⚑ 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 2010-07-08
H-60-10-ASAM-08; ALL H-60A/L SERIES AIRCRAFT, AUXILIARY POWER UNIT (APU) AND APU FIREWALL COMPLIED WITH AT 4880.1 ACFT HRS D URING RESET. MODIFICATION KIT WAS INSTALLED DUE TO EVIDENCE O
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
403.0
DueCondComp install (hrs)403
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 988
maintenance records (213 faults, 775 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 safety items requiring immediate attention before flight. The aircraft is restricted from IMC/overwater operations due to trim inoperative, and cargo hook operations are restricted due to intermittent manual release. VHF and FM2 backlighting are inoperative, and a deice system MOC is required. Additionally, the aircraft was inducted into the BEST program in April 2026 with no scheduled maintenance performed after that date.
Fault
2025-02-129,053.3 hrshigh
Aircraft restricted from IMC and overwater operations due to inoperative trim and DGNS limitations per AWR.
OPERATE WITHIN THE LIMITATIONS PRESCRIBED IN THE ENCLOSED AWR’ S: AWR2369R3 DTD 28 MAR 24 (DGNS, AN/ASN-128D): AWR2294R3 DTD 28 OCT 24 (PPA); AWR 2277R2 DTD 27SEP24 (Getac T800 Windows 1 0 Tablet); AWR 2261R2 DTD 01 MAY 24 (EFB); AWR…
Fault
2024-09-249,024.7 hrshigh
Aircraft restricted from cargo hook operations due to intermittent manual release.
ACFT restricted from cargo hook operations due to cargo hook m anual release intermittent operation. Cargo hook release fails step 6 of Operational Check - Manual Release Mode. TM 1-1520- 237-CL-1, page D4-1. | resolved: Completed cargo…
Fault
2024-11-269,049.3 hrshigh
VHF backlighting inoperative, open since November 2024.
VHF BACKLIGHTING INOP | status: open | recorded 2024-11-26 @ 9049.3h
Fault
2024-11-269,049.3 hrshigh
FM2 inoperative, removed due to BEST program induction.
FM2 INOP | resolved: FM'S REMOVED DUE TO INDUCTION INTO BEST PROGRAM. | status: closed | recorded 2024-11-26 @ 9049.3h | closed 2026-02-26 @ 9062.6h
Fault
2025-05-159,060.3 hrshigh
Deice system MOC required due to disconnection of deice cables on black main rotor blade.
DEICE SYSTEM MOC REQUIRED DUE TO DISCONNECTION OF DEICE CABLES ON BLACK M/R BLADE | status: open | recorded 2025-05-15 @ 9060.3h
Fault
2025-11-249,062.6 hrsmedium
Tail wheel valve cap not installed, missing part.
TAIL WHEEL VALVE CAP NOT INSTALLED, NOT ON ACFT, NSN: 1650-00- 222-4525 | status: open | recorded 2025-11-24 @ 9062.6h
One structural issue identified: the left-hand copilot's windshield was cracked in the outer pane only and has been replaced. No other open structural concerns are documented.
Fault
2025-04-279,056.6 hrshigh
Left-hand copilot windshield cracked on top side in outer pane only, cleared for one-time flight.
LH COPILOT'S WINDSHIELD CRACKED ON TOP SIDE IN THE OUTER PANE ONLY. AIRCRAFT CLEARED FOR ONE TIME FLIGHT FROM KCRP TO HOME S TATION AT KHLR PER LTC SAAD 2-227 GSAB BN COMMANDER | resolved: Writeup entered for one time flight. Upgraded to…
Fault
2025-04-279,060.3 hrshigh
Damaged windshield was replaced, closed fault documenting the repair.
LH COPILOT'S WINDSHIELD CRACKED ON TOP SIDE IN THE OUTER PANE ONLY. | resolved: REPLACED DAMAGED WINDSHEILD | status: closed | recorded 2025-04-27 @ 9060.3h | closed 2025-06-09 @ 9060.3h
This aircraft has multiple open Aviation Safety Action Messages requiring compliance. Critical items include H-60-26-SOF-02 (non-conforming primary main rotor servos), H-60-26-SOF-01 (non-conforming primary main rotor servos), GEN-26-AMAM-01 (recurring ADS-B inspection), H-60-25-ASAM-10 (pilot and copilot seat harness replacement due by 31 Jan 26), H-60-25-ASAM-11 (main landing gear axle radial movement inspection), and H-60-22-AMAM-08 (NAS1304 bolt inspection due by 14 Jul 26). Several historical ASAMs have been complied with.
Fault
2025-12-118,211.6 hrshigh
H-60-26-SOF-02 non-conforming primary main rotor servos not complied with, open at 8211.6 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
2025-12-116,912.6 hrshigh
H-60-26-SOF-02 non-conforming primary main rotor servos not complied with, duplicate entry at 6912.6 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
2025-12-116,127.6 hrshigh
H-60-26-SOF-02 non-conforming primary main rotor servos not complied with, duplicate entry at 6127.6 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
2025-12-049,062.6 hrshigh
H-60-26-SOF-01 non-conforming primary main rotor servos not complied with, open.
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
2026-01-179,062.6 hrshigh
GEN-26-AMAM-01 recurring ADS-B inspection not complied with, open.
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
2026-01-149,062.6 hrshigh
GEN-26-AMAM-01 recurring ADS-B inspection not complied with, duplicate entry.
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. IS DUE: 16 J AN 2026 CALENDAR | resolved: STATUS SYMBOL UPGRADED…
Fault
2025-07-089,062.6 hrshigh
H-60-25-ASAM-10 pilot and copilot seat harness assembly replacement due 22 Jan 26.
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
2025-07-109,062.6 hrshigh
H-60-25-ASAM-10 pilot seat harness assembly replaced, closed fault.
PILOT SEAT HARNESS ASSEMBLY REQUIRES REPLACEMENT PER H-60-25-A SAM-10 NO LATER THAN 31 JAN 26 | resolved: replaced seat belt | status: closed | recorded 2025-07-10 @ 9062.6h | closed 2025-09-04 @ 9062.6h
COPILOT SEAT HARNESS ASSEMBLY REQUIRES REPLACEMENT PER H-60-25 -ASAM-10 NO LATER THAN 31 JAN 26 | resolved: replaced seat belt assybly | status: closed | recorded 2025-07-10 @ 9062.6h | closed 2025-09-04 @ 9062.6h
Fault
2025-08-159,062.6 hrshigh
H-60-25-ASAM-11 main landing gear axle radial movement inspection due at 9062.6 hours at next scheduled inspection.
COMPLY WITH H-60-25-ASAM-11, MAIN LANDING GEAR AXLE RADIAL MOV EMENT INSEPECITON, AT 9062.6 ACFT HOURS AT THE NEXT SCHEDULED PREVENTIVE MAINTENANCE INSPECTION (PMI) BUT NOT TO EXCEED 14 A UG 2027. | status: open | recorded 2025-08-15 @…
Fault
2025-04-299,060.3 hrshigh
H-60-25-ASAM-07 reliability enhanced stabilator actuator inspection complied with prior to next flight.
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 INSPECION. | status:…
Fault
2025-04-299,060.3 hrshigh
H-60-25-ASAM-08 main generator lug terminal inspection complied with 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 2025-04-29 @ 9060.3h | closed 2025-05-05 @…
Fault
2025-04-299,060.3 hrshigh
H-60-25-ASAM-06 ADS-B inspection complied with 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 @ 9060.3h | closed 2025-06-16 @ 9060.3h
Fault
2025-04-299,060.3 hrshigh
H-60-25-ASAM-04 main rotor blade inspection complied with 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. THE FOLLOWING BLADES ARE AFFECTED AND REQUIRE…
Fault
2025-04-299,060.3 hrshigh
H-60-25-ASAM-05 T700 series accessory module replacement before 9070.3 hours, but not later than 11 May 25.
COMPLY WITH H-60-25-ASAM-05, T700 SERIES ACCESSORY MODULE REPL ACEMENT, BEFORE 9070.3 HOURS, BUT NOT LATER THAN 11 MAY 25. | resolved: COMPLIED WITH H-60-25-ASAM-05, T700 SERIES ACCESSORY SECTI ON MODULE REPLACEMENT. | status: closed |…
Fault
2022-07-158,767.9 hrshigh
H-60-22-AMAM-08 NAS1304 bolt inspection at next scheduled inspection, due by 14 Jul 26.
SAFETY MESSAGE NUMBER: H-60-22-AMAM-08 DESCRIPTION: COMPLY WIT H H-60-22-AMAM-08, NAS1304 BOLT INSPECTION AT THE NEXT SCHEDUL ED PMI BUT NOT TO EXCEED 14 JUL 26.. IS DUE: 14 JUL 2026 CALE NDAR | status: open | recorded 2022-07-15 @ 8767.9h
BOLTS NAS1304 ( INBOARD 2ND STAGE ATTACHMENT BOLTS 2EA) REQUIR ES REPLACEMENT PER "H-60-22AMAM-08 BY 14 JUL 26" | status: open | recorded 2023-07-05 @ 8899.1h
Fault
2023-07-058,899.1 hrshigh
H-60-22-AMAM-08 NAS1304 all 1st stage attachment bolts require replacement by 14 Jul 26.
BOLTS NAS1304 ( ALL 1ST STAGE ATTACHMENT BOLTS 4EA) REQUIRES R EPLACEMENT PER "H-60-22AMAM-08 BY 14 JUL 26" | status: open | recorded 2023-07-05 @ 8899.1h
Fault
2025-07-109,062.6 hrsEntry errormedium
Entry error: copilot seat harness assembly requires replacement per H-60-25-ASAM-10 no later than 31 Jan 26.
[ENTRY ERROR] COPILOT SEAT HARNESS ASSEMBLY REQUIRES REPLACEMENT PER H-60-25 -ASAM-10 NO LATER THAN 31 JAN 26 | resolved: CLOSED IN ERROR BY MUELLER, JASON CIV Entry made in error. | status: closed | recorded 2025-07-10 @ 9062.6h |…
Fault
2025-07-109,062.6 hrsEntry errormedium
Entry error: copilot seat harness assembly requires replacement per H-60-25-ASAM-10 no later than 31 Jan 26, duplicate.
[ENTRY ERROR] COPILOT SEAT HARNESS ASSEMBLY REQUIRES REPLACEMENT PER H-60-25 -ASAM-10 NO LATER THAN 31 JAN 26 | resolved: CLOSED IN ERROR BY MUELLER, JASON CIV Entry made in error. | status: closed | recorded 2025-07-10 @ 9062.6h |…
The aircraft was inducted into the BEST program on 06 April 2026 at 9062.6 hours, with no DA 2408-18 scheduled maintenance performed after that date. Multiple components are nearing end of life or require replacement, including main rotor blades requiring replacement per H-60-25-ASAM-04 at 9110.3 hours, and several 9-11 hour torque checks due on main rotor blade hardware. High-time items and accumulated wear are evident across multiple systems.
Fault
2026-04-239,062.6 hrshigh
Aircraft inducted into BEST program on 06 April 2026 at 9062.6 hours; 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 @ 9062.6h
Fault
2025-05-029,060.3 hrshigh
Main rotor blade PN 70150-09100-043F SN A007-16450 requires replacement per H-60-25-ASAM-04 at 9110.3 aircraft hours.
MAIN ROTOR BLADE PN 70150-09100-043F, SN A007-16450 REQUIRES R EPLACEMENT PER H-60-25-ASAM-04 AT 9110.3 AIRCRAFT HOURS, BUT N OT TO EXCEED 3 JUN 25. | resolved: REPLACED WITH SN: A007-19756 | status: closed | recorded 2025-05-02 @ 9060.3h…
Fault
2025-05-029,060.3 hrshigh
Main rotor blade PN 70150-09100-043F SN A007-07151 requires replacement per H-60-25-ASAM-04 at 9110.3 aircraft hours.
MAIN ROTOR BLADE PN 70150-09100-043F, SN A007-07151 REQUIRES R EPLACEMENT PER H-60-25-ASAM-04 AT 9110.3 AIRCRAFT HOURS, BUT N OT TO EXCEED 3 JUN 25. | resolved: REPLACED WITH SN: A007-19582 | status: closed | recorded 2025-05-02 @ 9060.3h…
Fault
2025-05-149,060.3 hrshigh
9-11 hour torque check required on black main rotor blade outboard damper attachment hardware due to replacement.
9-11 HOUR TORQUE CHECK REQUIRED ON BLACK MAIN ROTOR BLADE OUTB OARD DAMPER ATTACHMENT HDWR DUE TO THE REPLACEMENT OF BLACK SP INDLE. DUE BETWEEN 9069.3 TO 9071.3 FLIGHT HOURS. 2ND ATTEMPT | status: open | recorded 2025-05-14 @ 9060.3h
Fault
2025-05-159,060.3 hrshigh
9-11 hour torque check due on black spindle attachment hardware at 9069.3 to 9071.3 flight hours.
9-11 HR TQ CHECK DUE ON BLACK SPINDLE ATTACHMENT HARDWARE AT 9 069.3 TO 9071.3 FLIGHT HOURS DUE TO THE REPLACEMENT OF SPINDLE . 2ND ATTEMPT | resolved: WRITTEN UP TWICE | status: closed | recorded 2025-05-15 @ 9060.3h | closed 2025-06-16 @…
Fault
2025-05-159,060.3 hrsEntry errormedium
Entry error: 9-11 hour torque check due on spindle attachment hardware at 9069.3 to 9071.3 flight hours.
[ENTRY ERROR] 9-11 HR TQ CHECK DUE ON SPINDLE ATTACHMENT HARDWARE AT 9069.3 TO 9071.3 FLIGHT HOURS DUE TO THE REPLACEMENT OF SPINDLE. 2ND ATTEMPT | resolved: WRITTEN IN ERROR | status: closed | recorded 2025-05-15 @ 9060.3h | closed…
Fault
2024-12-199,049.3 hrshigh
Black outboard damper attachment hardware requires proseal after 9-11 hour torque stabilized, open since December 2024.
BLACK OUTBOARD DAMPER ATTACHMENT HARDWARE REQUIRES PROSEAL AFT ER 9-11 HOUR TORQUE STABILIZED | status: open | recorded 2024-12-19 @ 9049.3h
Fault
2024-12-199,049.3 hrshigh
9-11 hour torque check required on black main rotor blade spindle to blade bonding jumper hardware.
9-11 HOUR TORQUE CHECK REQUIRED ON BLACK MAIN ROTOR BLADE SPIN DLE TO BLADE BODING JUMPER HARDWARE DUE TO THE REPLACEMENT OF BLACK SPINDLE. DUE BETWEEN 9058.3 TO 9060.3 FLIGHT HOURS | resolved: comlpeted. tq'd to 713 in lbs | status:…
Fault
2024-12-199,049.3 hrshigh
9-11 hour torque check required on black main rotor blade outboard damper attachment hardware, duplicate entry.
9-11 HOUR TORQUE CHECK REQUIRED ON BLACK MAIN ROTOR BLADE OUTB OARD DAMPER ATTACHMENT HDWR DUE TO THE REPLACEMENT OF BLACK SP INDLE. DUE BETWEEN 9058.3 TO 9060.3 FLIGHT HOURS | resolved: COMPLETED. TQ CHECK FAILED | status: closed |…
Fault
2024-12-199,049.3 hrshigh
9-11 hour torque check due on spindle attachment hardware at 9058.3 to 9060.3 flight hours.
9-11 HR TQ CHECK DUE ON SPINDLE ATTACHMENT HARDWARE AT 9058.3 TO 9060.3 FLIGHT HOURS DUE TO THE REPLACEMENT OF BLACK SPINDLE | resolved: TQ CHECK FAILED. BOLTS 6,8, AND 11 FAILED TO STABILIZE | status: closed | recorded 2024-12-19 @…
Fault
2024-12-199,049.3 hrsEntry errormedium
Entry error: 9-11 hour torque check required on black main rotor blade anti-flap hardware due to replacement.
[ENTRY ERROR] 9-11 HOUR TORQUE CHECK REQUIRED ON BLACK MAIN ROTOR BLADE ANTI FLAP HDWR DUE TO THE REPLACEMENT OF BLACK SPINDLE. DUE BETWEEN 9058.3 TO 9060.3 FLIGHT HOURS | resolved: entered in error. tq verified to 195 in lbs | status:…
The seller has flagged critical items for buyer attention. The following items have been removed from the aircraft at the direction of the U.S. Government: specific components are listed in the notice to buyer. The aircraft was inducted into the BEST program on 23 February 2026 and transferred to ASF HOOD. Resample of APU and main transmission module is required prior to next start-up due to incomplete records. Batteries were removed due to ORF status.
Fault
2026-04-179,062.6 hrshigh
Notice to buyer: items have been removed from the aircraft at the direction of the 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…
Historical
2026-02-23high
Aircraft transferred to BEST program on 23 February 2026 for ARMY/BEST program by ASF HOOD at 9062.6 aircraft hours.
Aircraft transfered to BEST program on 23 February 2026 for AR MY / BEST program by ASF HOOD (W6TU14) @ 9062.6 acft hrs. Data Plate remains installed | at W6TU14 | on 2026-02-23
Fault
2026-04-239,062.6 hrshigh
Resample of APU SN SPE041042 required prior to next start-up due to incomplete records.
RESAMPLE OF APU SN: SPE041042 REQUIRED PRIOR TO NEXT START UP DUE TO INCOMPLETE RECORDS. | status: open | recorded 2026-04-23 @ 9062.6h
Fault
2026-04-239,062.6 hrshigh
Resample required of main transmission module SN A80301901 due to incomplete records.
RESAMPLE REQUIRED OF MAIN TRANSMISSION MODULE SN: A80301901 DU E TO INCOMPLETE RECORDS | status: open | recorded 2026-04-23 @ 9062.6h
Fault
2025-08-279,062.6 hrsmedium
Informational write-up: batteries were removed due to aircraft being on ORF status.
INFORMATIONAL WRITE-UP: THE FOLLOWING BATTERIES WERE REMOVED D UE TO THE AIRCRAFT BEING ON ORF STATUS. THE BATTERIES WILL BE REINSTALLED WHEN THE AIRCRAFT RETURNS TO A FLYABLE STATUS: GMR BATTERY, KGV BATTERY, KY-58 BATTERIES (2 EA),…
Historical
2025-07-10high
Pilot and copilot seat harness assembly replacement performed on 10 July 2025.
PILOT AND COPILOT SEAT HARNESS ASSEMBLY REPLACEMENT | at WYPPA0 TX,CO,CA,KS | on 2025-07-10
Several administrative gaps and data-quality issues are present. Multiple entry errors have been documented, including duplicate entries for seat harness replacement requirements and torque check requirements. One entry was made in error with incorrect tail number. These issues may indicate incomplete or inconsistent record-keeping.
[ENTRY ERROR] COPILOT SEAT HARNESS ASSEMBLY REQUIRES REPLACEMENT PER H-60-25 -ASAM-10 NO LATER THAN 31 JAN 26 | resolved: CLOSED IN ERROR BY MUELLER, JASON CIV Entry made in error. | status: closed | recorded 2025-07-10 @ 9062.6h |…
[ENTRY ERROR] COPILOT SEAT HARNESS ASSEMBLY REQUIRES REPLACEMENT PER H-60-25 -ASAM-10 NO LATER THAN 31 JAN 26 | resolved: CLOSED IN ERROR BY MUELLER, JASON CIV Entry made in error. | status: closed | recorded 2025-07-10 @ 9062.6h |…
Fault
2025-05-159,060.3 hrsEntry errorhigh
Entry error: 9-11 hour torque check due on spindle attachment hardware, administrative duplicate.
[ENTRY ERROR] 9-11 HR TQ CHECK DUE ON SPINDLE ATTACHMENT HARDWARE AT 9069.3 TO 9071.3 FLIGHT HOURS DUE TO THE REPLACEMENT OF SPINDLE. 2ND ATTEMPT | resolved: WRITTEN IN ERROR | status: closed | recorded 2025-05-15 @ 9060.3h | closed…
Fault
2024-12-199,049.3 hrsEntry errorhigh
Entry error: 9-11 hour torque check required on black main rotor blade anti-flap hardware, administrative duplicate.
[ENTRY ERROR] 9-11 HOUR TORQUE CHECK REQUIRED ON BLACK MAIN ROTOR BLADE ANTI FLAP HDWR DUE TO THE REPLACEMENT OF BLACK SPINDLE. DUE BETWEEN 9058.3 TO 9060.3 FLIGHT HOURS | resolved: entered in error. tq verified to 195 in lbs | status:…
Fault
2025-06-119,060.3 hrsEntry errormedium
Entry error: inspection manually generated, PMI due entry was made in error.
[ENTRY ERROR] INSP A399 PMI DUE FOR HELICPTR UTIL UH-60L CAGE: 78286 PN: UH- 60L NSN: 1520012984532 SN: 9826812 WAS DUE. STATUS UPGRADED TO X ON: 10 JUN 2025 REFERENCE: TM 1-1520-237-20P | resolved: Fault entered in error. PMI-2…
Historical
2022-01-31Entry errorhigh
Entry error: entry was made in error with incorrect tail number, late entry MEC F348328.
[ENTRY ERROR] THE FOLLOWING ENTRY WAS MADE IN ERROR, INCORRECT TAIL NUMBER " LATE ENRTY: MEC F348328 FT HOOD AMCOM LRC-A MAY REUSE THE ROTA RY INPUT BARRELS PROVIDED THAT THEY PASS THE NDI REQUIREMENT" | at WDX9A0 Hunter Army Airfield | on…
Custom Analysis
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