# N887EA: 1993 Dehavilland DHC-8-106, registration cancelled 2026-03-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 4, 2026 - Exported to: Canada - Status when cancelled: Valid registration - 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: 351 - Year built: 1993 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: April 6, 2013 - Certificate issued: December 16, 2025 - Last registry action: December 16, 2025 - Mode S code: AC383B - 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/N887EA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=887EA - Page: https://openairdocs.org/deregistered/N887EA-2026-03-04 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 Dehavilland DHC-8-106: https://openairdocs.org/model/dehavilland-dhc-8-106.md ## Service difficulty reports (85, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 7C7A2025050700016](https://openairdocs.org/sdr/7C7A2025050700016), May 5, 2025: SWITCH. FAILED. #2 ENG HYD PUMP CAUTION LIGHT CAME ON IN FLIGHT. - [SDR 7C7A2025030900012](https://openairdocs.org/sdr/7C7A2025030900012), Mar 9, 2025: TOILET. CLOGGED. LAVATORY "FLUSH" INTERMITTENTLY INOP - [SDR 7C7A2025030900011](https://openairdocs.org/sdr/7C7A2025030900011), Mar 9, 2025: GAUGE. INTERMITTENT. #2 ITT GAUGE INTERMITTENTLY INOP - [SDR 7C7A2025030900010](https://openairdocs.org/sdr/7C7A2025030900010), Mar 9, 2025: WHEEL. OUT OF BALANCE. NOSE WHEEL SHIMMY ON TAKEOFF. - [SDR 7C7A2025012800004](https://openairdocs.org/sdr/7C7A2025012800004), Jan 25, 2025: POWER SUPPLY. INOPERATIVE. CENTER AISLE MAIN ENTRANCE DOOR CEILING EMERGENCY EXIT SIGN INOP. - [SDR 7C7A2025011300001](https://openairdocs.org/sdr/7C7A2025011300001), Jan 13, 2025: CLAMP. LOOSE. RIGHT, #3 DE-ICE BOOT DOES NOT INFLATE. DE-ICE LIGHT DOES NOT ILLUMINATE. - [SDR 7C7A2023050400032](https://openairdocs.org/sdr/7C7A2023050400032), May 2, 2023: EEC. ERRATIC. #1 ENG MOMENTARILY HAD PROP RPM DECREASE FROM MIN AND TORQUE INCREASED 4 PERCENT. - [SDR 7C7A2023040600025](https://openairdocs.org/sdr/7C7A2023040600025), Apr 1, 2023: PCU. FAILED. THIS IS FILLING IN DETAILS FOR SDR FILED ON 4/1/2023 7C7A2023040100020 ENGINE TORQUE INCREASED 3% UNCOMMAND IN FLIGHT. REPEATED 2 MORE TIMES R/R #1 PCU - [SDR 7C7A2023040100020](https://openairdocs.org/sdr/7C7A2023040100020), Apr 1, 2023: UNKNOWN. UNKNOWN. PLACE HOLDER FOR #1 ENG. TORQUE INCREASE AND RPM DECREASE. FLIGHT WAS DIVERTED BACK TO ANC A/C IS STILL DOWN FOR MX - [SDR 7C7A2023031600016](https://openairdocs.org/sdr/7C7A2023031600016), Mar 16, 2023: HORN. INOPERATIVE. R ELEVATOR HORN HEAT CAUTION LIGHT ILLUMINATED. OHM CHECK BAD, R/R R/H ELEVATOR HORN - [SDR 7C7A2023022000014](https://openairdocs.org/sdr/7C7A2023022000014), Feb 20, 2023: TAB. CRACKED. IN PROCESS OF REPAIRIND DENTED SKIN REAR SPAR OF ELEVATOR TRIM TAB FOUND CRACKED - [SDR 7C7A2023020100012](https://openairdocs.org/sdr/7C7A2023020100012), Feb 1, 2023: SEAT TRACK. CORRODED. RH IB SEAT TRACK FOUND CORRODED BEYOND BTW X180 AND X387 - [SDR 7C7A2023012700008](https://openairdocs.org/sdr/7C7A2023012700008), Jan 27, 2023: TORQUE LINK. CORRODED. UPPER TORQUE LINK BUSHING BORE CORRODED. - [SDR 7C7A20230127006](https://openairdocs.org/sdr/7C7A20230127006), Jan 27, 2023: TRUNNION. CORRODED. NLG TRUNNION CAP CORRODED BEYOND LIMITS - [SDR 7C7A2023012700007](https://openairdocs.org/sdr/7C7A2023012700007), Jan 27, 2023: TRUNNION. CORRODED. NLG TRUNNION CORRODED BEYOND LIMITS. - [SDR 7C7A2022120800036](https://openairdocs.org/sdr/7C7A2022120800036), Dec 8, 2022: WIRE HARNESS. CORRODED. AUTO FEATHER DID NOT ARM WHEN T/O POWER APPLIED. - [SDR 7C7A2022062800023](https://openairdocs.org/sdr/7C7A2022062800023), Jun 28, 2022: DME. SHORTED. DME 1 CIRCUIT BREAKER POPPED WITH HEAVY ELECTRIC FIRE SMELL. - [SDR 7C7A2022041800015](https://openairdocs.org/sdr/7C7A2022041800015), Mar 18, 2022: CABLE ASSY. CORRODED. AUTO FEATHER FAILED TO ARM ON TAKEOFF. TAKE OFF ABORTED. FOUND CORRODED CANNON PLUG 9811-P14 AT R/H WING ROOT. THE PROBLEM WAS AT FIRST GLANCE THE CANNON PLUG L - [SDR 7C7A2021012600001](https://openairdocs.org/sdr/7C7A2021012600001), Jan 26, 2021: SKIN. DENTED. DENT IN FUSELAGE SKIN 85330131 BETWEEN F.S. X580.5 AND X600.0, STRS 23S AND 24S. DENT DIMENSIONS ARE 3.0"X1.75"X0.075". - [SDR 7C7A2019121600524](https://openairdocs.org/sdr/7C7A2019121600524), Dec 16, 2019: STOP FITTING. DAMAGED. DAMAGE TO THE ELEVATOR SPRING TAB STOP BRACKET FITTING (P/N 85520090). A PERMANENT REPAIR FOR DAMAGE TO THE ELEVATOR SRING TAB STOP BRACKET FITTING CONSISTS OF - [SDR 7C7A2019060300506](https://openairdocs.org/sdr/7C7A2019060300506), May 30, 2019: CONTROL PANEL. INTERMITTENT. EMERGENCY LIGHTS, GALLEY LIGHT, F/A PANEL LIGHTS, LIQUID WARMER LIGHTS FLICKERING INTERMITTENTLY. - [SDR 7C7A2018110300456](https://openairdocs.org/sdr/7C7A2018110300456), Nov 3, 2018: SWITCH. STICKS. EMERGENCY LIGHT SWITCH ON F/A PANEL IS STICKING AND LIGHTS ON SWITCH DO NOT WORK. - [SDR 7C7A2018020100366](https://openairdocs.org/sdr/7C7A2018020100366), Feb 1, 2018: SKIN. DENTED. MULTIPLE DENTS TO THE LT FUSELAGE SKIN PANEL BETWEEN BS 270.50 - 291.40 AND STRINGER 11 - 12L. REPAIRED THE SKIN AND WITHIN LIMITS IAW RD 8-53-15535, INSPECTED - [SDR 7C7A2018020100365](https://openairdocs.org/sdr/7C7A2018020100365), Feb 1, 2018: SKIN. DENTED. DENT DAMAGE TO THE RIGHT NACELLE, LEFT ENGINE COWLING CENTER PANEL. REMOVED DAMAGED AREA, CHECKED FOR CRACK INDICATIONS, AND INSTALLED AN EXTERNAL REPAIR DOUBLE - [SDR 7C7A2018020100364](https://openairdocs.org/sdr/7C7A2018020100364), Feb 1, 2018: SKIN. SCRATCHED. SCRATCH ON LOWER FUSELAGE SKIN, AFT OF STA X424.124, ALONG STA 31P. BLENDED AND POLISHED TO REMOVE DAMAGE TO THE LIMITS STATED IN RD 8-53-15536, INSPECTED THE E - [SDR 7C7A2018020100363](https://openairdocs.org/sdr/7C7A2018020100363), Feb 1, 2018: HANDLE. DENTED. MULTIPLE DENTS AND GOUGE DAMAGE TO THE CARGO DOOR HANDLE HOUSING (P/N 85230221). REPAIRED IAW RD 8-52-1563 AND ECO 008.52-18.02. - [SDR 7C7A2018020100362](https://openairdocs.org/sdr/7C7A2018020100362), Feb 1, 2018: SKIN. DAMAGED. DAMAGE ON THE RIGHT VERTICAL STABILIZER, UPPER SKIN PANEL P/N 85530012 BETWEEN RIBS 8 AND 9, AFT OF THE ACCESS PANEL CUTOUT. REMOVED DAMAGE , INSPECTED THE AREA - [SDR 7C7A2018013100361](https://openairdocs.org/sdr/7C7A2018013100361), Jan 31, 2018: SKIN. DENTED. MULTIPLE DENTS ON LEFT OTBD GROUND SPOILER UPPER SKIN. REPAIRED AND PROTECTING BARE METAL IAW ECO 008.57-18.03. - [SDR 7C7A2018013100360](https://openairdocs.org/sdr/7C7A2018013100360), Jan 31, 2018: SKIN. DENTED. MULTIPLE DENTS AND DEBONDING DAMAGE FOUND TO RIGHT OTBD GROUND SPOILER UPPER SKIN. REPAIRED AND PROTECTING BARE METAL IAW ECO 008.57-18.02. - [SDR 7C7A201801300359](https://openairdocs.org/sdr/7C7A201801300359), Jan 30, 2018: SKIN. DAMAGED. DAMAGE FOUND ON THE RIGHT ELEVATOR UPPER SKIN. REPAIRED IAW ECO 008.55-18-01. - [SDR 7C7A2018013000357](https://openairdocs.org/sdr/7C7A2018013000357), Jan 30, 2018: SKIN. DENTED. DAMAGE TO THE UPPER EDGE OF THE OUTER SKIN OF THE CARGO DOOR. REMOVED DAMAGE, INSPECTED FOR CRACKS, AND PROTECTED THE REPAIR AREAS WITH CORROSION INHIBITING COM - [SDR 7C7A2018012500356](https://openairdocs.org/sdr/7C7A2018012500356), Jan 19, 2018: SPOILER PANEL. DENTED. TWO DENTS ON RIGHT HAND INBOARD FLIGHT SPOILER. ONE WITH DISBOND. REPAIRED IAW ECO 008.57-18.01. - [SDR 7C7A2018012500355](https://openairdocs.org/sdr/7C7A2018012500355), Jan 19, 2018: SKIN PANEL. DENTED. DENT AND SCRATCH DAMAGE TO BOTTOM FUSELAGE SKIN PANEL (P/N 85320106) BETWEEN FRAME STATIONS X253.4 - X312.35 AND STRINGERS 31P - 33P. REPAIRED IAW ECO 008.53-18 - [SDR 7C7A2018012500354](https://openairdocs.org/sdr/7C7A2018012500354), Jan 19, 2018: SKIN PANEL. CHAFED. CHAFE DAMAGE TO THE OUTER SKIN (P/N 85230002) OF THE BAGGAGE DOOR ASSEMBLY (P/N 85230400-007) BELOW THE LOWER DOOR STOP AND BETWEEN X554.0 - X564.5. REPAIRED IA - [SDR 7C7A2018012500353](https://openairdocs.org/sdr/7C7A2018012500353), Jan 18, 2018: SKIN PANEL. DENTED. DENT AND OIL-CANNING DAMAGE ON SKIN PANEL BETWEEN X182.00 - X201.15 AND BETWEEN STRINGERS 23S - 24S. REPAIRED IAW ECO 008.53-18.03. - [SDR 7C7A2018012500352](https://openairdocs.org/sdr/7C7A2018012500352), Jan 15, 2018: SKIN PANEL. DENTED. MULTIPLE DENTS IN THE AIRSTAIR DOOR OUTER SKIN, P/N 85210021, ABOVE DOOR STOP 4. REPAIRED IAW ECO 008.52-18.01. - [SDR 7C7A2017112800348](https://openairdocs.org/sdr/7C7A2017112800348), Nov 28, 2017: BATTERY PACK. DISCHARGED. EMERGENCY EXIT SIGN LIGHT INOPERATIVE AT ROW 3 RIGHT. THE BATTERY PACK WAS FOUND DISCHARGED. - [SDR 7C7A2017051600327](https://openairdocs.org/sdr/7C7A2017051600327), May 16, 2017: BATTERY PACK. DISCHARGED. RT FRONT EMERGENCY DOOR SIGN LIGHT VERY DIM. R&R EMERGENCY LIGHT BATTERY PACK AT 3351PS2 IAW AMM 33-52-00. OPS CHECKED GOOD. OK FOR CONTINUED SERVICE. - [SDR 7C7A2017042500306](https://openairdocs.org/sdr/7C7A2017042500306), Apr 25, 2017: SEAT TRACK. DAMAGED. ELONGATED HOLES IN THE PILOTS OUTBOARD SEAT TRACK LOCATED BETWEEN X162 AND X164. REPAIRED IAW ECO 008.53-17.23. - [SDR 7C7A2016120200270](https://openairdocs.org/sdr/7C7A2016120200270), Dec 2, 2016: SWITCH. DIRTY. FA COM EMERGENCY SWITCH INTERMITTENT. CLEANED THE SWITCH AND OPS CHECKED GOOD. IAW 23-40-06-02. - [SDR 7C7A2016112000262](https://openairdocs.org/sdr/7C7A2016112000262), Nov 20, 2016: SKIN PANEL. CORRODED. CORROSION UNDER DG ANTENNA. REPAIRED IAW SRM 53-00-16. DOUBLER PN 85335123-109 SEE WC 53-158 - [SDR 7C7A2016112000261](https://openairdocs.org/sdr/7C7A2016112000261), Nov 20, 2016: SKIN PANEL. DENTED. DENT ON LT FUSELAGE TOP. PERMANENT ALLOWANCE IAW ECO 008.53-16.09. - [SDR 7C7A2016112000260](https://openairdocs.org/sdr/7C7A2016112000260), Nov 20, 2016: FLAP TRACK. CORRODED. CORROSION LT FLAP TRACK ATTACHMENT. REPAIRED IAW ECO 008.57-16.16. - [SDR 7C7A2016112000259](https://openairdocs.org/sdr/7C7A2016112000259), Nov 20, 2016: ANGLE. CRACKED. LT CLOSING ANGLE REPLACED FOR REQUIREMENT TO REPLACE ALL WHEN CRACKED. REPLACED PART IAW SRM 51-42-05. - [SDR 7C7A2016112000258](https://openairdocs.org/sdr/7C7A2016112000258), Nov 20, 2016: FLAP TRACK. CORRODED. CORROSION ON RT FLAP TRACK NR 5 AT ATTACHMENT. REPAIRED IAW ECO 008.57-16.15. - [SDR 7C7A2016091900255](https://openairdocs.org/sdr/7C7A2016091900255), Sep 19, 2016: SEAL. LEAKING. NR 2 ENGINE OIL PRESSURE WARNING ILLUMINATED. GAUGE INDICATED 50 PSI. ACCOMPOSHED LOW OIL PRESSURE QRH CHECKLIST. OIL PRESSURE INCREASED SLIGHTLY AND WARNING LI - [SDR 7C7A2016091900254](https://openairdocs.org/sdr/7C7A2016091900254), Sep 19, 2016: LINE. LEAKING. NR 1 ENGINE SHOWS SIGNS OF LEAKING FROM UNIT SPLIT LINE. REMOVED AND REPLACED PCU AND ADAPTOR SEALS. IAW CMM 61-22-00. - [SDR 7C7A2016073100251](https://openairdocs.org/sdr/7C7A2016073100251), Jul 31, 2016: CONNECTOR. DISCONNECTED. MULTIPLE EMERGENCY LIGHTS FOUND INOPERATIVE, REPLACED BATTERIES IN 3851 PS1, PS2, PS3 & 3352 PS2 FOUND CONNECTOR FOR OVERHEAD EMERGENCY LIGHT UNPLUGGED. CONNECT - [SDR 7C7A2016072900252](https://openairdocs.org/sdr/7C7A2016072900252), Jul 29, 2016: SKIN. DENTED. DENT DAMAGE ON THE LT SIDE AFT CENTER FUSELAGE SKIN PANEL BETWEEN BS 531.5 - 539.5 AND STRINGERS 19 - 20L. REPAIRED IAW RD8-53-117. - [SDR 7C7A20150914087](https://openairdocs.org/sdr/7C7A20150914087), Sep 14, 2015: FITTING. WORN. WEAR DAMAGE TO LOWER LUG OF FORE RUDDER FITTING, PN 85540103. REPAIRED IAW RD 8-55-092 & 8-55-2872. All 85: https://openairdocs.org/deregistered/N887EA-2026-03-04/reports.md ## Other aircraft with N887EA - [Cancelled 2007-06-11](https://openairdocs.org/deregistered/N887EA-2007-06-11): Dehavilland DHC-6-300, S/N 467. 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.