# N607AW: 1986 British Aerospace BAE 146 SERIES 200A, registration cancelled 2006-07-20

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 20, 2006
- 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: E2052
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: February 14, 1986
- Certificate issued: January 14, 1986
- Last registry action: May 16, 2006
- Mode S code: A7E155
- Owner when cancelled: [Wilmington Tr Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TR%20CO%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N607AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=607AW
- Page: https://openairdocs.org/deregistered/N607AW-2006-07-20

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 (72, newest 50)

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

- [SDR A6WA200560021](https://openairdocs.org/sdr/A6WA200560021), Mar 6, 2006: FLAP SYSTEM. MALFUNCTIONED. WHEN DEPARTING, FLAPS FAIL AT 18 DEGREES. BOTH FLAP INOP LIGHT AND FLAP FAULT LIGHT ILLUMINATED, FOLLOW ALL QRH CHECKLIST LANDING. ECU FAULT LED NR 4 SHOWING C/
- [SDR A6WA200460025](https://openairdocs.org/sdr/A6WA200460025), Jul 17, 2004: BOLT. CORRODED. FOUND CORROSION ELEVATOR HINGE A-FRAME ATTACHMENT BOLTS TWO EACH. REPLACED NEW. (M)
- [SDR A6WA200460027](https://openairdocs.org/sdr/A6WA200460027), Jul 17, 2004: ANGLE. CORRODED. FOUND CORROSION ON INTERCOSTAL AT CETNER JOINT PLATE 80 INCHES FROM DOOR 1L. REPLACED ANGLE, IAW BAE SRM 51-42-00 AND 51-23-00. (M)
- [SDR A6WA200460015](https://openairdocs.org/sdr/A6WA200460015), May 12, 2004: FLAP TRACK. WORN. NR 2 FLAP TRACK, WEAR FOUND ON NR 2 LT LOWER ROLLER THAT MEASURES .033 INCHES DEEP. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 607-1907002. MAINTENANCE REM
- [SDR A6WA200460030](https://openairdocs.org/sdr/A6WA200460030), May 11, 2004: INTERCOSTAL. CRACKED. FOUND INTERCOSTAL CRACKED BETWEEN FRAMES 22/23 AT STRINGER 21 RIGHT IN FORWRAD CARGO COMPARTMENT. MAINTENANCE REPLACED INTERCOSTAL IAW BAE SRM 51-23-00, 51-42-0
- [SDR A6WA200460031](https://openairdocs.org/sdr/A6WA200460031), May 11, 2004: INTERCOSTAL. CRACKED. FOUND INTERCOSTAL CRACKED BETWEEN FRAMES 21/22 AT STRINGER 21 RT IN FORWARD CARGO BAY. MAINTENANCE REPLACED INTERCOSTAL IAW SRM 51-23-00, 51-42-00, AND 51-43-00
- [SDR A6WA200460028](https://openairdocs.org/sdr/A6WA200460028), May 10, 2004: FLOOR SUPPORT. CORRODED. FOUND CORROSION ON FLOOR SUPPORT MEMBER ADJACENT TO FLOORBEAM 15.52 INCHES FROM DOOR 1L. MAINTENANCE REPLACED JOINT PLATE WITH MANUFACTURED REPAIR PART IAW BAE 
- [SDR A6WA200460029](https://openairdocs.org/sdr/A6WA200460029), May 10, 2004: STRINGER. CORRODED. FOUND CORROSION ON CENTER LINE STRINGER IN FORWARD CARGO PIT BETWEEN FORWARD AND AFT RADIO ALT ANTENNAS. MAINTENANCE REPLACED STRINGER WITH MANUFACTURED REPAIR 
- [SDR A6WA200460001](https://openairdocs.org/sdr/A6WA200460001), Jan 5, 2004: APU. INOPERATIVE. SMOKE IN CABIN WHEN APU IS SUPPLYING AIR TO PACKS. MAINTENANCE PERFORMED PACK BURNOUT AND REMOVED AND REPLACED APU. (M)
- [SDR A6WA200360070](https://openairdocs.org/sdr/A6WA200360070), Dec 12, 2003: STRINGER. CORRODED. FOUND STRINGER 34R HAS CORROSION. MAINTENANCE REPAIRED STRINGER 34R BETWEEN FRAMES 20B AND 21 IAW BAE FAX BARA/AVR/6609/03-DC AND IAW BAE SRM 51-43-00. (M)
- [SDR A6WA200360069](https://openairdocs.org/sdr/A6WA200360069), Dec 9, 2003: SKIN. DAMAGED. FOUND CRACKS ON THE LEFT AND RIGHT FUSELAGE ABOVE STRINGER 13 JUST AFT OF FRAME 29 EMANATING FROM THE RIVIT LOCATIONS. MAINTENANCE CUT OUT DAMAGE TO SKIN IAW BA
- [SDR A6WA200360067](https://openairdocs.org/sdr/A6WA200360067), Dec 9, 2003: STRUCTURE. DAMAGED. RIGHT FLAP AT THE NR 4 POSITION BETWEEN RIBS 33 AND 34 OVERSIZE BUSHING REQUIRED. BUSHING LOCALLY MANUFACTURED AT AAO AND CAD PLATED IAW BAE FAX BARA/AVR/6605/0
- [SDR A6WA20030069](https://openairdocs.org/sdr/A6WA20030069), Dec 9, 2003: SKIN. CRACKED. FOUND CRACKS ON THE LEFT AND RIGHT FUSELAGE ABOVE STRINGER 13 JUST AFT OF FRAME 29 EMANATING FROM THE RIVET LOCATIONS. MAINTENANCE REQUESTED REPAIR FROM BAE SYS
- [SDR A6WA200360068](https://openairdocs.org/sdr/A6WA200360068), Dec 9, 2003: FLAP TRACK. WORN. RT NR 1 FLAP TRACK WEAR UPPER AND LOWER RAILS OUTBOARD FACE. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1734-6070003. LPI C/O ON BLENDED FLAP T
- [SDR A6WA200350067](https://openairdocs.org/sdr/A6WA200350067), Dec 9, 2003: STRUCTURE. DAMAGED. RIGHT FLAP AT THE NR 4 POSITION BETWEEN RIBS 33 AND 34 OVERSIZE BUSHING REQUIRED. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 134-6070002. (M)
- [SDR A6WA200360064](https://openairdocs.org/sdr/A6WA200360064), Oct 29, 2003: WIRE. BURNED. APU GENERATOR INOPERATIVE. DURING MAINTENANCE CORRECTIVE ACTION FOUND 3 APU GENERATOR WIRES IN FORWARD CARGO BAY CEILING BURNED AND EVIDENCE OF ARCHING ON CARGO
- [SDR A6WA200360039](https://openairdocs.org/sdr/A6WA200360039), Sep 22, 2003: SKIN. CRACKED. RIGHT FUSELAGE SKIN AT FRAME 32 ABOVE STRINGER 19 HAS A .0250 INCH CRACK ORIGINATING AT FASTENER. REPAIR I/P. (M)
- [SDR A6WA200360004](https://openairdocs.org/sdr/A6WA200360004), Mar 28, 2003: FUEL CONTROL. MALFUNCTIONED. AT FL280, OAT -40 DEGREES C, TMS OFF, ANY REDUCTION IN POWER OF NR 3 ENGINE FUEL FLOW WOULD DROP TO 300 NR A FEW SECONDS. OTHER ENGINE INSTRUMENTS WOULD DROP AC
- [SDR A6WA200100027](https://openairdocs.org/sdr/A6WA200100027), Mar 29, 2001: SLIDE. UNSERVICEABLE. FOUND THE FWD PAX DOOR EVACUATION SLIDE CABLE RELEASE NOT ATTACHED TO GIRT BAR. MAINTENANCE REMOVED AND REPAIRED EVACUATION SLIDE.
- [SDR A6WA200100013](https://openairdocs.org/sdr/A6WA200100013), Jan 26, 2001: SLIDE. WILL NOT TEST. LIGHTS ON EMERGENCY ESCAPE SLIDE NOT ILLUMINATE DUE TO PIN IN BATTERY NOT BEING PULLED OUT UPON DEPLOYMENT. SNAP THAT HOLDS PIN LANYARD BECAME DETACHED INSTEAD.
- [SDR A6WA9900082](https://openairdocs.org/sdr/A6WA9900082), Jul 24, 1999: SWITCH. DIRTY. LOWER DOOR NOT SHUT ON MWS PANEL, CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF AND VERIFIED ALL DOORS SHUT. CLEANED AND INSPECTED LOWER DOOR SWITCHES, ALL CHECK
- [SDR A6WA9900046](https://openairdocs.org/sdr/A6WA9900046), May 27, 1999: BEARING. FAILED. REMOVED NR 1 TIRE ASSY, FOUND NR 1 WHEEL INNER BEARING SEIZED ONTO THE AXEL. REMOVED AND REPLACED LEFT MLG AXEL, WHEELS AND NR 1 HEAT PACK AND BRAKE. NR 1 BRAKE
- [SDR 99ZZZM792](https://openairdocs.org/sdr/99ZZZM792), Feb 16, 1999: COMPRESSOR. DAMAGED. NR 1 ENGINE VIBRATION 2.5 AIRBORN ENGINE SHUTDOWN BY EMERGENCY CHECKLIST. INSPECTED AND FOUND BLADES MISSING FROM NR 3 AND NR 4 WHEEL AND DAMAGE TO NR 2 WHEEL A
- [SDR 99ZZZX2697](https://openairdocs.org/sdr/99ZZZX2697), Feb 6, 1999: COMPRESSOR. FAILED. DEN - FLT 595 - NR 1 ENGINE: VIBRATION 2.5 AIR-BORN. ENGINE SHUT DOWN BY EMERGENCY CHECKLIST. INSPECTED AND FOUND BLADES MISSING FROM NR 3 AND NR 4 WHEEL AND DA
- [SDR 99ZZZX2698](https://openairdocs.org/sdr/99ZZZX2698), Jan 23, 1999: PIN. FAILED. UPON REMOVAL OF NOSE LANDING GEAR RETRACTION JACK, FOUND PIN AT GEAR BAY SIDEWALL SHEARED. RETRACTION JACK REMOVED FOR E.O. E98/002/632. REMOVED AND REPLACED TH
- [SDR 99ZZZM551](https://openairdocs.org/sdr/99ZZZM551), Jan 23, 1999: ACTUATOR. FAILED. UPON REMOVAL OF NOSE LANDING GEAR RETRACTION JACK FOUND PIN AT GEAR BAY SIDEWALL SHEARED. RETRACTION JACK REMOVED FOR EO E98/002/632. REMOVED AND REPLACED THE N
- [SDR 98ZZZM691](https://openairdocs.org/sdr/98ZZZM691), Feb 27, 1998: TRIM. BINDS. ELEVATOR TRIM BINDS AT ALL SPEEDS, ALL ALTITUDES WHEN MOVED FORWARD OF 3 ON THE TRIM INDICATOR.
- [SDR 98ZZZM692](https://openairdocs.org/sdr/98ZZZM692), Feb 26, 1998: TRIM. BINDS. AT 20,000 FT 290 KTS ELEV TRIM BINDS WHEN TRYING TO TRIM NOSE DOWN, NOSE UP FEELS NORMAL. PERFORMED ELEV TRIM CIRCUIT FRICTION TST, ALSO PERFORMED CLUTCH FRICTI
- [SDR 98ZZZX1183](https://openairdocs.org/sdr/98ZZZX1183), Nov 19, 1997: PANEL. LOOSE. ATW - FLT 505 - ON CLIMB-OUT ACCELERATING THROUGH 240-250 KNOTS, FELT SLIGHT AIRFRAME VIBRATION. AS SPEED INCREASED, VIBRATION INCREASED. REPLACED PANEL ON RT T
- [SDR 98ZZZX1188](https://openairdocs.org/sdr/98ZZZX1188), Nov 2, 1997: RETRACT MECH. MALFUNCTIONED. DEN - FLT 669 - FLAPS WOULD NOT MOVE FROM THE 24 DEGREE POSITION IN THE AIR. CLEARED FLAP FAULT AND OPS TESTED GOOD.
- [SDR 98ZZZX1189](https://openairdocs.org/sdr/98ZZZX1189), Nov 1, 1997: AIR DISTRIBUTION. ODOR. ATW - WHEN SWITCHING AIR FROM APU TO ENG AIR, NR 1 PACK GIVES A STRONG OIL BURNING SMELL FOR A FEW MINUTES THEN IT CLEARS. OPS CHECKED NR 1 PACK ON THE GROUND W
- [SDR 98ZZZM90](https://openairdocs.org/sdr/98ZZZM90), Sep 14, 1997: LINE. FAILED. GREEN HYD SYSTEM LOW QTY AND LOW PRESS IN FLT. REPLACED HYD RETURN HOSE TO LEFT MLG RETRACTION JACK. (M)
- [SDR 98ZZZM89](https://openairdocs.org/sdr/98ZZZM89), Aug 22, 1997: TERMINAL BLOCK. CORRODED. TWO TERMINAL BLOCKS BELOW THE INBOARD AIRSTAIR DRIP TRAY FOR THE PAX DOOR ARE CORRODED AND NEEDS TO BE CLEANED. REPLACED TERMINAL BLOCKS AA AND AB IN ZONE 131-0
- [SDR 98ZZZM88](https://openairdocs.org/sdr/98ZZZM88), Aug 18, 1997: BRACKET. WORN. NLG AFT DOOR STOP ASSY MATERIAL MORE THAN 50 PERCENT WORN. REPLACED DOOR STOP BRACKET. DOOR CLEARANCES TO BE CHECKED ON GEAR SWING INSTALLATION. (M)
- [SDR 98ZZZM87](https://openairdocs.org/sdr/98ZZZM87), Aug 18, 1997: SEAT RAIL. CORRODED. FORWARD RIGHT I/N SEAT RAIL HAS CORROSION PAST LIMITS (FWD 23 INCHES). REMOVED 24 INCHES OF SEAT RAIL RT INBOARD FORWARD AND SPLICED IN NEW SECTION OF SEAT RAIL
- [SDR 98ZZZM63](https://openairdocs.org/sdr/98ZZZM63), Aug 15, 1997: TRACK. WORN. LEFT NR 1 FLAP TRACK SHOWS WEAR ON OUTBOARD SURFACES OF UPPER AND LOWER RAILS. BLENDED WORN AREAS IAW BAE ATW FAX DJR/RJ0647-97. MAX CLEARANCE WITH NEWPADS IS .
- [SDR 98ZZZM62](https://openairdocs.org/sdr/98ZZZM62), Aug 15, 1997: ROLLER. CORRODED. LEFT FLAP NR 1 CARRIAGE ROLLER ASSY TO LICK ATTACH BOLT CORRODED. REMOVED AND REPLACED CORRODED ROLLER TO CARRIAGE ATTACH BOLT.
- [SDR 98ZZZM61](https://openairdocs.org/sdr/98ZZZM61), Aug 15, 1997: SEAT RAIL. CORRODED. FORWARD LEFT .1B SEAT RAIL HAS CORROSION PAST LIMITS, APPROX 64 INCH LENGTH. REMOVED 65 INCHES FORWARD SECTION OF LEFT INBOARD SEAT RAIL ASSY AND SPLICED REPLAC
- [SDR 98ZZZM60](https://openairdocs.org/sdr/98ZZZM60), Aug 13, 1997: CONTROL CABLE. CORRODED. RIGHT AILERON CABLES CORRODED AT BELLCRANK AT RIB NR 10. REMOVED AND REPLACED BOTH RIGHT MAIN AILERON OUTER CONTROL CABLES, TENSIONED AND SAFETIED IAW BAE MM.
- [SDR 98ZZZM59](https://openairdocs.org/sdr/98ZZZM59), Aug 13, 1997: CONTROL CABLE. CORRODED. LEFT OUTER AILERON CONTROL CABLE HAS RUST ON OUTER CABLE QUANDRANT. REMOVED AND REPLACED BOTH LEFT MAIN AILERON OUTER CONTROL CABLES, TENSIONED AND SAFETIED IAW
- [SDR 98ZZZM58](https://openairdocs.org/sdr/98ZZZM58), Aug 8, 1997: STIFFENER. CRACKED. LEFT WING, TRAILING EDGE AREA AFT OF REAR SPAR HAS A CRACKED STIFFENER ON LOWER SHROUD SKIN BETWEEN WING RIBS NR 7 AND 8. REPLACED STIFFENER AND PAINTED.
- [SDR 98ZZZM57](https://openairdocs.org/sdr/98ZZZM57), Aug 7, 1997: STIFFENER. CRACKED. LEFT WING T/E SHROUD AREA BETWEEN WING WIBS NR 8 AND 9 HAS THE TWO UPPER SKIN STIFFENERS WITH CRACKS AT THEIR FWD ENDS. REPAIRED OUTBOARD STIFFENER PER FAX JM/R
- [SDR 98ZZZM56](https://openairdocs.org/sdr/98ZZZM56), Aug 6, 1997: BRACKET. CRACKED. LEFT WING T/E AREA AT WING RIB NR 8 HAS A CRACKED HYD LINE BRACKET WHICH IS ALLOWING HYD LINE TO CHAF ON THE TAIL RIB. HYD LINE IS GOING OUT OT OUTBOARD LIFT SP
- [SDR 98ZZZM55](https://openairdocs.org/sdr/98ZZZM55), Aug 5, 1997: BRACKET. CRACKED. NR 4 ENGINE LEFT FAN DOOR HAS ONE BRACKET CRACKED AND ONE RIVET HEAD SHEARED ON BOTTOM SPLITTER. REPLACED ONE SHEARED RIVET HEAD AND ONE BRACKET ON NR 4 ENGINE 
- [SDR 98ZZZM54](https://openairdocs.org/sdr/98ZZZM54), Aug 5, 1997: ANGLE. CRACKED. CENTER MLG BAFFLE UPPER ATTACHMENT ANGLE CRACKED THROUGH TWO RIVETS 1.5625 INCHES IN LENGTH. REPAIR/REPLACE NO LATER THAN 34926 TCA AS PER AVRO FAX DJR/RJ1322-9
- [SDR 98ZZZM53](https://openairdocs.org/sdr/98ZZZM53), Aug 4, 1997: JAMB. CRACKED. NR 4 ENGINE RIGHT FAN DOOR BOTTOM EDGE MEMBER NEEDS A CRACK DRESSED OUT AND TREATED. DRESSED OUT DOOR EDGE MEMBER CRACK AT REQUESTED AT THIS TIME. REPAINTED ENT
- [SDR 98ZZZM52](https://openairdocs.org/sdr/98ZZZM52), Aug 4, 1997: MOUNT BOLT. DAMAGED. LEFT ELEVATOR NR 2 HINGE A FRAME UPPER MOUNT BOLT FAILS DETAILED VISUAL INSPECTION. REPLACED UPPER MOUNT BOLT WITH SERVICEABLE BOLT.
- [SDR 98ZZZM51](https://openairdocs.org/sdr/98ZZZM51), Aug 2, 1997: MOUNT PLATE. CRACKED. LIFT SPOILER VALVE MOUNT PLATE CRACKED IN RT WING ROOT. REMOVED VALVE, REPLACED PLATE AND REINSTALLED VALVE, GEN W/C DO LEAK AND OPS CHECK.
- [SDR 98ZZZM50](https://openairdocs.org/sdr/98ZZZM50), Aug 1, 1997: STIFFENER. CRACKED. LEFT WING TRAILING EDGE AREA AFT OF REAR SPAR BETWEEN WING RIBS NR 7 AND 8 HAS AN UPPER SKIN STIFFENER THATS CRACKED AT FORWARD END. REPAIRED IAW ATTACHED FAXES
- [SDR 97ZZZM789](https://openairdocs.org/sdr/97ZZZM789), Jun 30, 1997: SMOKE HOOD. DAMAGED. REQ MAINTENANCE CHECK, AFT PBE FOR SERVICEABILITY. REMOVED AND REPLACED AFT PBE MAS ASSY. (M)

All 72: https://openairdocs.org/deregistered/N607AW-2006-07-20/reports.md

## FAA accident and incident reports (6)

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 19980311007009I](https://openairdocs.org/incident/19980311007009I), Mar 11, 1998: Bag BAE146200A (N607AW), Aspen, CO, Minor damage. Narrative: on March 11, 1998 at 1552 hrs local, a BAE-146-200 operated by air Wisconsin airlines ran off the runway at Aspen, Colorado. The aircraft (N607AW)…
- [Incident 19920820037369I](https://openairdocs.org/incident/19920820037369I), Aug 20, 1992: Bag BAE146200A (N607AW), Chicago, IL. Fumes in cabin while taxiing for takeoff. Found a cracked hydraulic pressure supply line.
- [Incident 19900928059069I](https://openairdocs.org/incident/19900928059069I), Sep 28, 1990: Bac 146200A (N607AW), Champaign-Urban, IL. First officer had a seizure and passed out. Diverted for landing.
- [Incident 19900628033589I](https://openairdocs.org/incident/19900628033589I), Jun 28, 1990: Bac 146200A (N607AW), Chicago, IL, Minor damage. Flight attendant advised pilot of engine fire. No cockpit warning. Returned. Manifold was leaking fuel.
- [Incident 19900529028159I](https://openairdocs.org/incident/19900529028159I), May 29, 1990: Bac 146200A (N607AW), Lexington, KY. Emergency landing due to passenger medical problem. Removed to hospital and resumed flight.
- [Incident 19861024079642I](https://openairdocs.org/incident/19861024079642I), Oct 24, 1986: Bac 146200A (N607AW), Chicago, IL, Substantial damage. While holding for departure, aircraft vertical stabilizer was struck by taxiing N4718U.

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