⚑ 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.
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
480.0
DueCondComp install (hrs)480
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 769
maintenance records (632 faults, 137 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 aircraft is restricted from cargo hook operations due to removed squib hardware, restricted from known icing conditions due to engine inlet anti-ice system failures, and has open wire strike damage requiring pro-seal. Day-VFR-only restrictions apply due to inoperative landing lights and wiper malfunctions.
Fault
2026-01-097,743.7 hrshigh
Aircraft restricted from cargo hook operations due to removal of squib for BEST program turn-in, limiting slingload capability.
AIRCRAFT RESTRICTED FROM CARGO HOOK OPERATIONS DUE TO REMOVAL OF SQUIB FOR BEST PROGRAM TURN IN | status: open | recorded 2026-01-09 @ 7743.7h
Fault
2025-09-027,714.0 hrshigh
Aircraft restricted from flying into known icing conditions due to engine inlet anti-ice not turning on during ground test.
ACFT RESTRICTED FROM FLYING INTO KNOWN ICING CONDITIONS DUE TO #1 AND #2 ENG INLET ANTI-ICE NOT TURNING ON DURING TEMPERATUR ES BELOW 4 DEG CELSIUS ( THERMO SWITCH REQ'S REPLACEMENT) | resolved: REPLACED THERMAL SWITCHES | status: closed |…
Fault
2025-08-217,711.9 hrshigh
Aircraft restricted from flying into known icing conditions due to engine inlet anti-ice not turning on during ground test (duplicate restriction).
ACFT RESTRICTED FROM FLYING INTO KNOWN ICING CONDITIONS DUE TO #1 AND #2 ENG INLET ANTI-ICE NOT TURNING ON DURING TEMPERATUR ES BELOW 4 DEG CELSIUS | resolved: REMOVED ENG INLETS TO CHECK FOR DEBRIS AND CLEAN. REINSTAL LED ENG INLETS. |…
Fault
2026-01-087,742.7 hrshigh
Open wire strikes on No.1 and No.2 require pro-seal application, affecting airworthiness.
NO.1 AND NO.2 WIRE STRIKES REQ'R PRO SEAL | status: open | recorded 2026-01-08 @ 7742.7h
Fault
2025-09-267,735.3 hrshigh
Aircraft restricted to day-only flight due to landing light being inoperative.
ACFT RESTRICTED TO DAY ONLY FLIGHT DUE TO LANDING LIGHT BEING INOP | resolved: MOC COMPLETED COULD NOT DUPLICATE | status: closed | recorded 2025-09-26 @ 7735.3h | closed 2025-09-29 @ 7735.3h
Fault
2025-08-267,711.9 hrshigh
Right-hand wiper blade parked in middle of windshield and will not move, restricting visibility and flight operations.
R/H WIPER BLADE PARKED IN THE MIDDLE OF WINDSHIELD. WIPER BLAD E WILL NOT MOVE ACROSS WINDSHIELD | status: open | recorded 2025-08-26 @ 7711.9h
Fault
2025-07-227,706.5 hrsmedium
Hydraulic reservoir pumping unit filter requires replacement at 7790.4 aircraft hours, approaching compliance deadline.
Hydraulic Reservior Pumping Unit Filter Requires replacment pe r H-60-25-ASAM-09 at (7790.4) aircraft hours not to exceed 31 JAN 26 | resolved: ASAM DOES NOT APPLY TO UH-60L | status: closed | recorded 2025-07-22 @ 7706.5h | closed…
This aircraft has multiple open structural defects including cabin floor stringer and firewall cracks, a damaged sliding pylon fairing with voids, and a torn main transmission drip pan drain tube. These issues compromise airframe integrity and require repair before the aircraft can be considered structurally sound.
Fault
2024-03-277,622.6 hrshigh
Right-hand cabin floor stringer is open and requires structural repair.
R/H CABIN FLOOR STRINGER CRACKED | status: open | recorded 2024-03-27 @ 7622.6h
Fault
2024-03-277,622.6 hrshigh
Right-hand engine firewall K-frame is open and requires structural repair.
R/H ENGINE FIREWALL K-FRAME CRACKED | status: open | recorded 2024-03-27 @ 7622.6h
Fault
2024-03-277,622.6 hrshigh
Three loose fasteners on 295 frame to stringer are open and require attention.
3 EA LOOSE FASTENERS ON 295 FRAME TO STRINGER | status: open | recorded 2024-03-27 @ 7622.6h
Fault
2025-08-267,711.9 hrshigh
Sliding pylon has damage on mating surface to wrap-around fairing and multiple voids requiring further inspection.
SLIDING PYLON HAS CRACK ON MATING SURFACE TO WRAP AROUND FAIRI NG AND MULTIPLE VOIDS REQUIRES FURTHER INSPECTION. | status: open | recorded 2025-08-26 @ 7711.9h
Fault
2024-03-277,622.6 hrsmedium
Left-hand firewall damage at aft latch box aft outer corner was stop-drilled, indicating prior repair.
Right side flare bucket is open and chipped, requiring replacement.
RIGHT SIDE FLARE BUCKET IS CRACKED AND CHIPPED. REQUIRES REPLA CEMENT. | status: open | recorded 2024-08-22 @ 7629.2h
Fault
2025-06-117,696.6 hrshigh
Number 2 engine cowling latch support tube is punctured and open, requiring replacement.
#2 ENGINE CAWLING LATCH SUPPORT TUBE IS PUNCTURED, REQ'S REPLA CEMENT | status: open | recorded 2025-06-11 @ 7696.6h
This aircraft has two open compliance items: H-60-26-SOF-02 (non-conforming primary main rotor servos) with a deadline of 17 Dec, and H-60-25-ASAM-10 (pilot and copilot seat harness assemblies) with a deadline of 31 Jan 26. Additionally, H-60-25-ASAM-09 (hydraulic reservoir filter replacement) is approaching its compliance hour at 7790.4. Historical records show the aircraft has not complied with H-60-25-ASAM-10 and H-60-25-ASAM-11 as of the BEST induction date.
Fault
2026-01-087,742.7 hrshigh
H-60-26-SOF-02 non-conforming primary main rotor servos compliance required prior to next flight, but not to exceed 17 Dec.
COMPLY WITH H-60-26-SOF-02, NON-CONFORMING PRIMARY MAIN ROTOR SERVOS, PRIOR TO NEXT FLIGHT, BUT NOT TO EXCEED 17 DEC 25. | resolved: COMPLETE | status: closed | recorded 2026-01-08 @ 7742.7h | closed 2026-01-08 @ 7742.7h
Fault
2025-07-087,702.3 hrshigh
H-60-25-ASAM-10 copilot seat harness assembly requires replacement no later than 31 Jan 26.
COPILOT SEAT HARNESS ASSEMBLY REQUIRES REPLACEMENT IAW H-60-25 -ASAM-10 NO LATER THAN 31 JAN 26 | status: open | recorded 2025-07-08 @ 7702.3h
Fault
2025-07-087,702.3 hrshigh
H-60-25-ASAM-10 pilot seat harness assembly requires replacement no later than 31 Jan 26.
PILOT SEAT HARNESS ASSEMBLY REQUIRES REPLACEMENT IAW H-60-25-A SAM-10 NO LATER THAN 31 JAN 26 | status: open | recorded 2025-07-08 @ 7702.3h
Fault
2025-07-227,706.5 hrshigh
H-60-25-ASAM-09 hydraulic reservoir pumping unit filter replacement due at 7790.4 aircraft hours.
Hydraulic Reservior Pumping Unit Filter Requires replacment pe r H-60-25-ASAM-09 at (7790.4) aircraft hours not to exceed 31 JAN 26 | resolved: ASAM DOES NOT APPLY TO UH-60L | status: closed | recorded 2025-07-22 @ 7706.5h | closed…
Fault
2025-08-157,707.3 hrshigh
H-60-25-ASAM-11 main landing gear axle radial movement inspection due at 7790.4 aircraft hours at the next 120-hour inspection.
Comply with H-60-25-ASAM-11, Main Landing Gear Axle Radial Mov ement Inspection, at [7790.4] aircraft hours at the NEXT sched uled Preventive Maintenance Inspection (PMI), but not to excee d 14 AUG 27. | status: open | recorded 2025-08-15…
Historical
2026-04-24high
H-60-25-ASAM-10 copilot seat harness assembly was not complied with prior to BEST induction.
COPILOT SEAT HARNESS ASSEMBLY REQUIRES REPLACEMENT IAW H-60-25 -ASAM-10 NO LATER THAN 31 JAN 26 ; NOT COMPLIED WITH | at W6TU14 | on 2026-04-24
Historical
2026-04-24high
H-60-25-ASAM-10 pilot seat harness assembly was not complied with prior to BEST induction.
PILOT SEAT HARNESS ASSEMBLY REQUIRES REPLACEMENT IAW H-60-25-A SAM-10 NO LATER THAN 31 JAN 26 ; NOT COMPLIED WITH | at W6TU14 | on 2026-04-24
Historical
2026-04-24high
H-60-25-ASAM-11 main landing gear axle radial movement inspection compliance required at 7790.4 aircraft hours at next 120-hour inspection.
Comply with H-60-25-ASAM-11, Main Landing Gear Axle Radial Mov ement Inspection, at [7790.4] aircraft hours at the NEXT sched uled Preventive Maintenance Inspection (PMI), but not to excee | at W6TU14 | on 2026-04-24
The aircraft was inducted into the BEST program on 06-Apr-2026 at 7747.0 hours. Multiple fire extinguisher cartridges exceeded service life on 28 Feb 2026. The main transmission requires resampling prior to next flight due to incomplete records. Several high-time components and approaching time-change items present moderate lifecycle risk.
Fault
2026-04-237,747.0 hrshigh
Aircraft inducted into BEST program on 06-Apr-2026; no DA 2408-18 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 @ 7747h
Fault
2026-04-237,747.0 hrshigh
Resample of main transmission required prior to next flight due to incomplete records.
RESAMPLE OF MAIN TRANSMISSION SN: A80301961, REQUIRED PRIOR TO NEXT FLIGHT DUE TO INCOMPLETE RECORDS | status: open | recorded 2026-04-23 @ 7747h
Fault
2026-02-281,010.3 hrshigh
Forward fire extinguisher cartridge service life exceeded on 28 Feb 2026.
ACTUATED DEVICE SERVICE LIFE EXCEEDED ON 28 FEB 2026 FOR CTG A IRCRAFT FIRE EXT CAGE: 30003 PN: 1512AS105 SN: 452#1FWD LOT NU MBER: ESD15K258-001 | status: open | recorded 2026-02-28 @ 1010.3h
Fault
2026-02-281,010.3 hrshigh
Second forward fire extinguisher cartridge service life exceeded on 28 Feb 2026.
ACTUATED DEVICE SERVICE LIFE EXCEEDED ON 28 FEB 2026 FOR CTG A IRCRAFT FIRE EXT CAGE: 30003 PN: 1512AS105 SN: 452#2FWD LOT NU MBER: ESD15K258-001 | status: open | recorded 2026-02-28 @ 1010.3h
Fault
2026-02-011,010.3 hrshigh
Fire extinguisher cartridge service life will be exceeded on 28 Feb 2026.
ACTUATED DEVICE SERVICE LIFE WILL BE EXCEEDED ON 28 FEB 2026 F OR CTG AIRCRAFT FIRE EXT CAGE: 30003 PN: 1512AS105 SN: 452#1FW D LOT NUMBER: ESD15K258-001 | resolved: STATUS SYMBOL UPGRADED TO X SEE FAULT ON 2026-02-28 00:00: 51.9126995…
Fault
2026-02-011,010.3 hrshigh
Fire extinguisher cartridge service life will be exceeded on 28 Feb 2026.
ACTUATED DEVICE SERVICE LIFE WILL BE EXCEEDED ON 28 FEB 2026 F OR CTG AIRCRAFT FIRE EXT CAGE: 30003 PN: 1512AS105 SN: 452#2FW D LOT NUMBER: ESD15K258-001 | resolved: STATUS SYMBOL UPGRADED TO X SEE FAULT ON 2026-02-28 00:00: 51.9126995…
The seller has flagged multiple items for buyer attention. Components were removed for ASF Hood lateral transfer, including blanking plates required on areas where components were removed. A formal notice lists removed items per U.S. Government direction. The aircraft was prepared for lateral transfer with multiple components removed and documented in associated records.
Fault
2026-04-177,747.0 hrshigh
Formal notice to buyer listing items removed from aircraft at direction of U.S. Government.
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
2026-01-137,747.0 hrshigh
Aircraft prepared for lateral transfer to ASF Hood with multiple components removed; see associated records for details.
ACFT PREPARED FOR LATERAL TRANSFER TO ASF HOOD. SEE 13-2'S FOR FOLLOWING COMPONENTS RMVD. | resolved: COMPONENTS RMVD | status: closed | recorded 2026-01-13 @ 7747h | closed 2026-01-13 @ 7747h
Fault
2026-01-137,747.0 hrshigh
Blanking plates required on areas where components were removed for ASF Hood lateral transfer.
BLANKING PLATES REQUIRED ON AREAS WHERE COMPONENTS WERE RMVD F OR ASF HOOD LATERAL TRANSFER. | resolved: HDWR AND CANNON PLUGS COVERED ALONG W/ BLANKING PLATES. RE FER TO 13-1 "LATERAL TRANSFER COMPONENT REMOVAL" FOR LOCAT IONS COVERED. |…
Fault
2026-01-097,743.7 hrshigh
Aircraft restricted from cargo hook operations due to removal of squib for BEST program turn-in.
AIRCRAFT RESTRICTED FROM CARGO HOOK OPERATIONS DUE TO REMOVAL OF SQUIB FOR BEST PROGRAM TURN IN | status: open | recorded 2026-01-09 @ 7743.7h
Historical
2026-01-23high
Transfer statement documenting aircraft transfer to BEST program on 23 Jan 2026 by 2-501st GSAB Fort Bliss TX.
TRANSFER STATMENT: AIRCRAFT TRANSFER TO BEST PROGRAM ON 23 JAN 2026 FOR ARMY BEST PROGRAM BY 2-501st GSAB FORT BLISS TX @ 77 47.0 DATA PLATE REMAINED INSTALLED | at WAX8A0 Ft. Bliss, TX | on 2026-01-23
The aircraft has numerous administrative entries marked as [ENTRY ERROR] that were entered in error and subsequently closed. One significant administrative issue involved record discrepancies that required correction. Data quality appears generally acceptable, though the volume of error entries suggests some process control issues during maintenance documentation.
Fault
2025-07-217,706.5 hrshigh
Aircraft was admin grounded for record discrepancies; discrepancies were subsequently corrected.
ADMIN GROUNDED FOR RECORD DISCREPANCIES | resolved: RECORD DISCREPANCIES CORRECTED | status: closed | recorded 2025-07-21 @ 7706.5h | closed 2025-07-22 @ 7706.5h
Fault
2025-11-107,742.7 hrsEntry errormedium
Entry error for MLG service requirement, entered in error.
[ENTRY ERROR] MLG REQUIRES SERVICE | resolved: ENTERRED IN ERROR | status: closed | recorded 2025-11-10 @ 7742.7h | closed 2025-11-10 @ 7742.7h
Fault
2025-11-107,742.7 hrsEntry errormedium
Entry error for MLG service requirement, entered in error.
[ENTRY ERROR] MLG REQUIRES SERVICE | resolved: ENTERRED IN ERROR | status: closed | recorded 2025-11-10 @ 7742.7h | closed 2025-11-10 @ 7742.7h
Fault
2023-10-047,440.4 hrsEntry errorlow
Entry error for pilot/copilot step ballast plate inspection.
[ENTRY ERROR] INSP A801 PILOT/COPILOT STEP BALLAST PLATE INSPECTTION EVERY P MI 2 FOR HELICPTR UTIL UH-60L CAGE: 78286 PN: UH-60L NSN: 1520 012984532 SN: 9026307 IS DUE. STATUS WILL UPGRADE TO X ON: 922 5.4 AIRCRAFT HOURS REFERENCE: AWR…
Fault
2025-04-147,658.6 hrsEntry errorlow
Entry error for tail rotor de-ice bracket screws, fault description entered in error.
[ENTRY ERROR] TWO SCREWS ON THE BLACK T/R DE ICE BRACKET UNINSTALLED | resolved: FAULT DESCRIPTION ENTERED IN ERROR | status: closed | recorded 2025-04-14 @ 7658.6h | closed 2025-04-22 @ 7664.6h
Fault
2025-10-227,742.3 hrsEntry errorlow
Entry error for aircraft folded for transport, entered in error due to server transfer.
[ENTRY ERROR] ACFT FOLDED FOR TRANSPORT | resolved: 13-1 ENTERED IN ERROR DUE TO SERVER TRANSFER | status: closed | recorded 2025-10-22 @ 7742.3h | closed 2025-10-23 @ 7742.3h
Custom Analysis
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