# N611AW: 1988 British Aerospace BAE 146 SERIES 300A, registration cancelled 2008-02-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 7, 2008
- Exported to: South Africa
- Status when cancelled: Valid registration
- Airframe: [British Aerospace BAE 146 SERIES 300A](https://openairdocs.org/model/british-aerospace-bae-146-series-300a) (registry code 1500267)
- 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: E3120
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, normal
- Airworthiness date: May 22, 1989
- Certificate issued: May 5, 2007
- Last registry action: May 5, 2007
- Mode S code: A7F28A
- 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/N611AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=611AW
- Page: https://openairdocs.org/deregistered/N611AW-2008-02-07

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 300A: https://openairdocs.org/model/british-aerospace-bae-146-series-300a.md

## Service difficulty reports (90, newest 50)

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

- [SDR A6WA200460020](https://openairdocs.org/sdr/A6WA200460020), Jun 7, 2004: SILL. CORRODED. L1 SILL PLATE CORRODED BEYOND LIMITS. SIL PLATE L1 REPAIRED IAW BAE SRM 51-43-00, 51-42-00 AND 51-23-00. (M)
- [SDR A6WA200460019](https://openairdocs.org/sdr/A6WA200460019), Jun 2, 2004: SKIN. SCRATCHED. AFT CARGO DOOR SCRATCHES BEYOND THE ALLOWABLE SRM LIMITS. MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS. MAINTENANCE CUT DAMAGED AREA OUT IAW BAE SRM 52-32-11 F
- [SDR A6WA200460018](https://openairdocs.org/sdr/A6WA200460018), May 28, 2004: FLAP TRACK. WORN. LT NR 2 FLAP TRACK HAS WEAR BEYOND THE SRM LIMITS MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS REF AVMAX FAX 611-1908004. DAMAGED AREA MAPPED AND SUBMITTED TO 
- [SDR A6WA200460017](https://openairdocs.org/sdr/A6WA200460017), May 28, 2004: FLAP TRACK. WORN. RT NR 2 FLAP TRACK HAS WEAR BEYOND THE SRM LIMITS. MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS REF AVMAX FAX 611-1908003. MAINTENANCE MAPPED AND SUBMITTED TO 
- [SDR A6WA200460016](https://openairdocs.org/sdr/A6WA200460016), May 26, 2004: FLOORBEAM. CRACKED. CRACK LOCATED IN THE LOWER RADIUS OF FLOORBEAM 33B AT LBL 62.0 INCHES. MAINTENANCE REQUESTED REPAIRS FROM MFG SYSTEMS REF AVMAX FAX 611-1908002. REPAIRED IAW BA
- [SDR A6WA200460014](https://openairdocs.org/sdr/A6WA200460014), May 9, 2004: FUEL CONTROL. FLUCTUATES. WHILE IN VMC CLIMBING THROUGH 16000 FEET THE NR 3 ENGINE N1 FLUCTUATION FOLLOWED BY FUEL FLOW DROPPING TO ZERO. ENGINE WAS SHUTDOWN, REMAINDER OF FLT MIN N2 OF 
- [SDR A6WA200360044](https://openairdocs.org/sdr/A6WA200360044), Oct 2, 2003: SKIN. LIGHTNING STRIKE. DAMAGE NOTED ON LEFT SIDE OF FUSELAGE DURING LIGHTNING STRIKE INSPECTION. EXIT BURN MARK LOCATED 8 INCHES AFT OF FRAME 19C BETWEEN STRINGER 21 AND 22 AT CENTER 
- [SDR A6WA200360029](https://openairdocs.org/sdr/A6WA200360029), May 23, 2003: CONDUIT. DAMAGED. FLANGED CONDUIT P/N HC535B0285-000 IS KINKED AND HAS TWO HOLES. MAINTENANCE WELDED CONDUIT IAW BAE FAX BARA/AVR/6411/03-DC. (M)
- [SDR A6WA200100050](https://openairdocs.org/sdr/A6WA200100050), Aug 3, 2001: ODOR. DETECTED. AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED SMELL IN FWD GALLEY AREA, GALLEY LOAD SHED, SMELL DISSIPATED. MAINTENANCE INSPECTED FWD CABIN AND GALLEY AREA, RAN ENGI
- [SDR A6WA200100011](https://openairdocs.org/sdr/A6WA200100011), Feb 3, 2001: COMPUTER. MALFUNCTIONED. AFTER TAKEOFF, FLAPS RETRACTED TO BETWEEN 0-18 DEGREES AND THEN STOPPED. AFTER CHECKLIST, RETRACTED TO 18 DEGREES RETURNED TO LANDING FLAP FAULT ILLUMINATED. MA
- [SDR A6WA200100010](https://openairdocs.org/sdr/A6WA200100010), Jan 21, 2001: CONNECTOR. DISCONNECTED. THREE LIGHTS IN FRONT OF PASSENGER CABIN NOT ILLUMINATING. MAINTENANCE CLEANED AND RESECURED CONNECTOR PLUG TO EMERGENCY POWER SUPPLY ABOVE ROW 7, OPS CHECKED G
- [SDR A6WA200000072](https://openairdocs.org/sdr/A6WA200000072), Dec 17, 2000: PROXIMITY SENSOR. MALFUNCTIONED. UNSAFE RIGHT MLG INTRANSIT LIGHT ON WITH GEAR SELECTED UP ALSO ASSOCIATED GEAR HANDLE LIGHT ON. MAINTENANCE CLEANED DOOR UPLOCK PROXY SENSORS AND GEAR PROXY SEN
- [SDR 99ZZZM603](https://openairdocs.org/sdr/99ZZZM603), Nov 11, 1998: FIRE BOTTLE. DAMAGED. ENGINE NOSE COWL WO NR BY8402 HAD FIRE BOTTLE CL978M HAS WORN THREADS ON JUNCTION BOX AND CONTROL HEAD. REM AND REPLACED FIRE BOTTLE. (M)
- [SDR 99ZZZM599](https://openairdocs.org/sdr/99ZZZM599), Jul 28, 1998: MASK. CRACKED. FORWARD AFT FACING F/A OXYGEN BOTTLE, MASK FACE PIECE CRACKED. REPLACED OXYGEN MASK, OPS CHECKS OK. (M)
- [SDR 99ZZZM600](https://openairdocs.org/sdr/99ZZZM600), Jul 27, 1998: VALVE. FAILED. CABIN OXYGEN SYSTEM FAILED LEAK CHECK. TROUBLESHOOT SYSTEM. REPLACED PAX ISO VLV, 5 QUICK DISC (OUTLETS), 4 RT BOX ASSY. SEE W/C'S FOR PARTS CHANGED, SYSTEM LEA
- [SDR 99ZZZM591](https://openairdocs.org/sdr/99ZZZM591), Jul 27, 1998: MASK. TORN. OXYGEN MASK AT 9 RT FACE PIECE TORN. REPLACED OXYGEN MASK 9 RT, OPS AND LEAK CHECKS OK. (M)
- [SDR 99ZZZM585](https://openairdocs.org/sdr/99ZZZM585), Jul 27, 1998: OUTLETS. LEAKING. FOUND OXYGEN OUTLETS AT RT 6, 14, 17, 20, AND 21 LEAKING. REPLACED OUTLETS AT RT 6, 14, 17, 20, AND 21. LEAK CHECK OK. (M)
- [SDR 99ZZZM583](https://openairdocs.org/sdr/99ZZZM583), Jul 27, 1998: OXYGEN BOX. LEAKING. FOUND OXYGEN BOX AT 4 RT LEAKING THROUGH MASK WITH PIN INSTALLED. REPLACED OXYGEN BOX ASSY, OPS AND LEAK CHECKS OK.
- [SDR 99ZZZM580](https://openairdocs.org/sdr/99ZZZM580), Jul 23, 1998: MANIFOLD. LEAKING. FOUND 4 RT OXYGEN BOX, 2 MASK LEAKING WITH PINS INSTALLED, OXYGEN MASK FACE PIECE TORN. REPLACED 4 RIGHT OXYGEN MANIFOLD, OPS AND LEAK CHECKS OK. REPLACED MASK 
- [SDR 99ZZZM590](https://openairdocs.org/sdr/99ZZZM590), Jul 21, 1998: DOOR. CHAFED. NR 3 ENGINE INBOARD FAN DOOR LOWER SPLITTER AREA, 2ND STIFFENER FROM FORWARD CHAFED. REPLACED THE NR 3 ENGINE INBOARD FAN DOOR LOWER SPLITTER AREA, 2ND STIFFENE
- [SDR 99ZZZM589](https://openairdocs.org/sdr/99ZZZM589), Jul 20, 1998: DOOR. DAMAGED. NR 1 EIGNE INBOARD REAR COWL DOOR HAS A HOLE WORN THROUGH THE TOP 3RD RIB BACK FROM THE FRONT CORNER OF THE DOOR. REPLACED THE TOP THIRD RIB FROM THE FRONT EDGE
- [SDR 99ZZZM587](https://openairdocs.org/sdr/99ZZZM587), Jul 20, 1998: STIFFENER. CRACKED. LT WING TOP SKIN TE SHROUD OUTBOARD STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 8/9. REPAIRED ABOVE STIFFENER PER BAE FAX JM/RJO317/97 USING 2 024T3 .050. (M)
- [SDR 99ZZZM572](https://openairdocs.org/sdr/99ZZZM572), Jul 20, 1998: INTERCOSTAL. CRACKED. AFT AIRSTAIR OUTBOARD RAIL INTERCOSTAL CRACK AT FLOOR, AFT END. REMOVED AND REPLACED AFT AIRSTAIR OUTBOARD RAIL INTERCOSTAL AT AFT END OF RAIL. WORK DONE IAW BA
- [SDR 99ZZZM596](https://openairdocs.org/sdr/99ZZZM596), Jul 17, 1998: BRACKET. CRACKED. LEFT WING HYD LINE CLAMP BRACKET CRACKED AT FALSE SPAR, RIB NR 3. REMOVED AND REPLACED ABOVE BRACKET. (M)
- [SDR 99ZZZM592](https://openairdocs.org/sdr/99ZZZM592), Jul 17, 1998: TREAD PLATE. CORRODED. LEFT FORWARD TREAD PLATE (E804) HAS CORROSION ON INNER SURFACE. REMOVED CORROSION ON LT FORWARD TREAD PLATE 9E804). (M)
- [SDR 99ZZZM613](https://openairdocs.org/sdr/99ZZZM613), Jul 15, 1998: STRUCTURE. CORRODED. FOUND CORROSION AROUND MOUNTING HOLES FOR GALLEY. REMOVED CORROSION, TREATED, PRIMED AND PAINTED APPLICABLE AREAS AROUND GALLEY MOUNTING HOLES. (M)
- [SDR 99ZZZM612](https://openairdocs.org/sdr/99ZZZM612), Jul 15, 1998: RIVETS. FAILED. CABIN FLOOR OUTBOARD SUPPORT ANGLE HAS 2 POPPED RIVETS AT FRAME 26 (RIGHT SIDE AFT OF FRAME). REPLACED RIVETS. (M)
- [SDR 99ZZZM597](https://openairdocs.org/sdr/99ZZZM597), Jul 15, 1998: FLOORBEAM. CRACKED. CABIN PRESS FLOORBEAM NR 3 CRACKED AT FRAME 29, LEFT OUTBOARD SEAT RAIL. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. (M)
- [SDR 99ZZZM588](https://openairdocs.org/sdr/99ZZZM588), Jul 15, 1998: COWL. CRACKED. NR 2 ENGINE PYLON SHOULDER COWL HAS CRACKED SKIN BETWEEN THE BIG HYD PIPE AND THE DRAIN TUBE. REPAIRED ABOVE CRACK USING .040 TA 2 PER FAX KG/0603-91 AND SRM. (
- [SDR 99ZZZM582](https://openairdocs.org/sdr/99ZZZM582), Jul 15, 1998: STEP. CORRODED. AFT AIRSTAIRS, SECOND FROM THE TOP STEP CORRODED. REPLACED STEP.
- [SDR 99ZZZM579](https://openairdocs.org/sdr/99ZZZM579), Jul 15, 1998: FLOORBEAM. CRACKED. CABIN PRESS FLOORBEAM NR 19 (RIGHT OUTBOARD SEAT RAIL) CRACKED AT FRAME 29. REPAIRED PER FAX REF DJR/RJO207-97 AND REPAIR DRAWING HC536H9211. (M)
- [SDR 99ZZZM578](https://openairdocs.org/sdr/99ZZZM578), Jul 15, 1998: FLOORBEAM. CRACKED. CABIN PRESSURE FLOORBEAM NR 13 CRACKED AT FRAME 29. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97.
- [SDR 99ZZZM577](https://openairdocs.org/sdr/99ZZZM577), Jul 15, 1998: FLOORBEAM. CRACKED. CABIN PRESS FLOORBEAM NR 15 CRACKED AT FRAME 29, RIGHT INBOARD SEAT RAIL. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. (M)
- [SDR 99ZZZM576](https://openairdocs.org/sdr/99ZZZM576), Jul 15, 1998: FLOORBEAM. CRACKED. CABIN PRESS FLOORBEAM NR 3 CRACKED AT FRAME 29, LT OUTBOARD SEAT RAIL. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. (M)
- [SDR 99ZZZM575](https://openairdocs.org/sdr/99ZZZM575), Jul 15, 1998: FLOORBEAM. CRACKED. CABIN PRESS FLOORBEAMS NR 9 CRACKED AT FRAME 29. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. (M)
- [SDR 99ZZZM571](https://openairdocs.org/sdr/99ZZZM571), Jul 15, 1998: SILL. CORRODED. PAX DOOR SILL PLATE SOME LIGHT SURFACE CORROSION, MARKED W/DOT. REMOVED CORROSION, TREATED, PRIMED AND PAINTED APPLICABLE AREA. (M)
- [SDR 99ZZZM584](https://openairdocs.org/sdr/99ZZZM584), Jul 14, 1998: DOOR. CHAFED. NR 3 ENGINE INBOARD FAN DOOR INNER TITANIUM DISHING CHAFED THROUGH. REPAIRED CHAGED AREA OF NR 3 ENGINE INBOARD FAN DOOR INNER SKIN IAW 146 RIL HC711H9047. (M)
- [SDR 99ZZZM586](https://openairdocs.org/sdr/99ZZZM586), Jul 13, 1998: DOOR. CHAFED. NR 4 ENGINE INBOARD FAN DOOR INNER TITANIUM SKIN CHAFED THROUGH JUST ABOVE DISHING AREA. REPAIRED CHAFED AREA IAW RIL HC711H9047. (M)
- [SDR 99ZZZM581](https://openairdocs.org/sdr/99ZZZM581), Jul 13, 1998: STAIR. CORRODED. AFT AIRSTAIRS, SECOND FROM THE TOP STEP CORRODED. REPLACED STEP.
- [SDR 99ZZZM595](https://openairdocs.org/sdr/99ZZZM595), Jul 10, 1998: BRACKET. CRACKED. RIGHT WING TE HYD CLAMP BRACKET CRACKED AT FALSE SPAR, RIB 6. ALSO, HYD CLAMP LOOSE OUTBOARD OF RIB 6. REPLACED ONE RIGHT WING TRAILING EDGE HYD CLAMP BRACKET (
- [SDR 99ZZZM594](https://openairdocs.org/sdr/99ZZZM594), Jul 9, 1998: STRUCTURE. WORN. NR 3 PYLON SHOULDER COWL AFT LORD MOUNT ATTACH HOLES WORN AND SLOPPY AT SHOULDER COWL STRUCTURE. REPAIR PER RI HC710H9033. REPAIRED NR 3 PYLON SHOULDER COWL AFT
- [SDR 99ZZZM593](https://openairdocs.org/sdr/99ZZZM593), Jul 9, 1998: ANGLE. CRACKED. RIGHT WING TE LOWER SKIN, INBOARD STIFFENER BETWEEN RIBS 8/9 TAG ANGLE CRACKED AFT END OF STIFFENER. REPLACED SAID TAG ANGLE AND FOUND SERVICEABLE. (M)
- [SDR 99ZZZM573](https://openairdocs.org/sdr/99ZZZM573), Jul 9, 1998: CONTROL CABLE. CORRODED. BOTH CENTER AILERON INTERCONNECT CABLES ARE CORRODED. REMOVED AND REPLACED BOTH CENTER AILERON INTERCONNECT CABLES, GENERATED NEW WC FOR TRAVEL CHECKS AND FREED
- [SDR 99ZZZM574](https://openairdocs.org/sdr/99ZZZM574), Jul 7, 1998: TRIM STRIP. CORRODED. FRAME 18 TRIM STRIP FOR UNDER RIGHT BULKHEAD BADLY CORRODED, REPLACED. REMOVED AND REPLACED FRAME 18 TRIM STRIP.
- [SDR 99ZZZM598](https://openairdocs.org/sdr/99ZZZM598), Jul 1, 1998: SLIDE. CRACKED. LEFT FORWARD EVAC SLIDE PACK BOARD CRACKED AT TOP MOUNT PP PIN. REMOVED SLIDE ASSY AND PLACED ON W/O, P/N 31050-105, S/N 0093, REF W/C 8012 FOR INSTALLATION. (M
- [SDR 99ZZZM535](https://openairdocs.org/sdr/99ZZZM535), Jan 16, 1998: ENGINE. FAILED. NR 1 ENGINE FAILED ON CLIMB-OUT FROM SBA TO DEN. DIVERTED TO LAS. REMOVED AND REPLACED NR 1 ENGINE IAW AWAC ENDING CHANGE CHECKLIST AND AIRCRAFT MM. (M)
- [SDR 98ZZZX1197](https://openairdocs.org/sdr/98ZZZX1197), Jan 16, 1998: ENGINE. FAILED. SBA - FLT 586 - NR 1 ENGINE FAILED ON CLIMB-OUT FROM SBA TO DEN - DIVERTED TO LAS. UNDER FURTHER INVESTIGATION.
- [SDR 98ZZZM96](https://openairdocs.org/sdr/98ZZZM96), Jul 29, 1997: VALVE. FAILED. NR 3 NOSE COWL FLOW CONTROL VALVE WAS FOUND TO HAVE A RIVET IN THE FAIL/SAFE MODE TO BE WORN EXCESSIVELY. REPLACED VALVE. (M)
- [SDR 97ZZZX3050](https://openairdocs.org/sdr/97ZZZX3050), Jun 26, 1997: FIRE WIRE. CHAFED. ATW - NR 2 ENGINE INBOARD FIRE EXTINGUISHER WIRES ARE CHAFED BY NOSE COWL DISCONNECT. REPLACED WIRES 2WB170 AND 2WB173. SEE ENGINE CHANGE CHECK LIST FOR TEST OF
- [SDR 97ZZZX3109](https://openairdocs.org/sdr/97ZZZX3109), Apr 3, 1997: SKIN. CRACKED. LEFT WING TOP TRAILING EDGE SHROUD HAS A STIFFENER WITH A CRACK AT FORWARD END APPROXIMATELY .75 INCH LONG LOCATED IN AREA BETWEEN WING RIBS 5 AND 6. REPAIRED T

All 90: https://openairdocs.org/deregistered/N611AW-2008-02-07/reports.md

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CHI95IA079](https://openairdocs.org/ntsb/CHI95IA079), Jan 27, 1995: British Aerospace BAE-146-300 (N611AW), Madison, WI, incident, no damage. Probable cause: A fuel leak in the no. 2 engine left fuel manifold segment due to a design defect which led to a fatigue crack.
- [NTSB CHI93IA312](https://openairdocs.org/ntsb/CHI93IA312), Jul 21, 1993: British Aerospace 146-300A (N611AW), Chicago, IL, incident, minor damage. Probable cause: was a crack in the fuel system fuel flow distribution manifold which resulted from an inadequate design by the manufacturer.

## Other aircraft with N611AW

- [Registered now](https://openairdocs.org/aircraft/N611AW): Cirrus Design SR22T, S/N 11020, built 2025

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