# N882EA: Boeing / Dehavilland DHC-8-103, registration cancelled 2013-11-20 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 20, 2013 - 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: [NONE](https://openairdocs.org/engine/none) (registry code 00000) - Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM) (OpenAirDocs) - Serial number: 098 - Type of aircraft: Fixed wing multi engine - Engine type: None - Last registry action: November 20, 2013 - Mode S code: AC25A8 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N882EA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=882EA - Page: https://openairdocs.org/deregistered/N882EA-2013-11-20 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 Boeing / Dehavilland DHC-8-103: https://openairdocs.org/model/boeing-dehavilland-dhc-8-103.md ## Service difficulty reports (68, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ERAA201309170063](https://openairdocs.org/sdr/ERAA201309170063), Sep 14, 2013: GENERATOR. DEFECTIVE. ACFT NR 2 GENERATOR FAILED. R & R NR 2 AC GENERATOR IAW MM 24-21-01. OPS AND LEAK CHECKED GOOD. - [SDR ERAA201308260056](https://openairdocs.org/sdr/ERAA201308260056), Aug 23, 2013: OIL COOLER. DEFECTIVE. NR 2 AC GENERATOR HOT ANNUNCIATOR ILLUMINATED ON TAKEOFF. ENGINE OIL TEMP 110 DEGREES INDICATED. TAKEOFF ABORTED-NO FLIGHT. R & R NR 2 ENGINE OIL COOLER TEMPERA - [SDR ERAA20130024](https://openairdocs.org/sdr/ERAA20130024), Feb 21, 2013: LIGHT. INOPERATIVE. EMERGENCY LIGHT INOP AFT ROW CEILING. RELAMPED AS REQUIRED, OPS CHECK GOOD. - [SDR ERAA20120132](https://openairdocs.org/sdr/ERAA20120132), Dec 8, 2012: FRAME. CRACKED. CRACK FOUND ON RIGHT FUSELAGE FRAME AT STATION X354 BETWEEN STATION 20S AND 33S. - [SDR ERAA20120131](https://openairdocs.org/sdr/ERAA20120131), Dec 8, 2012: SKIN PANEL. GOUGED. SKIN DAMAGE TO RIGHT FUSELAGE SKIN AT STATION X342 BETWEEN STRINGER 12S AND 13S. REPAIRED TO BOMBARDIER REPAIR DRAWING 8-53-2181. - [SDR ERAA201212080130](https://openairdocs.org/sdr/ERAA201212080130), Dec 8, 2012: SKIN. NICKED. NICK ON SKIN AT RIGHT FUSELAGE AT STATION X342 BETWEEN STRINGER 12S AND 13S. REPAIRED TO BOMBARDIER REPAIR DRAWING 853-2181. - [SDR ERAA20120130](https://openairdocs.org/sdr/ERAA20120130), Dec 8, 2012: SEAT TRACK. CORRODED. CORROSION FOUND ON LEFT INBOARD SEAT TRACK. REPAIRED TO BOMBARDIER REPAIR DRAWING 8-53-3074. - [SDR ERAA20120129](https://openairdocs.org/sdr/ERAA20120129), Dec 8, 2012: FRAME. CORRODED. FRAME FOUND CORRODED AT STATION X312 BETWEEN STRINGER 29P AND 30P AND 31P AND 32P. REPAIRED TO BOMBARDIER SRM 53-00-16. - [SDR ERAA2120128](https://openairdocs.org/sdr/ERAA2120128), Dec 7, 2012: SEAT TRACK. CORRODED. CORROSION FOUND ON LEFT SEAT TRACK BETWEEN SAT X526 AND X 600. REMOVED AND REPLACED WITH NEW BY BOMBARDIER SRM 51-40-10. - [SDR ERAA20120127](https://openairdocs.org/sdr/ERAA20120127), Dec 7, 2012: ACCESS PANEL. CORRODED. RIGHT STRESS PANEL HAS CORROSION UNDER COUNTERSINK SCREW HOLES. REPLACED RIGHT STRESS PANEL 85711802-005. - [SDR ERAA20120126](https://openairdocs.org/sdr/ERAA20120126), Dec 7, 2012: ACCESS PANEL. CORRODED. LEFT STRESS PANEL HAS CORROSION UNDER COUNTERSINK SCREW HOLES. REPLACED LEFT STRESS PANEL P/N 85711802-005. - [SDR ERAA20120124](https://openairdocs.org/sdr/ERAA20120124), Dec 6, 2012: SEAT TRACK. CORRODED. CORROSION FOUND ON RIGHT ONBOARD SEAT TRACK BETWEEN STATION X262 AND X526. REPAIRED USING BOMBARDIER REPAIR DRAWING 8-53-1339. - [SDR ERAA201201223](https://openairdocs.org/sdr/ERAA201201223), Dec 6, 2012: INTERCOSTAL. CORRODED. LIGHT SURFACE CORROSION FOUND AT STEP OF PASSENGER DOOR ENTRANCE. REPLACED INTERCOSTAL IN ACCORDANCE WITH BOMBARDIER SRM 52-10-00. - [SDR ERAA20120122](https://openairdocs.org/sdr/ERAA20120122), Dec 6, 2012: FRAME. CORRODED. FRAME CORRODED AT STATION X446 BETWEEN STRINGERS 32S AND 33. FRAME REPLACED WITH NEW TO BOMBARDIER SRM 53-20-21. - [SDR ERAA20120121](https://openairdocs.org/sdr/ERAA20120121), Dec 6, 2012: SPAR. CORRODED. LEFT WING FRONT SPAR AT UPPER AND LOWER LEADING EDGE SEATS HAVE BARE METAL AND CORROSION. REPAIRED BETWEEN YW57 AND YW 139 TO BOMBARDIER REPAIR DRAWING 8-57-811 - [SDR ERAA20120120](https://openairdocs.org/sdr/ERAA20120120), Dec 6, 2012: SEAT TRACK. CORRODED. CORROSION FOUND RIGHT SEAT TRACK BETWEEN STATION X264 AND X504. REPAIRED TO BOMBARDIER REPAIR DRAWING 8-53-1342. - [SDR ERAA2120119](https://openairdocs.org/sdr/ERAA2120119), Dec 6, 2012: SEAT TRACK. CORRODED. CORROSION FOUND ON LEFT INBOARD SEAT TRACK BETWEEN STATION X285 AND X526. REPAIRED TO BOMBARDIER REPAIR DRAWING 8-53-1339. - [SDR ERAA20120118](https://openairdocs.org/sdr/ERAA20120118), Dec 6, 2012: FRAME. CRACKED. FUSELAGE FRAME FOUND CRACKED AT X264.1 AND STR 21S AND INTERCOSTAL X264.4 CRACKED AT SEAT TRACK LEVEL. NEW FRAME REPLACED P/N 85320534-007. - [SDR ERAA20120117](https://openairdocs.org/sdr/ERAA20120117), Dec 6, 2012: BRACKET. CRACKED. PASSENGER DOOR SHELL FORWARD LOWER BRACKET CRACKED. REPLACED BRACKET P/N 85210223-101 WITH NEW. - [SDR ERAA2120116](https://openairdocs.org/sdr/ERAA2120116), Dec 4, 2012: SILL. CORRODED. AFT CARGO DOOR SILL FOUND WITH SURFACE CORROSION. - [SDR ERAA20120115](https://openairdocs.org/sdr/ERAA20120115), Dec 4, 2012: STRUCTURE. CORRODED. BARE METAL AND LIGHT SURFACE CORROSION AT LOWER SECTION OF INSIDE OF PASSENGER DOOR SHELL. - [SDR ERAA20120114](https://openairdocs.org/sdr/ERAA20120114), Dec 4, 2012: CASTING. CORRODED. LAVATORY CASTING FOUND SLIGHTLY CORRODED. REPLACED CASTING P/N 85320980-105. - [SDR ERAA20120113](https://openairdocs.org/sdr/ERAA20120113), Dec 3, 2012: STOP FITTING. WORN. CARGO DOOR STOPS FOUND WORN. BLENDED STOPS IN ACCORDANCE WITH BOMBARDIER REPAIR DRAWING 8-53-104. P/NS 8533064,85332439, 85330365, 85330366, 85332440, 85330367 - [SDR ERAA2120112](https://openairdocs.org/sdr/ERAA2120112), Dec 1, 2012: SEAT TRACK. CORRODED. CORROSION FOUND ON RIGHT INBOARD SEAT TRACK BETWEEN STATIONS X182 AND X 262. - [SDR ERAA20120111](https://openairdocs.org/sdr/ERAA20120111), Dec 1, 2012: SEAT TRACK. CORRODED. CORROSION FOUND ON LEFT OUTBOARD SEAT TRACK BETWEEN STATION X504 AND X545. - [SDR ERAA2120110](https://openairdocs.org/sdr/ERAA2120110), Nov 29, 2012: SKIN PANEL. DENTED. DENT FOUND ON RIGHT STATION FORWARD BOTTOM VERTICAL STAB SKIN PANEL P/N 85530011 BETWEEN THE FRONT SPAR AND MIDDLE SPAR AT STIFFENER 85530107-105 BETWEEN RIBS T - [SDR ERAA20120109](https://openairdocs.org/sdr/ERAA20120109), Nov 27, 2012: FITTING. CORRODED. FITTING CORRODED BEYOND SRM LIMITS AT STA X531 AND STR 31P - [SDR ERAA20120108](https://openairdocs.org/sdr/ERAA20120108), Nov 26, 2012: SKIN PANEL. GOUGED. GOUGE DAMAGE TO THE RIGHT EMERGENCY DOOR OUTER SKIN PART NUMBER 85220030. - [SDR ERAA20120107](https://openairdocs.org/sdr/ERAA20120107), Nov 24, 2012: SHEAR WEB. CORRODED. REMOVAL OF THE AFT CARGO SEAT TRACK REVEALED CORROSION UNDER THE RIGHT AFT CARGO TRACK AND DAMAGE TO THE SHEAR WEB P/N 85330431 BETWEEN X580.5 AND X600 STA 31S. - [SDR ERAA20120106](https://openairdocs.org/sdr/ERAA20120106), Nov 22, 2012: SKIN PANEL. CHAFED. VISUAL INSPECTION OF FUSELAGE PANEL P/N 85350327 REVEALED WEAR DAMAGE TO LOWER SURFACE OF THE PANEL. - [SDR ERAA20120105](https://openairdocs.org/sdr/ERAA20120105), Nov 22, 2012: NUT PLATE. STRIPPED. FUNCTIONAL CHECK OF THE LEFT NR 1 FLAP TRACK FASTENERS FAILED TORQUE CHECK. ON FLAP SUPPORT TRACK P/N 85780039. FAILED AT THREE LOCATIONS. - [SDR ERAA20120104](https://openairdocs.org/sdr/ERAA20120104), Nov 20, 2012: FLAP. DELAMINATED. DELAMINATION DAMAGE FOUND ON TRAILING EDGE FLAP ON LEFT WING P/N 85750233 AND P/N 85750245. TWO AREAS 1. 5.3" IN LENGTH 2. 7.1" IN LENGTH. - [SDR ERAA20120103](https://openairdocs.org/sdr/ERAA20120103), Nov 19, 2012: STRAP. CRACKED. CRACKED LOWER REINFORCEMENT STRAPS ON LEFT WING STRINGER 12-16. PART NUMBER 85711248 AT YW197 - [SDR ERAA20120102](https://openairdocs.org/sdr/ERAA20120102), Nov 16, 2012: PLATE. CRACKED. CRACK AT RIGHT WING LADDER PLATE AT OUTBOARD OF YW139.2 AND STRINGER 4. PLATE P/N 85711069 - [SDR ERAA20120101](https://openairdocs.org/sdr/ERAA20120101), Nov 16, 2012: SKIN PANEL. SCRATCHED. SCRATCH DAMAGE FOUND AT LOWER FUSELAGE SKIN PNL 8532016 BETWEEN FRAME STATION X222.0 -X-240.5 ALONG STR 32P. NO CRACK OR DISBOND BOUND. - [SDR ERAA20120100](https://openairdocs.org/sdr/ERAA20120100), Nov 15, 2012: ATTACH ANGLE. CRACKED. DURING INSPECTION OUTBOARD CLOSING ANGLES FOUND TO BE CRACKED. 34848 CYC SINCE INSTALLATION OF ANGLES. ONE CRACK ON EACH ANGLE ONE P/N 8530016-015 2.5 INCHES AN - [SDR ERAA20120099](https://openairdocs.org/sdr/ERAA20120099), Nov 14, 2012: SKIN PANEL. CRACKED. CRACK AT RIGHT WING LADDER PLATE AT YW42.0 AND STR 4. - [SDR ERAA20120076](https://openairdocs.org/sdr/ERAA20120076), Oct 4, 2012: CIRCUIT BREAKER. DEFECTIVE. NR 1 STANDBY HYDRAULIC GAUGE INDICATES PRESSURE WITH SWITCH SELECTED TO "NORMAL" (OFF) POSITION. INSTALLED SERVICEABLE A/C PUMP C/B IN RIGHT WHEEL A/C CONTACTOR - [SDR ERAA20120059](https://openairdocs.org/sdr/ERAA20120059), Sep 7, 2012: GENERATOR. DEFECTIVE. NR 1 AC GEN CAUTION LIGHT - NO LOAD LEFT SIDE. REMOVED AND REPLACED NR 1 AC GENERATOR IAW PSM 1-8-10, RUN UP CHECK GOOD. NO LEAKS FOUND, OK FOR SERVICE. - [SDR ERAA20120038](https://openairdocs.org/sdr/ERAA20120038), Apr 19, 2012: TARGET. MISSING. "WT ON WHEELS" CAUTION LIGHT ILLUMINATED. INSTRUCTED BY OPS AND MAINTENANCE TO RETURN TO ANC. FOUND FAULT ON RIGHT NLG PROX SWITCH AND TARGET MISSING FROM LOWER - [SDR ERAA201200009](https://openairdocs.org/sdr/ERAA201200009), Feb 4, 2012: DRIVE SHAFT. CORRODED. ROLL CONTROL VERY STIFF. TENSIONED AILERON FUSELAGE CABLES AND LUBRICATED AILERION QUADRANT BEARINGS EXTERNALLY FOR TROUBLESHOOTING. OPERATIONAL CHECK FLIGHT-RO - [SDR ERAA201200004](https://openairdocs.org/sdr/ERAA201200004), Jan 23, 2012: BATTERY PACK. WEAK. OVERHEAD AISLE EMERGENCY EXIT LIGHTS MID-CABIN WEAK. REMOVED AND REPLACED EMERGENCY BATTERY PACK IN AFT RIGHT POSITION IAW DHC-8 MAINTENANCE MANUAL 33-51-00. EM - [SDR ERAA201200001](https://openairdocs.org/sdr/ERAA201200001), Jan 7, 2012: CONTROL QUADRANT. DIRTY. RETURNED TO ANC DUE TO VERY STIFF CONTROL YOKE MOVEMENT TO THE LEFT, OK UNTIL ABOUT 20 DEGREES PAST CENTER, ALSO SEEMS NORMAL ON GROUND, AIRSPEED OR CONFIGURATI - [SDR ERAA201100011](https://openairdocs.org/sdr/ERAA201100011), Dec 24, 2011: DRAG BRACE. DEFECTIVE. UNABLE TO EXTEND NOSE GEAR, MANUAL GEAR EXTEND COMPLETED UPON RETURN TO ANC. REMOVED AND REPLACED NLG DRAG BRACE IAW DASH 8 MAINTENANCE MANUAL 32-30-36 AND C/W - [SDR ERAA2012F00003](https://openairdocs.org/sdr/ERAA2012F00003), Oct 26, 2011: SELECTOR. INTERMITTENT. LANDING GEAR HANDLE AND RED NOSE GEAR LIGHT FLASHED 3 SEPARATE TIMES MIDFLIGHT AND NOSEGEAR WAS FELT HITTING GEAR DOORS ON 2 OF THESE OCCASIONS. REMOVED LANDING - [SDR ERAA201100001](https://openairdocs.org/sdr/ERAA201100001), Jan 4, 2011: ACTUATOR. FRACTURED. ON LANDING PILOT REPORTED TWO CAUTION LIGHTS, NR 1 HYD ISO VLV AND ROLL SPLR INBD HYD AND LOSS OF BRAKING. MAINTENANCE FOUND RIGHT, INBOARD ROLL SPOILER ACTUATO - [SDR V0XR201011020002](https://openairdocs.org/sdr/V0XR201011020002), Nov 2, 2010: STRUT. CORRODED. (V0XR) STRUT AT STR 31P, STA 531.5 IS CORRODED. R & R STRUT. - [SDR V0XR201011020001](https://openairdocs.org/sdr/V0XR201011020001), Nov 2, 2010: FRAME. CORRODED. (V0XR) RT SIDE FRAME AT STA 510 IS CORRODED. R & R SPLICE IAW RD8-53-11498. - [SDR V0XR201010290007](https://openairdocs.org/sdr/V0XR201010290007), Oct 29, 2010: FITTING. CORRODED. (V0XR) JOINT FITTING AFT KEEL AT LT FRAME STN 531.5. R & R FITTING. - [SDR V0XR201010290006](https://openairdocs.org/sdr/V0XR201010290006), Oct 29, 2010: STRINGER. CORRODED. (V0XR) CORROSION ON STRINGER AT STN 525.0 AT STR 32L. R & R STRINGER. All 68: https://openairdocs.org/deregistered/N882EA-2013-11-20/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 20111219028149I](https://openairdocs.org/incident/20111219028149I), Dec 19, 2011: Boeing / Dehavilland DHC-8-103 (N882EA), Fairbanks, AK, Minor damage. Ptrs number: AL07201201274DURING the deicing process the hageland (epua) contract deice truck operator was having issues with the trucks intercom system, got… - [Incident 20030719016329I](https://openairdocs.org/incident/20030719016329I), Jul 19, 2003: Dhav DHC8103 (N882EA), Fairbanks, AK. (-23) 70 Knmi south of fai, aircraft began experiencing uncommanded radio transmissions causing interference with communications between ATC and all aircraft… --- 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.