# N881EA: 1990 Bombardier DHC-8-106, registration cancelled 2012-11-15 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 15, 2012 - Exported to: Canada - Status when cancelled: Valid registration - Airframe: [Bombardier DHC-8-106](https://openairdocs.org/model/bombardier-dhc-8-106) (registry code 1390012) - Engine: [Pratt & Whitney Canada PW120](https://openairdocs.org/engine/pratt-whitney-canada-pw120) (registry code 52114) - Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs) - Serial number: 233 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: November 6, 1990 - Certificate issued: November 5, 2012 - Last registry action: November 5, 2012 - Mode S code: AC21F1 - Owner when cancelled: [Aec-341 LLC](https://openairdocs.org/faa-owner/AEC-341%20LLC) - Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage) - Owner type: Corporation - Owner's area on the map: 61.2181° N, 149.9003° W: Placed by OpenAirDocs: center of Anchorage, AK, within about 23 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N881EA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=881EA - Page: https://openairdocs.org/deregistered/N881EA-2012-11-15 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 Bombardier DHC-8-106: https://openairdocs.org/model/bombardier-dhc-8-106.md ## Service difficulty reports (48) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ERAA20120062](https://openairdocs.org/sdr/ERAA20120062), Sep 11, 2012: LIGHT. INOPERATIVE. ROW 1D UPPER EMERGENCY SIGN INOP. REMOVED AND REPLACED BAD LAMPS, OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME. - [SDR ERAA20120057](https://openairdocs.org/sdr/ERAA20120057), Sep 3, 2012: WARNING SYSTEM. FALSE ACTIVATION. GEAR FAILED TO RETRACT PROPERLY - BOTH MAIN "AMBER" ADVISORY LIGHTS ON, RED NOSEWHEEL LIGHT ILLUMINATED. JACKED AIRCRAFT AND PERFORMED OPERATIONAL CHECK OF THE - [SDR ERAA20120049](https://openairdocs.org/sdr/ERAA20120049), Jun 27, 2012: PRESSURE SWITCH. FAULTY. DEPARTURE IN ANC 07:45 NR 2 RUDDER HYDRAULIC LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 RUDDER LOW PRESSURE SWITCH AT RUDDER DAMPER ASSEMBLY AND OPS AND LEAK - [SDR ERAA20120042](https://openairdocs.org/sdr/ERAA20120042), May 14, 2012: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT FOUND INOP ON PREFLIGHT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS IAW DHC MM 33-52-00, OPS CHECK GOOD. - [SDR ERAA20120033](https://openairdocs.org/sdr/ERAA20120033), Mar 10, 2012: SMOKE DETECTOR. NO TEST. NR 2 BAG SMOKE WARNING TEST FAILED. REMOVED AND REPLACED NR 2 AFT BAGGAGE SMOKE DETECTOR. OPS CHECK GOOD. - [SDR ERAA201202160029](https://openairdocs.org/sdr/ERAA201202160029), Feb 16, 2012: SKIN. CRACKED. LT WING LIGHTNING STRIPS HAVE TWO CRACKS AT STA 178. REPLACED STRIPS. - [SDR ERAA201202160028](https://openairdocs.org/sdr/ERAA201202160028), Feb 16, 2012: SKIN. CRACKED. RT WING LIGHTNING STRIP HAVE FOUR CRACKS BETWEEN STA YW 139.00 & YW 250.00. REPLACE STRIPS. - [SDR ERAA201200027](https://openairdocs.org/sdr/ERAA201200027), Feb 14, 2012: SKIN. CRACKED. LT NACELLE OUTBD NACELLE SKIN CRACKED AT STA ZN 0-00 AND ZN 130.00. REPLACED SKIN. - [SDR ERAA201200026](https://openairdocs.org/sdr/ERAA201200026), Feb 11, 2012: FIREWALL. CRACKED. REPAIRED CRACK IN LT ENGINE NACELLE FIREWALL OUTBD SKIN IAW RD8-54-0651 PERMANENT REPAIR. - [SDR ERAA201200025](https://openairdocs.org/sdr/ERAA201200025), Feb 11, 2012: FASTENER. LOOSE. REPLACED 8 LOOSE FASTENERS WITH JOBOLTS IAW RD8-55-032. - [SDR ERAA201200024](https://openairdocs.org/sdr/ERAA201200024), Feb 11, 2012: STRINGER. CORRODED. REPLACED SECTION OF CORRODED STRINGER 32R STA 281 IAW SRM 53-10-21. - [SDR ERAA201200023](https://openairdocs.org/sdr/ERAA201200023), Feb 9, 2012: FLAP TRACK. CORRODED. REMOVED LIGHT SURFACE CORROSION ON LT NR 4 FLAP TRACK IAW RD8-57-988. - [SDR ERAA201200022](https://openairdocs.org/sdr/ERAA201200022), Feb 9, 2012: STRINGER. CORRODED. REPAIRED CORROSION ON FUSELAGE STRINGER 31S AT X436 IAW RD8-53-3044. - [SDR ERAA201200020](https://openairdocs.org/sdr/ERAA201200020), Feb 8, 2012: SKIN PANEL. CORRODED. REPAIRED SKIN PANEL CORROSION ON WAFFLE DOUBLER OF SKIN PANEL STA X275 BETWEEN STR 32P - 32S BY BLENDING IAW RD8-53-12242. - [SDR ERAA201200019](https://openairdocs.org/sdr/ERAA201200019), Feb 8, 2012: SKIN PANEL. CORRODED. REPAIRED SKIN PANEL CORROSION AT STA X429 BETWEEN STRINGER 32P & 31S, CUT AWAY SKIN IAW RD8-53-12243 ISSUE 2 AND INSTALLED EXTERNAL DOUBLER. - [SDR ERAA201200018](https://openairdocs.org/sdr/ERAA201200018), Feb 8, 2012: SKIN PANEL. CORRODED. REPAIRED SKIN PANEL CORROSION AND DISBONDED DOUBLER STA X167 AT STRINGER 33, CUT AWAY SKIN IAW RD8-53-12241 AND INSTALLED EXTERNAL DOUBLER. - [SDR ERAA201200017](https://openairdocs.org/sdr/ERAA201200017), Feb 8, 2012: PIN. CORRODED. RIGHT MLG DRAG STRUT TO SHOCKSTRUT ATTACH PIN REPLACED DUE TO PITTING. - [SDR ERAA201200016](https://openairdocs.org/sdr/ERAA201200016), Feb 8, 2012: SKIN. CORRODED. CORROSION AND SKIN DISBOND AT LOWER FUSELAGE STA X506. - [SDR ERAA201200015](https://openairdocs.org/sdr/ERAA201200015), Feb 8, 2012: ATTACH BOLT. CRACKED. LEFT FUSELAGE TO WING ATTACH BOLT HEAD CRACKED. - [SDR ERAA201200014](https://openairdocs.org/sdr/ERAA201200014), Feb 8, 2012: STIFFENER. CORRODED. CORROSION DAMAGE ON STIFFENER AT WEB STA 387.5. REPLACED STIFFENER. - [SDR ERAA201200013](https://openairdocs.org/sdr/ERAA201200013), Feb 8, 2012: RIB. CRACKED. CRACKED RIB ON RT NACELLE FIREWALL ON INBD SIDE. - [SDR ERAA201200012](https://openairdocs.org/sdr/ERAA201200012), Feb 8, 2012: DOUBLER. CRACKED. CRACKED DOUBLER ON LT NACELLE FIREWALL ON INBD SIDE. - [SDR ERAA201200011](https://openairdocs.org/sdr/ERAA201200011), Feb 8, 2012: STRINGER. CRACKED. TWO CRACKS ON LT NACELLE SKIN STRINGERS UNDER EXHAUST FINGERNAIL. - [SDR ERAA201200010](https://openairdocs.org/sdr/ERAA201200010), Feb 8, 2012: STRINGER. CORRODED. CORROSION ON STRINGER 31R, STA 156 - 159. - [SDR ERAA2012F00051](https://openairdocs.org/sdr/ERAA2012F00051), Feb 8, 2012: STRINGER. CORRODED. CORROSION ON STRINGER 31R, STA 156 - 159. - [SDR ERAA201100004](https://openairdocs.org/sdr/ERAA201100004), Apr 3, 2011: SKIN. DENTED. LOWER FUSELAGE SKIN DENT BEYOND AIRWORTHY LIMITS, STA X290.5 ABOVE STR 26P APPROXIMATELY 0.3 INCH ABOVE EDGE OF BONDED WAFFLE. OBTAINED RD FROM MANUFACTURERS EN - [SDR ERAA201000005](https://openairdocs.org/sdr/ERAA201000005), Oct 3, 2010: SMOKE DETECTOR. INTERMITTENT. SMOKE WARNING LIGHT CAME ON INTERMITTENTLY IN FLIGHT. (NO EVIDENCE OF SMOKE OR FIRE IN AFT CARGO COMPARTMENT.) REPLACED SMOKE DETECTOR IAW MM CHAPTER 26-12-01, - [SDR V0XR201004280003](https://openairdocs.org/sdr/V0XR201004280003), Apr 28, 2010: SKIN. DENTED. (V0XR) DENT ON RT FUSELAGE AT 1.5 INCHES FWD OF STA X312.35 BETWEEN STR 7R AND 8R IS BEYOND LIMITS. REPAIRED DENT ON RT FUSELAGE. W/C 2182. - [SDR V0XR201004280002](https://openairdocs.org/sdr/V0XR201004280002), Apr 28, 2010: SKIN. CRACKED. (V0XR) CRACK ON LT WING UPPER SKIN LADDER PLATE OTBD OF AFT CORNER UNDER PANEL 522AT AT WS YW 137.0. REPAIRED WING UPPER SKIN LADDER PLATE. W/C 5073. - [SDR V0XR201004280001](https://openairdocs.org/sdr/V0XR201004280001), Apr 28, 2010: SHEAR WEB. CORRODED. (V0XR) LT REAR BAGGAGE FLOOR INBD OF AFT DOOR SILL IS CORRODED BEYOND LIMITS. REMOVED AND REPAIRED BAGGAGE COMPARTMENT FLOOR, SHEAR WEB. W/C 1082. - [SDR V0XR201004260003](https://openairdocs.org/sdr/V0XR201004260003), Apr 26, 2010: SEAT TRACK. CORRODED. (V0XR) RT UPPER SEAT TRACK FR 46-52 CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 1098. - [SDR V0XR201004260002](https://openairdocs.org/sdr/V0XR201004260002), Apr 26, 2010: SEAT TRACK. CORRODED. (V0XR) LT SEAT TRACK DRIP RAIL CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2225. - [SDR V0XR201004260001](https://openairdocs.org/sdr/V0XR201004260001), Apr 26, 2010: SEAT TRACK. CORRODED. (V0XR) RT SEAT TRACK RAIL FR 182.0 TO 424.12 CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 1087. - [SDR V0XR201004160002A](https://openairdocs.org/sdr/V0XR201004160002A), Apr 16, 2010: GUSSET. CORRODED. CTR GUSSET FR 59-61 IS CORRODED BEYOND LIMITS. R & R CTR GUSSET. W/C 1154. (V0XR) - [SDR V0XR201004160001](https://openairdocs.org/sdr/V0XR201004160001), Apr 16, 2010: SEAT TRACK. CORRODED. LT SEAT TRACK FR 182-484 IS CORRODED BEYOND LIMITS. R &R LT SEAT TRACK. - [SDR ERAA200900004](https://openairdocs.org/sdr/ERAA200900004), Aug 5, 2009: CONTROLLER. UNRELIABLE. AIRCRAFT DEPRESSURIZED AT FL 230 AND EMERGENCY DESCENT WAS PERFORMED, AT 12,000 FEET PRESSURIZATION RETURNED TO NORMAL. - [SDR ERAA200900003](https://openairdocs.org/sdr/ERAA200900003), Jun 24, 2009: NUT. LOOSE. WHILE ATTEMPTING TO DEPLANE PASSENGERS, FOUND THE MAIN CABIN DOOR STUCK CLOSED. PASSENGERS DEPLANED VIA ALTERNATE EXIT. FOUND JAM NUT ON UPPER END OF OVER CENTE - [SDR ERA2005F00009](https://openairdocs.org/sdr/ERA2005F00009), Nov 8, 2005: PLATE. CORRODED. FOUND WHILE AIRCRAFT UNDERGOING C1-CHECK, AWC 19810. CORROSION ON LT NLG TRUNNION PLATE BEYOND MFG LIMITS. REPLACED LT NLG TRUNNION PLATE IAW DWG. (K) - [SDR ERA2005F00000](https://openairdocs.org/sdr/ERA2005F00000), Nov 1, 2005: SEAT TRACK. CORRODED. FOUND WHILE AIRCRAFT WAS UNDERGOING C1 CHECK, AWC 19412, FOUND LT FWD SEAT RAIL CORROSION BEYOND MFG LIMITS. REPAIRED IAW RO. (K) - [SDR ERA2005F00001](https://openairdocs.org/sdr/ERA2005F00001), Oct 26, 2005: SKIN. GOUGED. FOUND WHILE AIRCRAFT UNDERGOING C1 CHECK, AWC 19438, FOUND GOUGE IN RT TOP SKIN AT STRINGER 3R BETWEEN FRAME YW207, STA YW137. REPAIRED IAW RO. (K) - [SDR ERA2005F00002](https://openairdocs.org/sdr/ERA2005F00002), Oct 25, 2005: SKIN. DENTED. FOUND WHILE AIRCRAFT UNDERGOING C1 CHECK, AWC 19388. FOUND DENT UNDER RT ICE SHIELD BETWEEN FUSELAGE STRINGER 14S AND 15S AT STATION X323.1. REPAIRED IAW MFG RD - [SDR ERA2005F00003](https://openairdocs.org/sdr/ERA2005F00003), Oct 24, 2005: PLATE. CRACKED. FOUND WHILE AIRCRAFT UNDERGOING C1-CHECK, AWC 19419. FOUND CRACK IN RT IB LADDER PLATE BETWEEN STRINGER 4 AND 6 AT WING STA YW137. REPAIRED IAW RD. (K) - [SDR ERAA200000001](https://openairdocs.org/sdr/ERAA200000001), Nov 28, 2000: INDICATOR. BURNED OUT. RIGHT MAIN GEAR GREEN (DOWN/LOCKED) LIGHT DID NOT COME ON UPON EXTENSION. ALTERNATE EXTENSION LIGHTS (3 GREEN) APPEARED NORMAL. VISUAL INSPECTION ALSO APPEARED - [SDR 20000816AP011](https://openairdocs.org/sdr/20000816AP011), Jun 2, 2000: SWITCH. STUCK. AFTER TAKEOFF AUTOFEATHER SELECT SWITCH WILL NOT TURN OFF. RETURNED AND MADE UNEVENTFUL LANDING ANC. REPLACED AUTOFEATHER SELECT SWITCH, GROUND TEST GOOD. (M) - [SDR 99ZZZM667](https://openairdocs.org/sdr/99ZZZM667), Aug 31, 1999: PACKING. CUT. OIL PRESS CAUTION LIGHT FLICKERED DURING CLIMB-OUT FROM CDV. NR 2 ENGINE OIL PRESS DROPPED TO ZERO IN CRUISE. SHUTDOWN NR 2 ENGINE AND MADE UNEVENTFUL LANDING A - [SDR 98ZZZM596](https://openairdocs.org/sdr/98ZZZM596), Jul 1, 1998: SMOKE DETECTOR. CONTAMINATED. CARGO COMPARTMENT SMOKE DETECTOR WARNING AFTER TAKEOFF, FOR APPROX 3 MINUTES. MADE UNEVENTFUL PRECAUTIONARY LANDING AT ENG. CAUTION LIGHT WENT OUT PRIOR TO LAND - [SDR 98ZZZX2420](https://openairdocs.org/sdr/98ZZZX2420), Jun 12, 1998: PCU. INOPERATIAVE. NR 2 ENGINE PROPELLER RPM FLUCTUATING BETWEEN 1032 AND 1088. UNABLE TO CONTROL PROP RPM. SHUT DOWN ENGINE AND MADE UNEVENTFUL LANDING AT ANC. REPLACED NR 2 PCU, - [SDR ERA96002](https://openairdocs.org/sdr/ERA96002), Jul 8, 1996: SPUR GEAR. FAILED. ENGINE NR 2 FLAME-OUT IN CRUISE AT 20,000 FT. SECURED ENGINE AND DIVERTED TO HOM. ENGINE NR 2 FUEL PUMP DRIVE SPUR GEAR FAILURE RESULTING IN LOSE OF FUEL AND OI ## Other aircraft with N881EA - [Registered now](https://openairdocs.org/aircraft/N881EA): Tomark Aero CZ Sro VIPER SD-4, S/N 41881, built 2025 --- 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.