# N179US: British Aerospace BAE 146 SERIES 200A, registration cancelled 2006-06-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 30, 2006
- Exported to: Denmark
- 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: E2041
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: September 6, 1985
- Certificate issued: February 29, 2000
- Last registry action: April 18, 2006
- Mode S code: A13C6F
- Owner when cancelled: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N179US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=179US
- Page: https://openairdocs.org/deregistered/N179US-2006-06-30

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 (63, newest 50)

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

- [SDR A6WA200560016](https://openairdocs.org/sdr/A6WA200560016), Jul 14, 2005: FUEL CONTROL. UNSERVICEABLE. CLIMBING THRU 9000 FT NR 1 ENGINE STARTED TO WIND DOWN. BOTH N1 AND N2 WERE DROPPING, TGT APPEARED TO BE RISING. SECURED ENGINE, PERFORMED IMMEDIATE ACTION CHEC
- [SDR A6WA200160048](https://openairdocs.org/sdr/A6WA200160048), Oct 7, 2004: STRUCTURE. WORN. WEAR DAMAGE TO THE LOWER L/E OF THE LT FLAP IN THE RECESSED AREA BETWEEN RIBS 25 AND 31. MAINTENANCE REPAIRED WEAR DAMAGE IAW BAE FAX BARA/AVR/6894/04-DC.
- [SDR A6WA200460009](https://openairdocs.org/sdr/A6WA200460009), Mar 18, 2004: HOOK. DAMAGED. DAMAGE TO DOOR HOLD OPEN HOOK AREA ON THE DOOR, AND ASSOCIATED RECEPTICLE ON THE FUSELAGE, FORWARD PASSENGER DOOR. MAINTENANCE REPLACED UPPER HINGE AND HOLD OPE
- [SDR A6WA200260046](https://openairdocs.org/sdr/A6WA200260046), Oct 21, 2002: CONTROL VALVE. MALFUNCTIONED. DURING CLIMB, EXPERIENCED SLIGHT HAZE IN COCKPIT FOLLOWING SHUTDOWN OF NR 1 AND NR 2 PACKS, HAZE DISSIPATED. MAINTENANCE RAN BOTH PACKS, VERIFIED NR 1 PACK INOP
- [SDR A6WA200260021](https://openairdocs.org/sdr/A6WA200260021), Jun 21, 2002: FRAME. CRACKED. CRACKS AND CORROSION TO LOWER HALF OF FRAME 18 FROM 18L TO STR 18R.
- [SDR A6WA200100023](https://openairdocs.org/sdr/A6WA200100023), Mar 25, 2001: ENGINE. POWER LOSS. ON CLIMBOUT IN ICING CONDITIONS, NR 1 ENGINE POWER DECAYED WITH TAIL AND WING ANTI-ICE ON N1 WENT TO 82 PERCENT, N2 WENT TO 84 PERCENT. MAINTENANCE INSPECTED AL
- [SDR A6WA200000080](https://openairdocs.org/sdr/A6WA200000080), Dec 24, 2000: AILERON. MALFUNCTIONED. AILERON OUT OF TRIM LIGHT ON M/A TURNED OFF A/P MASTER SWITCH, ALL FLIGHT CONTROLS AND TRIM WORK OK. MAINTENANCE OPERATIONAL TEST OK, COULD NOT DUPLICATE.
- [SDR A6WA200000060](https://openairdocs.org/sdr/A6WA200000060), Aug 28, 2000: SKIN. DENTED. DENT AT FRAME 20-20A STRINGER 18 LT SIDE. REPAIRED DENT AT FRAME 20-20A STRINGER 18 LT SIDE IAW BAE FAX REF BARA/AVR/5135/00 AND RIC HC536H9251. NO FURTHER REIN
- [SDR A6WA0000015](https://openairdocs.org/sdr/A6WA0000015), Feb 12, 2000: PUMP. MALFUNCTIONED. WHILE EN ROUTE, MWS LIGHT CAME ON, HYD PANEL SHOWED LOW PRESSURE AND LOW QUANTITY YELLOW SYSTEM. REMOVED AND REPLACED NR 3 ENGINE DRIVEN HYDRAULIC PUMP. (M)
- [SDR A6WA9900059](https://openairdocs.org/sdr/A6WA9900059), Jun 18, 1999: BRACKET. CRACKED. LEFT GLIDESLOPE ANTENNA BRACKET IS CRACKED. REPLACED ANTENNA BRACKET. (X)
- [SDR A6WA9900060](https://openairdocs.org/sdr/A6WA9900060), Jun 17, 1999: STRUCTURE. CRACKED. AFT CARGO DOOR, AFT UPPER HINGE POINT IS CRACKED. REPAIRED CRACKS IAW BAE REPAIR NR HC523H9001. RE-PROFILED AFT BOTTOM SEAL CAGE. (X)
- [SDR A6WA9900078](https://openairdocs.org/sdr/A6WA9900078), Jun 9, 1999: SEAT. CRACKED. SEAT PAN ON SEAT 3C IS CRACKED. REPLACED SEAT PAN 3C. (X)
- [SDR A6WA9900077](https://openairdocs.org/sdr/A6WA9900077), Jun 9, 1999: SEAT. CRACKED. SEAT PANS 4A AND 4C ARE CRACKED. REPLACED SEAT PANS 4A AND 4C. REF: OPERATOR CONTROL NR 99ZZZX3107. (X)
- [SDR A6WA9900076](https://openairdocs.org/sdr/A6WA9900076), Jun 9, 1999: SEAT. CRACKED. SEAT PAN 7C IS CRACKED. REPLACED SEAT PAN 7C. (X)
- [SDR A6WA9900075](https://openairdocs.org/sdr/A6WA9900075), Jun 9, 1999: SEAT. CRACKED. SEAT PAN 9A IS CRACKED. REPLACED SEAT PAN 9A. (X)
- [SDR A6WA9900074](https://openairdocs.org/sdr/A6WA9900074), Jun 9, 1999: SEAT. CRACKED. SEAT PAN 10A AND 10C ARE CRACKED. REPLACED SEAT PANS 10A AND 10C. REF: OPERATOR CONTROL NR 99ZZZX3109. (X)
- [SDR A6WA9900073](https://openairdocs.org/sdr/A6WA9900073), Jun 9, 1999: SEAT. CRACKED. SEAT PAN 1D IS CRACKED. REPLACED SEAT PAN 1D.
- [SDR A6WA9900072](https://openairdocs.org/sdr/A6WA9900072), Jun 9, 1999: SEAT. CRACKED. SEAT PANS 7D AND 7F ARE CRACKED. REPLACED SEAT PAN 7D AND 7F. REF: OPERATOR CONTROL NR 99ZZZX3108. (X)
- [SDR A6WA9900071](https://openairdocs.org/sdr/A6WA9900071), Jun 9, 1999: SEAT. CRACKED. SEAT PAN 8F IS CACKED. REPLACED SEAT PAN 8F. (X)
- [SDR A6WA9900070](https://openairdocs.org/sdr/A6WA9900070), Jun 9, 1999: SEAT. CRACKED. SEAT PAN 10D IS CRACKED. REPLACED SEAT PAN 10D. (X)
- [SDR A6WA9900069](https://openairdocs.org/sdr/A6WA9900069), Jun 9, 1999: SEAT. CRACKED. SEAT PAN 13D IS CRACKED. REPLACED SEAT PAN 13D. (X).
- [SDR A6WA9900068](https://openairdocs.org/sdr/A6WA9900068), Jun 9, 1999: SEAT. CRACKED. SEAT PAN 15D IS CRACKED. REPLACED SEAT PAN 15D. (X)
- [SDR 99ZZZX3109](https://openairdocs.org/sdr/99ZZZX3109), Jun 9, 1999: SEAT. CRACKED. SEAT PAN 10A AND 10C ARE CRACKED. REPLACED SEAT PANS 10A AND 10C. REF: OPERATOR CONTROL NR A6WA9900074.
- [SDR 99ZZZX3108](https://openairdocs.org/sdr/99ZZZX3108), Jun 9, 1999: SEAT. CRACKED. SEAT PANS 7D AND 7F ARE CRACKED. REPLACED SEAT PAN 7D AND 7F. REF: OPERATOR CONTROL NR A6WA9900072.
- [SDR 99ZZZX3107](https://openairdocs.org/sdr/99ZZZX3107), Jun 9, 1999: SEAT. CRACKED. SEAT PANS 4A AND 4C ARE CRACKED. REPLACED SEAT PANS 4A AND 4C. REF: OPERATOR CONTROL NR A6WA9900077.
- [SDR A6WA9900067](https://openairdocs.org/sdr/A6WA9900067), Jun 7, 1999: STIFFENER. CRACKED. FROM EO E95/003/653 STIFFENERS ON FORWARD SIDE FRA 29 STA 25.94 LEFT AND RIGHT AND 31.13 LEFT AND RIGHT HAVE ONE A-BOLT HOLE CRACKED. EO E95/005/653 NEEDS COMPL
- [SDR A6WA9900066](https://openairdocs.org/sdr/A6WA9900066), Jun 7, 1999: FASTENER. DAMAGED. PERFORMED RIL HC571H9033 LEFT RIB 2 OUTBOARD JO-BOLTS. C/W RIL HC571H9033 TO LEFT RIB 2 JO-BOLT REPLACEMENT. (X)
- [SDR A6WA9900065](https://openairdocs.org/sdr/A6WA9900065), Jun 7, 1999: FASTENER. DAMAGED. PERFORMED RIL HC571H9033 LEFT RIB 2 INBOARD JO-BOLTS. C/W RIL HC571H9033 TO ABOVE LEFT RIB 2 JO-BOLT REPLACEMENT. (X)
- [SDR A6WA9900064](https://openairdocs.org/sdr/A6WA9900064), Jun 7, 1999: FASTENER. DAMAGED. PERFORMED RIL HC571H9033 LT CENTER TANK RIB 0 JO-BOLTS. C/W RIL HC571H9033 TO LEFT CENTER TANK RIB 0 JO-BOLT REPLACEMENT. (X)
- [SDR A6WA9900063](https://openairdocs.org/sdr/A6WA9900063), Jun 7, 1999: FASTENERS. DAMAGED. PERFORMED RIL HC571H9033 RT RIB 2 OUTBOARD JO-BOLTS. C/W RIL HC571H0933 RT WING SIDE OF RIB 2 JO-BOLT REPLACEMENT. (X)
- [SDR A6WA9900062](https://openairdocs.org/sdr/A6WA9900062), Jun 7, 1999: FASTENER. DAMAGED. PERFORMED RIL HC571H9033 ON RT RIB 2 INBOARD JO-BOLTS. C/W RIL HC571H0933 RT RIB 2 CENTER TANK SIDE JO-BOLT REPLACEMENT. (X)
- [SDR A6WA9900061](https://openairdocs.org/sdr/A6WA9900061), Jun 7, 1999: FASTENER. DAMAGED. PERFORMED RIL HC571H9033, RT RIB 0 JO BOLTS. C/W RIL - HC571H9033 TO RT CENTER TANK RIB 0 JO-BOLT REPLACEMENT. (X)
- [SDR A6WA9900058](https://openairdocs.org/sdr/A6WA9900058), Jun 5, 1999: DOOR. CRACKED. FORWARD LAVATORY SERVICE DOOR CRACKED NEAR HINGE AREA. REPAIRED IAW BAE FAX REF NR BARA/AVR/3589/99. (X)
- [SDR A6WA9900042](https://openairdocs.org/sdr/A6WA9900042), May 10, 1999: FLOW VALVE. FAILED. DURING E.O. INSPECTION, VALVE FAILED STEP 3. FLAP VALVE MOVED COMPLETELY FREE WITH NO DAMPING ACTION ABOUT THE HOLLOW RIVET. REMOVED AND REPLACED VALVE ASSY. (X
- [SDR 98ZZZX3966](https://openairdocs.org/sdr/98ZZZX3966), Sep 17, 1998: BOLT. CRACKED. ATW - NLG UPPER ACTUATOR MOUNT BOLT HEAD HAS CRACKED INDICATION. VERIFIED BY NDT 8-31-98 ID NR 042. REPLACED BOLT (INNER) ONE-HALF DIAMETER AT NL9 UPPER ATTACH 
- [SDR 98ZZZX3965](https://openairdocs.org/sdr/98ZZZX3965), Sep 17, 1998: DIAPHRAGM. CRACKED. ATW - REF W/C 7030, NLG DIAPHRAGM AT ATTACHMENT POINT OF NLG RAM HAS BEEN FOUND CRACKED AT 6 O'CLOCK POSITION. CRACK EXTENDS DOWNWARD FROM AND INTO THE PIN HOLE
- [SDR 98ZZZX3969](https://openairdocs.org/sdr/98ZZZX3969), Sep 15, 1998: LONGERON. CHAFED. ATW - AIRBRAKE ACTUATOR HAS CHAFED RIGHT FUSELAGE UPPER LONGERON APPROXIMATELY .030 INCH DEEP. REPAIRED RT FUSELAGE UPPER LONGERON AT AIRBRAKE ACTUATOR IAW BAE 
- [SDR 98ZZZX3955](https://openairdocs.org/sdr/98ZZZX3955), Sep 15, 1998: BULKHEAD. CORRODED. ATW - BULKHEAD AFT OF FRAME 50 (ABOVE AIRBRAKE ACTUATOR) IS CRACKED IN RT LOWER CORNER AND ABOUT 4 INCHES FROM LEFT CORNER. ALSO, RIVETS LOOSE IN BOTH CORNERS. 
- [SDR 98ZZZX3972](https://openairdocs.org/sdr/98ZZZX3972), Sep 14, 1998: SEAT TRACK. WORN. ATW - SEAT TRACK RAIL, STA 252.33, FRAMES 20-20A, LT INBOARD CORRODED AND WORN BEYOND LIMITS. REPLACED FORWARD SECTION OF SEAT RAIL 87 INCHES TOTAL AND SPLICED 
- [SDR 98ZZZX3964](https://openairdocs.org/sdr/98ZZZX3964), Sep 11, 1998: BRACKET. CORRODED. ATW - REF EO E92/067/632 REV A, LEFT HINGE BRACKET MISSING BUSHING, HOLE OVER SIZE, CORROSION AROUND HOLE IAW ITEM 6 SECT I. REMOVED LEFT HINGE BRACKET WRK 1032
- [SDR 98ZZZX3963](https://openairdocs.org/sdr/98ZZZX3963), Sep 11, 1998: SKIN. LIGHTNING STRIKE. ATW - DURING LIGHTNING STRIKE INSPECTION, NOTED ONE MINOR SKIN PIT BETWEEN FRAMES 4 AND 5, STR 19L. CLEANED AND PREPPED AREA. DAMAGE MEASURED AT .014 INCH DEPTH
- [SDR 98ZZZX3961](https://openairdocs.org/sdr/98ZZZX3961), Sep 11, 1998: SKIN. LIGHTNING STRIKE. ATW - DURING LIGHTNING STRIKE INSPECTION, NOTED ONE MINOR SKIN PIT BETWEEN FRAMES 5 AND 7 APPROXIMATELY STR 19L. CLEANED AND PREPPED AREA. DAMAGED MEASURED AT .
- [SDR 98ZZZM831](https://openairdocs.org/sdr/98ZZZM831), Sep 11, 1998: BRACKET. DAMAGED. REF EO E92/067/632 REV A, RIGHT HINGE BRACKET HAS DEEP IMPACT DAMAGE AROUND BOLT HOLE AND CORROSION IAW ITEM 10 SECTION I. REMOVED RIGHT HINGE BRACKET WRK 1032.
- [SDR 98ZZZX3990](https://openairdocs.org/sdr/98ZZZX3990), Sep 7, 1998: SKIN. GOUGED. ATW - PER FAX DS/W/TJ/28015/97 AND DJR/RJ0912-96. SEVERAL GOUGES TO DENTS AFT OF FRAME 20 AND ABOVE LAP SEAM AT STR 19 MUST BE REPAIRED BY TCA OF 22593 TCA TO C
- [SDR 98ZZZX3974](https://openairdocs.org/sdr/98ZZZX3974), Sep 4, 1998: LONGERON. CRACKED. ATW - FRAME 29 TOP LANDING GEAR LONGERONS CRACKED NR 3 AND NR 19 OUTBOARD OF BOTH OUTBOARD SEAT TRACK RAILS. REPAIRED AT FRAME 19, FLOOR BEAMS NR 3 AND NR 19 AT
- [SDR 98ZZZX3968](https://openairdocs.org/sdr/98ZZZX3968), Sep 4, 1998: INTERCOSTAL. CORRODED. ATW - FORWARD VEST INTERCOSTALS, SILL PLATES NEED CLEANING AND SEALANT, INSPECTED FOR CORROSION. CLEANED AND INSPECTED. REMOVED MINOR CORROSION AND TREATED META
- [SDR 98ZZZX3975](https://openairdocs.org/sdr/98ZZZX3975), Sep 3, 1998: DOOR SILL. CORRODED. ATW - SURFACE CORROSION ON AFT PASSENGER DOOR SILL PLATE. CLEANED CORROSION, TREATED, PRIMED, PAINTED AND SEALED DOOR SILL. (X)
- [SDR 98ZZZX3962](https://openairdocs.org/sdr/98ZZZX3962), Sep 3, 1998: SKIN. CORRODED. ATW - LEFT FORWARD PASSENGER DOOR HAS 2 EACH CRACKS IN THE HANDLE BOX AREA. REPLACED BOTH BOX ANGLES IAW FAX DJR/RJ0318-97 AND BAE SRM. ANGLES MADE PER PS1.
- [SDR 98ZZZX3967](https://openairdocs.org/sdr/98ZZZX3967), Sep 2, 1998: CONTROL CABLE. CORRODED. ATW - THE CENTER SECTION MAIN AILERON INTERCONNECT CABLES ARE CORRODED AT THE WING ROOT AREA. REMOVED AND REPLACED MAIN AILERON INTERCONNECT CENTER CABLES. GEN 
- [SDR 98ZZZX3960](https://openairdocs.org/sdr/98ZZZX3960), Sep 2, 1998: CONTROL CABLE. CORRODED. ATW - THE RIGHT MAIN AILERON CENTER SECTION OF CABLES ARE CORRODED AT THE LOWER PULLEY IN THE WING ROOT JUST AFT OF FRAME NR 29. REMOVED AND REPLACED THE RIGHT 

All 63: https://openairdocs.org/deregistered/N179US-2006-06-30/reports.md

## FAA accident and incident reports (1)

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 19961207041789I](https://openairdocs.org/incident/19961207041789I), Dec 7, 1996: Bag BAE146200A (N179US), Springfield, MO. On climbout low oil pressure NR3 engine. Shutdown. Returned sgf. Unable cause. Ferried. Clogged line. Worn gearbox.

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