# N886EA: 1990 Boeing / Dehavilland DHC-8-103, registration cancelled 2023-08-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 2, 2023 - Exported to: Canada - Status when cancelled: Valid registration - Airframe: [Boeing / Dehavilland DHC-8-103](https://openairdocs.org/model/boeing-dehavilland-dhc-8-103) (registry code 1386005) - 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: 215 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: March 28, 2012 - Certificate issued: November 2, 2020 - Last registry action: April 1, 2023 - Mode S code: AC3484 - Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N886EA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=886EA - Page: https://openairdocs.org/deregistered/N886EA-2023-08-02 From the FAA registry file of November 7, 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 Boeing / Dehavilland DHC-8-103: https://openairdocs.org/model/boeing-dehavilland-dhc-8-103.md ## Service difficulty reports (88, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2023F00008](https://openairdocs.org/sdr/2023F00008), Dec 29, 2022: PUMP. FAULTED. #1 STBY HYD PUMP HOT LIGHT ILLUMINATED IN FLIGHT. REPLACED LH STBY JPUMP WITH REPAIRED UNIT. - [SDR 7C7A2022122980050](https://openairdocs.org/sdr/7C7A2022122980050), Dec 28, 2022: PUMP. OVERTEMP. #1 STBY HYD PUMP HOT LIGHT ILLUMINATED IN FLIGHT - [SDR 7C7A2022122000041](https://openairdocs.org/sdr/7C7A2022122000041), Dec 20, 2022: ANNUNCIATOR. INOPERATIVE. CHECK FIRE DET WARNING LIGHT WONT STAY LATCHED. R&R WARNING ANNUNCIATOR PANEL - [SDR 7C7A2022122000040](https://openairdocs.org/sdr/7C7A2022122000040), Dec 20, 2022: WARNING MESSAGE. ILLUMINATED. DURING CLIMB OUT OF ANC THE CHECK FIRE DTC LIGHT ON THE MASTER WARNING PANEL BECAME INOPERATIVE. THE CREW ATTEMPTED TO FIX THE PROBLEM WITH PROCEDURES ADVISED D - [SDR 7C7A2022120500032](https://openairdocs.org/sdr/7C7A2022120500032), Dec 1, 2022: FLIGHT RECORDER. FAULTED. FLT DATA RECORDER CAUTION LIGHT ILLUMINATED PRIOR TO TAKE OFF. - [SDR 7C7A2021100800019](https://openairdocs.org/sdr/7C7A2021100800019), Oct 8, 2021: NONE. NONE. FOUND LOOSE CANNON PLUG ON POWER SUPPLY 3352-PS1, 3351-PS3 AND 3351-PS4 TIGHTENED AS REQUIRED POWER DHC-8-100 AMM 33-51-00 OPS CHECK GOOD. NRW-23529 - [SDR 7C7A2020040100023](https://openairdocs.org/sdr/7C7A2020040100023), Mar 31, 2020: SKIN. DENTED. RIGHT WING, INBOARD FLIGHT SPOILER, UPPER SURFACE HAS 5 DENTS. - [SDR 7C7A2020032700021](https://openairdocs.org/sdr/7C7A2020032700021), Mar 27, 2020: SKIN. DEBONDED. LEFT INBOARD GROUND SPOILER ASSEMBLY (P/N 85770001-007) HAS DENT (7 ON UPPER SURFACE) AND DIS-BOND DAMAGE. - [SDR 7C7A2020032700020](https://openairdocs.org/sdr/7C7A2020032700020), Mar 26, 2020: SKIN. DEBONDED. LEFT INBOARD FLIGHT SPOILER ASSEMBLY (P/N 85770012-001) HAS DENT (4 ON LOWER SURFACE AND 11 ON UPPER SURFACE) AND DIS-BOND DAMAGE. - [SDR 7C7A2020032700019](https://openairdocs.org/sdr/7C7A2020032700019), Mar 26, 2020: FITTING. WORN. LEFT ELEVATOR TRIM TAB, INBOARD SIDE, DRIVE FITTING (P/N: 85520205) IS WORN. - [SDR 7C7A2020032700018](https://openairdocs.org/sdr/7C7A2020032700018), Mar 26, 2020: SKIN. DENTED. THREE DENTS WERE FOUND ON THE LEFT ELEVATOR SPRING TAB, UPPER SURFACE. - [SDR 7C7A2020032400011](https://openairdocs.org/sdr/7C7A2020032400011), Mar 24, 2020: SKIN. DEBONDED. MULTIPLE DENTS (23) AND DIS-BOND DAMAGE NOTED ON RIGHT WING INBOARD GROUND SPOILER UPPER SURFACE SKIN. - [SDR 7C7A2020032400015](https://openairdocs.org/sdr/7C7A2020032400015), Mar 23, 2020: SKIN. DEBONDED. MULTIPLE DENTS (1 ON UPPER SURFACE AND 2 ON LOWER SURFACE) AND DIS-BOND DAMAGE NOTED ON RIGHT WING, OUTBOARD FLIGHT SPOILER, SKIN. - [SDR 7C7A2020032400013](https://openairdocs.org/sdr/7C7A2020032400013), Mar 23, 2020: SKIN. DEBONDED. MULTIPLE DENTS (8) AND DIS-BOND DAMAGE NOTED ON LEFT WING, OUTBOARD GROUND SPOILER, SKIN UPPER SURFACE. - [SDR 7C7A2020032400012](https://openairdocs.org/sdr/7C7A2020032400012), Mar 23, 2020: SKIN. DEBONDED. MULTIPLE DENTS (8 UPPER SURFACE AND 1 LOWER SURFACE) AND DIS-BOND DAMAGE NOTED ON LEFT WING, OUTBOARD FLIGHT SPOILER, SKIN. - [SDR 7C7A2020032500016](https://openairdocs.org/sdr/7C7A2020032500016), Mar 19, 2020: SKIN. CRACKED. A SMALL (0.22 IN LONG) CRACK WAS FOUND ON THE LEFT ELEVATOR, UPPER SURFACE, INBOARD CORNER, ALONG TRAILING EDGE (P/N: 85520057) - [SDR 7C7A2020032400014](https://openairdocs.org/sdr/7C7A2020032400014), Mar 16, 2020: SHROUD. CHAFED. LEFT NACELLE, CENTER EXHAUST SHROUD, LOWER HALF HAS 2 CHAFED HOLES. - [SDR 7C7A2020032300003](https://openairdocs.org/sdr/7C7A2020032300003), Mar 13, 2020: SKIN. SCRATCHED. BAGGAGE DOOR, EXTERNAL SKIN, HAS 5 SCRATCHES ON IT. - [SDR 7C7A2020032400010](https://openairdocs.org/sdr/7C7A2020032400010), Mar 11, 2020: FITTING. WORN. LEFT WING, INBOARD FLAP ASSEMBLY (P/N: 85750002-005), #2 TRACK FITTING HAS RUBBING-WEAR DAMAGE (P/N: 85750302). - [SDR 7C7A2020032600017](https://openairdocs.org/sdr/7C7A2020032600017), Mar 10, 2020: FIREWALL. CRACKED. LEFT NACELLE, INBOARD SIDE, LOWER SHEAR WEB (FIREWALL, P/N: 85410594-111) HAS A CRACK (0.550 INCHES LONG). - [SDR 7C7A2020032400008](https://openairdocs.org/sdr/7C7A2020032400008), Mar 10, 2020: SEAT TRACK. CORRODED. RIGHT OUTBOARD SEAT TRACK BETWEEN X445.50 AND X467.00 HAS CORROSION DAMAGE (P/N: 85330507). - [SDR 7C7A2020032300005](https://openairdocs.org/sdr/7C7A2020032300005), Mar 10, 2020: SKIN PANEL. GOUGED. SKIN PANEL ON LEFT SIDE OF FUSELAGE HAS A DENT WITH A GOUGE. X387.35-X405.737 AND STR. 30P-31P - [SDR 7C7A2020032300004](https://openairdocs.org/sdr/7C7A2020032300004), Mar 10, 2020: SKIN. GOUGED. FUSELAGE SKIN PANEL ON RIGHT SIDE HAS GOUGE DAMAGE. - [SDR 7C7A2020032400007](https://openairdocs.org/sdr/7C7A2020032400007), Mar 9, 2020: SEAT TRACK. DAMAGED. RIGHT OUTBOARD SEAT TRACK BETWEEN X270.50 AND X370.80 HAS PITTING AND GOUGE DAMAGE (P/N: 85320701). - [SDR 7C7A2020032300006](https://openairdocs.org/sdr/7C7A2020032300006), Mar 9, 2020: SHEAR WEB. CORRODED. CORROSION DAMAGE WAS NOTED ON AFT CENTER FUSELAGE LEFT SIDE SHEAR WEB (CARGO FLOOR). - [SDR 7C7A201906050507](https://openairdocs.org/sdr/7C7A201906050507), Jun 4, 2019: HANDLE. LOOSE. TESTING FUEL PULL OFF HANDLE, INTERMITTENTLY VALVE DOES NOT CLOSE AND/OR AFT EXTINGUISHER BOTTLE DOES NOT ARM. SECURED LOOSE T-HANDLE SWITCH PACK MOUNTING HARDW - [SDR 7C7A2019031300491](https://openairdocs.org/sdr/7C7A2019031300491), Mar 13, 2019: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHT INOPERABLE. BATTERY POWER SUPPLY REMOVED AND REPLACED REFERENCING 7H-NRW-6949 - [SDR 7C7A2018052400444](https://openairdocs.org/sdr/7C7A2018052400444), May 24, 2018: RELAY. HOT. ELECTRICAL SMELL COMING FROM CLOSET IN CABIN. - [SDR 7C7A2018040900392](https://openairdocs.org/sdr/7C7A2018040900392), Apr 11, 2018: SKIN. DENTED. PERMANENT REPAIR FOR 2 DENTS RT FUSELAGE SKIN PANEL BTW X240.5-X253.4 AND STR 31S-32S. COMPLETED WITH ECO 008.53-18.13 AND RD 8-53-15612. - [SDR 7C7A2018040900340](https://openairdocs.org/sdr/7C7A2018040900340), Apr 6, 2018: DOOR TRACK. CHAFED. CHAFE DAMAGE TO FWD CARGO DOOR TRACK PN:85230460, PERMANENT ALLOWANCE FOR CHAFE DAMAGE PROVIDED BY ECO 008.52-18.07 AND RD 8-52-1439. - [SDR 7C7A2018041900399](https://openairdocs.org/sdr/7C7A2018041900399), Apr 4, 2018: WINDOW FRAME. CORRODED. LEFT PASSENGER CABIN WINDOW FRAME AT BS 436.5 CORRODED BEYOND LIMITS. THE WINDOW FRAME WAS REPLACED IAW 51-42-05. - [SDR 7C7A2018041900398](https://openairdocs.org/sdr/7C7A2018041900398), Apr 4, 2018: WINDOW FRAME. CORRODED. LEFT PASSENGER CABIN WINDOW FRAME AT BS 396.74 FOUND CORRODED BEYOND LIMITS. REPLACED WINDOW FRAME IAW SRM 51-42-05. - [SDR 7C7A2018041900397](https://openairdocs.org/sdr/7C7A2018041900397), Apr 4, 2018: WINDOW FRAME. CORRODED. LEFT PASSENGER CABIN WINDOW FRAME AT BS 282.40 IS CORRODED BEYOND LIMITS. THE WINDOW FRAME REPLACED IAW SRM 51-42-05. - [SDR 7C7A2018040900388](https://openairdocs.org/sdr/7C7A2018040900388), Apr 2, 2018: SKIN. DENTED. 3 DENTS TO FORWARD LT FUSELAGE SKIN OF AIRCRAFT. STA X167-X182 BETWEEN STR 26P-27P. COMPLETED PERMANENT REPAIR WITH ECO 008.53-17.27 AND RD 8-53-15288. - [SDR 7C7A2018040900389](https://openairdocs.org/sdr/7C7A2018040900389), Mar 29, 2018: SKIN. DEBONDED. DISBOND DAMAGE TO CENTER FUSELAGE LOWER SKIN PN:85330022 BETWEEN X445.5-X488.5 AND STR. 31S-33. COMPLETED REPAIR WITH ECO 008.53-18.12 AND RD 8-53-15613. - [SDR 7C7A2018030700369](https://openairdocs.org/sdr/7C7A2018030700369), Mar 6, 2018: WARNING LIGHT. FALSE ACTIVATION. AFTER TAKEOFF, AND GEAR UP SELECTED, GEAR & GEAR DOOR LIGHTS WENT OUT THEN THE LT DOOR LIGHT ILLUMINATED. CYCLED THE GEAR DOWN THEN UP AND NO FURTHER LIGHT. - [SDR 7C7A2018013000358](https://openairdocs.org/sdr/7C7A2018013000358), Jan 27, 2018: BULB. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE. REPLACED THE BULB. - [SDR 7C7A201709020206](https://openairdocs.org/sdr/7C7A201709020206), Sep 1, 2017: BATTERY. DISCHARGED. MID CABIN EXIT AND EMERGENCY LIGHTS INOPERATIVE. FOUND THE BATTERY DISCHARGED. - [SDR 7C7A2016062900248](https://openairdocs.org/sdr/7C7A2016062900248), Jun 29, 2016: PROXIMITY SENSOR. MALFUNCTIONED. NOSE LANDING GEAR NORMAL INDICATOR RED WITH GEAR EXTENDED AND HANDLE LIGHT ILLUMINATED. ALT GEAR INDICATOR LIGHTS ALL GREEN. PSEU MEMORY RECALL REVEALED NLG DOW - [SDR 7C7A201602140](https://openairdocs.org/sdr/7C7A201602140), Apr 2, 2016: BATTERY PACK. DISCHARGED. SOME EMERGENCY LIGHTING INOPERATIVE. - [SDR 7C7A2015123028](https://openairdocs.org/sdr/7C7A2015123028), Dec 30, 2015: RUDDER. DENTED. REPAIR FOR DENT DAMAGE TO LOWER TRAILING RUDDER, PN 85540002 AN CAP0086. REPAIRED IAW ECO 008 55-15 06. - [SDR 7C7A2015123101](https://openairdocs.org/sdr/7C7A2015123101), Dec 30, 2015: RUDDER. DENTED. REPAIR FOR DENT DAMAGE TO LOWER TRAILING RUDDER, PN 85540002 AN CAP0086. REPAIRED IAW ECO 008 55 15 06. - [SDR 7C7A20151104095](https://openairdocs.org/sdr/7C7A20151104095), Nov 4, 2015: PANEL. CORRODED. CORROSION FOUND ON LADDER PLATE PANEL, OUT OF LIMITS OF GENERIC RD 8-57-320. REPAIRED IAW RD 8-57-7157. - [SDR 7C7A20151104093](https://openairdocs.org/sdr/7C7A20151104093), Nov 4, 2015: STRUCTURE. DENTED. MULTIPLE DENT DAMAGE IN FWD FUSELAGE. PERMANENT ALLOWANCE IAW RD 8-53-14396. - [SDR 7C7A20151028092](https://openairdocs.org/sdr/7C7A20151028092), Oct 28, 2015: DUCT. GOUGED. GOUGE DAMAGE IN CTR SHROUD ASSEMBLY EXHAUST SYS. - [SDR 7C7A20151215100](https://openairdocs.org/sdr/7C7A20151215100), Oct 15, 2015: PANEL. DAMAGED. LADDER PLATE FOR 624CT AFT INBD SCREW HOLE IS ELONGATED AT STATION YW335, RD 8-57-7149. - [SDR 7C7A20151015090](https://openairdocs.org/sdr/7C7A20151015090), Oct 14, 2015: SKIN. DENTED. DENT LT SIDE FORE RUDDER SKIN. - [SDR 7C7A20151014089](https://openairdocs.org/sdr/7C7A20151014089), Oct 14, 2015: SKIN. DAMAGED. FUSELAGE SKIN WAFFLED AND DENTED. - [SDR ERAA201409180055](https://openairdocs.org/sdr/ERAA201409180055), Sep 17, 2014: SEQUENCE VALVE. DEFECTIVE. NOSE WHEEL FAILED TO EXTEND WHEN GEAR SELECTED DOWN. AFTER GO-AROUND, 30-40 SECS, GEAR CAME DOWN ON ITS OWN. R AND R NLG MECHANICAL SEQUENCE VALVE, BLED AND LEA - [SDR ERAA201408250051](https://openairdocs.org/sdr/ERAA201408250051), Aug 23, 2014: BATTERY PACK. DISCHARGED. LOWER EMER LIGHTS DO NOT WORK. R & R FWD RT EMER BATTERY PACK ABOVE ROW 1CD. OPERATIONAL CHECKED GOOD, OK FOR SERVICE. All 88: https://openairdocs.org/deregistered/N886EA-2023-08-02/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DCA12IA141](https://openairdocs.org/ntsb/DCA12IA141), Sep 5, 2012: De Havilland DHC8 (N886EA), Soldotna, AK, incident, no damage. Probable cause: an in-flight loss of control due to the flight crew's inattention to airspeed, pitch attitude, and engine power during the climb leading to an aerodynamic stall. Contributing to the incident was the… ## FAA accident and incident reports (1) 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 20120905023859I](https://openairdocs.org/incident/20120905023859I), Sep 5, 2012: Boeing / Dehavilland DHC-8-103 (N886EA), Anchorage, AK, Minor damage. Era 874, dash 8, departed ted stevens international airport, Anchorage, AK on a scheduled flight to homer, AK with 12 passengers and three crewmembers. The… ## Other aircraft with N886EA - [Cancelled 2007-06-11](https://openairdocs.org/deregistered/N886EA-2007-06-11): Dehavilland DHC-6-300, S/N 756. Exported to Canada. Owner: [Alberta Aircraft Leasing Inc](https://openairdocs.org/faa-owner/ALBERTA%20AIRCRAFT%20LEASING%20INC), [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas) --- 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.