Component lifecycle analysis across airframe and engines
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Records Search
Semantic search across 1130
maintenance records (493 faults, 637 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, restricted from NVD flight due to radar altimeter failure, restricted from cargo hook operations due to removed squib, and restricted from Satcom usage due to torn coax connector. Additionally, the aircraft is restricted to day-VFR-only operations due to de-ice system failure.
Fault
2025-03-247,192.5 hrshigh
Coax connector torn at Satcom antenna, restricting aircraft from Satcom usage.
Coax Connector Torn At Satcom Antenna, Aircraft Restricted Fro m Satcom Usage | status: open | recorded 2025-03-24 @ 7192.5h
Fault
2025-07-197,246.3 hrshigh
Copilot and pilot radar altimeter read zero, restricting aircraft from NVD flight operations.
COPILOT AND PILOT RADAR ALTIMETER READ ZERO. AIRCRAFT RESTRICT ED FROM NVD FLIGHT IAW AR 95-1 TABLE 5-2 | resolved: CO-PILOT RADAR ALTIMETER (SN: 1119GGA) REPLACED WITH (SN: 1530AA) | status: closed | recorded 2025-07-19 @ 7246.3h |…
Fault
2026-01-097,297.0 hrshigh
Aircraft restricted from cargo hook operations due to removal of squib for aircraft turn-in.
ACFT RESTRICTED FROM CARGO HOOK OPERATIONS DUE TO REMOVAL OF S QUIB FOR ACFT TURN IN | status: open | recorded 2026-01-09 @ 7297h
Fault
2025-08-157,270.1 hrshigh
Aircraft restricted from flight into moderate icing conditions due to failure of de-ice EOT check.
AIRCRAFT RESTRICTED FROM FLIGHT INTO MODERATE ICING CONDITIONS DUE TO FAILURE OF DE-ICE EOT CHECK. DE-ICE EOT CHECK FAILED S TEP 8, M/R DE-ICE FAIL AND M/R DE-ICE FAULT CAUTIONS ILLUMINAT ED IMMEDIATELY. | resolved: Replaced DCIU SN: 0390…
Fault
2025-07-127,238.1 hrshigh
Aircraft restricted from external loads and terrain flight due to intermittent radar altimeter below 20 feet.
ACFT RESTRICTED FROM EXTERNAL LOADS AND TERRAIN FLIGHT DUE TO INTERMITENT RADAR ALTIMETER BELOW 20FT | resolved: REPLACED COPILOT ALTIMETER. SEE CLOSED CLOSED FAULTS DATED 21JUL25 FOR 13-2s | status: closed | recorded 2025-07-12 @ 7238.1h…
Fault
2025-07-097,231.6 hrshigh
Left hand crew chief forward facing inertia reel does not lock when testing harness.
LEFT HAND CREW CHIEF FWD FACING INERTIA REEL DOES NOT LOCK WHE N TESTING HARNESS. REQUIRES FURTHER INSPECTION | resolved: FAULT COULD NOT BE DUPLACATED | status: closed | recorded 2025-07-09 @ 7231.6h | closed 2025-08-11 @ 7270.1h
Fault
2025-07-217,246.3 hrsmedium
Copilot radar altimeter lower LH screw not installed due to nutplate not installed.
COPILOT RADAR ALTIMETER LOWER LH SCREW NOT INSTALLED DUE TO NU TPLATE NOT INSTALLED | status: open | recorded 2025-07-21 @ 7246.3h
This aircraft has several open structural issues requiring attention. A thermal blanket on the front bleed air tube to mixing valve is torn and requires replacement. The main transmission drip pan drain tube is torn. Additionally, the number 1 engine A sump oil drain line has a small tear next to the lower engine mount.
Fault
2024-09-067,138.9 hrshigh
Thermal blanket on front bleed air tube to mixing valve torn, requires replacement.
THERMAL BLANKET ON FRONT BLEED AIR TUBE TO MIXING VALVE TORN R EQUIRES REPLACEMENT | status: open | recorded 2024-09-06 @ 7138.9h
Fault
2025-05-047,209.0 hrshigh
Number 1 engine A sump oil drain line has a small tear next to the lower engine mount.
#1 ENG A sump oil drain line has a small tear next to the lowe r ENG mount | status: open | recorded 2025-05-04 @ 7209h
Fault
2025-09-257,290.2 hrshigh
Number 1 IPS blower exhaust duct has 5 inch crack on previous repair.
No.1 IPS Blower exhaust duct has 5 inch crack on preivous repa ir. | resolved: REPAIRED USING FIBERGLASS PATCH AND EA9313 | status: closed | recorded 2025-09-25 @ 7290.2h | closed 2025-09-29 @ 7290.2h
Fault
2025-07-027,230.1 hrshigh
Number 1 engine IPS blower duct has 2 inch crack.
#1 ENG IPS BLOWER DUCT HAS 2" CRACK | resolved: REPAIRED CRACK | status: closed | recorded 2025-07-02 @ 7230.1h | closed 2025-09-04 @ 7275.1h
Fault
2025-06-257,217.0 hrshigh
Number 1 engine IPS blower duct has crack requiring repair.
#1 ENG IPS BLOWER DUCT HAS CRACK. REQUIRES REPAIR. | resolved: DUPLICATE WRITE UP REFER TO OTHER 13-1 REFERENCING 2" CRAC K | status: closed | recorded 2025-06-25 @ 7217h | closed 2025-07-03 @ 7230.1h
This aircraft has one critical open Aviation Safety Action Message (H-60-26-SOF-02) requiring compliance prior to next flight but not to exceed 17 Dec 25. The message addresses non-conforming primary main rotor servos. Additionally, the aircraft has an open requirement for pilot and copilot seat harness assembly replacement per H-60-25-ASAM-10 no later than 31 Jan 26.
Fault
2026-01-087,297.0 hrshigh
H-60-26-SOF-02 non-conforming primary main rotor servos compliance required prior to next flight but not to exceed 17 Dec 25.
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: COMPLIED WITH | status: closed | recorded 2026-01-08 @ 7297h | closed 2026-01-08 @ 7297h
Fault
2025-07-107,231.6 hrshigh
H-60-25-ASAM-10 pilot seat harness assembly replacement required 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 | status: open | recorded 2025-07-10 @ 7231.6h
Fault
2025-07-107,231.6 hrshigh
H-60-25-ASAM-10 copilot seat harness assembly replacement required no later than 31 Jan 26.
COPILOT SEAT HARNESS ASSEMBLY REQUIRES REPLACEMENT PER H-60-25 -ASAM-10 NO LATER THAN 31 JAN 26 | status: open | recorded 2025-07-10 @ 7231.6h
Fault
2025-07-097,230.1 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: COMPLIED WITH H-60-25-ASAM-10 PILOT AND COPILOT HARNESS RE PLACEMENT | status: closed |…
SAFETY MESSAGE NUMBER: H-60-25-ASAM-06 DESCRIPTION: "COMPLY WI TH H-60-25-ASAM-06, AUTOMATIC DEPENDENT SURVEILLANCE - BROADCA ST (OUT) (ADS-B (OUT)) INSPECTION BY 24 MAY 25". IS DUE: 24 M AY 2025 CALENDAR | resolved: COMPLIED WITH…
Fault
2025-05-197,209.0 hrshigh
ATC confirmation of successful in-flight ADS-B (OUT) data transmission required by 18 Jun 25.
ATC CONFIRMATION OF SUCCESSFUL IN-FLIGHT ADS-B (OUT) DATA TRAN SMISSION REQUIRED BY 18 JUN 25 | resolved: "Complied with H-60-25-ASAM-06, Automatic Dependent Survei lance-Broadcast (OUT) ADS-B (OUT)) Inspection." | status: closed |…
This aircraft was inducted into the BEST Program on 27 Apr 2026, with no scheduled maintenance performed after this date. The aircraft has accumulated 7301.1 hours at induction. Several components are nearing or at end of life, including batteries and filters. The yellow main rotor blade taco patch is worn and disbonding beyond limits, requiring repair.
Fault
2026-04-277,301.1 hrshigh
Aircraft inducted into the BEST Program on 27 Apr 2026; 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 @ 7301.1h
Fault
2025-09-097,278.1 hrshigh
Yellow main rotor blade taco patch worn and disbonding beyond limits, requires repair.
YELLOW MR BLADE TACO PATCH WORN AND DISBONDING BEYOND LIMITS. REQUIRES REPAIR | status: open | recorded 2025-09-09 @ 7278.1h
Fault
2025-07-027,230.1 hrshigh
Yellow main rotor blade taco patch worn, requires further inspection.
YELLOW M/R BLADE TACO PATCH WORN, REQUIRES FURTHER INSPECTION | resolved: RE ENTRY AS / SEE WRITE UP 09 SEP 2025 | status: closed | recorded 2025-07-02 @ 7230.1h | closed 2025-09-09 @ 7278.1h
Fault
2025-08-027,267.4 hrshigh
Main module oil filter button indicator popped, requires filter replacement and inspection.
MAIN MOD OIL FILTER BUTTON INDICATOR POPPED REQ'S FILTER REPLA CEMENT/ INSP | resolved: replaced filters | status: closed | recorded 2025-08-02 @ 7267.4h | closed 2025-08-02 @ 7267.4h
Historical
2011-09-22medium
Main module impending bypass button extended at 5432.9 aircraft hours.
MAIN MOD IMPENDING BY PASS BUTTON EXTENDED AT 5432.9 ACFT HRS Original Location: D CO 7-101ST GSAB FT. CAMPBELL, KY 42223-50 00 | at WHNRA0 Ft. Drum, NY | on 2011-09-22
The seller has flagged multiple items for buyer attention. Prior to delivery, several components will be removed from the aircraft including crypto equipment, radios, and mission-specific systems. Blanking plates are required on areas where components were removed for lateral transfer. The aircraft has missing cabin floor tie-down rings (2 EA) and a missing vent blower O-ring. Wire strikes on number 1 and number 2 require proseal. The aircraft was prepared for lateral transfer to ASF Hood with multiple components removed.
Fault
2026-05-187,301.1 hrshigh
REMARK/NOTICE TO BUYER: Prior to delivery, multiple items will be removed from the aircraft.
“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
2026-05-127,301.1 hrsEntry errorhigh
NOTICE TO BUYER: Multiple items have been removed from the aircraft at the direction of the 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
2026-05-047,301.1 hrshigh
REMARK/NOTICE TO BUYER: Prior to delivery, multiple items will be removed from the aircraft.
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
2026-01-147,301.1 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 DER TO 13-1 "LATERAL TRANSFER COMPONENT REMOVAL" FOR LOCAT IONS COVERED. |…
Fault
2026-01-147,301.1 hrshigh
Aircraft prepared for lateral transfer to ASF Hood; see 13-2s for components removed.
ACFT PREPARED FOR LATERAL TRANSFER TO ASF HOOD. SEE 13-2'S FOR FOLLOWING COMPONENTS RMVD. | resolved: COMPONENTS RMVD | status: closed | recorded 2026-01-14 @ 7301.1h | closed 2026-01-14 @ 7301.1h
Fault
2024-06-267,111.9 hrshigh
Cabin floor tie-down rings (2 EA) not installed.
CABIN FLOOR TIE-DOWN RINGS 2 EA NOT INSTALLED | status: open | recorded 2024-06-26 @ 7111.9h
Fault
2025-05-047,209.0 hrshigh
Vent blower O-ring between blower and hydraulic sliding door not installed.
Vent blower oring between blower and hydraulic sliding door no t installed | status: open | recorded 2025-05-04 @ 7209h
Fault
2026-01-087,297.0 hrshigh
Number 1 and number 2 wire strikes require proseal.
NO.1 AND NO.2 WIRE STRIKES REQ'R PRO SEAL | status: open | recorded 2026-01-08 @ 7297h
Fault
2026-01-097,297.0 hrshigh
Proseal required on blue pitch control rod hardware and jamnut after 9-11 torque check stabilization.
PROSEAL REQUIRED ON BLUE PC ROD HDWR AND JAMNUT AFTER 9-11 TQ CHECK STABALIZATION | status: open | recorded 2026-01-09 @ 7297h
This aircraft has multiple [ENTRY ERROR] records that indicate data-quality issues in the maintenance tracking system. These errors span various inspection types including bleed-air shutoff valve cleaning, IVHUMS vibration data upload, preventive maintenance daily inspections, and engine max power verification. Additionally, APU oil sample historical information is not available within ACN, preventing appropriate records generation.
Fault
2025-08-037,270.1 hrsEntry errorhigh
[ENTRY ERROR] for number 1 bleed-air shutoff valve cleaning inspection.
[ENTRY ERROR] INSP A819 #1 BLEED-AIR SHUTOFF VALVE CLEANING DUE FOR HELICPTR UTIL UH-60L CAGE: 78286 PN: UH-60L NSN: 1520012984532 SN: 932 6513 WAS DUE. STATUS UPGRADED TO X ON: 7194.1 AIRCRAFT HOURS REFERENCE: SOP TM 1-1520-237-23 |…
Fault
2025-10-237,297.0 hrsEntry errorhigh
[ENTRY ERROR] for IVHUMS vibration data upload inspection.
[ENTRY ERROR] INSP A822 2408-15-2 UPLOAD OF IVHUMS VIBRATION DATA FOR ENG'S, OIL COOLER AND TAIL ROTOR FOR HELICPTR UTIL UH-60L CAGE: 7828 6 PN: UH-60L NSN: 1520012984532 SN: 9326513 WAS DUE. STATUS UP GRADED TO X ON: 7284.3 AIRCRAFT HOURS…
Fault
2025-08-037,270.1 hrsEntry errorhigh
[ENTRY ERROR] for 120 hour engine max power verification after completion of engine flushes.
[ENTRY ERROR] INSP A815 120 HOUR ENG MAX POWER VERIFICATION AFTER COMPLETION OF ENG FLUSHES FOR HELICPTR UTIL UH-60L CAGE: 78286 PN: UH-60 L NSN: 1520012984532 SN: 9326513 WAS DUE. STATUS UPGRADED TO X ON: 7198.1 AIRCRAFT HOURS REFERENCE:…
Fault
2025-10-237,297.0 hrsEntry errorhigh
[ENTRY ERROR] for preventive maintenance daily inspection.
[ENTRY ERROR] INSP A805 PREVENTIVE MAINTENANCE DAILY DUE FOR HELICPTR UTIL U H-60L CAGE: 78286 PN: UH-60L NSN: 1520012984532 SN: 9326513 WA S DUE. STATUS UPGRADED TO X ON: 22 NOV 2024 REFERENCE: TM 1- 1520-237-23&P, WP 0354-0361 |…
Fault
2025-09-247,290.2 hrsEntry errorhigh
[ENTRY ERROR] for 120 hour engine max power verification after completion of engine flushes.
[ENTRY ERROR] INSP A815 120 HOUR ENG MAX POWER VERIFICATION AFTER COMPLETION OF ENG FLUSHES FOR HELICPTR UTIL UH-60L CAGE: 78286 PN: UH-60 L NSN: 1520012984532 SN: 9326513 WAS DUE. STATUS UPGRADED TO X ON: 7198.1 AIRCRAFT HOURS REFERENCE:…
Fault
2025-09-247,290.2 hrsEntry errorhigh
[ENTRY ERROR] for number 2 bleed-air shutoff valve cleaning inspection.
[ENTRY ERROR] INSP A820 # 2 BLEED-AIR SHUTOFF VALVE CLEANING DUE FOR HELICPT R UTIL UH-60L CAGE: 78286 PN: UH-60L NSN: 1520012984532 SN: 93 26513 WAS DUE. STATUS UPGRADED TO X ON: 7194.1 AIRCRAFT HOURS REFERENCE: SOP, TM1-1520-237-23 |…
Fault
2026-05-277,301.1 hrshigh
APU oil sample historical information not available within ACN; appropriate records cannot be generated.
2408-20 APU oil sample historical information not avaiable wit hin ACN, appropriate records can not be generated. | status: open | recorded 2026-05-27 @ 7301.1h
Fault
2025-05-057,209.0 hrsEntry errormedium
[ENTRY ERROR] for maintenance test flight required due to removal and reinstallation of number 1 engine load-demand rotary input.
[ENTRY ERROR] MTF REQUIRED DUE TO REMOVAL AND REINSTALLATION OF #1 ENG LOAD- DEMAND ROTARY INPUT FROM THE HMU | resolved: CLOSED IN ERROR BY MORALES, HECTOR SGT Entry made in erro r. | status: closed | recorded 2025-05-05 @ 7209h | closed…
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