# N91050: 1988 Airbus Industrie A300 B4-605R, registration cancelled 2011-08-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 26, 2011 - Status when cancelled: Valid registration - Airframe: [Airbus Industrie A300 B4-605R](https://openairdocs.org/model/airbus-industrie-a300-b4-605r) (registry code 3930308) - Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025) - Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs) - Serial number: 423 - Year built: 1988 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 18, 1988 - Certificate issued: April 20, 1988 - Last registry action: January 21, 2011 - Mode S code: AC99CB - Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%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/N91050 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=91050 - Page: https://openairdocs.org/deregistered/N91050-2011-08-26 From the FAA registry file of October 28, 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 Airbus Industrie A300 B4-605R: https://openairdocs.org/model/airbus-industrie-a300-b4-605r.md ## Service difficulty reports (88, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AALA2009051500002](https://openairdocs.org/sdr/AALA2009051500002), May 15, 2009: GCU. FAULTY. MIA - AIRCRAFT REPORTED PITCH TRIM SYSTEM FAIL. EMERGENCY DECLARED, RETURNED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND ALL PARAMETERS SPIKED WH - [SDR AALA2009041800776](https://openairdocs.org/sdr/AALA2009041800776), Apr 18, 2009: POWER SUPPLY. INOPERATIVE. JFK - RIGHT NUMBER 2 DOOR EXIT SIGN INOPERATIVE. REPLACED POWER UNIT AT RIGHT NUMBER 2 DOOR PANEL. - [SDR AALA2009040300707](https://openairdocs.org/sdr/AALA2009040300707), Apr 3, 2009: BATTERY PACK. DISCHARGED. MIA - EMERGENCY LIGHTS IN AFT CABIN AT SEAT 29C VERY DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CABIN AT SEAT 29C. - [SDR AALA200802685](https://openairdocs.org/sdr/AALA200802685), Oct 7, 2008: JACKSCREW. MALFUNCTIONED. MIA - CREW REPORTED FAULT FOR FLAP SYSTEM NUMBER ONE AND TWO. FLAPS DID NOT EXTEND. ABORTED APPROACH AND FLEW AROUND FOR SECOND APPROACH. SLATS AND FLAPS WORKED - [SDR AALA20071816](https://openairdocs.org/sdr/AALA20071816), Sep 27, 2007: BATTERY PACK. INOPERATIVE. LGA - EMERGENCY LIGHT AT STATION 243 INOPERATIVE. REPLACED BATTERY PACK AND MODULE FOR EMERGENCY LIGHT AT STATION 243. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20071657](https://openairdocs.org/sdr/AALA20071657), Aug 30, 2007: BATTERY PACK. INOPERATIVE. JFK - EMERGENCY LIGHT AT SEAT MOUNTED RIGHT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT MOUNTED RIGHT FIRST CLASS. SYSTEM GROUND - [SDR AALA20071658](https://openairdocs.org/sdr/AALA20071658), Aug 30, 2007: BATTERY PACK. INOPERATIVE. JFK - EMERGENCY LIGHT AT SEAT MOUNTED RIGHT MID CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT MOUNTED RIGHT MID CLASS. SYSTEM GROUND CHEC - [SDR AALA20050091](https://openairdocs.org/sdr/AALA20050091), Feb 7, 2005: CIRCUIT BOARD. BURNED. JFK - EMERGENCY EXIT LIGHT AT LEFT 2 DOOR INOPERATIVE. FOUND BURNED CIRCUIT BOARD ON LIGHT ASSEMBLY AT LEFT NUMBER 2 DOOR FOR EMERGENCY EXIT LIGHT. REPLACED LIG - [SDR AALA20040696](https://openairdocs.org/sdr/AALA20040696), Jun 24, 2004: CYLINDER. FAILED. DURING SLIDE RAFT DEPLOYMENT TEST LEFT 4 DOOR FAILED TO FULLY OPEN. REPLACED EMERGENCY OPERATION CYLINDER. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20040695](https://openairdocs.org/sdr/AALA20040695), Jun 23, 2004: FLAP TRACK. CORRODED. TUL - NUMBER ONE LEFT HAND FLAP TRACK HAS LIGHT CORROSION INSIDE RADIUS AFT END OF NUMBER ONE FLAP TRACK ATTACH POINT BARREL NUT. CORRODED AREA IS ONE INCH BY O - [SDR AALA20040693](https://openairdocs.org/sdr/AALA20040693), Jun 23, 2004: SKIN. CORRODED. TUL - SKIN CORRODED BETWEEN STRINGERS 53L AND 54L AT FRAME 65 IN AFT CARGO AT STATION NUMBER 4256. AREA OF CORROSION IS 3.75 INCHES BY 4.88 INCHES. INSTALLED SK - [SDR AALA20040694](https://openairdocs.org/sdr/AALA20040694), Jun 23, 2004: FLAP TRACK. GOUGED. TUL - FLAP TRACK NUMBER ONE LIFT GOUGED INSIDE AFT ATTACH POINT BARREL NUT HOLE. AREA OF DISCREPANCY IS ONE INCH BY ONE INCH AND LOCATED AT STATION 3300. REPAIR - [SDR AALA20040692](https://openairdocs.org/sdr/AALA20040692), Jun 23, 2004: SKIN. CORRODED. CORROSION ON LOWER RIGHT WING SKIN INSIDE SLAT TRACK SEVEN TRACK WELL. AREA OF CORROSION IS SEVEN INCHES BY FIVE INCHES AND LOCATED A STATION NUMBER 1260. REPAI - [SDR AALA20040691](https://openairdocs.org/sdr/AALA20040691), Jun 21, 2004: STRINGER. CORRODED. STRINGER 56L IS CORRODED JUST AFT OF FRAME 54. CORRODED AREA WAS 2 INCH BY 2 INCH. REPAIRED STRINGER 56L PER 51-71-10-0. - [SDR AALA20040665](https://openairdocs.org/sdr/AALA20040665), Jun 17, 2004: BUTT JOINT. CORRODED. CIRCUMFERENTIAL JOINT SPLICE STRAP CORRODED AT FRAME 65 BETWEEN STRINGERS 54 AND 55L. AREA IS 2 INCHES BY 5 INCHES IN THE AFT CARGO AREA. INSTALLED NEW BUTTSTRA - [SDR AALA20021385](https://openairdocs.org/sdr/AALA20021385), Sep 29, 2002: PIN. BACKED OUT. MIA - EMERGENCY SEAT MOUNTED LIGHT AT 32G INOPERATIVE. RESECURED PIN THAT WAS FOUND OUT OF CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20000132](https://openairdocs.org/sdr/AALA20000132), Jan 22, 2000: SWITCH. FAILED. JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EVACUATION SIGNAL CUT OFF SWITCH AT DOOR R1 DOES NOT CUT OFF. REPLACED EMERGENCY EVACUATION SIGNAL CUT OFF SWITCH - [SDR AALA991971](https://openairdocs.org/sdr/AALA991971), Dec 26, 1999: WIRE. CHAFED. PTY - FLT 917 - DURING FLIGHT ELECTRICAL BURING SMELL AROUND BUSINESS CLASS VIDEO RECORDER. DIVERTED AND LANDED PTY WITHOUT INCIDENT. REPAIRED CHAFED WIRING. SY - [SDR AALA991871](https://openairdocs.org/sdr/AALA991871), Dec 3, 1999: SHEAR TIE. CORRODED. TUL - FOUND CORROSION ON SHEAR TIE AT FRAME 59 AND BETWEEN STRINGER 46R AND 47R. INSTALLED NEW SHEAR TIE PER SRM 51-74-10. (M) - [SDR AALA991870](https://openairdocs.org/sdr/AALA991870), Dec 3, 1999: SPLICE. CORRODED. TUL - STRINGER SPLICE CORRODED ON STRINGER 54 LEFT BETWEEN FRAMES 32 AND 34. REPLACED STRINGER SPLICE PER SRM 51-72-10. (M) - [SDR AALA991834](https://openairdocs.org/sdr/AALA991834), Dec 2, 1999: STRINGER. CORRODED. TUL - FOUND CORROSION ON STRINGER 52R AT FRAME 59. INSTALLED REPAIR DOUBLER PER SRM 53-10-14. (M) - [SDR AALA991833](https://openairdocs.org/sdr/AALA991833), Dec 2, 1999: SHEAR TIE. CORRODED. TUL - SHEAR TIE HAS CORROSION AT FRAME 59 AND BETWEEN STRINGER 53R AND 54R. INSTALLED MANUFACTURED SHEAR TIE PER SRM 51-75-10. (M) - [SDR AALA991832](https://openairdocs.org/sdr/AALA991832), Nov 30, 1999: FITTING. CORRODED. FOUND CORROSION ON STRINGER 51L AND FITTING AT FRAME 80. INSTALLED NEW STRINGER END FITTING PER SRM 51-75-10. (M) - [SDR AALA991822](https://openairdocs.org/sdr/AALA991822), Nov 30, 1999: SPLICE. CORRODED. TUL - FOUND CORROSION ON STRINGER SPLICE 39 LEFT AT FRAME 58. INSTALLED NEW SPLICE PER SRM 51-72-10. (M) - [SDR AALA991821](https://openairdocs.org/sdr/AALA991821), Nov 30, 1999: SPLICE. CORRODED. TUL - FOUND CORROSION ON STRINGER SPLICE 37L AT FRAME 58. INSTALLED NEW STRINGER SPLICE PER SRM 51-72-10. (M) - [SDR AALA991102](https://openairdocs.org/sdr/AALA991102), Jul 28, 1999: CONNECTOR. LOOSE. JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT CABIN INOPERATIVE. RESECURED CONNECTOR TO AFT CABIN EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKE - [SDR AALA971983](https://openairdocs.org/sdr/AALA971983), Oct 17, 1997: FITTING. CORRODED. TUL - LOWER AFT MAN HOLE ACCESS FITTING HAS SEVERAL POCKETS WITH HEAVY CORROSION AROUND FASTENERS. INSTALLED DOUBLERS PER ESO 30595 DATED 10-15-97. TST: 26,111. - [SDR AALA971990](https://openairdocs.org/sdr/AALA971990), Oct 16, 1997: ROLLER TRAY. CORRODED. TUL - ROLLER TRAY NR 3 AT FRAME 60 HAS DEEP CORROSION CENTER OF TRAY. REPLACED CORRODED SECTION OF TRAY WITH NEW SERVICEABLE SECTION PER SRM 51-72-10. TST: 26,1 - [SDR AALA971989](https://openairdocs.org/sdr/AALA971989), Oct 16, 1997: ROLLER PAN. CORRODED. TUL - CORROSION UNDER POWER ROLLER PAN AND AROUND TEMPORARY REPAIR PAN BETWEEN NR 2 AND NR 3 ROLLER TRAYS AND FRAMES 61 AND 62. INSTALLED NEW POWER ROLLER PAN P - [SDR AALA971988](https://openairdocs.org/sdr/AALA971988), Oct 16, 1997: ROLLER TRAY. CORRODED. TUL - CORROSION IN AND AROUND FASTENER HOLES, NR 3 ROLLER TRAY AT FRAME 63. REPLACED CORRODED SECTION OF TRAY WITH NEW SERVICEABLE SECTION PER SRM 51-72-10. TST - [SDR AALA971987](https://openairdocs.org/sdr/AALA971987), Oct 16, 1997: ROLLER TRAY. CORRODED. TUL - NR 6 ROLLER TRAY FROM FRAMES 60 TO 61 HAS CORROSION. INSTALLED NEW DOOR SEAL ROLLER TRAY PER SRM 51-72-10-0. TST: 26,111.18 HOURS. CYCLES: 10,811. (X) - [SDR AALA971986](https://openairdocs.org/sdr/AALA971986), Oct 16, 1997: ROLLER TRAY. CORRODED. TUL - CORROSION NR 3 ROLLER TRAY UNDER SIDE AT DOME NUTS BETWEEN FRAMES 61 AND 62. REPLACED CORRODED SECTION OF TRACK WITH NEW SERVICEABLE SECTION OF TRACK PER - [SDR AALA971985](https://openairdocs.org/sdr/AALA971985), Oct 16, 1997: ROLLER TRAY. CORRODED. TUL - CORROSION ON NR 6 ROLLER TRAY OUTBOARD FLANGE AT FASTENER BETWEEN FRAMES 59 AND 60. REPLACED ROLLER TRAY SECTION WITH NEW PER SRM 53-10-15. TST: 26,111.18 - [SDR AALA971984](https://openairdocs.org/sdr/AALA971984), Oct 16, 1997: ROLLER TRAY. CORRODED. TUL - ROLLER TRAY NR 6 BETWEEN FRAMES 57.2 AND 57.3 HAS CORROSION AT FLOOR BOARD ATTACH HOLE. REPLACED ROLLER TRAY SECTION WITH NEW ONE PER SRM 53-10-15. TST: 2 - [SDR AALA971972](https://openairdocs.org/sdr/AALA971972), Oct 10, 1997: BEAM. CORRODED. TUL - DOOR SEAL BEAM HAS DEEP CORROSION BETWEEN FRAME 59 AND 60. INSTALLED DOUBLER PER SRM 51-71-50-2 PAGE 205. (M) - [SDR AALA971963](https://openairdocs.org/sdr/AALA971963), Oct 10, 1997: SUPPORT. CORRODED. TUL - FLOOR SUPPORT HAS CORROSION DAMAGE AT RIGHT AISLE, FOURTH TRACK FROM RIGHT SIDE. INSTALLED NEW FLOOR SUPPORT BETWEEN FRAME 70 TO 72 PER 51-72-10 AND ESO 3 - [SDR AALA971969](https://openairdocs.org/sdr/AALA971969), Oct 9, 1997: SPLICE. CORRODED. TUL - FOUND CORROSION ON STRINGER SPLICE STRINGER 44L AT FRAME 58. REMOVED AND REPLACED STRINGER SPLICE AT FRAME 58 AT 44L PER SRM 53-10-14. (M) - [SDR AALA971945](https://openairdocs.org/sdr/AALA971945), Oct 9, 1997: FRAME. CORRODED. TUL - BELL FRAME NR 58 HAS CORROSION FROM 54L TO 54R. CUT OUT CORROSION AND INSTALLED DOUBLER PER SRM 53-10-13. (M) - [SDR AALA971942](https://openairdocs.org/sdr/AALA971942), Oct 9, 1997: STRINGER. CORRODED. TUL - STRINGER 44L IS CORRODED AT FRAME 69. REMOVED CORRODED AREA AND INSTALLED NEW SECTION OF STRINGER PER SRM 53-10-14-2. (M) - [SDR AALA971937](https://openairdocs.org/sdr/AALA971937), Oct 9, 1997: STRINGER. CORRODED. TUL - STRINGER 46L AT FRAME 69 HAS CORROSION. REMOVED CORROSION STRINGER AND INSTALLED NEW SECTION PER SRM 53-10-17-2. (M) - [SDR AALA971926](https://openairdocs.org/sdr/AALA971926), Oct 9, 1997: SUPPORT. CORRODED. TUL - FLOOR SUPPORT, 4TH FROM LEFT SIDE, TOP SURFACE HAS CORROSION DAMAGE BETWEEN FRAMES 70 TO 74. INSTALLED FLOOR SUPPPORT AND SPLICED AT FRAME 70 PER ESO 3059 - [SDR AALA971925](https://openairdocs.org/sdr/AALA971925), Oct 9, 1997: SEAT TRACK. CORRODED. TUL - SEAT TRACK NR 8 HAS CORROSION DAMAGE ON TOP SURFACE FROM FRAME 26 TO FRAME 33. REPLACED SEAT TRACK NR 8 AT AND BETWEEN PRODUCTION SPLICES IAW 51-72-10-00 - [SDR AALA971956](https://openairdocs.org/sdr/AALA971956), Oct 8, 1997: SKIN. CORRODED. TUL - TRAILING EDGE OF WING APPROX 7 FEET FROM WINGLET HAS DEEP CORROSION. REPAIRED AREA IAW ESO30595 DATED 10-07-97. (M) - [SDR AALA971953](https://openairdocs.org/sdr/AALA971953), Oct 8, 1997: STATIC WICK. CORRODED. TUL - HEAVY CORROSION UNDER AND AROUND STATIC WICK INBOARD OF WINGLET AT TRAILING EDGE. REPAIRED CORROSION PER ESO 30595 DATED 10-07-97. (M) - [SDR AALA971951](https://openairdocs.org/sdr/AALA971951), Oct 8, 1997: SEAT TRACK. CORRODED. TUL - FOUND CORROSION AROUND FLOORBOARD ATTACHMENT HOLES AND SEAT LOGS, TRACK NR 10 RIGHT SIDE. REPLACED SECTION OF SEAT TRACK BETWEEN FRAMES 21 TO 26 PER AARD - [SDR AALA971924](https://openairdocs.org/sdr/AALA971924), Oct 8, 1997: SILL. CORRODED. TUL - CORROSION ON DOOR SILL BEAM AT STA 1678; PRIOR BLENDING OF AREA WAS DONE. BLEND WAS BEYOND LIMITS. FASTENER HOLES WERE DRILLED, BUT NEVER INSTALLED OR PLU - [SDR AALA971971](https://openairdocs.org/sdr/AALA971971), Oct 7, 1997: SUPPORT. CORRODED. TUL - FOUND CORRODED BEYOND LIMITS TOP FWD SIDE LEFT NOSE GEAR DOOR SUPPORT FOR UPLOCK. REPLACED PART AND RIGGED PER CARD NR 7209/ E58 NR 0095203. (M) - [SDR AALA971922](https://openairdocs.org/sdr/AALA971922), Oct 7, 1997: SUPPORT. CORRODED. TUL - OUTER FLOOR BOARD ATTACHMENT FLANGE AREAS HAVE CORROSION DAMAGE RT SIDE AT LAVATORY. INSTALLED NEW SECTION OF FLOOR SUPPORT PER AARD 51-10-00-3, AND SPLIC - [SDR AALA971917](https://openairdocs.org/sdr/AALA971917), Oct 7, 1997: SUPPORT. CORRODED. TUL - SECOND AFT LAVATORY SUPPORT, LEFT OF CENTER, TOP SURFACE HAS CORROSION DAMAGE. REPLACED FLOOR STRUCTURE COMPONENT PER SRM 51-72-10-0. TST: 26,111 HOURS. C - [SDR AALA971916](https://openairdocs.org/sdr/AALA971916), Oct 6, 1997: SUPPORT. CORRODED. TUL - LAVATORY SUPPORT HAS CORROSION. INSTALLED NEW SUPPORT OR LAVATORY PER SRM 51-72-10-00. TST: 26,111 HOURS. CYCLES: 10,811. (X) All 88: https://openairdocs.org/deregistered/N91050-2011-08-26/reports.md ## 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 19891120046099I](https://openairdocs.org/incident/19891120046099I), Nov 20, 1989: Airbus A300B4605R (N91050), Boston, MA. Smoke indications in equipment bay on rotation. Returned. No evidence of fire. Had glycol odor from deicing bath. - [Incident 19880510025169I](https://openairdocs.org/incident/19880510025169I), May 10, 1988: Airbus A300B4103 (N91050), Bermuda, BD, Minor damage. Extensive fuel burn on right engine. Diverted to Bermuda. Landed safely. Found the engine fuel pump case cracked. ## Other aircraft with N91050 - [Cancelled 1971-06-01](https://openairdocs.org/deregistered/N91050-1971-06-01): Cessna 207, S/N 20700037. Exported to Bolivia. Owner: [Roth Dawn](https://openairdocs.org/faa-owner/ROTH%20DAWN), [Houston, TX](https://openairdocs.org/faa-place/TX/Houston) - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N91050-undated): Piper PA-25-235, S/N 258156020 --- 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.