# N290UE: British Aerospace BAE 146 SERIES 200A, registration cancelled 2007-02-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 14, 2007 - Exported to: Bolivia - Status when cancelled: Triennial form not returned - Airframe: [British Aerospace BAE 146 SERIES 200A](https://openairdocs.org/model/british-aerospace-bae-146-series-200a) (registry code 1500266) - Engine: [Lycoming ALF-502 SER. series](https://openairdocs.org/engine/lycoming-alf-502-ser-series) (registry code 41580) - Data sheets: [TCDS A49EU](https://openairdocs.org/tcds/A49EU), [TCDS E6NE](https://openairdocs.org/tcds/E6NE) (OpenAirDocs) - Serial number: E2080 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, normal - Airworthiness date: February 5, 1988 - Certificate issued: December 28, 1987 - Last registry action: October 18, 2005 - Mode S code: A2F741 - 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: 40.7558° 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/N290UE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=290UE - Page: https://openairdocs.org/deregistered/N290UE-2007-02-14 From the FAA registry file of October 29, 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 British Aerospace BAE 146 SERIES 200A: https://openairdocs.org/model/british-aerospace-bae-146-series-200a.md ## Service difficulty reports (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR A6WA200560020](https://openairdocs.org/sdr/A6WA200560020), Dec 3, 2005: SEAL. LEAKING. RT ZONE HI TEMP CAPTAIN ILLUMINATED ENROUTE IN ICING CONDITIONS. REPLACED SEALS AT NR 4 PYLON LEADING EDGE AND LEAK CHECKED WING ANTI-ICE. OPS CHECKED GOOD. (K) - [SDR A6WA200460034](https://openairdocs.org/sdr/A6WA200460034), Aug 31, 2004: BOTTLE. DISCHARGED. NR 1 INTAKE ASSEMBLY INBOARD FIRE BOTTLE EXCEEDS LOW WEIGHT LIMIT. REMOVED AND REPLACED FIRE BOTTLE. (M) - [SDR A6WA200360032](https://openairdocs.org/sdr/A6WA200360032), Aug 19, 2003: SMOKE. DETECTED. ON TAXI, CABIN AND COCKPIT FILLED WITH SMOKE. MAINTENANCE PERFORMED DUCT CONTAMINATION CLEARING PROCEDURES PER SUP 96-31. CABIN TEMP CONTROL OPS NORMAL, OK FOR - [SDR A6WA200360023](https://openairdocs.org/sdr/A6WA200360023), Apr 25, 2003: SKIN. DENTED. DENTS OUT OF LIMITS ON THE RT AIR BRAKE. REPAIR REQUESTED FOR BAE SYSTEM REF AVMAX FAX 1584-6900003. - [SDR AW6A200360021](https://openairdocs.org/sdr/AW6A200360021), Apr 25, 2003: PANEL. DENTED. DENTS OUT OF LIMITS ON THE LT WING PANEL BETWEEN RIB 14A AND 15. REPAIR REQUESTED FOR BAE SYSTEM REF. - [SDR A6WA200360022](https://openairdocs.org/sdr/A6WA200360022), Apr 25, 2003: STRUCTURE. DENTED. DENTS OUT OF LIMITS ON THE RT ELEVATOR AND TABS. REPAIR REQUESTED FOR BAE SYSTEM REF AVMAX FAX 1584. - [SDR A6WA200360012](https://openairdocs.org/sdr/A6WA200360012), Apr 21, 2003: LONGERON. CORRODED. FORWARD CARGO DOOR CUTOUT LOWER LONGEORN CORROSION DAMAGE COMPLETELY THROUGH THE FACE LONGERON. REPAIR REQUESTED FOR BEE SYSTEM REF AVMAX-FAX 1584-60000. (M) - [SDR A6WA200360010](https://openairdocs.org/sdr/A6WA200360010), Apr 9, 2003: FRAME. CRACKED. FRAME 32 MLG WHEEL WELL RIGHT AFT BULKHEAD CRACKED IN TWO PLACES IN LOWER FALSE DIAPHRAGM FOR FAIRING ATTACHMENT. PATCH TWO ABOVE AREAS PER SRM 51-71-11. DOUBLE - [SDR A6WA200100058](https://openairdocs.org/sdr/A6WA200100058), Oct 7, 2001: FCU. MALFUNCTIONED. DURING CLIMB NR 3 ENGINE DID NOT RESPOND TO THRUST LEVER POWER CHANGES THEN NR 3 ENGINE TGT STARTED CLIMBING TO 870 DEGRESS PERFORMED SHUTDOWN. MAINTENANCE REMO - [SDR A6WA200100024](https://openairdocs.org/sdr/A6WA200100024), Mar 27, 2001: CABLE. DETACHED. FWD PAX SLIDE DEPLOY CABLE NOT ATTACHED TO GIRT BAR. MAINTENANCE REMOVED AND REPLACED EVACUATION SLIDE ASSEMBLY. - [SDR A6WA200100015](https://openairdocs.org/sdr/A6WA200100015), Feb 10, 2001: UNKNOWN. ODOR. FLIGHT ATTENDANT REPORTED LIGHT SMOKE ODOR COMING FROM SEAT 18 D&F AREA INFLIGHT. MAINTENANCE INSPECTED SEAT AREA, NO ODOR NOTED. NO ODOR NOTED FROM AIR CONDITI - [SDR A6WA0000020](https://openairdocs.org/sdr/A6WA0000020), Mar 2, 2000: BATTERY. DISCHARGED. NR 2 EVAC SLIDE LIGHTING BATTERY FAILS VOLTAGE CHECK. REMOVED AND REPLACED NR 2 SLIDE ASSY. (M) - [SDR A6WA0000019](https://openairdocs.org/sdr/A6WA0000019), Feb 25, 2000: VALVE. OUT OF ADJ. NR 2 ENGINE PRODUCED 89.0 PERCENT N1 ON FULL POWER APPLICATION AT ASE N1 REF CALLED FOR 93.4 PERCENT ENGINE ANTI-ICE ON 904 TGT. REMOVED AND REPLACED NR 2 ENGIN - [SDR A6WA9900032](https://openairdocs.org/sdr/A6WA9900032), Feb 15, 1999: RIB. CRACKED. AFT CARGO DOOR UPPER MOST RIB IS CRACKING LOCATED UNDER UPPER AFT HINGE 'L' BRACKET ON UPPER MOST RIB IAW BAE REPAIR DRAWING REF HC523H9001 AND FOUND SERVICEABL - [SDR A6WA9900031](https://openairdocs.org/sdr/A6WA9900031), Jan 29, 1999: BRACKET. CRACKED. LEFT WING TE SHROUD LOWER SKIN STIFFENER AFT (TAG) ANGLE BRACKET CRACKED BETWEEN RIB 8 AND RIB 9. REPLACED BRACKET. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) - [SDR A6WA9900030](https://openairdocs.org/sdr/A6WA9900030), Jan 29, 1999: STIFFENER. BROKEN. LEFT WING TE TOP SHROUD SKIN STIFFENER TO FALSE SPAR (AFT END) BROKEN BETWEEN RIBS 7 AND 8. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) - [SDR A6WA9900029](https://openairdocs.org/sdr/A6WA9900029), Jan 27, 1999: BRACKET. CRACKED. LEFT WING TE SHROUD UPPER SKIN STIFFENER TO FALSE SPARE ANGLE BRACKET CRACKED BETWEEN RIBS 7 AND 8. REPLACED BRACKET. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X - [SDR A6WA9900028](https://openairdocs.org/sdr/A6WA9900028), Jan 20, 1999: ANGLE. CORRODED. RIGHT WEB CLOSING ANGLE AFT OF FRAME 50 HAS ONE INCH CRACK. REPAIRED IAW BAE SRM 51-71-11 FIG 2. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) - [SDR A6WA9900033](https://openairdocs.org/sdr/A6WA9900033), Jan 16, 1999: STIFFENER. CRACKED. RIGHT WING STIFFENER BETWEEN RIBS 7 AND 8 CRACKED AT FORWARD END. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) - [SDR A6WA9900027](https://openairdocs.org/sdr/A6WA9900027), Jan 16, 1999: STIFFENER. CRACKED. LEFT WING STIFFENER BETWEEN RIBS 7 AND 8 CRACKED AT FORWARD ENGINE. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) - [SDR A6WA9900038](https://openairdocs.org/sdr/A6WA9900038), Jan 14, 1999: STRUCTURE. CRACKED. FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT UPPER AIRBRAKE HINGE CORNER IS CRACKED. REPAIRED PER BAE FAX JM/RJ0491-96. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. ( - [SDR A6WA9900037](https://openairdocs.org/sdr/A6WA9900037), Jan 14, 1999: STRUCTURE. CRACKED. FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE RIGHT UPPER AIRBRAKE HINGE CORNER IS CRACKED. REPAIRED PER FAX JM/RJ049-96. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) - [SDR A6WA9900036](https://openairdocs.org/sdr/A6WA9900036), Jan 14, 1999: RIVET. SHEARED. FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE RT UPPER AIRBRAKE HINGE HAS RIVETS SHEARED OFF FOR CORNER ANGLE BRACKET. REPLACED RIVETS. ACFT TT: 19,327 HOURS. ACFT T - [SDR A6WA9900035](https://openairdocs.org/sdr/A6WA9900035), Jan 14, 1999: RIVET. SHEARED. FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT AIRBRAKE HINGE HAS RIVETS SHEARED OFF FOR CORNER ANGLE BRACKET. REPLACED RIVETS. ACFT TT: 19,327 HOURS. ACFT TC: 22, - [SDR A6WA9900034](https://openairdocs.org/sdr/A6WA9900034), Jan 14, 1999: GUSSET. CRACKED. FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT UPPER AIRBRAKE HINGE HAS A FILLER PANEL CRACKED AT THE LIGHTNING HOLE. REPLACED GUSSET PLATE. ACFT TT: 19,327 HOURS. - [SDR A6WA9900022](https://openairdocs.org/sdr/A6WA9900022), Jan 10, 1999: ANGLE. CRACKED. FORWARD PASSENGER DOOR HAS 2 EACH CRACKED ANGLES IN THE HANDLE BOX AREA. MFG AND REPLACED PER BAE DRAWINGS HC521H0507 AND HC521H0508. INSTALLED ANGLES PER SRM A - [SDR A6WA9900026](https://openairdocs.org/sdr/A6WA9900026), Jan 9, 1999: GUSSET. CORRODED. SEVERAL GUSSET PLATES ON FLOOR ARE CORRODED (SURFACE CORROSION) AFT VESTIBULE. REPLACED CORRODED GUSSET PLATES, 2 EACH. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. - [SDR A6WA9900025](https://openairdocs.org/sdr/A6WA9900025), Jan 9, 1999: SEAT. CRACKED. FORWARD F/A SEAT PAN CRACKED. REPLACED PAN. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) - [SDR A6WA9900024](https://openairdocs.org/sdr/A6WA9900024), Jan 6, 1999: LONGERON. CRACKED. FRAME 29 MLG BAY ROOF LONGERONS CRACKED, NR 3 AND NR 15, NEAR FORWARD ENG. REPAIRED PER BAE REPAIR DRAWING HC536H9211. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. ( - [SDR A6WA9900023](https://openairdocs.org/sdr/A6WA9900023), Jan 6, 1999: BOLT. BROKEN. FRAME 29 LEFT AND RIGHT BOTTOM BOLT OF WING ATTACHMENT BRACKET HEAD APPEARS TO BE BROKEN. REMOVED BOLT, CLEANED AND INSPECTED HOLE, PREP, ALODINE, PRIMED AND IN - [SDR 99ZZZM601](https://openairdocs.org/sdr/99ZZZM601), Sep 13, 1998: STRUCTURE. CRACKED. DURING SCHEDULED NDT INSPECTION OF NGL RETRACTION JACK MOUNT STRUCTURE, FOUND CRAKS IN JACK PIN STRUCTURE BORE. (M) - [SDR 98ZZZX3983](https://openairdocs.org/sdr/98ZZZX3983), Apr 29, 1998: SWITCH. CONTAMINATED. MYR - FLT 690 - UPON GEAR RETRACTION, LANDING GEAR DID NOT RETRACT. CLEANED SQUAT SWITCHES. - [SDR 98ZZZX3984](https://openairdocs.org/sdr/98ZZZX3984), Mar 20, 1998: ROD. BROKEN. ATW - FORWARD PASSENGER DOOR DROPS BELOW DOOR FRAME WHEN OPENED AND DOES NOT DROP AND LATCH PROPERLY WHEN CLOSED. REPLACED BROKEN LOWER ROD END ON THE CONTROL S ## 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 19920106001959I](https://openairdocs.org/incident/19920106001959I), Jan 6, 1992: Bag BAE146200A (N290UE), Reno, NV. NR1 engine oil pressure fluctuating en route. Shut down before landing. Found oil pump had failed. - [Incident 19891006062909I](https://openairdocs.org/incident/19891006062909I), Oct 6, 1989: Bac 146200A (N290UE), Burbank, CA. Smoke from right engine on approach. Landed safely. Vapor trail caused by airflow disruption over broken tailpipe. --- 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.