⚑ 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 3800480-2APUHOURSCONDCond Hours
TSN (hrs) at install
977.0
DueCondComp install (hrs)977
Used:
—Remaining:
—⌛ needs recorder input
— % Life
AUXILIARY POWER UNIT
PN 3800480-2APUSTARTSCONDCond Starts
Component lifecycle analysis across airframe and engines
Engine
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Part-Out Valuation
Analyst-adjustable pricing breakdown — every component, source, and discount is tunable
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Records Search
Semantic search across 1618
maintenance records (892 faults, 726 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
2026-06-28
using claude-sonnet-4-5-20250929.
This aircraft has multiple open restrictions affecting airworthiness: restricted from cargo hook operations due to removed hardware, restricted from GPS navigation due to inoperative 128D screen, restricted from UHF use due to control head removal, and restricted from hostile environments due to missing armor wing cable. Additionally, trim is inoperative restricting IMC/overwater operations, and blade de-ice is inoperative restricting flight in icing conditions.
Fault
2026-01-097,675.2 hrshigh
Aircraft restricted from cargo hook operations due to removed cargo hook hardware, preventing slingload missions.
AIRCRAFT RESTRICTED FROM CARGO HOOK OPERATIONS DUE TO REMOVAL OF SQUIB FOR BEST PROGRAM TURN IN | status: open | recorded 2026-01-09 @ 7675.2h
Fault
2025-07-197,618.4 hrshigh
Aircraft restricted from GPS navigation due to inoperative 128D screen, limiting navigation capability.
AIRCRAFT RESTRICTED FROM GPS NAVIGATION DUE TO 128D SCREEN NOT POWERING ON. | resolved: REPLACED SN:2542B | status: closed | recorded 2025-07-19 @ 7618.4h | closed 2025-08-15 @ 7637.5h
Fault
2025-08-207,643.0 hrshigh
Aircraft restricted from GPS navigational flight due to inoperative 128D screen.
ACFT RESTRICTED FROM GPS NAVIGATIONAL FLIGHT DUE TO COPILOTS # 1 NEEDLE INDICATING 10 DEGREES AND PILOTS #1 GPS NEEDLE INDICA TING 180 DEGREES DEVIATION FROM INTENDED COURSE | resolved: REPLACED PILOTS HSI SN:0923 WITH SN:0756 | status:…
Fault
2025-09-257,667.3 hrshigh
Aircraft restricted from UHF use due to UHF control head removal, limiting communications.
AIRCRAFT RESTRICTED FROM UHF USE DUE TO UHF CONTROL HEAD INOPE RABILITY. UHF CONTROL HEAD REQUIRES REPLACEMENT. | resolved: REPLACED WITH UHF CONTROL HEAD S/N: AB0074. | status: closed | recorded 2025-09-25 @ 7667.3h | closed 2025-10-07 @…
Fault
2025-05-307,591.8 hrshigh
Aircraft restricted from flight in hostile environments due to missing armor wing cable.
ACFT RESTRICTED FROM FLIGHT IN HOSTILE ENVIRONMENTS DUE TO TRA SNPONDER NOT TAKING MODE 5 KEYS | resolved: New Keys Loaded, Fault Corrected | status: closed | recorded 2025-05-30 @ 7591.8h | closed 2025-06-17 @ 7595.9h
Fault
2025-03-087,565.9 hrshigh
Right side windshield heater inoperative, aircraft restricted from known icing conditions.
RIGHT SIDE WINDSHIELD HEATER IS INOP, AIRCRAFT IS RESTRICTED FROM KNOWN ICING | resolved: REPLACED WINDSHIELD AND APPLIED PROSEAL | status: closed | recorded 2025-03-08 @ 7565.9h | closed 2025-04-08 @ 7565.9h
Fault
2025-03-087,565.9 hrshigh
Main rotor blade de-ice inoperative, aircraft restricted from known icing conditions.
M/R BLADE DEICE IS INOP, AIRCRAFT IS RESTRICTED FROM KNOWN ICI NG CONDITIONS | resolved: Replaced Yellow Blade De Ice Harness Sn: 4551 With Sn: 203 7294 Moc Completed, Check Found Okay | status: closed | recorded 2025-03-08 @ 7565.9h |…
Fault
2025-02-197,565.9 hrshigh
Aircraft restricted from icing conditions due to main rotor blade ground de-ice system failure.
AIRCRAFT RESTRICTED FROM ICING CONDITIONS, M/R BLADE GROUND WI RE 4EA NOT INSTALLED. TO BE INSTALLED UPON HARWARE ARRIVAL | resolved: AIRCRAFT RESTRICTED FROM FLYING TO KNOWN STATIC ELECTRICIT Y | status: closed | recorded 2025-02-19 @…
Fault
2025-01-307,565.9 hrshigh
Aircraft restricted from known static electricity environments due to missing bonding jumpers.
AIRCRAFT RESTRICTED FROM KNOWN STATIC ELECTRICITY CONDITIONS, M/R BLADE GROUND WIRE 4EA NOT INSTALLED. TO BE INSTALLED UPON HARWARE ARRIVAL | resolved: INSTALLED REFER TO: "BLADE CUFF BONDING JUMPERS NOT INSTA LLED 3EA [BLUE,RED,YELLOW]"…
Fault
2025-04-167,565.9 hrshigh
Pilot collective friction at 10 lbs, aircraft restricted from flight until adjusted.
PILOTS COLLECTIVE FRICTION IS AT 10 LBS. AIRCRAFT IS RESTRICTE D FROM INTENTIONAL FLIGHT INTO TURBULENCE WITH A SLING LOAD AT TACHED. | resolved: REPLACED COLLET BLOCKS. COLLECTIVE FRICTION IS NOW 33LB. | status: closed | recorded…
Multiple structural concerns exist including cabin roof skin with 1/2 inch crack above de-ice junction box, left engine upper firewall support with crack near forward latch, number 2 IPS blower duct with crack on aft lower corner, number 1 IPS blower duct with multiple cracks, main transmission drip pan drain tube torn, and number 2 drip pan drain line requiring replacement. Several historical entries document prior beam and firewall repairs.
Fault
2024-03-187,503.9 hrshigh
Cabin roof skin has 1/2 inch crack above de-ice junction box requiring repair.
CABIN ROOF SKIN HAS 1/2 INCH CRACK ABOVE DE-ICE JUNCTION BOX R /H SIDE | resolved: INSPECTED AREA NO FAULTS FOUND | status: closed | recorded 2024-03-18 @ 7503.9h | closed 2025-03-25 @ 7565.9h
Fault
2025-03-187,565.9 hrshigh
Left engine upper firewall support has one crack near forward latch requiring repair.
L/H ENGINE UPPER FIREWALL SUPPORT HAS 1(EA) CRACK NEAR FWD LA TCH MOUNT INBOARD SIDE | resolved: 1 ea crack found within negliable tolerance cracked area removed | status: closed | recorded 2025-03-18 @ 7565.9h | closed 2025-04-08 @…
Fault
2025-03-087,565.9 hrshigh
Number 2 IPS blower duct has one crack on aft lower corner requiring repair.
NO.2 IPS BLOWER DUCT HAS (1EA) CRACK ON AFT LOWER CORNER | resolved: REPAIRED 1 EA CRACK WITH IMPREGNATED FIBERGLASS PATCH WITH ADHESIVE | status: closed | recorded 2025-03-08 @ 7565.9h | closed 2025-03-15 @ 7565.9h
Fault
2025-03-087,565.9 hrshigh
Number 1 IPS blower duct is cracked, four cracks repaired.
NO.1 IPS BLOWER DUCT IS CRACKED | resolved: REPAIRED 4 EA CRACKS WITH IMPREGNATED FIBERGLASS PATCHES W ITH ADHESIVE | status: closed | recorded 2025-03-08 @ 7565.9h | closed 2025-03-15 @ 7565.9h
Fault
2025-08-157,637.5 hrshigh
Number 1 engine IPS blower duct has 3 cracks requiring repair.
#1 ENG IPS BLOWER DUCT HAS 3 CRACKS, REQUIRES REPAIR. | resolved: REPAIRED #1 ENG IPS BLOWER DUCT WITH 9313. | status: closed | recorded 2025-08-15 @ 7637.5h | closed 2025-08-25 @ 7644.2h
Fault
2025-03-197,565.9 hrsmedium
Crack in fiberglass on number 1 air inlet repaired.
CRACK IN FIBERGLASS ON #1 AIR INLET | resolved: Repaired 1 ea crack with impregnated fiberglass patch with adhesive | status: closed | recorded 2025-03-19 @ 7565.9h | closed 2025-03-19 @ 7565.9h
Fault
2025-04-167,565.9 hrsmedium
Threads worn on main transmission drip pan nut plate requiring replacement.
THREADS WORN ON MAIN XSMN DRIP PAN NUT PLATE, REQUIRES REPLACE MENT | status: open | recorded 2025-04-16 @ 7565.9h
Fault
2025-03-227,565.9 hrsmedium
Number 2 drip pan drain line by strut requires replacement.
#2 DRIP PAN DRAIN LINE BY STRUT REQ REPLACEMENT | resolved: REPLACED | status: closed | recorded 2025-03-22 @ 7565.9h | closed 2025-03-22 @ 7565.9h
OIL COOLER PNEUMATIC TUBE CRACKED REQS REPLACEMENT | resolved: REINSTALLED NO CRACK FOUND | status: closed | recorded 2025-06-04 @ 7591.8h | closed 2025-06-09 @ 7591.8h
Fault
2025-06-097,591.8 hrsmedium
Number 2 upper door track has crack, stop drilled and repaired.
#2 upper door track has crack | resolved: STOP DRILLED CRACK WAS PERFORMED IAW TM 1-1500-204-23-10. | status: closed | recorded 2025-06-09 @ 7591.8h | closed 2025-06-10 @ 7591.8h
Aircraft has one open critical safety message: H-60-26-SOF-02 regarding non-conforming primary main rotor servos not complied with. Multiple historical compliance entries exist for prior messages including H-60-25-ASAM-04 (main rotor blade), H-60-25-ASAM-03 (tail rotor), H-60-25-ASAM-06 (ADS-B), H-60-25-ASAM-07 (servo), H-60-25-ASAM-08 (main rotor), H-60-25-ASAM-10 (pilot seat), and H-60-25-ASAM-11 (main landing gear axle).
Fault
2026-01-077,675.1 hrshigh
H-60-26-SOF-02 non-conforming primary main rotor servos not complied with, open safety message.
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 2026-01-07 @ 7675.1h | closed 2026-01-07 @ 7675.1h
Fault
2025-03-247,565.9 hrsmedium
H-60-ASAM-05 T700 series accessory module compliance required.
COMPLY WITH H-60-ASAM-05, T700 SERIES ACCESORY MODULE REPLACEM ENT, BEFORE [1338.8] AIRCRAFT HOURS, BUT NOT LATER THAN 07 APR 25 | resolved: COMPLIED WITH H-60-25-ASAM-05 | status: closed | recorded 2025-03-24 @ 7565.9h | closed 2025-03-24…
Fault
2025-03-107,565.9 hrsmedium
H-60-25-ASAM-04 main rotor blade compliance required.
Comply with H-60-25-ASAM-04, Main Rotor Blade PN 70150-09100-0 43 Inspection | resolved: Complied with "H-60-25-ASAM-04 Main Rotor Blade PN 70150-0 9100-043 Inspection. | status: closed | recorded 2025-03-10 @ 7565.9h | closed 2025-03-10 @…
Fault
2025-03-10814.9 hrsmedium
H-60-25-ASAM-04 main rotor blade compliance message.
SAFETY MESSAGE NUMBER: H-60-25-ASAM-04 DESCRIPTION: MAIN ROTOR BLADE PN 70150-09100-043 INSPECTION FOR MAIN ROTOR BLADE ASSY CAGE: 78286 PN: 70150-09100-043 NSN: 1615011061903 SN: A00717 045 IS DUE: 17 MAR 2025 CALENDAR | resolved: Comply…
Fault
2025-03-104,818.3 hrsmedium
H-60-25-ASAM-04 main rotor blade compliance message.
SAFETY MESSAGE NUMBER: H-60-25-ASAM-04 DESCRIPTION: MAIN ROTOR BLADE PN 70150-09100-043 INSPECTION FOR MAIN ROTOR BLADE ASSY CAGE: 78286 PN: 70150-09100-043 NSN: 1615011061903 SN: A00703 246 IS DUE: 17 MAR 2025 CALENDAR | resolved: Comply…
Fault
2025-03-061,571.4 hrsmedium
H-60-25-ASAM-03 tail rotor compliance message.
SAFETY MESSAGE NUMBER: H-60-25-ASAM-03 DESCRIPTION: TAIL ROTOR BLADE SPAR INSPECTION INTERVAL CHANGE FOR TAIL ROTOR BLADE AS SY CAGE: 78286 PN: 70101-31000-043 NSN: 1615011138188 SN: A009 -09593 WAS DUE: 17 DEC 2024 CALENDAR | resolved:…
Fault
2025-03-062,336.4 hrsmedium
H-60-25-ASAM-03 tail rotor compliance message.
SAFETY MESSAGE NUMBER: H-60-25-ASAM-03 DESCRIPTION: TAIL ROTOR BLADE SPAR INSPECTION INTERVAL CHANGE FOR TAIL ROTOR BLADE AS SY CAGE: 78286 PN: 70101-31000-043 NSN: 1615011138188 SN: A009 06692 WAS DUE: 17 DEC 2024 CALENDAR | resolved:…
Fault
2025-04-071,571.4 hrsmedium
H-60-25-ASAM-03 tail rotor compliance message.
SAFETY MESSAGE NUMBER: H-60-25-ASAM-03 DESCRIPTION: (UPDATE) T AIL ROTOR BLADE SPAR INSPECTION INTERVAL CHANGE FOR TAIL ROTOR BLADE ASSY CAGE: 78286 PN: 70101-31000-043 NSN: 1615011138188 SN: A009-09593 WAS DUE: 30 DEC 2024 CALENDAR |…
Fault
2025-04-072,336.4 hrsmedium
H-60-25-ASAM-03 tail rotor compliance message.
SAFETY MESSAGE NUMBER: H-60-25-ASAM-03 DESCRIPTION: (UPDATE) T AIL ROTOR BLADE SPAR INSPECTION INTERVAL CHANGE FOR TAIL ROTOR BLADE ASSY CAGE: 78286 PN: 70101-31000-043 NSN: 1615011138188 SN: A00906692 WAS DUE: 30 DEC 2024 CALENDAR |…
Fault
2025-03-106,653.9 hrsmedium
H-60-25-ASAM-04 main rotor blade compliance message.
SAFETY MESSAGE NUMBER: H-60-25-ASAM-04 DESCRIPTION: MAIN ROTOR BLADE PN 70150-09100-043 INSPECTION FOR MAIN ROTOR BLADE ASSY CAGE: 78286 PN: 70150-09100-043 NSN: 1615011061903 SN: A007-0 7662 IS DUE: 17 MAR 2025 CALENDAR | resolved: Comply…
Fault
2025-03-102,154.0 hrsmedium
H-60-25-ASAM-04 main rotor blade compliance message.
SAFETY MESSAGE NUMBER: H-60-25-ASAM-04 DESCRIPTION: MAIN ROTOR BLADE PN 70150-09100-043 INSPECTION FOR MAIN ROTOR BLADE ASSY CAGE: 78286 PN: 70150-09100-043 NSN: 1615011061903 SN: A00715 388 IS DUE: 17 MAR 2025 CALENDAR | resolved: Comply…
COMPLY WITH H-60-25-ASAM-07, RELIABILITY ENHANCED STABILATOR A CTUATOR INSPECTION, PRIOR TO NEXT FLIGHT, BUT NOT TO EXCEED 01 MAY 25 | resolved: INSP OK | status: closed | recorded 2025-04-28 @ 7566.3h | closed 2025-04-28 @ 7566.3h
Fault
2025-05-027,574.8 hrsmedium
H-60-25-ASAM-08 main rotor blade compliance message.
SAFETY MESSAGE NUMBER: H-60-25-ASAM-08 DESCRIPTION: MAIN GENER ATOR LUG TERMINAL INSPECTION. IS DUE: 12 MAY 2025 CALENDAR | resolved: AIRCRAFT RECORDS INSPECTED MWO 1-1520-280-50-26 AND MWO 1- 1520-237-50-121 HAVE NOT BEEN APPLIED …
Fault
2025-07-117,609.7 hrsmedium
H-60-25-ASAM-10 pilot seat compliance message.
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-ASAM-19 PILOT AND COPILOT SEAT HARNESS ASSEMBLY REPLACEMENT | status:…
Fault
2025-08-157,637.5 hrsmedium
H-60-25-ASAM-11 main landing gear axle radial bearing compliance.
Comply with H-60-25-ASAM-11, Main Landing Gear Axle Radial Mov ement Inspection, at [8046.3] 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…
Fault
2025-05-197,582.3 hrshigh
H-60-22-ASAM-02 verification required for aircraft admin grounded until compliance.
ACFT ADMIN GROUNDED UNTIL VERIFICATION OF H-60-22-ASAM-02 AND H-60-22-ASAM-03 IS COMPLETE | resolved: COMPLIED WITH H-60-22-ASAM-02 AND H-60-22-ASAM-03 SPLIT HO RN TAIL ROTOR BLADE S/N VERIFICATION | status: closed | recorded 2025-05-19 @…
Aircraft inducted into BEST Program on 06-APR-2026 with no flight operations authorized. Multiple high-time components nearing replacement intervals including pilot and copilot seat harness assemblies worn excessively, number 1 engine combustion drain line worn beyond limits, and various battery replacements due. Engine records show one engine removed for internal leak and another for low ETFs requiring QCA. Historical records indicate 7678.0 aircraft hours at BEST induction.
Fault
2026-04-237,678.0 hrshigh
Aircraft inducted into BEST Program on 06-APR-2026, no flight operations authorized, end of service life phase.
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 @ 7678h
Fault
2025-03-087,565.9 hrshigh
Number 1 pilot shoulder seat harness webbing worn excessively, requires replacement.
#1 PILOT SHOULDER SEAT HARNESS WEBBING IS WORN EXCESSIVELY | resolved: INSPECTED FOUND TO BE WITHIN LIMITS | status: closed | recorded 2025-03-08 @ 7565.9h | closed 2025-04-14 @ 7565.9h
Fault
2025-03-087,565.9 hrshigh
Number 2 pilot shoulder seat harness webbing worn excessively, requires replacement.
#2 PILOT SHOULDER SEAT HARNESS WEBBING IS WORN EXCESSIVELY | resolved: INSPECTED IN ACCORDANCE WITH 1500-204-23. FOUND TO BE WITH ING LIMITS | status: closed | recorded 2025-03-08 @ 7565.9h | closed 2025-04-11 @ 7565.9h
Fault
2025-04-157,565.9 hrshigh
Number 2 pilot shoulder seat harness webbing worn beyond limits, requires replacement.
#2 PILOT SHOULDER SEAT HARNESS WEBBING IS WORN BEYOND LIMITS | resolved: REPLACED | status: closed | recorded 2025-04-15 @ 7565.9h | closed 2025-04-16 @ 7565.9h
Fault
2025-08-277,644.2 hrshigh
Number 1 engine combustion drain line worn beyond limits, requires replacement.
#1 ENGINE COMBUSTION DRAIN LINE WORN BEYOND LIMITS. REQUIRES R EPLACEMENT. | resolved: REPLACED | status: closed | recorded 2025-08-27 @ 7644.2h | closed 2025-09-04 @ 7644.2h
Fault
2025-08-277,644.2 hrshigh
Number 1 side engine combustion drain hose melted down to metal braid, requires replacement.
#1 SIDE ENGINE COMBUSTION DRAIN HOSE IS MELTED DOWN TO FABRIC LINER. REQUIRES FURTHER INSPECTION. | resolved: INSPECTION COMPLETED. REFERENCE FURTHER 13-1 ANNOTATED 8 A UG 2027 | status: closed | recorded 2025-08-27 @ 7644.2h | closed…
Fault
2025-08-257,644.2 hrsmedium
Number 1 and 2 engine LDS cables have tears measuring less than one inch, nearing replacement criteria.
#1 & #2 ENGINE LDS CABLES HAVE TEARS MEASURING LESS THEN 1IN. RTV REPAIR APPLIED AT 14:00 REQ'D 24 HOUR CURE TIME | resolved: CURING COMPLETE | status: closed | recorded 2025-08-25 @ 7644.2h | closed 2025-08-27 @ 7644.2h
Fault
2025-04-177,566.3 hrshigh
Number 2 engine requires removal due to internal leak, component at end of service interval.
#2 ENGINE REQ REMOVAL DUE TO INTERNAL LEAK | resolved: REINSTALLED SN-GE-E-762584 REFER TO 13-1 "INSP OF #2 ENG R EQ DUE TO OIL LEAK" DATED 22 APR 2025 ENG SN: GE-E-762584 | status: closed | recorded 2025-04-17 @ 7566.3h | closed…
Fault
2025-04-217,566.3 hrshigh
Engine number 1 removed due to low ETFs, QCA required, component nearing retirement.
REMOVAL OF ENG # 1 DUE TO LOW ETFs QCA REQ ENG S/N: GEE-761734 C | resolved: QCA COMPLETED NEW ENG S/N: GE-E614164 | status: closed | recorded 2025-04-21 @ 7566.3h | closed 2025-04-22 @ 7566.3h
Fault
2026-04-167,678.0 hrsmedium
Engine serial GEE614184 records indicate component time accumulation requiring attention.
In reference to Aircraft Engine S/N: GEE614184, the following components S/N:'s must be verified at next engine "tear down" Power Turbine Module Power Turbine Rotor Stage 3 Turbine D isk Stage 4 Turbine Disk Power Turbine Shaft No. 5…
Seller has flagged critical items for buyer: blanking plates required on areas where components were removed, aircraft prepared for lateral transfer to ASF Hood with multiple removed items, and notice to buyer regarding removed components including aft cabin soundproofing not installed, armor wing cable not installed, and cargo hook hardware removed. Aircraft folded for transport multiple times and configured for shipment.
Fault
2026-04-177,678.0 hrshigh
NOTICE TO BUYER: multiple items removed from aircraft including aft cabin soundproofing, armor wing cable, cargo hook hardware, and other components.
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
2026-01-137,678.0 hrshigh
Blanking plates required on areas where components were removed, indicating missing equipment.
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
2026-01-137,678.0 hrshigh
Aircraft prepared for lateral transfer to ASF Hood, see 13-2 entries for removed components.
ACFT PREPARED FOR LATERAL TRANSFER TO ASF HOOD. SEE 13-2'S FOR FOLLOWING COMPONENTS RMVD. | resolved: RMVD COMPONENTS | status: closed | recorded 2026-01-13 @ 7678h | closed 2026-01-14 @ 7678h
Fault
2025-06-067,591.8 hrshigh
Aft cabin soundproofing not installed, flagged as open item.
AFT CABIN SOUNDPROOFING NOT INSTALLED | status: open | recorded 2025-06-06 @ 7591.8h
Fault
2023-03-317,223.1 hrsmedium
Aft cabin soundproofing not installed, write up could not duplicate.
AFT CABIN SOUND PROOFING NOT INSTALLED | resolved: WRITE UP HAS BEEN ACTIONED. SEE WRITE UP DATED 06JUN25 FOR FURTHER INFORMATION. | status: closed | recorded 2023-03-31 @ 7223.1h | closed 2025-06-10 @ 7591.8h
Fault
2025-10-237,675.1 hrsmedium
Aircraft folded for transport, unfolded and closed, indicates shipment preparation.
ACFT FOLDED FOR TRANSPORT | resolved: ACFT UNFOLDED COMPLETED | status: closed | recorded 2025-10-23 @ 7675.1h | closed 2026-01-07 @ 7675.1h
Fault
2025-10-227,675.1 hrsEntry errorlow
Aircraft folded for transport entry error, closed in error.
[ENTRY ERROR] ACFT FOLDED FOR TRANSPORT | resolved: CLOSED IN ERROR BY Acevedo Gonzalez, Jonathan SSG Entry m ade in error. | status: closed | recorded 2025-10-22 @ 7675.1h | closed 2025-10-23
Fault
2025-10-227,675.1 hrsEntry errorlow
Aircraft folded for transport entry error, closed in error.
[ENTRY ERROR] ACFT FOLDED FOR TRANSPORT | resolved: CLOSED IN ERROR BY Acevedo Gonzalez, Jonathan SSG Entry m ade in error. | status: closed | recorded 2025-10-22 @ 7675.1h | closed 2025-10-23
Fault
2025-10-237,675.1 hrsEntry errorlow
Folding of main rotor blades required entry error.
[ENTRY ERROR] D.Co FOLDING OF MAIN ROTOR BLADES REQUIRED | resolved: CLOSED IN ERROR BY Acevedo Gonzalez, Jonathan SSG Entry m ade in error. | status: closed | recorded 2025-10-23 @ 7675.1h | closed 2025-10-23
Fault
2025-10-237,675.1 hrsEntry errormedium
Main rotor blades folded for shipment, reinstalled.
[ENTRY ERROR] M/R BLADES FOLDED FOR SHIPMENT | resolved: ENTERRED IN ERROR | status: closed | recorded 2025-10-23 @ 7675.1h | closed 2025-10-23 @ 7675.1h
Multiple administrative issues exist including entry errors for inspections, admin grounds for record discrepancies regarding PMD requirements and flight hour documentation, and data quality issues with entries closed in error. Several entries marked as entry error for inspections and maintenance actions that were incorrectly documented.
Fault
2025-09-097,644.7 hrshigh
Admin ground due to record discrepancies for PMD dated 13-1, requires correction.
ADMIN GROUND DUE TO RECORD DISCREPANCIES: 2408-13-1 "PMD REQ B EFORE NEXT FLIGHT" DATED 07 SEP 25 HAS NO TOOL BOX NUMBER ON 2 408-13-2 "TOOLBOX INV DUE" | resolved: CORRECTIVE COMPLETED | status: closed | recorded 2025-09-09 @ 7644.7h |…
Fault
2025-09-097,644.7 hrshigh
Admin ground due to record discrepancies for A110 PMS 40 hour inspection dated 13-1.
ADMIN GROUND DUE TO RECORD DISCREPANCIES: 2408-13-1 "A110 40 H OUR INSPECTION (PMS)" HAS NO TQ VALUE, VOID DATE OR SERIAL NUM BER ON 2408-13-2 ON FUEL ENCLOSURE PANEL. | resolved: CORRECTION COMPLETED | status: closed | recorded 2025-09-09…
Fault
2025-08-127,637.5 hrshigh
Admin ground for record discrepancy, no PMD required prior to flight on 11 AUG 25.
ADMIN GROUND FOR RECORD DISCREPANCY: NO "PMD REQD" PRIOR TO FL IGHT DATED 16 JULY 25 | resolved: COMPLETED | status: closed | recorded 2025-08-12 @ 7637.5h | closed 2025-08-12 @ 7637.5h
Fault
2025-08-127,637.5 hrshigh
Admin ground for record discrepancy, DA 2408-12 for flight dated 11 AUG 25 missing.
ADMIN GROUND FOR RECORD DISCREPANCY: DA 2408-12 FOR FLIGHT DAT ED 12 JUL 25 "MISSING" TRAINING TAB | resolved: COMPLETED | status: closed | recorded 2025-08-12 @ 7637.5h | closed 2025-08-12 @ 7637.5h
Fault
2025-08-127,637.5 hrshigh
Aircraft admin grounded due to potential FOD, 100% inspection required.
ACFT ADMIN GROUNDED DUE TO POTENTIAL FOD. 100% INSP REQ'D | resolved: COMPLETED | status: closed | recorded 2025-08-12 @ 7637.5h | closed 2025-08-14 @ 7637.5h
Fault
2025-03-037,565.9 hrsEntry errormedium
Entry error, left internal CE ICS does not transmit or receive, data quality issue.
[ENTRY ERROR] L/H INSTERNAL CE ICS DOES NOT TRANSMIT OR RECEIVE | resolved: ENTERED IN ERROR (DUPLICATE) REFER TO 2408-13-1 LABELED "L /H CE ICS BOX WILL NOT TRANSMIT/RECIEVE " DATED 08 MAR 202 5 | status: closed | recorded 2025-03-03 @…
Fault
2025-10-237,675.1 hrsEntry errormedium
Entry error for inspection A803 10HR/14 day visual inspection of SATCOM.
[ENTRY ERROR] INSP A803 10HR/14 DAY VISUAL INSPECTION OF SATCOM IAW AWR 1037 FOR HELICPTR UTIL UH-60L CAGE: 78286 PN: UH-60L NSN: 15200129 84532 SN: 8926180 WAS DUE. STATUS UPGRADED TO X ON: 7567.0 AIR CRAFT HOURS OR 18 NOV 2024 …
Fault
2025-10-237,675.1 hrsEntry errormedium
Entry error for inspection A822 upload of IVHUMS software.
[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: 8926180 WAS DUE. STATUS UP GRADED TO X ON: 7624.4 AIRCRAFT HOURS…
Fault
2025-10-227,675.1 hrsEntry errormedium
Entry error for inspection A803 10HR/14 day visual inspection of SATCOM.
[ENTRY ERROR] INSP A803 10HR/14 DAY VISUAL INSPECTION OF SATCOM IAW AWR 1037 FOR HELICPTR UTIL UH-60L CAGE: 78286 PN: UH-60L NSN: 15200129 84532 SN: 8926180 WAS DUE. STATUS UPGRADED TO X ON: 18 NOV 202 4 OR 7567.0 AIRCRAFT HOURS …
Fault
2025-10-237,675.1 hrsEntry errormedium
Entry error for inspection A822 upload of IVHUMS software.
[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: 8926180 WAS DUE. STATUS UP GRADED TO X ON: 7624.4 AIRCRAFT HOURS…
Fault
2025-10-227,675.1 hrsEntry errormedium
Entry error for inspection A822 upload of IVHUMS software.
[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: 8926180 WAS DUE. STATUS UP GRADED TO X ON: 7624.4 AIRCRAFT HOURS…
Fault
2025-10-237,675.1 hrsEntry errormedium
Entry error for inspection A822 upload of IVHUMS software.
[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: 8926180 WAS DUE. STATUS UP GRADED TO X ON: 7624.4 AIRCRAFT HOURS…
Fault
2025-10-237,675.1 hrsEntry errormedium
Entry error for inspection A822 upload of IVHUMS software.
[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: 8926180 WAS DUE. STATUS UP GRADED TO X ON: 7624.4 AIRCRAFT HOURS…
Fault
2025-10-237,675.1 hrsEntry errormedium
Entry error for inspection A822 upload of IVHUMS software.
[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: 8926180 WAS DUE. STATUS UP GRADED TO X ON: 7624.4 AIRCRAFT HOURS…
Fault
2025-10-237,675.1 hrsEntry errormedium
Entry error for inspection A822 upload of IVHUMS software.
[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: 8926180 WAS DUE. STATUS UP GRADED TO X ON: 7624.4 AIRCRAFT HOURS…
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