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Aircraft record

N810HC1994 Aerospatiale/Alenia ATR-72-212

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled May 6, 2022.

Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply86 service difficulty reports

Registration
Deregistered
Last based in
Honolulu, HI
owner city / state
Engine
PW127 · 2475 hp
P&W Canada
Owners
1
since 2015
NTSB events
None
since 1982
ADs may apply
4
confirm with A&P
Service reports
86
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Airline Contract Maintenance And Equipment INC
Owner type
Corporation
City, state
Honolulu, HI
Certificate issued
Aug 27, 2015
Canceled
May 6, 2022
Airworthiness
Standard · Transport
Airworthiness date
Feb 16, 2018

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Aerospatiale/Alenia
Model
ATR-72-212
Year
1994
Serial number
423
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
76
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
AB0A0E

Engine

Make and model
P&W Canada Pw127
Type
Turbo-prop
Power
2475 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2015 – 2022Airline Contract Maintenance And Equipment INCHonolulu, HI

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

ADs published since 1998 that may apply (4)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2014-14-02Pratt & Whitney Canada Corp. Turboprop EnginesAug 15, 2014Engine (PW127)Only with: PW120, PW121, PW121A engines with Post SB21610 configuration; PW124B, PW127, PW127E, PW127F engines with Post SB21607 and/or Post SB21705 configuration; PW127G and PW127M engines unconditionally.
2013-15-08Pratt & Whitney Canada Corp. Turboprop EnginesSep 17, 2013Engine (PW127)Serial numbers per Table 1 of the Appendix of P&WC Service Bulletin No. PW100-72-21823, Revision 3. Only with: First-stage power turbine blade P/N 3120973-01, 3120983-01, or 3054053-01 installed with a serial number listed in the referenced SB table.
2012-26-08Pratt & Whitney Canada Corp. Turboprop EnginesFeb 15, 2013Engine (PW127)Serial numbers per P&WC ASB No. PW100-72-A21813 Rev 3, PW100-72-A21802 Rev 4, and PW100-72-A21798 Rev 5. Only with: Engines with propeller shafts having serial numbers listed in the referenced P&WC ASBs.
2004-20-01Pratt & Whitney Canada Models PW123, PW123B, PW123C, PW123D, PW123E, PW123AF, PW124B…Nov 5, 2004Engine (PW127)Only with: Mechanical fuel controls (MFCs) P/Ns 3244841-21, 3244853-17, 3244855-15, 3244857-14, 3244858-23, 3244871-5, 3244873-4, and 3244874-4 installed.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (86)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Hydraulic power · pump · failedJan 15, 2020

    FLIGHT 301,AIR TURNBACK. BLUE SIDE LOW LEVEL WARNING LIGHT AND CCAS BLUE HYDRAULIC CAUTION IN FLIGHT. AIRCRAFT WAS RETURNED TO HNL. EMERGENCY WAS DECLARED. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE BLUE HYDRAULIC PUMP, HYDRAULIC HOSE AND GREEN HYDRAULIC SYSTEM PRESSURE FILTER. OPS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedOct 22, 2019

    WO 205731 NR 200141 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER L/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 40-41, ABOVE STRINGER 7L. CORRECTIVE ACTION: DOUBLER REPAIRED PER SRM 530000-300-803-A01.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead · corrodedOct 8, 2019

    WO 205731 NR 200135 HEAVY CHECK COE/MAJOR REPAIR: FORWARD PRESSURE BULKHEAD UPPER L/H INBOARD CORNER BOND AREA HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107423_01...15385 ISSUE A, DATED 11/20/2019.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · skin · corrodedOct 6, 2019

    WO 205731 NR 200085 HEAVY CHECK COE/MAJOR REPAIR: FWD FUSELAGE UPPER R/H INTERIOR SURFACE HAS LEVEL 2 CORROSION FWD OF FRAME 17 BETWEEN STRINGERS 9R-10R. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-803-A01.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedOct 6, 2019

    WO 205731 NR 200109 REAR FUSELAGE LOWER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 32-33 STRINGERS 12R-13R. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-805-A01.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · shear tie · corrodedOct 6, 2019

    WO 205731 NR 200071 HEAVY CHECK COE/MAJOR REPAIR: FRAME 41 SHEAR TIE STRINGER 4L-5L HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED BY FABRICATION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedOct 6, 2019

    WO 205731 NR 200080 HEAVY CHECK COE/MAJOR REPAIR: FORWARD FUSELAGE R/H UPPER SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 13-14, STRINGERS 5R-6R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107816_01...15468 ISSUE A, DATED 11/15/2019.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedOct 6, 2019

    WO 205731 NR 200130 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28-28A STRINGERS 7R-8R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedOct 6, 2019

    WO 205731 NR 200125 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28C-28D BETWEEN STRINGERS 8R-10R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedOct 6, 2019

    WO 205731 NR 200127 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28A-28B BETWEEN STRINGERS 10R-11R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 86 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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