# N885EA: 1992 Dehavilland DHC-8-106, registration cancelled 2025-07-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 23, 2025
- Exported to: Canada
- Status when cancelled: Sale reported
- Airframe: [Dehavilland DHC-8-106](https://openairdocs.org/model/dehavilland-dhc-8-106) (registry code 2809020)
- Engine: [Pratt & Whitney Canada PW121](https://openairdocs.org/engine/pratt-whitney-canada-pw121) (registry code 52124)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 341
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: September 4, 2012
- Last registry action: June 16, 2025
- Mode S code: AC30CD
- Location: [Xxx, OK](https://openairdocs.org/faa-place/OK/Xxx)
- Owner type: Individual
- Owner's area on the map: 35.3806° N, 97.6484° W: Placed by OpenAirDocs at the center of ZIP code 73169, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N885EA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=885EA
- Page: https://openairdocs.org/deregistered/N885EA-2025-07-23

From the FAA registry file of November 5, 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 Dehavilland DHC-8-106: https://openairdocs.org/model/dehavilland-dhc-8-106.md

## Service difficulty reports (63, newest 50)

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

- [SDR 7C7A2025021300006](https://openairdocs.org/sdr/7C7A2025021300006), Feb 12, 2025: TORQUE SENSOR. MALFUNCTIONED. FLAP DRIVE CAUTION LIGHT ILLUMINATED AFTER TAKEOFF W/FLAPS SELECTED 5 DEGREES.
- [SDR 7C7A2024111200009](https://openairdocs.org/sdr/7C7A2024111200009), Nov 10, 2024: GENERATOR. WARNING LIGHT. #2 DC GEN CAUTION LIGHT ILLUMINATED. RESET FAILED.
- [SDR 7C7A2024071100004](https://openairdocs.org/sdr/7C7A2024071100004), Jul 11, 2024: SEQUENCE VALVE. FAULTED. LH INBOARD REAR MLG DOOR OPENED IN FLIGHT. REPLACED LH MLG SOLENOID SEQUENCE VALVE AND AFT LH MLG INBOARD DOOR.
- [SDR 7C7A2023110400058](https://openairdocs.org/sdr/7C7A2023110400058), Nov 4, 2023: RELAY. FAILED. FIRE PROTECTION PANEL INOP. R/R RELAY X-D4N OPS CHECK GOOD
- [SDR 7C7A2023081900049](https://openairdocs.org/sdr/7C7A2023081900049), Aug 19, 2023: SENSOR. FAULTY. #2 OIL PRESSURE GAUGE SHOWED LOW MOMENTARILY THEN CAME BACK UP. EMERGENCY WAS DECLARED AND RETURNED TO ANC. R/R#2 OIL PRESSURE SENSOR SWITCH.
- [SDR 7C7A2023081800048](https://openairdocs.org/sdr/7C7A2023081800048), Aug 18, 2023: SMOKE DETECTOR. INTERMITTENT. LAV SMOKE DETECTOR INTERMITTENTLY CHIRPS FOR NOT REASON (LAV WASN'T ON FIRE)
- [SDR 7C7A2023062700040](https://openairdocs.org/sdr/7C7A2023062700040), Jun 27, 2023: MASTER CAUTION. ERRATIC. CAUTION LIGHT PANEL LIGHTS RANDOMLY TURNING ON AND OFF DURING TEST. WHEN #2 ENG RUNNING AND #2 ENG OFF, #1 ENG CAUTION LIGHTS THAT SHOULD BE ON WERE NOT. WHEN U
- [SDR 2023F00007](https://openairdocs.org/sdr/2023F00007), Dec 29, 2022: SPU. FAULTED. #2 STBY HUD PRESSURE IS 0 PSI. R&R #2 SPU IAW DHC-8 100 AMM 29-11-17. LEAK AND OPS CHECK FAILED SEE ITEM 3 FOR CONTINUED MAINTENANCE. C/W BLEED LEAK AND OPS CHE
- [SDR 7C7A2022122000042](https://openairdocs.org/sdr/7C7A2022122000042), Dec 20, 2022: SPU. FAILED. NO.2 STBY HYDRAULIC PRESSURE INDICATES ZERO WHEN ON. NO ASSOCIATED CAUTION LIGHTS. REPLACED #2 STANDBY POWER UNIT
- [SDR 7C7A2022212100037](https://openairdocs.org/sdr/7C7A2022212100037), Dec 12, 2022: PUMP. WARNING LIGHT. 7H-DIS-27219 #2 ENG HYD PUMP CAUTION LIGHT CAME ON INTERMITTENTLY. FOLLOWED THE QEH.
- [SDR 7C7A2022031700012](https://openairdocs.org/sdr/7C7A2022031700012), Mar 17, 2022: SKIN. CORRODED. CORROSION DAMAGE ON CENTER FUSELAGE RH TOP SKIN PANEL ASSEMBLY PN 85320282 BETWEEN X291.40 -X312.35 AND STR. 1-2S. REF. 008.53-22.07
- [SDR 7C7A2022031700011](https://openairdocs.org/sdr/7C7A2022031700011), Mar 17, 2022: SKIN. DAMAGED. DAMAGE TO LH AILERON SPRING TAB LOWER SKIN. REF. 008.27-22.02
- [SDR 7C7A2022031700010](https://openairdocs.org/sdr/7C7A2022031700010), Mar 17, 2022: SKIN. CRACKED. CRACK DAMAGE ON RH AILERON LOWER SKIN PANEL PN 85740055 AT TAB HINGE STATIONS YW 442.50 AND YW471.50 ALONG THE REAR SPAR. REF 008.27-22.01
- [SDR 7C7A2022031700009](https://openairdocs.org/sdr/7C7A2022031700009), Mar 17, 2022: SHEAR WEB. CORRODED. CORROSION DAMAGE TO BAGGAGE DOOR SURROUND SHEAR WEB PN 85330431 BETWEEN X545 - X564.50 OUTBOARD OF Y-19.23. REF 008.53-22.06
- [SDR 7C7A2022031700008](https://openairdocs.org/sdr/7C7A2022031700008), Mar 17, 2022: FRAME. CHAFED. CHAFE DAMAGE TO THE CENTER FUSE FRAME X253.40 PN 85320575. REF 008.53-22.03
- [SDR 7C7A2022031700007](https://openairdocs.org/sdr/7C7A2022031700007), Mar 17, 2022: STRAP. CORRODED. CORROSION DAMAGE TO THE INNER CAP STRAPS PN 8533501 STRAPS AT FRAME AT X618 BETWEEN STR. 20S-22S. REF. 008.53-22.12
- [SDR 7C7A2022031700006](https://openairdocs.org/sdr/7C7A2022031700006), Mar 17, 2022: FRAME. DAMAGED. MULTIPLE SCRATCH DAMAGE TO FRAME CAP REINFORCING STRAPS PN 85333501-139/-137/-134 AT X636.0 AND BETWEEN STR. 21S-23S. REF. 008.53-22.09
- [SDR 7C7A2022031700005](https://openairdocs.org/sdr/7C7A2022031700005), Mar 17, 2022: SKIN. CRACKED. CRACK DAMAGE TO UPPER SKIN PANEL PN 85740016 OF RH AILERON ASSY. PN 85740002-003 AT YW 491 ALONG THE FRONT SPAR. REF. 008.27-22.03
- [SDR 7C7A2022031700004](https://openairdocs.org/sdr/7C7A2022031700004), Mar 17, 2022: STRAP. CHAFED. CHAFE DAMAGE TO TOP STRAP PN 85322331 OF BOTTOM FRAME ASSEMBLY PN 8533086 AT X510 BETWEEN STR. 23S AND 24S. REF. 008.53-22.05
- [SDR 7C7A2022031700003](https://openairdocs.org/sdr/7C7A2022031700003), Mar 17, 2022: FRAME. CHAFED. CHAFE DAMAGE TO THE CENTER FUSELAGE FRAME X253.40 PN 85320575. REF. 008.53-22.03
- [SDR 7C7A2022031700002](https://openairdocs.org/sdr/7C7A2022031700002), Mar 17, 2022: FRAME. CHAFED. CHAFE DAMATE TO RH FRAME X531.50 PN 85330133 INBD FLANGE TO STRAP PN 85322331-179 AT STR. 23S. REF. ECO 008.53-22.04
- [SDR 7C7A2021100100019](https://openairdocs.org/sdr/7C7A2021100100019), Oct 12, 2021: DOOR. DENTED. GROUND DAMAGE TO AIRSTAIR DOOR SKIN. PN 85210003-001. ACCEPTABLE ALLOWANCE FOR 300 HRS UNTIL PERMANENT REPAIR IS REQUIRED. IAW ECO 008.52-21.03
- [SDR 7C7A2018081700017](https://openairdocs.org/sdr/7C7A2018081700017), Aug 17, 2021: WINDSHIELD. CRACKED. FIRST OFFICERS WINDSHIELD CRACKED
- [SDR 7C7A2019112620522](https://openairdocs.org/sdr/7C7A2019112620522), Nov 22, 2019: PSEU. ABNORMAL. ALL GEAR DOORS OPENED AFTER GEAR EXTENSION. DOOR LIGHTS WERE OFF. CAME BACK ON, DOORS ARE OPEN.
- [SDR 7C7A2019010600472](https://openairdocs.org/sdr/7C7A2019010600472), Jan 6, 2019: THRESHOLD. CORRODED. PAX DOOR THRESHOLD CORROSION. PART REPLACED AT W/C 53-356.
- [SDR 7C7A2019010300471](https://openairdocs.org/sdr/7C7A2019010300471), Jan 3, 2019: SKIN. NICKED. NICKS ON FUSELAGE SKIN AT STA X370.8 ON STR 29S. ECO 008.53-18.54 C/W.
- [SDR 7C7A2018123100470](https://openairdocs.org/sdr/7C7A2018123100470), Dec 31, 2018: SKIN. DENTED. MULTIPLE DENTS LH FUSELAGE SKIN STA X270.5-X291.4 & BTW STR 8P-9P. ECO 008.53-18.55.
- [SDR 7C7A2018123100469](https://openairdocs.org/sdr/7C7A2018123100469), Dec 31, 2018: SKIN. NICKED. BLENDING OF NICKS AT STA X250.00 ABOVE STR 33. ECO 008.53-18.58.
- [SDR 7C7A2018123100468](https://openairdocs.org/sdr/7C7A2018123100468), Dec 31, 2018: SKIN. NICKED. SEVERAL NICKS ON FUSELAGE SKIN BTW X377-396 & BTW STR 30-32P
- [SDR 7C7A2018123100467](https://openairdocs.org/sdr/7C7A2018123100467), Dec 31, 2018: SKIN. DENTED. MULTIPLE DENTS LH FUSE STA 103-110 BTW STIFF 11-12. ECO 008.53-18.57.
- [SDR 7C7A2018123100466](https://openairdocs.org/sdr/7C7A2018123100466), Dec 31, 2018: SKIN. DENTED. DENT RH FUSE AT STA X109. ECO 008.53-18.56
- [SDR 7C7A2018123100465](https://openairdocs.org/sdr/7C7A2018123100465), Dec 31, 2018: SKIN. DENTED. DENT ON MED. ECO 008.52-18.11.
- [SDR 7C7A2018102600455](https://openairdocs.org/sdr/7C7A2018102600455), Sep 27, 2018: LUG. BROKEN. BROKEN LUG.
- [SDR 7C7A2018090700454](https://openairdocs.org/sdr/7C7A2018090700454), Sep 7, 2018: BEAM. CRACKED. BEAM IN NOSE WHEEL WELL CRACKED BEYOND GENERIC RD ALLOWANCES.
- [SDR 7C7A2018020500366](https://openairdocs.org/sdr/7C7A2018020500366), Feb 5, 2018: LIGHT. INOPERATIVE. EMERGENCY EXIT BACKLIGHTING OVER AIRSTAIR INOP.
- [SDR 7C7A2018013000359](https://openairdocs.org/sdr/7C7A2018013000359), Jan 30, 2018: INVERTER. FAILED. STRONG ODOR EMANATING FROM THE COCKPIT. REPLACED THE INVERTER.
- [SDR 7C7A2017101300338](https://openairdocs.org/sdr/7C7A2017101300338), Oct 13, 2017: PLATE. DAMAGED. RIGHT WING LADDER PLATE UNDER FUEL PANEL 624BT, HAD 3 SCREW HOLES ELONGATED. REPAIRED IAW ECO 008.57-17.03.
- [SDR 7C7A2017101300337](https://openairdocs.org/sdr/7C7A2017101300337), Oct 13, 2017: SKIN. DAMAGED. DAMAGE TO FUSELAGE SKIN AT BS 322 AND BETWEEN STRINGERS 29R AND 30R. REPAIRED IAW ECO 008.53-17.29.
- [SDR 7C7A2017082600335](https://openairdocs.org/sdr/7C7A2017082600335), Aug 26, 2017: BATTERY PACK. INOPERATIVE. LOWER EMERGENCY EXIT DOOR LIGHT INOPERATIVE, REMOVED AND REPLACED BATTERY POWER SUPPLY BOX
- [SDR 7C7A2016121600273](https://openairdocs.org/sdr/7C7A2016121600273), Dec 16, 2016: WINDOW FRAME. CORRODED. AT BS 302, WINDOW FRAME CORRODED. REPLACED IAW SRM 51-40-05.
- [SDR 7C7A2016120500269](https://openairdocs.org/sdr/7C7A2016120500269), Dec 5, 2016: STRINGER. CORRODED. STRINGER 31L BETWEEN BS 467 & 510 CORRODED. REPAIRED IAW SRM AND RD8-53-1834.
- [SDR 7C7A2016120500268](https://openairdocs.org/sdr/7C7A2016120500268), Dec 5, 2016: THRESHOLD. CORRODED. PAX DOOR THRESHOLD CORRODED. REMOVED AND REPLACED AND REPAIRED SUPPORT OF THRESHOLD REF. RD8-53-8421 AND SRM WC 53-136
- [SDR 7C7A2016112900267](https://openairdocs.org/sdr/7C7A2016112900267), Nov 29, 2016: SKIN. DENTED. DENT DAMAGE TO LT FUSELAGE SKIN UNDER THE ICE SHIELD. REPAIRED IAW RD8-53-14891.
- [SDR 7C7A2016112900266](https://openairdocs.org/sdr/7C7A2016112900266), Nov 29, 2016: SKIN. DENTED. DENT TO THE PAX DOOR BEYOND SRM LIMITS. REPAIRED IAW RD8-52-1475
- [SDR 7C7A2016112500264](https://openairdocs.org/sdr/7C7A2016112500264), Nov 25, 2016: LIGHT. INOPERATIVE. R FWD OUTSIDE EMERGENCY LIGHT OUT. REPLACED BULB, OPS CHECK GOOD.
- [SDR 7C7A2016112400263](https://openairdocs.org/sdr/7C7A2016112400263), Nov 24, 2016: FIREWALL. DAMAGED. CHAFING DAMAGE TO LOWER COWLING DECKING. REPAIRED WITH PATCH IAW 8-71-1196 AND ECO008-54-16-07
- [SDR 7C7A2016071200249](https://openairdocs.org/sdr/7C7A2016071200249), Jul 12, 2016: FIREWALL. DAMAGED. RIGHT FIREWALL HAS ACRING DAMAGE, DISCOVERED DURING INSPECTION IAW SB 8-24-92. REPAIR BY CUTTING OUT DAMAGE HFEC INSPECTION AND INSTALLATION OF PATCH IAW 54-382
- [SDR 7C7A2016042501](https://openairdocs.org/sdr/7C7A2016042501), Apr 25, 2016: DOOR. DENTED. DENT DAMAGE TO PAX DOOR. TEMP ALLOWANCE IAW RD 8-52-1466 ISSUE 1.
- [SDR 7C7A2016010801](https://openairdocs.org/sdr/7C7A2016010801), Jan 7, 2016: BATTERY PACK. DISCHARGED. ROW 4 EXIT LIGHTS FLICKERED DURING FLIGHT, ALL EXIT LIGHTS ILLUMINATED BRIEFLY. MOSTLY OVERHEAD LIGHT AT 4. R & R PS2 BATTERY PACK FOR ROW 4. OPERATIONS CHECKED
- [SDR 7C7A20151123097](https://openairdocs.org/sdr/7C7A20151123097), Nov 21, 2015: OIL COOLER. LEAKING. APPROX 1 HR INTO THE FLIGHT, THE MASTER WARNING LT INTERMITTENTLY FLASHED. A COUPLE MINUTES LATER WE NOTICED NR 1 ENG OIL PRESS FLUCTUATIONS, 60-45 APPROX, WE F

All 63: https://openairdocs.org/deregistered/N885EA-2025-07-23/reports.md

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20210817008639I](https://openairdocs.org/incident/20210817008639I), Aug 17, 2021: Dehavilland DHC-8-106 (N885EA), Anchorage, AK, Minor damage. On departure with the aircraft leveling off at 6000 feet, the flight crew noticed that the copilot's windshield began to crack. The crew requested a return to…
- [Incident 20150512007009I](https://openairdocs.org/incident/20150512007009I), May 12, 2015: Dehavilland DHC-8-106 (N885EA), Anchorage, AK, No damage. On 5/12/2015 at 1445 local time N885EA, a corvus airlines owned DHC-8-106 departed Anchorage, AK for kodiak, AK. On a scheduled FAR 121 filight. Wx was clear,…

## Other aircraft with N885EA

- [Cancelled 2007-02-16](https://openairdocs.org/deregistered/N885EA-2007-02-16): Dehavilland DHC-6 TWIN OTTER, S/N 454, built 1975. Exported to Canada. Owner: [Era Aviation Inc](https://openairdocs.org/faa-owner/ERA%20AVIATION%20INC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage)

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