# N811HC: 1991 Atr-Gie Avions De Transport ATR-72-201, registration cancelled 2023-10-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 16, 2023
- Exported to: Hungary
- Status when cancelled: Valid registration
- Airframe: [Atr-Gie Avions De Transport ATR-72-201](https://openairdocs.org/model/atr-gie-avions-de-transport-atr-72-201) (registry code 8681903)
- Engine: [Pratt & Whitney Canada PW124B](https://openairdocs.org/engine/pratt-whitney-canada-pw124b) (registry code 52217)
- Data sheets: [TCDS A53EU](https://openairdocs.org/tcds/A53EU), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 227
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: February 24, 2017
- Certificate issued: September 8, 2015
- Last registry action: June 10, 2023
- Mode S code: AB0DC5
- Owner when cancelled: [Airline Contract Maintenance & Equipment Inc](https://openairdocs.org/faa-owner/AIRLINE%20CONTRACT%20MAINTENANCE%20%26%20EQUIPMENT%20INC)
- Location: [Honolulu, HI](https://openairdocs.org/faa-place/HI/Honolulu)
- Owner type: Corporation
- Owner's area on the map: 21.3477° N, 157.8767° W: Placed by OpenAirDocs at the center of ZIP code 96819, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N811HC
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=811HC
- Page: https://openairdocs.org/deregistered/N811HC-2023-10-16

From the FAA registry file of November 3, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Atr-Gie Avions De Transport ATR-72-201: https://openairdocs.org/model/atr-gie-avions-de-transport-atr-72-201.md

## Service difficulty reports (133, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR COEA2020091002811](https://openairdocs.org/sdr/COEA2020091002811), Sep 9, 2020: ACM. FAILED. 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 D
- [SDR COEA2020020674811](https://openairdocs.org/sdr/COEA2020020674811), Dec 27, 2019: FAILSAFE. CRACKED. 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.
- [SDR COEA2020021941811](https://openairdocs.org/sdr/COEA2020021941811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200161 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 40-41 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 8L-9L. CORRECTIVE ACTION: REP
- [SDR COEA2020021940811](https://openairdocs.org/sdr/COEA2020021940811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200174 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 39-40 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 5R-6R. CORRECTIVE ACTION: REP
- [SDR COEA2020021939811](https://openairdocs.org/sdr/COEA2020021939811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200184 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 33-34 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 4L-5L. CORRECTIVE ACTION: REP
- [SDR COEA202021937811](https://openairdocs.org/sdr/COEA202021937811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200316 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE L/H UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION FRAMES 23-23A BETWEEN STRINGERS 6A
- [SDR COEA2020021496811](https://openairdocs.org/sdr/COEA2020021496811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200207 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 29-30 HAS LEVEL 2 CORROSION STRINGERS 5R-6R. CORRECTIVE ACTION: REPAIRED PE
- [SDR COEA2020021495811](https://openairdocs.org/sdr/COEA2020021495811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200199 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 30-31 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 10L-11L. CORRECTIVE ACTION: R
- [SDR COEA2020021494811](https://openairdocs.org/sdr/COEA2020021494811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200198 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 30-31 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 8L-10L. CORRECTIVE ACTION: RE
- [SDR COEA2020021493811](https://openairdocs.org/sdr/COEA2020021493811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200196 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 31-32 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 8L-10L. CORRECTIVE ACTION: RE
- [SDR COEA2020021492811](https://openairdocs.org/sdr/COEA2020021492811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200321 HEAVY CHECK COE/MAJOR REPAIR: FORWARD FUSELAGE R/H UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION FWD OF FRAME 23 BETWEEN STRINGERS
- [SDR COEA202002131811](https://openairdocs.org/sdr/COEA202002131811), Dec 9, 2019: SKIN. CORRODED. 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: REP
- [SDR COEA2020021390011](https://openairdocs.org/sdr/COEA2020021390011), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200244 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 24-25 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 6R-7R. CORRECTIVE ACTION: REP
- [SDR COEA202002139811](https://openairdocs.org/sdr/COEA202002139811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200200 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 30-31 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 5R-6R. CORRECTIVE ACTION: REP
- [SDR COEA2020021398811](https://openairdocs.org/sdr/COEA2020021398811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200188 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 33-34 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 7R-8R. CORRECTIVE ACTION: REP
- [SDR COEA2020021397811](https://openairdocs.org/sdr/COEA2020021397811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200183 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 34-35 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 5R-6R. CORRECTIVE ACTION: REP
- [SDR COEA2020021326811](https://openairdocs.org/sdr/COEA2020021326811), Dec 9, 2019: SKIN. CORRODED. 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: R
- [SDR COEA2019120925811](https://openairdocs.org/sdr/COEA2019120925811), Dec 9, 2019: SKIN. CORRODED. 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: REP
- [SDR COEA2020021394811](https://openairdocs.org/sdr/COEA2020021394811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200283 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 23B-23C CORRODED BETWEEN STRINGERS 5AR-6R. CORRECTIVE ACTION: REPAIRED PER 
- [SDR COEA2020021393811](https://openairdocs.org/sdr/COEA2020021393811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200310 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN AFT OF FRAME 23 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 6AR-7R. CORRECTIVE ACTION: REPAIRE
- [SDR COEA2020021392811](https://openairdocs.org/sdr/COEA2020021392811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200304 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 23A-23B HAS LEVEL 2 CORROSION BETWEEN STRINGERS 12R-13R. CORRECTIVE ACTION:
- [SDR COEA2020021391811](https://openairdocs.org/sdr/COEA2020021391811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200242 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 24-25 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 13-14R. CORRECTIVE ACTION: RE
- [SDR COEA2020021390811](https://openairdocs.org/sdr/COEA2020021390811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200205 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 29-30 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 12R-13R. CORRECTIVE ACTION: R
- [SDR COEA2020021399811](https://openairdocs.org/sdr/COEA2020021399811), Dec 9, 2019: SKIN. CORRODED. WO 209669 NR 200145 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 42-43 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 2R-3R. CORRECTIVE ACTION: REP
- [SDR COEA2020020695811](https://openairdocs.org/sdr/COEA2020020695811), Dec 9, 2019: SKIN. CORRODED. 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: REP
- [SDR COEA2020012410811](https://openairdocs.org/sdr/COEA2020012410811), Dec 9, 2019: SKIN. CORRODED. HEAVY CHECK: TAIL FUSELAGE LT PANEL INTERIOR SURFACE WAS CORRODED FRAMES 43-44 BETWEEN STRINGERS 9L-10L. REPAIRED PER SRM 530000-300-803-A01.
- [SDR COEA2000012198811](https://openairdocs.org/sdr/COEA2000012198811), Dec 9, 2019: SKIN. CORRODED. 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.
- [SDR COEA2020011607811](https://openairdocs.org/sdr/COEA2020011607811), Dec 9, 2019: SKIN. CORRODED. 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
- [SDR COEA2020011003811](https://openairdocs.org/sdr/COEA2020011003811), Dec 9, 2019: SKIN PANEL. CORRODED. 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-1
- [SDR COEA2020020788811](https://openairdocs.org/sdr/COEA2020020788811), Dec 8, 2019: INTERCOSTAL. CRACKED. WO 209669 NR 800012 HEAVY CHECK COE/MINOR REPAIR: PASSENGER DOOR INTERCOSTAL FWD OF PRESSURE RELIEF DOOR IS CRACKED. CORRECTIVE ACTION: REPLACED INTERCOSTAL WIT
- [SDR COEA2020020677811](https://openairdocs.org/sdr/COEA2020020677811), Dec 7, 2019: FAILSAFE. CORRODED. WO 209669 NR 100021 HEAVY CHECK COE/MAJOR REPAIR: FRAME 23A FAIL SAFE HAS LEVEL 2 CORROSION ABOVE STRINGER 21L. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-8
- [SDR COEA2020020673811](https://openairdocs.org/sdr/COEA2020020673811), Dec 7, 2019: WEB. CORRODED. WO 209669 NR 100030 HEAVY CHECK COE/MINOR REPAIR: CARGO DOOR SILL HORIZONTAL WEB HAS LEVEL 2 CORROSION BETWEEN FRAMES 14-20. CORRECTIVE ACTION: REPLACED WEB WIT
- [SDR COEA202001249811](https://openairdocs.org/sdr/COEA202001249811), Dec 7, 2019: FRAME. CORRODED. HEAVY CHECK. FRAME 17 FORWARD SIDE HAS CORROSION BETWEEN STRINGERS 17L-20L. REPLACED THE FRAME SEGMENT.
- [SDR COEA2020011605811](https://openairdocs.org/sdr/COEA2020011605811), Dec 7, 2019: DOUBLER. CORRODED. HEAVY CHECK COE/MINOR REPAIR: CARGO DOOR THRESHOLD VERTICAL PLATE REPAIRED DOUBLER HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED DOUBLER.
- [SDR COEA2020011604811](https://openairdocs.org/sdr/COEA2020011604811), Dec 7, 2019: CREASE BEAM. CORRODED. HEAVY CHECK COE/MAJOR REPAIR: RT CREASE BEAM WEB BETWEEN FRAMES 22-23 UPPER SURFACE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH FABRICATION.
- [SDR COEA2020020612811](https://openairdocs.org/sdr/COEA2020020612811), Dec 6, 2019: FLOORBEAM. CORRODED. WO 209669 NR 100019 HEAVY CHECK COE/MINOR REPAIR: FLOORBEAM 36 UPPER SURFACE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED RH OB SECTION PER SRM 530000-300
- [SDR COEA2020020611811](https://openairdocs.org/sdr/COEA2020020611811), Dec 6, 2019: FLOORBEAM. CORRODED. WO 209669 NR 100016 HEAVY CHECK COE/MINOR REPAIR: FLOORBEAM 30 UPPER SURFACE HAS MULTIPLE AREAS OF LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART.
- [SDR COEA2020020656811](https://openairdocs.org/sdr/COEA2020020656811), Dec 5, 2019: SKIN. CRACKED. WO 209669 NR 800010 HEAVY CHECK COE/MAJOR REPAIR: PASSENGER DOOR INNER SKIN CRACKED JUST FORWARD OF PRESSURE RELIEF FOOR, COMMON TO THE STAIR NUT PLATE. CORRECT
- [SDR COEA2020011606811](https://openairdocs.org/sdr/COEA2020011606811), Dec 3, 2019: COWLING. LOOSE. HEAVY CHECK COE/MAJOR REPAIR: RT ENGINE CENTER HINGE COWL IS LOOSE AT FORWARD AND AFT ATTACH POINTS. CORRECTIVE ACTION: REPAIRED PER SRM 541162-300-801-A01.
- [SDR COEA2019090602811](https://openairdocs.org/sdr/COEA2019090602811), Sep 6, 2019: SKIN PANEL. DENTED. WO 206741 NR 2 DISCREPANCY: LT FUSELAGE SIDE DENT ON SKIN PANEL, FWD OF MAIN CARGO DOOR AFT OF FRAME 12 & BELOW STRINGER 11. CORRECTIVE ACTION: REPAIR PER SRAS 
- [SDR COEA2019051601811](https://openairdocs.org/sdr/COEA2019051601811), May 16, 2019: STRUCTURE. DAMAGED. WO 201960/DISCREPANCY: FASTENER HOLE ELONGATED ON LT WING LOWER SIDE FOR ICE DETECTOR PROBE. CORRECTIVE ACTION: TEMPORARY REPAIR PER SRAS ES-0098805-01...14613,
- [SDR COEA2018040202811](https://openairdocs.org/sdr/COEA2018040202811), Apr 2, 2018: STRINGER. CORRODED. STRINGER 6R CORRODED. REPAIRED AND SPLICED BETWEEN FRAMES 16-17.
- [SDR COEA2018050127811](https://openairdocs.org/sdr/COEA2018050127811), Mar 25, 2018: TRUSS. CORRODED. THE LT R/S SHEAR TRUSS MEMBER HAD CORROSION. REPAIRED IAW SRM 535730-300-801-A01.
- [SDR COEA2018050126811](https://openairdocs.org/sdr/COEA2018050126811), Mar 23, 2018: FITTING. CORRODED. RIGHT MLG FORWARD TRUNNION STRUT LOWER FITTING ON FUSELAGE HAS CORROSION AROUND LINK ATTACH HOLE. REPAIRED SRM 53-57-30-300-801-A01.
- [SDR COEA2018032125811](https://openairdocs.org/sdr/COEA2018032125811), Mar 21, 2018: TRUSS. CORRODED. LEFT MLG TRUSS SHEAR MEMBER FORWARD SUPPORT TRUSS HAD CORROSION AROUND AFT SIDE OF FITTING ATTACH HOLE. REPAIRED IAW SRM 535730-300-801-A01.
- [SDR COEA2018042704811](https://openairdocs.org/sdr/COEA2018042704811), Mar 21, 2018: TRUSS. CORRODED. LEFT MLG TRUSS SHEAR MEMBER CORRODED AROUND FORWARD FITTING ATTACH HOLE. REPAIRED IAW SRM 53-57-30-300-801-A01.
- [SDR COEA2018042703811](https://openairdocs.org/sdr/COEA2018042703811), Mar 21, 2018: TRUSS. CORRODED. RIGHT MLG TRUSS SHEAR MEMBER CORRODED AROUND FORWARD FITTING ATTACH HOLE COMMON TO FORWARD SUPPORT TRUSS. REPAIRED IAW SRM 53-57-30-300-801-A01.
- [SDR COEA2018031722811](https://openairdocs.org/sdr/COEA2018031722811), Mar 17, 2018: FITTING. CORRODED. RIGHT WHEEL WELL AFT TRUNNION SUPPORT FUSELAGE FITTING CORRODED BY THE BORE. REPAIRED IAW SRM 53-57-30-300-801-A01.
- [SDR COEA2018031721811](https://openairdocs.org/sdr/COEA2018031721811), Mar 17, 2018: FITTING. CORRODED. LEFT WHEEL WELL, AFT TRUNNION SUPPORT HAS 2 CORROSION BY THE BORE. REPAIRED IAW SRM 53-57-30-300-801-A01.
- [SDR COEA201804260811](https://openairdocs.org/sdr/COEA201804260811), Mar 17, 2018: STRINGER. CORRODED. STRINGER 6R CORRODED BETWEEN FRAMES 16 - 17. REPAIRED THE STRINGER IAW SRM 53-00-00-300-824-A01.

All 133: https://openairdocs.org/deregistered/N811HC-2023-10-16/reports.md

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