed due to aircraft being divested in BEST program.
BFT Antenna cracked | resolved: Equipment removed due to aircraft being divested in the BE ST program. | status: closed | recorded 2025-02-20 @ 7876.5h | closed 2026-05-14 @ 7912.8h
Fault
2025-06-057,902.8 hrshigh
Heater duct required removal due to presence of a crack.
REMOVAL OF HEATER DUCT REQUIRED DUE TO CRACK | resolved: REPAIRED HEAT AIR EXHAUST. | status: closed | recorded 2025-06-05 @ 7902.8h | closed 2025-06-06 @ 7902.8h
Historical
2019-01-28high
34.5 beam cracked during ACE inspection; repaired at 6964.1 aircraft hours.
34.5 BEAM CRACKED, FOUND DURING ACE INSPECTION. REPAIRED I/A/W MEC F347984 B. AT ACFT HRS. 6964.1 Original Location: LRC-A FORT HOOD FT HOOD, TX 76544 | at WH6BA0 Ft. Hood, TX | on 2019-01-28
Historical
2019-02-11high
MEC F347984B complied with for repair of R/H 34.5 beam and 308 tab at 6964.1 aircraft hours.
MEC F347984B WAS COMPLIED WITH AT 6964.1 ACFT HRS. CRACK WAS R EPAIRED ON THE R/H 34.5 BEAM AND 308 TAB Original Location: LR C-A FORT HOOD TEXAS FT HOOD, TX 76544 | at WH6BA0 Ft. Hood, TX | on 2019-02-11
This aircraft has two open primary main rotor servo compliance messages that must be addressed prior to next flight. Additionally, several one-time inspections and recurring compliance items are due or overdue.
Fault
2025-12-047,912.8 hrshigh
H-60-26-SOF-01 non-conforming primary main rotor servos compliance required prior to next flight.
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.. IS DUE: 07 DEC 2025 CALENDAR | resolved: Complied with…
Fault
2025-12-116,542.8 hrshigh
H-60-26-SOF-02 non-conforming primary main rotor servos not complied with at 6542.8 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: 70410-02820-054…
Fault
2025-12-114,914.8 hrshigh
H-60-26-SOF-02 non-conforming primary main rotor servos not complied with at 4914.8 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: 70410-02820-054…
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…
Fault
2025-04-297,882.5 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: MOC COMPLETE CHECK FOUND GOOD | status: closed | recorded 2025-04-29 @ 7882.5h | closed 2025-05-27 @ 7884.8h
Fault
2025-08-157,912.8 hrshigh
H-60-25-ASAM-11 main landing gear axle radial movement inspection due at 8262.6 aircraft hours.
COMPLY WITH H-60-25-ASAM-11, MAIN LANDING GEAR AXLE RADIAL MOV EMENT INSEPECITON, AT 8262.6 ACFT HOURS AT THE NEXT SCHEDULED PREVENTIVE MAINTENANCE INSPECTION (PMI) BUT NOT TO EXCEED 14 A UG 2027. | status: open | recorded 2025-08-15 @…
BOLTS, SHEAR, PN NAS1304 TAIL ROTOR SELF-SEALING COUPLINGS REQ UIRES REPLACEMENT PER "H-60-22-AMAM-08 BY 14 JUL26" | status: open | recorded 2023-11-03 @ 7782.6h
Fault
2025-07-087,912.8 hrshigh
H-60-25-ASAM-10 pilot and copilot seat harness assembly replacement due 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
2025-07-107,912.8 hrshigh
Pilot seat harness assembly requires replacement per H-60-25-ASAM-10 no later than 31 JAN 26.
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 @ 7912.8h | closed 2025-09-10 @ 7912.8h
Fault
2025-07-107,912.8 hrshigh
Copilot seat harness assembly requires replacement per H-60-25-ASAM-10 no later than 31 JAN 26.
COPILOT SEAT HARNESS ASSEMBLY REQUIRES REPLACEMENT PER H-60-25 -ASAM-10 NO LATER THAN 31 JAN 26 | resolved: REPLACED | status: closed | recorded 2025-07-10 @ 7912.8h | closed 2025-09-10 @ 7912.8h
Historical
2026-05-14high
H-60-25-ASAM-11 main landing gear axle radial movement inspection at 8262.6 aircraft hours at next scheduled phase.
COMPLY WITH H-60-25-ASAM-11, MAIN LANDING GEAR AXLE RADIAL MOV EMENT INSEPECITON, AT 8262.6 ACFT HOURS AT THE NEXT SCHEDULED PREVENTIVE MAINTENANCE INSPECTION (PMI) BUT NOT TO EXCEED 14 A | at W6TU14 | on 2026-05-14
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 | at W6TU14 | on 2026-05-14
Historical
2025-12-04high
H-60-26-SOF-01 non-conforming primary main rotor servos compliance prior to next flight but not to exceed 7 DEC 25.
COMPLY WITH H-60-26-SOF-01, NON-CONFORMING PRIMARY MAIN ROTOR SERVOS, PRIOR TO NEXT FLIGHT, BUT NOT TO EXCEED 7 DEC 2025. | at WYPPA0 TX,CO,CA,KS | on 2025-12-04
This aircraft was inducted into the BEST program on 27 APR 2026 at 7912.8 hours. No scheduled maintenance has been performed after induction. The buyer should assess the aircraft's maintenance status and plan for deferred inspections and component replacements.
Fault
2026-04-277,912.8 hrshigh
Aircraft inducted into BEST Program on 27-APR-2026; no DA 2408-18 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 @ 7912.8h
Fault
2026-05-277,912.8 hrshigh
Main rotor blade S/N A007-15357 has BIM indicator showing red; requires attention.
MAIN ROTOR BLAS S/N: A007-15357 HAS BIM INDICATOR SHOWING RED | status: open | recorded 2026-05-27 @ 7912.8h
Fault
2024-11-127,872.2 hrshigh
Oil consumption check required on #1 engine before and after flight; inspections to be recorded in 13-2s after each flight.
OIL CONSUMPTION CHECK REQUIRED ON #1 ENG BEFORE AND AFTER FLIG HT. INSPECTIONS ARE TO BE RECORDED IN 13-2's AFTER EACH FLIGHT . | status: open | recorded 2024-11-12 @ 7872.2h
Fault
2024-11-137,872.2 hrsmedium
Center GPS annunciator panel bulb burnt out; uneconomical repair, cannot be repaired at current maintenance level.
INFORMATIONAL: CENTER GPS ANNUNCIATOR PANEL BULB BURNT OUT. UN ECONOMICAL REPAIR. CANNOT BE REPAIRED AT CURRENT FACILITY. | status: open | recorded 2024-11-13 @ 7872.2h
Fault
2025-05-297,887.1 hrsmedium
#2 side vertical speed indicator backlighting inoperative; troubleshooting did not resolve issue.
#2 side vertical speed indicator backlighting is INOP. Crew tr ouble shot by resetting circuit breakers. Did not fix problem. Aircraft restricted from N/NG flight per table 5-2 AR95-1. | resolved: tested could not duplicate fault |…
Historical
2026-05-14high
Aircraft transferred to BEST program on 27 APR 2026 at 7912.8 hours; data entry by ASF HOOD.
AIRCRAFT TRANSFERRED TO BEST PROGRAM ON 27 APR 2026 FOR ARMY / BEST PROGRAM BY ASF HOOD (W6TU14) AT 7912.8 HRS. DATA PLATE RE MAINED INSTALLED. | at W6TU14 | on 2026-05-14
The seller has explicitly flagged items for buyer attention. Prior to delivery, batteries and other components will be removed from the aircraft. The buyer must verify the complete list of removed items and plan for replacement or reinstallation.
Fault
2026-05-187,912.8 hrshigh
Remark/Notice to Buyer: items will be removed from aircraft prior to delivery to buyer.
“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
2026-05-047,912.8 hrshigh
Remark/Notice to Buyer: items will be removed from aircraft prior to delivery to buyer.
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
2025-12-017,912.8 hrshigh
Informational write-up: batteries removed due to aircraft being on ORF status; batteries will be reinstalled.
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 (3 EA), DOPPLER GPS…
Fault
2025-09-167,912.8 hrshigh
GPS battery removed for storage; see fault dated 1 DEC 2025 sequence #1.
GPS BATTERY REMOVED FOR STORAGE | resolved: SEE FAULT DATED 1 DEC 2025, SEQUENCE #1 | status: closed | recorded 2025-09-16 @ 7912.8h | closed 2025-12-01 @ 7912.8h
Fault
2025-06-167,907.8 hrshigh
ASE removal required due to return to home station; ASE removal complete.
ASE REMOVAL REQUIRED DUE TO RETURN TO HOME STATION. | resolved: ASE REMOVAL COMPLETE | status: closed | recorded 2025-06-16 @ 7907.8h | closed 2025-06-16 @ 7907.8h
Historical
2026-05-14high
ENG1 final reading at induction: SN GEE613210, LCF1 661, LCF2 212, INDEX 1647, HOURS 1514.
ENG1 FINAL READING; SN: GEE613210, HIST REC SN: LMDBH872, LCF1 : 661, LCF2: 212, INDEX: 1647, HOURS: 1514 | at W6TU14 | on 2026-05-14
Historical
2026-05-14high
ENG2 final reading at induction: SN GEE613185, LCF1 646, LCF2 3893, INDEX 1650, HOURS 1517.
ENG2 FINAL READING; SN: GEE613185, HIST REC SN: LMDBH861, LCF1 : 646, LCF2: 3893, INDEX: 1650, HOURS: 1517 | at W6TU14 | on 2026-05-14
Historical
2026-05-14high
APU final reading at induction: SN SPE112488, HRS 386, EVENTS 1908.
APU FINAL READINGG; SN: SPE112488, HRS: 386, EVENTS: 1908 | at W6TU14 | on 2026-05-14
This aircraft has one entry error flagged in the records. The buyer should review the complete logbook for accuracy and completeness, particularly around the BEST program induction date.
Fault
2026-05-127,912.8 hrsEntry errorhigh
Entry error: notice to buyer regarding items removed from 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
2025-06-177,907.8 hrsEntry errormedium
Entry error: center windshield antiice bracket disbonded status symbol entered in error; see entry dated 8 AUG 2025.
[ENTRY ERROR] CENTER WINDSHIELD ANTIICE BRACKET DISBONDED | resolved: status symbol entered in error. see entry dated 8 aug 25 f or correct status symbol | status: closed | recorded 2025-06-17 @ 7907.8h | closed 2025-08-08 @ 7912.8h
Custom Analysis
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