# N810HC: 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: 423 - Year built: 1994 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: February 16, 2018 - Certificate issued: August 27, 2015 - Last registry action: March 11, 2021 - Mode S code: AB0A0E - 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/N810HC - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=810HC - Page: https://openairdocs.org/deregistered/N810HC-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 (86, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COEA2020011651810](https://openairdocs.org/sdr/COEA2020011651810), Jan 15, 2020: PUMP. FAILED. 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. LAND - [SDR COEA201911222810](https://openairdocs.org/sdr/COEA201911222810), Oct 22, 2019: SKIN. CORRODED. 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. C - [SDR COEA2019112287810](https://openairdocs.org/sdr/COEA2019112287810), Oct 8, 2019: BULKHEAD. CORRODED. 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: REPAIRE - [SDR COEA2019112640810](https://openairdocs.org/sdr/COEA2019112640810), Oct 6, 2019: SKIN. CORRODED. WO 205731 NR 200121 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28D-29 BETWEEN STRINGERS - [SDR COEA2019112639810](https://openairdocs.org/sdr/COEA2019112639810), Oct 6, 2019: SKIN. CORRODED. WO 205731 NR 200108 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION AFT OF FRAME 23C BELOW STRINGER 8R. CORR - [SDR COEA2019112638810](https://openairdocs.org/sdr/COEA2019112638810), Oct 6, 2019: SKIN. CORRODED. WO 205731 NR 200101 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION AFT OF FRAME 23B BELOW STRINGER 8R. CORR - [SDR COEA2019112236810](https://openairdocs.org/sdr/COEA2019112236810), Oct 6, 2019: SKIN. CORRODED. 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. C - [SDR COEA201911225810](https://openairdocs.org/sdr/COEA201911225810), Oct 6, 2019: SKIN. CORRODED. 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 - [SDR COEA201911224810](https://openairdocs.org/sdr/COEA201911224810), Oct 6, 2019: SKIN. CORRODED. 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 - [SDR COEA2019112263810](https://openairdocs.org/sdr/COEA2019112263810), Oct 6, 2019: SKIN. CORRODED. WO 205731 NR 200122 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28D-29 BETWEEN STRINGERS - [SDR COEA201911229810](https://openairdocs.org/sdr/COEA201911229810), Oct 6, 2019: SKIN. CORRODED. WO 205731 NR 200092 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 23-23A, STRINGERS 6AR-7R. - [SDR COEA201911228810](https://openairdocs.org/sdr/COEA201911228810), Oct 6, 2019: SKIN. CORRODED. WO 205731 NR 200091 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION FORWARD OF FRAME 23A, BETWEEN STRINGERS - [SDR COEA201911227810](https://openairdocs.org/sdr/COEA201911227810), Oct 6, 2019: SKIN. CORRODED. WO 205731 NR 200077 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION FORWARD OF FRAME 40, ABOVE STRINGER 6R. CO - [SDR COEA2019112264810](https://openairdocs.org/sdr/COEA2019112264810), Oct 6, 2019: SKIN. CORRODED. WO 205731 NR 200117 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 29-30, STRINGERS 3R-4R. COR - [SDR COEA2019112261810](https://openairdocs.org/sdr/COEA2019112261810), Oct 6, 2019: SKIN. CORRODED. WO 205731 NR 200079 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 39-40, STRINGERS 3R-4R. COR - [SDR COEA2019112260810](https://openairdocs.org/sdr/COEA2019112260810), Oct 6, 2019: SKIN. CORRODED. WO 205731 NR 200078 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 39-40, STRINGERS 4R-5R. COR - [SDR COEA2019112269810](https://openairdocs.org/sdr/COEA2019112269810), Oct 6, 2019: SKIN. CORRODED. WO 205731 NR 200064 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 40-41, STRINGERS 3R-4R. COR - [SDR COEA2019112268810](https://openairdocs.org/sdr/COEA2019112268810), Oct 6, 2019: SKIN. CORRODED. WO 205731 NR 200064 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION NEAR FRAMES 40-41, STRINGERS 3R-4R. CORREC - [SDR COEA2019112267810](https://openairdocs.org/sdr/COEA2019112267810), Oct 6, 2019: SKIN. CORRODED. WO 205731 NR 200061 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 41-42, STRINGERS 5R-6R. COR - [SDR COEA20191119810](https://openairdocs.org/sdr/COEA20191119810), Oct 6, 2019: SKIN. CORRODED. 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. - [SDR COEA2019111267810](https://openairdocs.org/sdr/COEA2019111267810), Oct 6, 2019: SHEAR TIE. CORRODED. 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. - [SDR COEA2019110865810](https://openairdocs.org/sdr/COEA2019110865810), Oct 6, 2019: SKIN. CORRODED. 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 - [SDR COEA2019110864810](https://openairdocs.org/sdr/COEA2019110864810), Oct 6, 2019: SKIN. CORRODED. 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. CORREC - [SDR COEA2019112215810](https://openairdocs.org/sdr/COEA2019112215810), Oct 1, 2019: DOUBLER. CORRODED. WO 205731 NR 100043 HEAVY CHECK COE/MAJOR REPAIR: EXTERNAL FUSELAGE #2 DME ANTENNA DOUBLER HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_010805 - [SDR COEA2019111491810](https://openairdocs.org/sdr/COEA2019111491810), Sep 29, 2019: CONTROL ROD. CORRODED. WO 205731 NR 600023 HEAVY CHECK COE/MINOR REPAIR: R/H WING AILERON TAB CONTROL ROD HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART. - [SDR COEA2019112298810](https://openairdocs.org/sdr/COEA2019112298810), Sep 28, 2019: PANEL. CORRODED. WO 205731 NR 400024 HEAVY CHECK COE/MAJOR REPAIR: L/H NACELLE PANEL LANDING FLANGE FOR OUTBOARD SIDE OF PANEL 477AB HAS LEVEL 2 FRETTING. CORRECTIVE ACTION: REP - [SDR COEA2019112085810](https://openairdocs.org/sdr/COEA2019112085810), Sep 28, 2019: LANDING. CORRODED. WO 205731 NR 400012 HEAVY CHECK COE/MINOR REPAIR: R/H NACELLE LANDING FOR THE AFT EDGE OF PANEL 487AB HAS LEVEL 2 FRETTING. CORRECTIVE ACTION: REPLACED WITH OEM - [SDR COEA2019112094810](https://openairdocs.org/sdr/COEA2019112094810), Sep 28, 2019: PANEL. CORRODED. WO 205731 NR 400009 HEAVY CHECK COE/MAJOR REPAIR: R/H NACELLE PANEL LANDING FOR INBOARD SIDE OF PANEL 487AB HAS LEVEL 2 FRETTING. CORRECTIVE ACTION: REPAIRED PE - [SDR COEA2019112023810](https://openairdocs.org/sdr/COEA2019112023810), Sep 28, 2019: PANEL. CORRODED. WO 205731 NR 400008 HEAVY CHECK COE/MAJOR REPAIR: R/H NACELLE PANEL LANDING OUTBOARD SIDE OF PANEL 487AB HAS LEVEL 2 FRETTING. CORRECTIVE ACTION: REPAIRED PER S - [SDR COEA2019112092810](https://openairdocs.org/sdr/COEA2019112092810), Sep 28, 2019: PANEL. CORRODED. WO 205731 NR 400007 HEAVY CHECK COE/MAJOR REPAIR: R/H NACELLE REBATE PANEL LANDING (484AR) HAS LEVEL 2 FRETTING. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0106922 - [SDR COEA201911129810](https://openairdocs.org/sdr/COEA201911129810), Sep 28, 2019: TEE FITTING. CORRODED. WO 205731 NR 400025 HEAVY CHECK COE/MINOR REPAIR: L/H NACELLE PANEL LANDING FLANGE FOR THE INBOARD SIDE OF PANEL 477AB HAS FRETTING, LEVEL 2. CORRECTIVE ACTION: - [SDR COEA201911128810](https://openairdocs.org/sdr/COEA201911128810), Sep 28, 2019: WEB. CORRODED. WO 205731 NR 400022 HEAVY CHECK COE/MINOR REPAIR: L/H NACELLE INBOARD REBATE HAS FRETTING AT THE AFT END OF PANEL 474AR, LEVEL 2. CORRECTIVE ACTION: REPLACED WI - [SDR COEA201911086810](https://openairdocs.org/sdr/COEA201911086810), Sep 28, 2019: LANDING. CORRODED. WO 205731 NR 400026 L/H NACELLE LANDING FOR AFT EDGE OF PANEL 477AB HAS FRETTING. LEVEL 2 CORRECTIVE ACTION: REPLACEMENT WITH OEM PART. - [SDR COEA2019112272810](https://openairdocs.org/sdr/COEA2019112272810), Sep 27, 2019: CHANNEL. CORRODED. WO 205731 NR 600016 HEAVY CHECK COE/MINOR REPAIR: R/H AILERON FIXED TAB CLOSEOUT CHANNEL HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART. - [SDR COEA2019112096810](https://openairdocs.org/sdr/COEA2019112096810), Sep 27, 2019: CHANNEL. CORRODED. WO 205731 NR 600013 HEAVY CHECK COE/MINOR REPAIR: R/H AILERON CONTROL TAB CLOSEOUT CHANNEL HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART. - [SDR COEA2019112291810](https://openairdocs.org/sdr/COEA2019112291810), Sep 26, 2019: ACCESS PANEL. CORRODED. WO 205731 NR 600008 HEAVY CHECK COE/MINOR REPAIR: R/H WING FUEL PANEL 623GT HAS LEVEL 2 CORROSION AROUND SCREWS. CORRECTIVE ACTION: REPLACED WITH OEM PART. - [SDR COEA2019112296810](https://openairdocs.org/sdr/COEA2019112296810), Sep 26, 2019: SKIN. DENTED. WO 205731 NR 205731 HEAVY CHECK COE/MAJOR REPAIR: DENTS ON CENTER FUSELAGE L/H UPPER SKIN PANEL FORWARD OF FRAME 23C BETWEEN STRINGERS 4L-7AL. CORRECTIVE ACTION - [SDR COEA2019110763810](https://openairdocs.org/sdr/COEA2019110763810), Sep 26, 2019: DOOR. CORRODED. WO 205731 NR 200005 HEAVY CHECK COE/MINOR REPAIR: POTABLE WATER SERVICE DOOR HAS LEVEL 2 CORROSION ON EXTERIOR AND INTERIOR SURFACES. CORRECTIVE ACTION: REPLACE - [SDR COEA2019082072810](https://openairdocs.org/sdr/COEA2019082072810), Aug 17, 2019: CONTROL UNIT. FAULTED. FLIGHT 1701, ENROUTE, AT 16,000 FT, THE NR 1 ENGINE TORQUE DROPPED FROM 70% TO 20% THEN RECOVERED. ALL OTHER PARAMETERS NORMAL. AFTER EXTENSIVE TROUBLESHOOTING, - [SDR COEA2019011801810](https://openairdocs.org/sdr/COEA2019011801810), Jan 18, 2019: PITOT TUBE. OBSTRUCTED. FLIGHT 1700, ENROUTE HNL - ITO DISCREPANCY: AMBER MESSAGE ON ADU DADC DATA INVALID AFTER V1, CONTINUED TAKE OFF. LOST AIRSPEED FO SIDE, NO YAW DAMP, NOT ABLE TO - [SDR COEA2017102029810](https://openairdocs.org/sdr/COEA2017102029810), Oct 20, 2017: STRINGER. DAMAGED. DAMAGED STRINGER 1AL BETWEEN FRAMES 17 - 18. INSTALLED A SPLICE REPAIR IAW SRM 53-00-00-300-847-A01. - [SDR COEA2018022230810](https://openairdocs.org/sdr/COEA2018022230810), Sep 22, 2017: STRINGER. DAMAGED. BRIDGING CHECK COE/MAJOR REPAIR: STRINGER 13R HAS DAMAGED HOLE. SPLICE REPAIR SRM 530000-300-824-A01. - [SDR COEA2017071916810](https://openairdocs.org/sdr/COEA2017071916810), Jul 19, 2017: FRAME. CORRODED. FOUND CORROSION ON FRAME 46 AFT SURFACE RIGHT OF BL 0 AT PASS THROUGH. REPAIRED IAW SRAS PCE-1389/17. - [SDR COEA2017071828810](https://openairdocs.org/sdr/COEA2017071828810), Jul 18, 2017: STRINGER. DAMAGED. DAMAGED STRINGER 2AL BETWEEN FRAMES 15 - 16. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-00-00-300-847-A01. - [SDR COEA2017071615810](https://openairdocs.org/sdr/COEA2017071615810), Jul 16, 2017: STRIP. DAMAGED. LEFT WING FRONT SPAR UPPER STRIP SLAT HAS ONE HOLE WITH DAMAGE, RIB 7 - 8. REPAIRED IAW SRAS ES-3446/17. - [SDR COEA2017071326810](https://openairdocs.org/sdr/COEA2017071326810), Jul 13, 2017: SHEAR TIE. CRACKED. FRAME 28D SHEAR TIE HAS A CRACK BETWEEN STRINGERS 1R-1AR. CORRECTIVE ACTION: REPLACED SHEAR TIE WITH NEW PART. - [SDR COEA2017071325810](https://openairdocs.org/sdr/COEA2017071325810), Jul 13, 2017: STRINGER CLIP. CORRODED. CORROSION ON STRINGER CLIP 19L, FRAME 13. REPLACED THE STRINGER CLIP. - [SDR COEA2017071324810](https://openairdocs.org/sdr/COEA2017071324810), Jul 13, 2017: STRINGER. CORRODED. CORROSION FOUND ON STRINGER 21R, BETWEEN FRAMES 12 & 13. REPLACED THE STRINGER. - [SDR COEA2017071323810](https://openairdocs.org/sdr/COEA2017071323810), Jul 13, 2017: HINGE FITTING. NICKED. RIGHT FUSELAGE OPENING FOR EMERGENCY EXIT, AFT LOWER HINGE FITTING IS NICKED ON BOTH EARS. REPAIRED IAW ES-3199/17. - [SDR COEA2017071322810](https://openairdocs.org/sdr/COEA2017071322810), Jul 13, 2017: HINGE FITTING. NICKED. RIGHT FUSELAGE OPENING FOR EMERGENCY EXIT, FWD LOWER HINGE FITTING IS NICKED ON BOTH EARS. REPAIRED IAW ES-3199/17. All 86: https://openairdocs.org/deregistered/N810HC-2022-05-06/reports.md --- 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.