# N805HC: 2004 Eads/Alenia ATR ATR 42-500, registration cancelled 2023-02-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 1, 2023
- Exported to: Canada
- Status when cancelled: Valid registration
- Airframe: [Eads/Alenia ATR ATR 42-500](https://openairdocs.org/model/eads-alenia-atr-atr-42-500) (registry code 868094C)
- Engine: [Pratt & Whitney Canada PW127E](https://openairdocs.org/engine/pratt-whitney-canada-pw127e) (registry code 52220)
- Data sheets: [TCDS A53EU](https://openairdocs.org/tcds/A53EU), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 625
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: February 24, 2014
- Certificate issued: September 5, 2013
- Last registry action: April 25, 2022
- Mode S code: AAF522
- 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/N805HC
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=805HC
- Page: https://openairdocs.org/deregistered/N805HC-2023-02-01

From the FAA registry file of October 31, 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 Eads/Alenia ATR ATR 42-500: https://openairdocs.org/model/eads-alenia-atr-atr-42-500.md

## Service difficulty reports (81, newest 50)

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

- [SDR COEA2020092404805](https://openairdocs.org/sdr/COEA2020092404805), Jul 9, 2020: BRACKET. CORRODED. HATS WO 176998 NR00616, WO 211916 HEAVY CHECK HATS/MINOR REPAIR: LEVEL 2 CORROSION ON MAIN ENTRY DOOR INNER SEAL JUST AFT OF FRAME 36. REPLACED PART BY FABRICAT
- [SDR COEA2020090103805](https://openairdocs.org/sdr/COEA2020090103805), Jul 2, 2020: BRACKET. CORRODED. HATS WO 176998 NR00615, WO 211916 HEAVY CHECK HATS/MINOR REPAIR. LEVEL 2 CORROSION ON BACKSIDE OF RT SIDE BRACKET FOR ELEVATOR PULLEY IN AFT ACCY COMPARTMENT. C
- [SDR COEA2020100605805](https://openairdocs.org/sdr/COEA2020100605805), Jun 22, 2020: FIREWALL. CRACKED. HATS WO 176998 NR00502, EMPIRE WO 211916 HEAVY CHECK. HATS/MAJOR REPAIR: RIGHT ENGINE UPPER FIREWALL HAS A CRACK AT APPROXIMATELY AREA 3. CORRECTIVE ACTION: REP
- [SDR COEA2020090102805](https://openairdocs.org/sdr/COEA2020090102805), Jun 10, 2020: PANEL. CORRODED. HATS WO 176998 NR00161, EMPIRE WO 211916 HEAVY CHECK HATS/MINOR REPAIR. EXFOLIATION LEVEL 2 CORROSION ON INBOARD OF HINGE ON FLAP DOOR PANEL 531BB. CORRECTIVE A
- [SDR COEA2020101307805](https://openairdocs.org/sdr/COEA2020101307805), Jun 2, 2020: FIREWALL. CRACKED. HATS WO 176998 NR00522, WO 211916 HEAVY CHECK HATS/MAJOR REPAIR. LEFT ENGINE UPPER FIREWALL HAS CRACK AT APPROXIMATELY AREA 3. CORRECTIVE ACTION: REPAIRED PER S
- [SDR COEA2020101306805](https://openairdocs.org/sdr/COEA2020101306805), Jun 2, 2020: SKIN. CORRODED. HATS WO 176998 NR00009, EMPIRE WO 211916 HEAVY CHECK HATS/MAJOR REPAIR. LEFT WING LOWER SKIN HAS LEVEL 2 CORROSION AT RIB 15 TRAILING EDGE. CORRECTIVE ACTION: R
- [SDR COEA2020090101805](https://openairdocs.org/sdr/COEA2020090101805), Jun 2, 2020: PANEL. CORRODED. HATS WO 176998 NR00010, WO 211916 HEAVY CHECK HATS/MINOR REPAIR. LEFT WING TRAILING EDGE PANEL 532AB HAS LEVEL 2 CORROSION ON HINGE. CORRECTIVE ACTION: REPLACED
- [SDR COEA2019081321805](https://openairdocs.org/sdr/COEA2019081321805), Aug 12, 2019: CIRCUIT BREAKER. TRIPPED. FLIGHT 672, AIR TURNBACK, DURING CLIMB OUT, NO BLUE SYSTEM HYDRAULIC PRESSURE. CREW ELECTED TO RETURN TO DEPARTURE. EMERGENCY DECLARED. LANDED WITHOUT FURTHER I
- [SDR COEA2018102119805](https://openairdocs.org/sdr/COEA2018102119805), Oct 21, 2018: TERMINAL. DAMAGED. FLIGHT 612, ENROUTE HNL-LNY/AIR TURNBACK. MULTIPLE ELECTRICAL FAILURES IN FLIGHT. EADI, EHSI, AIR DATA INSTRUMENTS, MC AND MW INDICATIONS, DEPRESSURIZATION/DECO
- [SDR COEA201808226805](https://openairdocs.org/sdr/COEA201808226805), Jul 16, 2018: WINDOW FRAME. CRACKED. COPILOT SIDE WINDOW LOWER FRAME CRACKED AT UPPER FWD LOCK FASTENER. REPAIRED IAW S531R5004.13332. MAJOR REPAIR
- [SDR COEA2018082213805](https://openairdocs.org/sdr/COEA2018082213805), Jul 16, 2018: FIREWALL. CRACKED. RT ENGINE UPPER FIREWALL AFT OUTBOARD AREA WAS CRACKED. REPAIRED IAW ES-3628/18.13303.
- [SDR COEA2018082177805](https://openairdocs.org/sdr/COEA2018082177805), Jul 13, 2018: RIB. CORRODED. LEFT HORIZONTAL STAB TIP RIB HAD CORROSION. REPAIRED IAW SRAS ES-4176/18.13322.
- [SDR COEA2018082318805](https://openairdocs.org/sdr/COEA2018082318805), Jul 12, 2018: SKIN. CORRODED. CORROSION FOUND ON THE RT HORIZONTAL STAB LEADING EDGE. REPAIRED IAW ES-1735/16.10237 ISSUE B. MAJOR REPAIR.
- [SDR COEA2018082317805](https://openairdocs.org/sdr/COEA2018082317805), Jul 11, 2018: FITTING. CORRODED. CORROSION AND ELONGATED HOLE IN THE FITTING OF THE RT COCKPIT FRAME 8 AT THE SIDE WINDOW UPPER SILL. REPAIRED IAW ES-4174/18.13325.
- [SDR COEA2018082215805](https://openairdocs.org/sdr/COEA2018082215805), Jul 11, 2018: FITTING. DAMAGED. LT ENGINE INBOARD AFT MOUNT FITTING AT JUNCTION OF TUBES 1 & 2 WAS DAMAGED. REPAIED IAW ES-3657/18.13301.
- [SDR COEA2018082214805](https://openairdocs.org/sdr/COEA2018082214805), Jul 11, 2018: CRANK ASSY. CORRODED. PASSENGER DOOR EXTERNAL HANDLE CRANK HAD CORROSION. REPLACED THE DOOR CRANK.
- [SDR COEA201808212805](https://openairdocs.org/sdr/COEA201808212805), Jul 11, 2018: SKIN. CORRODED. CORROSION WAS FOUND ON THE LT WING LOWER SKIN AROUND JACK ADAPTOR PLUG. REPAIR THE SKIN IAW ES-3676/18.13306.
- [SDR COEA20180821805](https://openairdocs.org/sdr/COEA20180821805), Jul 11, 2018: SKIN. DAMAGED. RIGHT LOWER LOBE, AFT PANEL WAS DAMAGED AT THE DC GROUND CONNECTION. REPAIRED THE SKIN ES-4648/15.13319.
- [SDR COEA2018082119805](https://openairdocs.org/sdr/COEA2018082119805), Jul 11, 2018: SEAT TRACK. CORRODED. CABIN ENTRANCE SEAT TRACK BETWEEN FRAMES 36-38 HAD CORROSION. THE SEAT TRACK WAS REPLACED WITH NEW.
- [SDR COEA2018082118805](https://openairdocs.org/sdr/COEA2018082118805), Jul 11, 2018: SKIN. CORRODED. CORROSION FOUND ON THE RT WING LOWER SKIN AROUND JACK ADAPTOR PLUG. REPAIRED IAW ES-3668/18.13300.
- [SDR COEA2018082115805](https://openairdocs.org/sdr/COEA2018082115805), Jul 11, 2018: ANGLE. CRACKED. STABILIZER RUDDER UPPER FITTING, UPPER HORIZONTAL ANGLE CRACKED. REPLACED.
- [SDR COEA2018082104805](https://openairdocs.org/sdr/COEA2018082104805), Jul 11, 2018: SKIN. CORRODED. RIGHT WING LOWER SKIN HAD CORROSION BETWEEN RIBS 4 - 5, AROUND WATER DRAIN. REPAIRED IAW ES-3693/18.13304.
- [SDR COEA2018082106805](https://openairdocs.org/sdr/COEA2018082106805), Jul 10, 2018: ACCESS PANEL. CORRODED. CORROSION WAS FOUND ON THE RT WING ACCESS PANEL 622FT BETWEEN RIBS 22-23. REPAIRED IAW CE-1744/16.0211 ISSUE B.
- [SDR COEA2018082103805](https://openairdocs.org/sdr/COEA2018082103805), Jul 10, 2018: BELLCRANK. CORRODED. LT WING REAR SPAR BELLCRANK HAD CORROSION AT RIB 21. BELLCRANK REPLACED.
- [SDR COEA2018082102805](https://openairdocs.org/sdr/COEA2018082102805), Jul 10, 2018: FITTING. CORRODED. LEFT OUTBOARD FLAP, INBOARD BEAM SUPPORT FITTING HAD CORROSION. FLAP BEAM SUPPORT FITTING WAS REPLACED.
- [SDR COEA2018011301805](https://openairdocs.org/sdr/COEA2018011301805), Jan 13, 2018: CONNECTOR. DIRTY. ABORTED TAKEOFF DUE TO A FUEL CCAS LIGHT ILLUMINATED BETWEEN 80-90 KTS. MAINTENANCE TROUBLESHOT AND SUMPED THE FUEL TANKS, CHECKED AND CLEANED ALL FUEL PROBE CO
- [SDR COEA2017072406805](https://openairdocs.org/sdr/COEA2017072406805), Jul 24, 2017: SEAT. MALFUNCTIONED. FLIGHT 651, JHM-HNL: UNCOMMANDED MOVEMENT OF CAPTAIN SEAT TO THE FULL AFT POSITION DURING TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND POWER LEVERS REDUCED TO GROU
- [SDR COEA2017060705805](https://openairdocs.org/sdr/COEA2017060705805), Jun 7, 2017: CONTROL SWITCH. FAULTED. AIR TURNBACK DUE TO A FLAP OVERSPEED WARNING FOLLOWED BY A FAILED ATTEMPT TO CYCLE THE FLAP HANDLE FROM THE 15 DEGREE POSITION. AIRCRAFT LANDED WITHOUT FURTHER 
- [SDR COEA2017032603805](https://openairdocs.org/sdr/COEA2017032603805), Mar 26, 2017: MODULE. FAILED. DURING CLIMB, THE CREW RECEIVED A NR 2 SINGLE CHANNEL CAUTION. CREW ELECTED TO RETURN TO DEPARTURE. NO EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCID
- [SDR COEA2017032602805](https://openairdocs.org/sdr/COEA2017032602805), Mar 26, 2017: WARNING MESSAGE. FALSE ACTIVATION. FLIGHT 612, ENROUTE, AIR TURNBACK, HYDRAULIC BLUE SYSTEM LOW LEVEL AND LOW PRESSURE WARNINGS IN FLIGHT. AFTER CONSULTING THE QRH, THE CREW RETURNED TO DEPARTURE
- [SDR COEA2017032101805](https://openairdocs.org/sdr/COEA2017032101805), Mar 21, 2017: GENERATOR. FAILED. CREW RECEIVED A NR 1 ACW FAULT DURING CLIMB OUT. ELECTED TO RETURN TO DEPARTURE, NO EMERGENCY DECLARED. REPLACED THE NR 1 ACW GENERATOR.
- [SDR COEA2016101344805](https://openairdocs.org/sdr/COEA2016101344805), Oct 13, 2016: AHRS. MALFUNCTIONED. FLT 610, ENROUTE, EFIS COMP ATTITUDE ON CAPTAIN`S SIDE DURING CLIMB AFTER TAKEOFF. CREW ELECTED TO RETURN TO DEPARTURE. NO EMERGENCY DECLARED. LANDED AIRCRAFT W
- [SDR COEA2016032943805](https://openairdocs.org/sdr/COEA2016032943805), Mar 29, 2016: SKIN. CORRODED. HEAVY CHECK COE & MAJOR REPAIR. LT HORIZONTAL STABILIZER LE 331 HAS LEVEL 2 CORROSION ON UPPER & LOWER INNER MATING SURFACES. REPAIR IAW SRAS ES 1754/16... 1023
- [SDR COEA2016032941805](https://openairdocs.org/sdr/COEA2016032941805), Mar 29, 2016: SKIN. CORRODED. HEAVY CHECK COE & MAJOR REPAIR. RT HORIZONTAL STABILIZER LE HAS LEVEL 2 CORROSION ON UPPER & LOWER INNER MATING SURFACES. REPAIR PER SRAS ES 1735 16 10237 DATED
- [SDR COEA2016032737805](https://openairdocs.org/sdr/COEA2016032737805), Mar 27, 2016: SKIN PANEL. DAMAGED. HEAVY CHECK COE MAJOR REPAIR. FWD CTR FUSELAGE CROWN, SKIN PANEL ADF2 ANTENNA LOCATION, MOUNTING HOLES ARE DEFORMED. REPAIR IAW CE 914 16 10212 DATED 5 10 16.
- [SDR COEA2016032736805](https://openairdocs.org/sdr/COEA2016032736805), Mar 27, 2016: SKIN PANEL. DAMAGED. HEAVY CHECK COE & MAJOR REPAIR. FWD CTR FUSELAGE CROWN, SKIN PANEL ADF 1 ANTENNA LOCATION, MOUNTING HOLES ARE DEFORMED. REPAIR PER CE 1914 16 10212 DATED 5 10 2
- [SDR COEA2016032634805](https://openairdocs.org/sdr/COEA2016032634805), Mar 26, 2016: BRACKET. CORRODED. HEAVY CHECK COE & MINOR REPAIR. LT PAX DOOR HINGE COVER BRACKET HAS LEVEL 2 CORROSION. REPLACED BRACKET WITH OEM PART.
- [SDR COEA2016032633805](https://openairdocs.org/sdr/COEA2016032633805), Mar 26, 2016: BRACKET. CORRODED. HEAVY CHECK COE & MINOR REPAIR. LT PAX DOOR HINGE COVER BRACKET HAS LEVEL 2 CORROSION. REPLACED BRACKET WITH OEM PART.
- [SDR COEA2016032632805](https://openairdocs.org/sdr/COEA2016032632805), Mar 26, 2016: ATTACH ANGLE. CORRODED. HEAVY CHECK COE & MINOR REPAIR. LT PAX DOOR, LOWER AIRSTAIR ATTACH ANGLE HAS LEVEL 2 CORROSION. REPLACED ANGLE WITH OEM PART.
- [SDR COEA2016032631805](https://openairdocs.org/sdr/COEA2016032631805), Mar 26, 2016: LANDING. DAMAGED. HEAVY CHECK COE & MAJOR REPAIR. RT UPPER WING INBD REMOVABLE PANEL LANDING FOR ACCESS PANEL 622CT HAS FRETTING LEVEL 2. REPAIR IAW SRAS CE 1721 16 10167 DATED 5
- [SDR COEA2016032630805](https://openairdocs.org/sdr/COEA2016032630805), Mar 26, 2016: SPLICE. CORRODED. HEAVY CHECK COE & MINOR REPAIR. AFT PAX DOOR, AIRSTAIR SPLICE ANGLE HAS LEVEL 2 CORROSION. REPLACED SPLICE ANGLE WITH OEM PART.
- [SDR COEA2016032539805](https://openairdocs.org/sdr/COEA2016032539805), Mar 25, 2016: SKIN. CORRODED. HEAVY CHECK COE & MAJOR REPAIR. TAIL SECTION LOWER SKIN DOOR. REINFORCEMENT HAS LEVEL 2 CORROSION AT FRAME 45, FWD EDGE OF AVIONICS ACCESS DOOR CUT OUT. REPAIR 
- [SDR COEA2016032538805](https://openairdocs.org/sdr/COEA2016032538805), Mar 25, 2016: PANEL. CORRODED. HEAVY CHECK COE & MAJOR REPAIR. OVERHEAD HATCH CUT OUT PANEL INTERNAL SURFACE HAS LEVEL 2 CORROSION. REPAIR IAW CE 1606 16 10213 DATED 5 10 2016.
- [SDR COEA2016032503805](https://openairdocs.org/sdr/COEA2016032503805), Mar 25, 2016: COVER PLATE. CORRODED. HEAVY CHECK COE & MINOR REPAIR. RT AOA PROBE COVER PANEL HAS LEVEL 2 CORROSION. REPLACED COVER PLATE WITH OEM PART.
- [SDR COEA2016032502805](https://openairdocs.org/sdr/COEA2016032502805), Mar 25, 2016: COVER PLATE. CORRODED. HEAVY CHECK COE & MINOR REPAIR. LT AOA PROBE COVER PANEL HAS LEVEL 2 CORROSION. REPLACED COVER PLATE WITH OEM PART.
- [SDR COEA2016032435805](https://openairdocs.org/sdr/COEA2016032435805), Mar 24, 2016: FLOOR SUPPORT. CORRODED. HEAVY CHECK COE & MINOR REPAIR. LT FLOOR SUPPORT ANGLE BETWEEN FRAMES 39 - 40 HAS LEVEL 2 CORROSION. REPLACED ANGLE WITH OEM PART.
- [SDR COEA2016032429805](https://openairdocs.org/sdr/COEA2016032429805), Mar 24, 2016: SEAT TRACK. CORRODED. HEAVY CHECK COE & MAJOR REPAIR. LT OTBD SEAT TRACK BETWEEN FRAMES 35-36 HAS AREAS OF LEVEL 2 CORROSION. REPAIRED IAW SRM 53-00-00-300-853-A01.
- [SDR COEA2016032428805](https://openairdocs.org/sdr/COEA2016032428805), Mar 24, 2016: GUIDE. CORRODED. HEAVY CHECK COE & MINOR REPAIR. RT OTBD FLAP 2ND CAM GUIDE FROM INBD END HAS AREAS OF LEVEL 2 CORROSION. REPLACED GUIDE WITH OEM PART.
- [SDR COEA2016032427805](https://openairdocs.org/sdr/COEA2016032427805), Mar 24, 2016: GUIDE. CORRODED. HEAVY CHECK COE & MINOR REPAIR. RT INBD FLAP 4TH CAM GUIDE FROM INBD END HAS AREAS OF LEVEL 2 CORROSION. REPLACED GUIDE WITH OEM PART.
- [SDR COEA2016032426805](https://openairdocs.org/sdr/COEA2016032426805), Mar 24, 2016: GUIDE. CORRODED. HEAVY CHECK COE & MINOR REPAIR. RT INBD FLAP 3RD CAM GUIDE FROM INBD END HAS LEVEL 2 CORROSION. REPLACED GUIDE WITH OEM PART.

All 81: https://openairdocs.org/deregistered/N805HC-2023-02-01/reports.md

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