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Aircraft record

N811HC1991 Atr-Gie Avions De Transport ATR-72-201

DeregisteredUnclaimedSource: FAA, updated Oct 18, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Oct 16, 2023.

Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply130 service difficulty reports

Registration
Deregistered
Last based in
Honolulu, HI
owner city / state
Engine
PW124B · 2160 hp
P&W Canada
Owners
1
since 2015
NTSB events
None
since 1982
ADs may apply
4
confirm with A&P
Service reports
130
since 1995

Registration

FAA Aircraft Registry · Oct 18, 2026
Last registered owner
Airline Contract Maintenance & Equipment INC
Owner type
Corporation
City, state
Honolulu, HI
Certificate issued
Sep 8, 2015
Canceled
Oct 16, 2023
Airworthiness
Standard · Transport
Airworthiness date
Feb 24, 2017

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
Atr-Gie Avions De Transport
Model
ATR-72-201
Year
1991
Serial number
227
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
AB0DC5

Engine

Make and model
P&W Canada Pw124b
Type
Turbo-prop
Power
2160 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 – 2023Airline Contract Maintenance & Equipment INCHonolulu, HI

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 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 (PW124B)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 (PW124B)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 (PW124B)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 (PW124B)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 (130)

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.

  • Air conditioning and pressurization · acm · failedSep 9, 2020

    FLIGHT 1704, ENROUTE HNL-OGG/AIR TURNBACK DISCREPANCY. NO PRESSURIZATION ON CLIMB OUT, DUCT TEMP OVER 50 DEGREES C. AIRCRAFT WAS RETURNED TO HNL, NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED. MAINTENANCE REPLACED THE AIR CYCLE UNIT AND TIC VALVE. PRESSURIZATION TEST AND OPS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · failsafe · crackedDec 27, 2019

    WO 209669 NR 100044 HEAVY CHECK COE/MAJOR REPAIR: FRAME 30 FAIL SAFE CRACKED AROUND STRINGER 15L. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-817-A01.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedDec 9, 2019

    DURING HEAVY CHECK, TAIL FUSELAGE LT CROWN PANEL INTERIOR SURFACE WAS CORRODED, FRAMES 43-44, STRINGERS 1L-2L. REPAIRED IAW SRM 530000-300-862-A01.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · skin · corrodedDec 9, 2019

    WO 209669 NR 200154 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 41-42 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 8R-9R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112414_01...15827 ISSUE A, DATED 2/10/2020.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin panel · corrodedDec 9, 2019

    WO 209669 NR 200182 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE R/H LOWER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION FRAMES 34-35 BETWEEN STRINGERS 11R-12R. CORRECTIVE ACTION: REPAIR PER SRM 530000-300-801-A01.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedDec 9, 2019

    HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 31-32 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 4L-5L. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-803-A01.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedDec 9, 2019

    HEAVY CHECK: TAIL FUSELAGE LT PANEL INTERIOR SURFACE WAS CORRODED FRAMES 43-44 BETWEEN STRINGERS 9L-10L. REPAIRED PER SRM 530000-300-803-A01.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedDec 9, 2019

    WO 209669 NR 200180 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 34-35 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 5L-6L. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-803-A01.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedDec 9, 2019

    WO 209669 NR 200245 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 24-25 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 5R-6R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112397_01...15822 ISSUE A, DATED 2/10/2020.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedDec 9, 2019

    WO 209669 NR 200165 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 40-41 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 11R-12R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112417_01...15813 ISSUE A, DATED 2/5/2020.

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

Showing the 10 most recent of 130 reports.

Related aircraft

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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