# N292UE: British Aerospace BAE 146 SERIES 200A, registration cancelled 2008-04-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 3, 2008
- Exported to: Peru
- 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: E2087
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, normal
- Airworthiness date: February 5, 1988
- Certificate issued: January 27, 1988
- Last registry action: November 15, 2005
- Mode S code: A2FEAF
- 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/N292UE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=292UE
- Page: https://openairdocs.org/deregistered/N292UE-2008-04-03

From the FAA registry file of October 31, 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 (39)

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

- [SDR A6WA200460058](https://openairdocs.org/sdr/A6WA200460058), Nov 16, 2004: HOUSING. CHAFED. CHAFING ON THE LT SIDE OF THE AFT NAVIGATION LIGHT HOUSING. MAINTENANCE REQUESTED REPAIR.
- [SDR A6WA200460057](https://openairdocs.org/sdr/A6WA200460057), Nov 16, 2004: BEAM. DAMAGED. (3) BOLT HOLES ARE ELONGATED ON THE BEAM AT FRAME 45 RT MAINTENANCE REQUESTED REPAIR.
- [SDR A6WA200460056](https://openairdocs.org/sdr/A6WA200460056), Nov 16, 2004: LONGERON. CHAFED. CHAFING ON THE RT AIRBRAKE UPPER HINGE CUTOUT UPPER LONGERON. MAINTENANCE REQUESTED REPAIR.
- [SDR A6WA200460005](https://openairdocs.org/sdr/A6WA200460005), Mar 6, 2004: LINE. BROKEN. NR 1 ENGINE ANTI-ICE PIPE FRACTURED. ASSOCIATED CLAMP BRACKET ALSO BROKE. FRACTURED AT 90 DEGREE ELBOW AT FORWARD END. REPLACED PIPE ASSEMBLY AND BRACKET PIPE A
- [SDR A6WA200360066](https://openairdocs.org/sdr/A6WA200360066), Nov 6, 2003: STRUCTURE. DAMAGED. OVERSIZED BUSHING REQUIRED IN TWO PLACES ON RIGHT FLAP P/N HC579L1400-001, S/N 838H52-86. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1701-692001. (M)
- [SDR A6WA200360033](https://openairdocs.org/sdr/A6WA200360033), Aug 31, 2003: SPRING. BROKEN. NLG RIGHT WHEEL BRAKE, SPRING BROKEN. MAINTENANCE REMOVED AND REPLACED BROKENS SPRING GUIDE TUBE, SPRING AND REPAIRED DAMAGE TO THE CEILING OVER NLG BAY. (M)
- [SDR A6WA200360031](https://openairdocs.org/sdr/A6WA200360031), Aug 3, 2003: CIRCUIT BREAKER. INOPERATIVE. SMELLED ELECTRICAL SMOKE, SAW SPARKS FROM APU/ENGINE START PANEL, APPEARED TO BE START AND CONTINUOUS (A) CENTRAL C/B AND ALL IGNITION (A) AND CONTINUOUS IGNITI
- [SDR A6WA200360025](https://openairdocs.org/sdr/A6WA200360025), May 1, 2003: WARNING LIGHT. ILLUMINATED. MWS RUDDER VALVE LIGHT IS ILLUMINATED IN FLIGHT AFTER DEPARTURE. AIR RETURN TO ORD. RESET ABD, TESTED IAW.
- [SDR A6WA200100068](https://openairdocs.org/sdr/A6WA200100068), Dec 11, 2001: SLEEVE. OUT OF POSITION. EN ROUTE NOTICED FAINT ELECTRICAL SMELL, SWITCHED TO FRESH AIR MODE, ODOR DIMINISHED, BUT STILL PRESENT. ON APPROACH SWITCHED TO APU AIR ODOR GONE. MAINTENANCE 
- [SDR A6WA200100022](https://openairdocs.org/sdr/A6WA200100022), Mar 17, 2001: SLIDE. DEFECTIVE. FOUND FWD SERVICE DOOR EVACUATION SLIDE DEPLOYMENT CABLE NOT ATTACHED AND BOTTLE VALVE CABLE MISROUTED. DEPLOYMENT CABLE CONNECTION PIECES MISSING. MAINTENANCE 
- [SDR A6WA200100009](https://openairdocs.org/sdr/A6WA200100009), Jan 21, 2001: WARNING LIGHT. ILLUMINATED. ON DEPARTURE FROM ORD LT GEAR INTRANSIT LIGHT REMAINS ILLUMINATED. MAINTENANCE SECURED LT MLG DOOR IN INFLIGHT POSITION.
- [SDR A6WA200100001](https://openairdocs.org/sdr/A6WA200100001), Jan 13, 2001: LANDING GEAR. ICED. RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. MAINTENANCE FOUND THAT MLG SWITCHES HAVE EXTREME ICE BUILD-UP. DEICED GEAR, INSPECTED AND FOUND NO DAMAGE TO GEAR.
- [SDR A6WA0000017](https://openairdocs.org/sdr/A6WA0000017), Feb 10, 2000: FCU. MALFUNCTIONED. NR 2 ENGINE WHEN AT CRUISE 89-90 PERCENT N1, EXPERIENCED UNCOMMANDED POWER BACK TO 60 PERCENT N1, OTHER INDICATIONS FOLLOWED, 30 SECOND =/1 MINUTE STABILIZED. T
- [SDR A6WA0000004](https://openairdocs.org/sdr/A6WA0000004), Jan 6, 2000: IGNITOR. CRACKED. NR 1 ENGINE COMBUSTOR OUTBOARD IGNITOR BASE HAS CRACKED IN WELD, NEED DYE PENETRANT TO VERIFY LENGTH FOR SERVICEABILITY. C/W PT INSPECTION PER ENGINE MM AND AWA
- [SDR A6WA0000003](https://openairdocs.org/sdr/A6WA0000003), Jan 1, 2000: LINK. CHAFED. NR 1 PYLON TO WING LINK CHAFED, TOP END OUTBOARD SIDE. BLENDED AND POLISHED ABOVE CHAFFED AREA IN PYLON TO WING OUTBOARD LINK, AREA DETAILED VISUAL AND NDT. NO 
- [SDR A6WA0000005](https://openairdocs.org/sdr/A6WA0000005), Dec 13, 1999: RIB. CRACKED. RIGHT WING TIP FALSE RIB HAS A CRACK. REPAIRED ASSY PER ABOVE IAW AW-57-02-9412-06. (M)
- [SDR A6WR95070](https://openairdocs.org/sdr/A6WR95070), Jan 17, 1996: RIVETS. SHEARED. DURING SCHEDULED INSPECTION FOUND 2 RIVETS SHEARED OFF IN NR 2 PYLON BOX AT POSITIONS C AND D. REPLACED FASTENERS IAW AVRO RIL HC546H9009. (X)
- [SDR A6WR95069](https://openairdocs.org/sdr/A6WR95069), Jan 17, 1996: RIVETS. SHEARED. DURING SCHEDULED INSPECTION, FOUND 4 RIVETS SHEARED OFF IN NR 3 PYLON BOX AT POSITIONS A, B, C, AND D. REPLACED FASTENERS IAW AVRO RIL HC546H9009. (X)
- [SDR A6WR95068](https://openairdocs.org/sdr/A6WR95068), Jan 17, 1996: BRACKET. CRACKED. DURING SCHEDULED INSPECTION, FOUND NR 2 PYLON LORD MOUNT EYE BOLT BRACKET CRACKED. REPLACED BRACKET. (X)
- [SDR A6WR95067](https://openairdocs.org/sdr/A6WR95067), Jan 17, 1996: BRACKET. CRACKED. DURING SCHEDULED INSPECTION, FOUND NR 1 PYLON SHOULDER COWL LORD MOUNT ATTACHMENT BRACKET CRACKED. REPLACED BRACKET. (X)
- [SDR A6WR95066](https://openairdocs.org/sdr/A6WR95066), Jan 17, 1996: INTERCOSTAL. CORRODED. DURING STRUCTURAL INSPECTION, FOUND 2ND INTERCOSTAL INBOARD FROM LT FORWARD PASSENGER DOOR, BETWEEN FRAMES 15 AND 18, CORRODED. REPLACED INTERCOSTAL. (X)
- [SDR A6WR95065](https://openairdocs.org/sdr/A6WR95065), Jan 17, 1996: PLATE. CORRODED. DURING STRUCTURAL INSPECTION, FOUND TWO SUPPORT PLATES AT 3RD INTERCOSTAL INBOARD FROM LT FORWARD PASSENGER DOOR BETWEEN FUSELAGE FRAMES 15 AND 18 CORRODED. REP
- [SDR A6WR95064](https://openairdocs.org/sdr/A6WR95064), Jan 17, 1996: JO-BOLT. FAILED. DURING SCHEDULED INSPECTION, FOUND BROKEN HEAD ON JO-BOLT AT FRAME 29, STR 12 RIGHT. REPLACED JO-BOLT. (X)
- [SDR A6WR95063](https://openairdocs.org/sdr/A6WR95063), Jan 17, 1996: CONTROL CABLE. CORRODED. DURING SCHEDULED INSPECTION FOUND AILERON INTERCONNECT CABLES CORRODED AT WING ROOT PULLEYS. REPLACED CABLES. REFERENCE: OPERATOR CONTROL NR 96ZZZX761. (X)
- [SDR A6WR95062](https://openairdocs.org/sdr/A6WR95062), Jan 17, 1996: PIVOT PIN. CRACKED. DURING SCHEDULED NDT INSPECTION, FOUND NR 3 RIGHT FLAP TRACK TAB OPERATING ROD-TO-CROSSHEAD, PIVOT PIN WITH CRACK INDICATION. REPLACED PIN. (X)
- [SDR A6WR95061](https://openairdocs.org/sdr/A6WR95061), Jan 17, 1996: BOLT. CRACKED. DURING SCHEDULED NDT INSPECTION, FOUND CRACK INDICATION ON LEFT WING INBOARD AFT SPOILER JACK ATTACH BOLT. REPLACED BOLT. (X)
- [SDR A6WR95060](https://openairdocs.org/sdr/A6WR95060), Jan 17, 1996: PYLON. RIVETS SHEARED. DURING SCHEDULED INSPECTION, FOUND 3 RIVETS SHEARED OFF IN NR 4 PYLON BOX AT POSITIONS B, C, D. REPLACED FASTENERS IAW AVRO RL HC546H9009. (X)
- [SDR A6WR95059](https://openairdocs.org/sdr/A6WR95059), Jan 17, 1996: BRACKET. BROKEN. DURING SCHEDULED INSPECTION, FOUND BOTH LEFT SIDE BRACKETS SUPPORTING PRESSURE REGULATING/ISOLATION VALVE BROKEN IN NR 4 PYLON. REPLACED BRACKETS. REFERENCE: OP
- [SDR A6WR95058](https://openairdocs.org/sdr/A6WR95058), Jan 17, 1996: COMBUSTION CASE. FLANGE CRACKED. DURING SCHEDULED INSPECTION, FOUND BLEED AIR FLANGE AT 3 O'CLOCK POSITION ON COMBUSTION CASE CRACKED. REPAIRED IAW TEXTRON (ALLIED SIGNAL) ENGINE MM. (X)
- [SDR A6WR95057](https://openairdocs.org/sdr/A6WR95057), Jan 17, 1996: BOLT. CORRODED. DURING STRUCTURAL INSPECTION, FOUND RIGHT AILERON RIB 18 UPPER A-FRAME BOLT CORRODED. REPLACED BOLT. (X)
- [SDR A6WR95056](https://openairdocs.org/sdr/A6WR95056), Jan 17, 1996: HOSE. DEFECTIVE. DURING SCHEDULED INSPECTION, FOUND EXTERIOR COVERING OF APU FUEL SUPPLY HOSE BROKEN OPEN. REPLACED FUEL HOSE. (X)
- [SDR A6WR95054](https://openairdocs.org/sdr/A6WR95054), Jan 17, 1996: BOLT. CORRODED. DURING STRUCTURAL INSPECTION, FOUND RT ELEVATOR NR 1 HINGE A-FRAME LOWER BOLT CORRODED. REPLACED BOLT. (X)
- [SDR A6WR95053](https://openairdocs.org/sdr/A6WR95053), Jan 17, 1996: BOLT. CORRODED. DURING STRUCTURAL INSPECTION, FOUND CORROSION ON LT ELEVATOR NR 2 HINGE UPPER A-FRAME BOLT. REPLACED BOLT. (X)
- [SDR A6WR95052](https://openairdocs.org/sdr/A6WR95052), Jan 17, 1996: BOLT. DAMAGED. DURING STRUCTURAL INSPECTION, FOUND LT ELEVATOR NR 2 HINGE LOWER A-FRAME BOLT TO HAVE DAMAGED THREADS AND CORROSION. REPLACED BOLTS. (X)
- [SDR A6WR95051](https://openairdocs.org/sdr/A6WR95051), Jan 17, 1996: FREIGHT ANGLE. CRUSHED. FORWARD CARGO BAY FREIGHT ANGLE AT FRAME 21 CRUSHED. REPLACED FREIGHT ANGLE. (X)
- [SDR A6WR95050](https://openairdocs.org/sdr/A6WR95050), Jan 17, 1996: ROD END. WORN. FOUND WORN ROD-END ON ELEVATOR G-WEIGHT CONNECTING ROD. REPLACED ROD-END AND RIGGED SYSTEM IAW AMM. (X)
- [SDR 96ZZZX824](https://openairdocs.org/sdr/96ZZZX824), Jan 17, 1996: PLATE. CORRODED. DURING STRUCTURAL INSPECTION, FOUND TWO SUPPORT PLATES AT 3RD INTERCOSTAL INBOARD FROM LT FORWARD PASSENGER DOOR BETWEEN FUSELAGE FRAMES 15 AND 18 CORRODED. REP
- [SDR 96ZZZX761](https://openairdocs.org/sdr/96ZZZX761), Jan 17, 1996: CONTROL CABLE. CORRODED. DURING SCHEDULED INSPECTION FOUND AILERON INTERCONNECT CABLES CORRODED AT WING ROOT PULLEYS. REPLACED CABLES. REFERENCE: OPERATOR CONTROL NR A6WR95063.
- [SDR 96ZZZX760](https://openairdocs.org/sdr/96ZZZX760), Jan 17, 1996: BRACKET. BROKEN. DURING SCHEDULED INSPECTION, FOUND BOTH LEFT SIDE BRACKETS SUPPORTING PRESSURE REGULATING/ISOLATION VALVE BROKEN IN NR 4 PYLON. REPLACED BRACKETS. REFERENCE: OP

## FAA accident and incident reports (3)

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 19990219015449I](https://openairdocs.org/incident/19990219015449I), Feb 19, 1999: Bag BAE146200A (N292UE), Peoria, IL. (-5)At approximately 800 feet, on departure from runway 31, at Peoria Illinois airport (pia), February 19, 1999, air Wisconsin airlines d.b.a. united express,…
- [Incident 19980707030599I](https://openairdocs.org/incident/19980707030599I), Jul 7, 1998: Bag BAE146200A (N292UE), Rapid City, SD. Fire damaged suitcase was recovered from class d cargo compartment. Following scheduled flight. Suitcase contained tightly-packed clothing and a 3 peice baby…
- [Incident 19900718056589I](https://openairdocs.org/incident/19900718056589I), Jul 18, 1990: Bag BAE146100A (N292UE), Reno, NV, Minor damage. Tug rolled into aircraft when driver left tug in neutral. He got out with brakes set to help connect tow bar.

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