# N807HC: 1994 Aerospatiale/Alenia ATR-72-212, registration cancelled 2022-05-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 6, 2022 - Exported to: Canada - Status when cancelled: Valid registration - Airframe: [Aerospatiale/Alenia ATR-72-212](https://openairdocs.org/model/aerospatiale-alenia-atr-72-212) (registry code 8680946) - Engine: [Pratt & Whitney Canada PW127](https://openairdocs.org/engine/pratt-whitney-canada-pw127) (registry code 52219) - Data sheets: [TCDS A53EU](https://openairdocs.org/tcds/A53EU), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs) - Serial number: 432 - Year built: 1994 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: July 9, 2019 - Certificate issued: June 29, 2015 - Last registry action: January 13, 2021 - Mode S code: AAFC90 - Owner when cancelled: [Airline Contract Maintenance And Equipment Inc](https://openairdocs.org/faa-owner/AIRLINE%20CONTRACT%20MAINTENANCE%20AND%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/N807HC - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=807HC - Page: https://openairdocs.org/deregistered/N807HC-2022-05-06 From the FAA registry file of October 29, 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 Aerospatiale/Alenia ATR-72-212: https://openairdocs.org/model/aerospatiale-alenia-atr-72-212.md ## Service difficulty reports (35) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COEA2020100604807](https://openairdocs.org/sdr/COEA2020100604807), Oct 3, 2020: CONNECTOR. DIRTY. FLIGHT 1700, ENROUTE HNL-ITO AIR TURNBACK/DISCREPANCY: NR 2 ENGINE TORQUE FLUCTUATES 10-15% IN CRUISE. RETURNED TO HNL. NO EMERGENCY DECLARED. LANDED WITHOUT IN - [SDR COEA2020040903807](https://openairdocs.org/sdr/COEA2020040903807), Apr 8, 2020: COMPUTER. FAULTY. FLIGHT 1700/ENROUTE HNL-ITO, AIR TURNBACK DISCREPANCY: ON CLIMB OUT AFTER TAKEOFF, RECEIVED A STICK PUSHER/SHAKER FAULT. RETURNED TO HNL. NO EMERGENCY DECLARED. - [SDR COEA2020020761807](https://openairdocs.org/sdr/COEA2020020761807), Feb 6, 2020: ANTENNA. CORRODED. FLIGHT 1700, ENROUTE HNL-ITO AIR TURNBACK/DISCREPANCY: FLIGHT CONTROL ILLUMINATED ON CAP WITH AMBER STICK PUSHER FAULT DURING CLIMB. AIRCRAFT WAS RETURNED TO HN - [SDR COEA201912204807](https://openairdocs.org/sdr/COEA201912204807), Dec 31, 2019: AOA. FAULTED. FLIGHT 1700, AIR TURNBACK, ON TAKEOFF, THE MASTER CAUTION, FLIGHT CTR ON CAS AND STICK PUSHER SHAKER FAULT LIGHTS ILLUMINATED. AIRCRAFT WAS RETURNED TO DEPARTUR - [SDR COEA2019110753807](https://openairdocs.org/sdr/COEA2019110753807), Nov 5, 2019: PROXIMITY SWITCH. FAULTY. FLIGHT 1700, HNL-ITO AIR TURNBACK/APPROX. 14:15 DISCREPANCY: AFTER GEAR WAS RETRACTED, FLIGHT CONTROL LIGHT ON CAP AND STICK SHAKER LIGHTS ILLUMINATED. AIRCRAFT - [SDR COEA2019110752807](https://openairdocs.org/sdr/COEA2019110752807), Nov 5, 2019: AOA. FAULTY. FLIGHT 1700, HNL-ITO/AIR TURNBACK AT APPROX.1045Z DISCREPANCY: FLIGHT CONTROL LIGHT ON CAP AND STICK SHAKER FAULT LIGHTS ILLUMINATED AFTER TAKEOFF. AIRCRAFT RET - [SDR COEA2019102541807](https://openairdocs.org/sdr/COEA2019102541807), Oct 24, 2019: AOA. FAULTY. FLIGHT 1700, HNL-ITO/ AIR TURNBACK DISCREPANCY: ON CLIMB OUT, THE STICK PUSHER/SHAKER FAULT LIGHT ILLUMINATED IN ADDITION TO THE MASTER CAUTION LIGHT. THE AIRCR - [SDR COEA2018111505807](https://openairdocs.org/sdr/COEA2018111505807), Nov 15, 2018: SKIN PANEL. CORRODED. WO 187945 NR 200099 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE LT UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 41-42, STRINGERS 3L-4L - [SDR COEA2018012063807](https://openairdocs.org/sdr/COEA2018012063807), Aug 8, 2018: PANEL. CORRODED. WO 187945 NR 500032 HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON LH OVERWING FUEL PANEL 523GT. CORRECTIVE ACTION: REPLACED WITH OEM PART. - [SDR COEA2018091301807](https://openairdocs.org/sdr/COEA2018091301807), Aug 8, 2018: PANEL. CORRODED. HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON RT OVERWING FUEL PANEL 623GT. REPLACED WITH OEM PART. - [SDR COEA2018080704807](https://openairdocs.org/sdr/COEA2018080704807), Aug 7, 2018: HINGE FITTING. CORRODED. HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON LT WING INBOARD AILERON HINGE FITTING. REPLACED FITTING WITH OEM PART. - [SDR COEA2018120632807](https://openairdocs.org/sdr/COEA2018120632807), Aug 3, 2018: STRINGER. CORRODED. WO 187945 NR 100012 HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON FRAME 29 STRINGER SPLICE 17R. CORRECTIVE ACTION: REPLACED WITH OEM STRINGER. - [SDR COEA2016080218807](https://openairdocs.org/sdr/COEA2016080218807), Aug 2, 2016: SKIN. CORRODED. LEFT HORIZONTAL STAB LEADING EDGE HAS CORROSION. REPLACED LEADING EDGE WITH NEW. - [SDR COEA2016061414807](https://openairdocs.org/sdr/COEA2016061414807), Jun 14, 2016: FLOORBEAM. CORRODED. FLOORBEAM, FRAME 17 HAS CORROSION. REPAIRED IAW 0043023. - [SDR COEA2016061413807](https://openairdocs.org/sdr/COEA2016061413807), Jun 14, 2016: FLOORBEAM. CORRODED. FLOORBEAM 15 HAS CORROSION BETWEEN CENTER SEAT TRACKS. REPAIRED IAW SRM 530000-300-852-A01. - [SDR COEA2016060315807](https://openairdocs.org/sdr/COEA2016060315807), Jun 3, 2016: SKIN. CRACKED. FWD CARGO DOOR, FWD LOWER CORNER, INTERNAL SURFACE OF OUTER SKIN HAS MULTIPLE AREAS WITH CRACKS. REPAIRED IAW SRAS S523R0080. - [SDR COEA2015111217807](https://openairdocs.org/sdr/COEA2015111217807), Nov 12, 2015: PAN. CORRODED. FWD CARGO DOOR HAS CORROSION AT INBOARD LOWER STRUCTURE. REPLACED LOWER PAN WITH OEM PART. - [SDR COEA2015081616807](https://openairdocs.org/sdr/COEA2015081616807), Aug 16, 2015: THRESHOLD. CORRODED. LEFT PASSENGER DOOR THRESHOLD, DOUBLER AND DRAIN CHANNEL HAVE CORROSION. REPLACED THRESHOLD WITH OEM PART. - [SDR COEA2015081612807](https://openairdocs.org/sdr/COEA2015081612807), Aug 16, 2015: CLOSEOUT PANEL. CORRODED. RIGHT OUTBOARD SEAT TRACK CLOSE OUT PANEL FRAMES 35-36 HAS CORROSION. REPLACED THE CLOSEOUT PANEL. - [SDR COEA2015081608807](https://openairdocs.org/sdr/COEA2015081608807), Aug 16, 2015: DOUBLER. CORRODED. BRIDGING CHECK COE & MINOR REPAIR. RT SERVICE DOOR THRESHOLD DOUBLER HAS LEVEL 2 CORROSION. REPLACED DOUBLER WITH OEM PART. - [SDR COEA2015081607807](https://openairdocs.org/sdr/COEA2015081607807), Aug 16, 2015: CHANNEL. CORRODED. BRIDGING CHECK COE & MINOR REPAIR. RT SERVICE DOOR THRESHOLD, DRAIN CHANNEL HAS LEVEL 2 CORROSION. REPLACED DRAIN CHANNEL WITH OEM. - [SDR COEA2015081606807](https://openairdocs.org/sdr/COEA2015081606807), Aug 16, 2015: BRACKET. CORRODED. BRIDGING CHECK COE & MINOR REPAIR. BRACKET AFT OF FRAME 37, HAS LEVEL 2 CORROSION AT THRESHOLD ATTACH LOCATION. REPLACED BRACKET WITH OEM PART. - [SDR COEA2015081602807](https://openairdocs.org/sdr/COEA2015081602807), Aug 16, 2015: DOUBLER. CORRODED. HEAVY CHECK COE & MAJOR REPAIR. FRAME 39 FWD DOUBLER AT LEVEL OF SERVICE DOOR, THRESHOLD HAS LEVEL 2 CORROSION. REPAIR IAW SRAS CE 4529 15 9581 DATED 10 1 15. - [SDR COEA2015081508807](https://openairdocs.org/sdr/COEA2015081508807), Aug 15, 2015: STRINGER CLIP. CORRODED. BRIDGING CHECK COE & MINOR REPAIR. STRINGER CLIP AT FRAME 13, STRINGER 20 LT, HAS LEVEL 2 CORROSION. REPLACED STRINGER CLIP WITH OEM PART. - [SDR COEA2015081506807](https://openairdocs.org/sdr/COEA2015081506807), Aug 15, 2015: STRINGER CLIP. CORRODED. BRIDGING CHECK COE & MINOR REPAIR. STRINGER CLIP AT FRAME 13, STRINGER 20 RT, HAS LEVEL 2 CORROSION. REPLACED STRINGER CLIP WITH OEM PART. - [SDR COEA2015081505807](https://openairdocs.org/sdr/COEA2015081505807), Aug 15, 2015: CREASE BEAM. CORRODED. BRIDGING CHECK COE & MAJOR REPAIR. LT CREASE BEAM OUTER CHORD HAS LEVEL 2 CORROSION, AT FRAMES 39 - 40. REPAIR IAW SRAS CE 4530 15 9582 DATED 10 5 15. - [SDR COEA2015081503807](https://openairdocs.org/sdr/COEA2015081503807), Aug 15, 2015: FRAME. CORRODED. HEAVY CHECK COE & MAJOR REPAIR. FRAME 13 HAS LEVEL 2 CORROSION ON THE AFT SIDE, BETWEEN STRINGER 19L - 20L. REPAIRED IAW SRAS ES-4388 15 9551 DATED 9 21 15. - [SDR COEA2015081501807](https://openairdocs.org/sdr/COEA2015081501807), Aug 15, 2015: FAILSAFE. CORRODED. HEAVY CHECK COE & MINOR REPAIR. FRAME 14 FAIL SAFE HAS LEVEL 2 CORROSION. STRINGER 20L - 21L. REPAIR IAW SRAS CE-4472 15 9584 DATED 9 17 2015. - [SDR COEA2015081209807](https://openairdocs.org/sdr/COEA2015081209807), Aug 12, 2015: SPLICE. CORRODED. WO 151753 NR 800007 BRIDGING CHECK COE & MINOR REPAIR. AFT PAX DOOR, UPPER PAN SPLICE ON AFT EDGE HAS LEVEL 2 SURFACE CORROSION. REPLACED SPLICE WITH OEM PART. - [SDR COEA2015081203807](https://openairdocs.org/sdr/COEA2015081203807), Aug 12, 2015: INTERCOSTAL. CORRODED. BRIDGING CHECK COE & MINOR REPAIR. AFT PAX DOOR, FWD SIDE OF VENT DOOR AREA HAS LEVEL 2 CORROSION ON INTERCOSTAL. REPLACED WITH OEM PART. - [SDR COEA2015081202807](https://openairdocs.org/sdr/COEA2015081202807), Aug 12, 2015: INTERCOSTAL. CORRODED. BRIDGING CHECK COE & MINOR REPAIR. AFT PAX DOOR, FWD SIDE OF VENT DOOR AREA HAS LEVEL 2 CORROSION ON INTERCOSTAL. REPLACED WITH OEM PART. - [SDR COEA2015081204807](https://openairdocs.org/sdr/COEA2015081204807), Aug 12, 2015: FITTING. CORRODED. BRIDGING CHECK COE & MINOR REPAIR. AFT PAX DOOR, FWD SIDE OF VENT DOOR AREA HAS LEVEL 2 CORROSION ON CLIP. REPLACED WITH OEM. - [SDR COEA2015081111807](https://openairdocs.org/sdr/COEA2015081111807), Aug 11, 2015: SKIN. GOUGED. LEFT WING UPPER COMPOSITE SKIN GOUGED BETWEEN RIB 25-26. REPAIRED IAW SRAS ES-4416/15.10341. - [SDR COEA2015080610807](https://openairdocs.org/sdr/COEA2015080610807), Aug 6, 2015: SPAR. GOUGED. LEFT WING FRONT SPAR UPPER LEADING EDGE FLANGE HAS NUMEROUS GOUGES, RIBS 25-31. REPAIRED IAW SRAS ES-4389/15.10431. - [SDR COEA2015080601807](https://openairdocs.org/sdr/COEA2015080601807), Aug 6, 2015: HINGE FITTING. CORRODED. BRIDGING CHECK COE & MINOR REPAIR. RT AILERON OTBD HINGE FITTING IS EXFOLIATED AT THE GROUNDING CONNECTION POINT. REPLACED WITH OEM PART. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.