# N883EA: 1991 Dehavilland DHC-8-106, registration cancelled 2025-05-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 23, 2025
- 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: 260
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: August 3, 2000
- Certificate issued: September 26, 2024
- Last registry action: September 26, 2024
- Mode S code: AC295F
- 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/N883EA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=883EA
- Page: https://openairdocs.org/deregistered/N883EA-2025-05-23

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 (88, newest 50)

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

- [SDR 7C7A2023080300045](https://openairdocs.org/sdr/7C7A2023080300045), Aug 3, 2023: COMPUTER. FAILED. ON ILS 7L INTO PANC @ X 1000' WITH AIRCRAFT ON DUAL APP A/C VEERED OFF TO THE RIGHT QUICKLY THEN SEEMED TO TRY AND CORRECT, BUT DISCONNECTED AUTOPILOT AT THAT P
- [SDR 7C7A2023051100035](https://openairdocs.org/sdr/7C7A2023051100035), May 11, 2023: LENS. DETACHED. EMERGENCY EXIT SIGN ABOVE AIR STAIR DOOR FELL DOWN
- [SDR 7C7A2023040300023](https://openairdocs.org/sdr/7C7A2023040300023), Apr 3, 2023: ADC. FAILED. DADC DATA INVALID MSG. ON #1 ADC
- [SDR 7C7A2022113000031](https://openairdocs.org/sdr/7C7A2022113000031), Nov 30, 2022: SELECTOR VALVE. INOPERATIVE. LANDING GEAR FAILED TO EXTEND, HAD TO EXTEND MANUALLY. CREW DECLARED AN EMERGENCY. REPLACED LANDING GEAR SELECTOR VALVE.
- [SDR 7C7A2022112800030](https://openairdocs.org/sdr/7C7A2022112800030), Nov 28, 2022: WARNING LIGHT. ILLUMINATED. CREW ATTEMPTED TO LOWER THE LANDING GEAR, RED IN TRANSIT LIGHTS CAME ON BUT NONE OF THE GEAR LOWERED. MANUAL GEAR EXTENSION PERFORMED.
- [SDR 7C7A2022040100014](https://openairdocs.org/sdr/7C7A2022040100014), Mar 29, 2022: NONE. NONE. L/H SEAT TRACK ON CARGO AREA FOUND CORRODED.
- [SDR 7C7A2022040100013](https://openairdocs.org/sdr/7C7A2022040100013), Mar 29, 2022: NONE. NONE. SEVERAL CORROSION SPOTS ON SKIN BTW STA X 487-510 BTW STR 31S-31P (INTERNAL).
- [SDR 7C7A2020031100002](https://openairdocs.org/sdr/7C7A2020031100002), Mar 7, 2020: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS ON IN ARM POSITION
- [SDR 7C7A2019032500494](https://openairdocs.org/sdr/7C7A2019032500494), Mar 9, 2019: SKIN. DENTED. DENTS ON BOTTOM SKIN LT OUTBOARD GROUND SPOILER.
- [SDR 7C7A2019032500493](https://openairdocs.org/sdr/7C7A2019032500493), Feb 28, 2019: PLATE. CRACKED. CRACK ON RT WING LADDER PLATE AT YW 137.0 JUST FORWARD OF STRINGER 6. P/N: 85711069.
- [SDR 7C7A2017072300331](https://openairdocs.org/sdr/7C7A2017072300331), Jul 23, 2017: SMOKE DETECTOR. DEFECTIVE. AFTER START UP A SMOKE LIGHT ILLUMINATED AND WOULD NOT GO OUT. FOUND THE NR 2 CARGO SMOKE DETECTOR STAYS IN TEST MODE. OPEN
- [SDR 7C7A2017042500307](https://openairdocs.org/sdr/7C7A2017042500307), Apr 25, 2017: O-RING. SPLIT. NR 1 HYDRAULIC ISOLATION VALVE LIGHT ON. FLAPS STOPPED DURING RETRACTION AT 4 DEGREES, REMOVED AND REPLACED THE 1 HYD PRESSURE MANIFOLD ASSY IAW MM 29-10-31, BL
- [SDR 7C7A2017040600303](https://openairdocs.org/sdr/7C7A2017040600303), Apr 6, 2017: STRINGER. CORRODED. CORROSION ON STRINGER 31L, BS 222.
- [SDR 7C7A2017040400302](https://openairdocs.org/sdr/7C7A2017040400302), Apr 4, 2017: SKIN. CORRODED. CORROSION UNDER BELLY ANTENNA.
- [SDR 7C7A2017033100300](https://openairdocs.org/sdr/7C7A2017033100300), Apr 1, 2017: STRINGER. CORRODED. CORRODED STRINGER.
- [SDR 7C7A2017032800299](https://openairdocs.org/sdr/7C7A2017032800299), Mar 28, 2017: STRINGER. CORRODED. CORROSION DAMAGE TO STRINGER 31. BLENDED AND REPAIR IAW RD8-53-15145 AND ECO008.53-17.16
- [SDR 7C7A2017031800298](https://openairdocs.org/sdr/7C7A2017031800298), Mar 18, 2017: SKIN PANEL. DENTED. REPAIR FOR DENT, SCRATCH DAMAGE TO EXTERIOR LOWER FUSELAGE SKIN. REPAIRED IAW RD8-53-15090, RD8-53-15104, RD8-53-15115 AND ECO008.53-17.11
- [SDR 7C7A2017031600297](https://openairdocs.org/sdr/7C7A2017031600297), Mar 16, 2017: SKIN. DENTED. DENTS ON SKIN BETWEEN BS 167 - 182, ABOVE AND BELOW STRINGER 24L. REPAIRED IAW RD8-53-15109 AND ECO008.53-17.13
- [SDR 7C7A2017031500296](https://openairdocs.org/sdr/7C7A2017031500296), Mar 15, 2017: FRAME. CHAFED. CHAFE DAMAGE TO LT MACHINED FRAME (P/N 85320575) AT X253.4 AND BETWEEN STR 23P & 24P. REPAIRED IAW RD 8-53-15102 AND ECO008.53-17.12.
- [SDR 7C7A2017031300295](https://openairdocs.org/sdr/7C7A2017031300295), Mar 13, 2017: SKIN. DAMAGED. DENT AND SCRATCH DAMAGE TO RT FUSELAGE SKIN, AFT AND BELOW ICE SHIELD. REPAIRED IAW RD 8-53-15089 AND ECO008.53-17-11.
- [SDR 7C7A2017031100294](https://openairdocs.org/sdr/7C7A2017031100294), Mar 11, 2017: SKIN PANEL. DENTED. DENT DAMAGE REPAIRED TO AFT CARGO DOOR IAW RD8-52-1509 AND ECO008.52-17-01
- [SDR 7C7A2017031100293](https://openairdocs.org/sdr/7C7A2017031100293), Mar 11, 2017: SKIN PANEL. DAMAGED. LOOSE FASTENERS AT UPPER ELEVATOR HORN TOP SKIN REPAIRED IAW RD8-553035 AND ECO008.55-17.02.
- [SDR 7C7A2017031100292](https://openairdocs.org/sdr/7C7A2017031100292), Mar 11, 2017: DOUBLER. CORRODED. CORROSION DAMAGE TO AFT CARGO DOOR SKIN DOUBLER. REPAIRED IAW RD8-53-15082 AND ECO008.53-17.06.
- [SDR 7C7A2017031000289](https://openairdocs.org/sdr/7C7A2017031000289), Mar 10, 2017: SKIN PANEL. DENTED. DENT DAMAGE TO LT FUSELAGE SKIN. REPAIRED IAW RD8-53-15088 AND ECO 008.53-17.10.
- [SDR 7C7A2017031000258](https://openairdocs.org/sdr/7C7A2017031000258), Mar 10, 2017: SKIN PANEL. DENTED. DENT DAMAGE TO THE LT SIDE FUSELAGE SKIN REPAIRED IAW RD 8-53-15085 AND ECO008.53-17.09.
- [SDR 7C7A2017030800287](https://openairdocs.org/sdr/7C7A2017030800287), Mar 8, 2017: SKIN PANEL. DENTED. DENT DAMAGE TO FUSELAGE SKIN PANEL 85310533 STA X123 STR 24S AND 25S. REPAIRED IAW ECO 008.53-17-05.
- [SDR 7C7A2017030700286](https://openairdocs.org/sdr/7C7A2017030700286), Mar 7, 2017: SKIN. DENTED. DENT DAMAGE TO THE FUSELAGE SKIN PANEL BETWEEN BS 291.4 AND 312.35, STRINGER 1-2R. REPAIRED IAW RD 8-53-15073 WC 53-123.
- [SDR 7C7A201502220013](https://openairdocs.org/sdr/7C7A201502220013), Feb 21, 2015: PANEL. CORRODED. RIGHT STRESS PANEL 624AT ONE COUNTERSINK CORRODED, REPAIRED WITH A BUSHING IAW RD 8-57-2673.
- [SDR 7C7A201502220012](https://openairdocs.org/sdr/7C7A201502220012), Feb 21, 2015: PANEL. CORRODED. LEFT STRESS PANEL 521AT 9EA COUNTERSINKS CORRODED. REPAIRED IAW RD 8-57-4240.
- [SDR 7C7A201502220011](https://openairdocs.org/sdr/7C7A201502220011), Feb 21, 2015: BOLT. CORRODED. LT AND RT REAR SPAR WING/FUSELAGE JOINT BOLTS CORRODED. REPLACED THE BOLTS IAW AMM .
- [SDR 7C7A201502220010](https://openairdocs.org/sdr/7C7A201502220010), Feb 21, 2015: STRINGER. CORRODED. CORROSION ON STRINGER 31P AT BS 354. SPLICED STRINGER IAW RD 8-53-2499.
- [SDR 7C7A201502220009](https://openairdocs.org/sdr/7C7A201502220009), Feb 21, 2015: FRAME SPLICE. CORRODED. CORROSION SPOTS UNDER COCKPIT AREA ZONE 121-122. REPAIRED CORROSION; REPLACED HORIZONTAL STIFFNER, REPLACED FRAME, REPLACED 4 FRAME LEGS.
- [SDR 7C7A201502220008](https://openairdocs.org/sdr/7C7A201502220008), Feb 21, 2015: CARGO TRACK. CORRODED. RT INBD CARGO TRACK CORRODED, REWORKED THE CARGO TRACK IAW RD 8-53-784 AND 8-53-4936.
- [SDR 7C7A201502220007](https://openairdocs.org/sdr/7C7A201502220007), Feb 21, 2015: WEB. CORRODED. BAGGAGE FLOOR WEB CORRODED AT SEVERAL PLACES, DOUBLER WEB INSTALLED SRM REPAIR.
- [SDR 7C7A201502220006](https://openairdocs.org/sdr/7C7A201502220006), Feb 21, 2015: CARGO TRACK. CORRODED. LT INBD CARGO TRACK CORRODED. REPLACED THE CARGO TRACK IAW WC 1062 RD 8-53-4472
- [SDR 7C7A201502220005](https://openairdocs.org/sdr/7C7A201502220005), Feb 21, 2015: THRESHOLD. CORRODED. CORROSION AT PAX DOOR THRESHOLD. BEYOND LIMITS PART REPLACED WC 1050
- [SDR ERAA201410310066](https://openairdocs.org/sdr/ERAA201410310066), Oct 30, 2014: GENERATOR. DEFECTIVE. NUMBER 1 AC GEN CAUTION LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF EJECTED. R & R NR 1 AC GENERATOR IAW DHC-8 PPBM 71-00-02. OPERATIONS & LEAK CHECKED GOOD. OK 
- [SDR ERAA20140050](https://openairdocs.org/sdr/ERAA20140050), Aug 19, 2014: INVERTER. FAILED. DURING PREFLIGHT WITH ENGS COLD 1ST OFFICER NOTED ELEC SMOKE ON THE FLIGHT DECK & HEARD 115 VOLT BUSS TIE CB POP. FOUND SECONDARY INVERTER BURNT UP. REPLACED IN
- [SDR ERAA201408010047](https://openairdocs.org/sdr/ERAA201408010047), Jul 31, 2014: ACTUATOR. CRACKED. NUMBER 1 HYD ISO VLV, ROLL SPOILER INBD, FLAP POWER CAUTION LIGHTS WITH LESS THAN MIN NR 1 HYD FLUID. FLAPS REMAINED AT 5 DEGREES. FOUND RT INBD ROLL SPOILER AC
- [SDR ERAA20140044](https://openairdocs.org/sdr/ERAA20140044), Jun 25, 2014: ACTUATOR. LEAKING. HYDRAULIC FLUID LEAKING FROM DRAIN HOLES ON WING FLAP FAIRINGS WITH NR 2 ENG RUNNING. R & R LT OTBD ROLL SPOILER ACTUATOR IAW MM 27-14-05. RIGGED IAW 27-14-00. 
- [SDR ERAA201406230043](https://openairdocs.org/sdr/ERAA201406230043), Jun 22, 2014: WIRE. DAMAGED. SPOILER 2 PUSH OFF SWITCH LIGHT CAME ON IN FLIGHT. VERIFIED PROBLEM ON RT WING BY DISCONNECTING 2700-P4 & THEN 9811-J172, IT WENT AWAY. RAN NEW WIRE FROM 9811-J
- [SDR ERAA20140009](https://openairdocs.org/sdr/ERAA20140009), Mar 23, 2014: AHRS. INACCURATE. NR 1 ADI SHOWING INCORRECT PITCH & ROLL INFORMATION. ADI PITCH & ROLL MISMATCH MESSAGES DISPLAYED ON 802 DISPLAY. R & R NR 1 AHRU IAW 34-20-06, OPERATIONS NORMA
- [SDR ERAA201309300066](https://openairdocs.org/sdr/ERAA201309300066), Sep 27, 2013: ROD END. OUT OF ADJUST. LEFT GEAR DOOR INTERMITTENTLY STAYS OPEN ON GEAR RETRACTION. ADJUSTED LEFT FWD GEAR DOOR ACTUATOR ROD END IAW MM 32-10-36. GEAR SWING C/W IAW MM 32-30-00. OK FO
- [SDR ERAA201309270065](https://openairdocs.org/sdr/ERAA201309270065), Sep 26, 2013: UNKNOWN. ODOR. F/A REPORTED ODOR OF "HOT OIL" ON DECENT. INSPECTED IAW FAULT ISOLATION 72-00-02. ENGINE OIL LEVELS CHECKED GOOD, NO STANDING OIL NOTED. ACM LEVELS CHECK OK. RA
- [SDR ERAA201309130061](https://openairdocs.org/sdr/ERAA201309130061), Sep 12, 2013: POWER SUPPLY. DEFECTIVE. EMEGENCY LIGHTS INOPERATIVE AT SIDE KICK PANELS AT ALL EMERGENCY EXITS. R & R NR 3 POWER SUPPLY UNIT AS REQUIRED WITH AN INSPECTED UNIT. OPS CHECKED GOOD. WORK 
- [SDR ERAA201309120060](https://openairdocs.org/sdr/ERAA201309120060), Sep 11, 2013: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS NOT ILLUMINATED. R & R BATTERY PACK AT STA X500. OPS CHECKED GOOD.
- [SDR ERAA20130058](https://openairdocs.org/sdr/ERAA20130058), Sep 5, 2013: PROXIMITY SENSOR. OUT OF RIG. LT MAIN GEAR DOOR CAUTION LIGHT STAYED ON WITH GEAR RETRACTION. VISUALLY CHECKED GEAR DOOR WAS OPEN. COMPLIED WITH TROUBLESHOOTING IAW MM SECTION 32-00-00. RIGG
- [SDR ERAA20130046](https://openairdocs.org/sdr/ERAA20130046), Jul 1, 2013: BRACKET. CRACKED. NLG UPLOCK ACTUATOR ATTACH BRACKET CRACKED. REMOVED FITTING, REINSTALLED BRACKET IAW RD 8-53-3805. OK FOR SERVICE.
- [SDR ERAA201306280042](https://openairdocs.org/sdr/ERAA201306280042), Jun 27, 2013: BATTERY. WEAK. RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOP. R & R BATTERY 3351P2 IAW MM 33-52-00. OPS CHECKS NORMAL. OK FOR SERVICE.
- [SDR ERAA201306280041](https://openairdocs.org/sdr/ERAA201306280041), Jun 27, 2013: CONNECTOR. FAILED. LEFT FWD EXTERIOR EGRESS EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTOR DISCONECTED AND WIRE DISCONNECTED FROM CONNECTOR SOCKET. INSTALLED NEW SOCKET, CONNECTED C

All 88: https://openairdocs.org/deregistered/N883EA-2025-05-23/reports.md

## 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 20010318003879I](https://openairdocs.org/incident/20010318003879I), Mar 18, 2001: Dhav DHC8106 (N883EA), Kodiak, AK. (-23) Pilot departed adq reported a gear warning light. A/c dumped fuel and landed at adq at 1655 without incident. A/c was ferried back to anchorage with gear…

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