# N510TA: 1980 Airbus Industrie A300 B4-203, registration cancelled 2012-07-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 25, 2012 - Status when cancelled: First renewal notice - Airframe: [Airbus Industrie A300 B4-203](https://openairdocs.org/model/airbus-industrie-a300-b4-203) (registry code 3930306) - Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018) - Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs) - Serial number: 100 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 5, 2002 - Certificate issued: September 25, 2008 - Last registry action: September 25, 2008 - Mode S code: A66319 - Owner when cancelled: [Sky Lease I Inc](https://openairdocs.org/faa-owner/SKY%20LEASE%20I%20INC) - Location: [Greensboro, NC](https://openairdocs.org/faa-place/NC/Greensboro) - Owner type: Corporation - Owner's area on the map: 36.0718° N, 79.9648° W: Placed by OpenAirDocs at the center of ZIP code 27409, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N510TA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=510TA - Page: https://openairdocs.org/deregistered/N510TA-2012-07-25 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 Airbus Industrie A300 B4-203: https://openairdocs.org/model/airbus-industrie-a300-b4-203.md ## Service difficulty reports (24) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR WRN2009F00000](https://openairdocs.org/sdr/WRN2009F00000), Dec 19, 2008: FIRE LOOP. DEFECTIVE. ENGINE NR 1 SHUT DOWN IN FLIGHT DUE TO A FIRE INDICATION DURING FLIGHT FROM BDL TO BQN. BOTH FIRE BOTTLES WERE DISCHARGED. WARNING LIGHT EXTINGUISHED. ACFT LAND - [SDR WRN2008F00004](https://openairdocs.org/sdr/WRN2008F00004), Jun 23, 2008: SILL. FOD. AC AFTER TAKEOFF, LOUD WHISTLING NOISE HEARD AND AC HAD PROBLEMS PRESSURIZING. AC MADE UNSCHEDULED STOP, WITH NORMAL LANDING. FOUND F.O.D. AND DEBRIS IN MAIN CA - [SDR WRN2008F00002](https://openairdocs.org/sdr/WRN2008F00002), Jun 16, 2008: VALVE. STUCK. AFTER TAKEOFF, PRESSURIZATION MALFUNCTION OCCURRED. ACCOMPLISHED ABNORMAL PROCEDURES. AC RETURNED TO FIELD. LANDING NORMAL. MX FOUND GROUND VENT VALVE STUCK CLO - [SDR WRNA200800037](https://openairdocs.org/sdr/WRNA200800037), Apr 29, 2008: CSD. MALFUNCTIONED. DURING FLIGHT, NR 1 CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY RISING OIL TEMPERATURE. DISCONNECTED CSD AND RETURNED TO MFM FOR A SAFE - [SDR WRNA200700064](https://openairdocs.org/sdr/WRNA200700064), Dec 28, 2007: DAMPER. MALFUNCTIONED. AFTER DEPARTURE WHEN RAISING GEAR, LEVER WOULD NOT GO PAST THE MID POSITION, GEAR POSITION LIGHTS REMAINED 'GREEN'. RETURNED TO FIELD AND MADE A SAFE LANDING. A - [SDR WRNA200700058](https://openairdocs.org/sdr/WRNA200700058), Oct 23, 2007: LINE. OBSTRUCTED. DURING TAKEOFF ROLL, FIRST OFFICERS AIR SPEED LAGGED BEHIND CAPTAINS BY 40-60 KNOTS, ABORTED TAKEOFF. FLUSHED DEBRIS FROM PITOT PRESSURE LINES, ACCOMPLISHED PIT - [SDR WRNA200700057](https://openairdocs.org/sdr/WRNA200700057), Oct 23, 2007: PITOT TUBE. LEAKING. DURING TAKEOFF THE FIRST OFFICERS AIRSPEED INDICATOR LAGGED 40-60 KNOTS BEHIND CAPTAINS AIRSPEED INDICATOR. FOUND RT PITOT PROBE LEAKING, REPLACED RT PITOT PROB - [SDR WRNA200700051](https://openairdocs.org/sdr/WRNA200700051), Oct 18, 2007: CIRCUIT BREAKER. WEAK. AFTER TAKEOFF, FUEL PUMP NR 1; 1A; 2 CIRCUIT BREAKERS POPPED, AND AFCS AND FLIGHT ENGINEER PANEL LIGHTS WENT OFF. RETURNED TO FIELD AND MADE A SAFE LANDIBG. REP - [SDR WRNA200700065](https://openairdocs.org/sdr/WRNA200700065), Oct 11, 2007: BULKHEAD. CRACKED. DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD AT STR TIE END ANGLE FITTING AT 35R. FABRIC - [SDR WRNA200700070](https://openairdocs.org/sdr/WRNA200700070), Oct 11, 2007: FITTING. CORRODED. DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 38R. FABRICATE - [SDR WRNA200700069](https://openairdocs.org/sdr/WRNA200700069), Oct 11, 2007: FITTING. CORRODED. DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 37R. FABRICATE - [SDR WRNA200700068](https://openairdocs.org/sdr/WRNA200700068), Oct 11, 2007: FITTING. CORRODED. DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 36R. FABRICATE - [SDR WRNA200700067](https://openairdocs.org/sdr/WRNA200700067), Oct 11, 2007: FITTING. CORRODED. DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 35R. FABRICATE - [SDR WRNA200700066](https://openairdocs.org/sdr/WRNA200700066), Oct 11, 2007: BOLT. CORRODED. DURING ACCOMPLISHMENT OF CPCP C54-400-03-00 AT M96 CHECK LEVEL II CORROSION WAS FOUND ON 4 HORIZONTAL BOLTS OF NR 2 ENGINE AFT MOUNT. REMOVED AND REPLACED 4 HOR - [SDR WRNA200700049](https://openairdocs.org/sdr/WRNA200700049), Aug 18, 2007: INDICATION SYS. MALFUNCTIONED. DURING TAKEOFF FOR TEST FLIGHT AFTER HEAVY MAINTENANCE VISIT, CONFIGURATION LIGHT AND WARNING HORN CAME ON, TAKEOFF ABORTED. REPLACED LEADING EDGE INSTRUMENTATI - [SDR WRNA200700053](https://openairdocs.org/sdr/WRNA200700053), Jul 23, 2007: SUPPORT. CRACKED. DURING M-96 CHECK, A 3 INCH CRACK WAS FOUND IN THE NR 2 ENGINE OUTBOARD CORE COWL SUPPORT. ACCOMPLISHED WELD REPAIR IAW ENGINEERING ORDER 2-54907-800 FROM EMTEQ - [SDR WRNA200700052](https://openairdocs.org/sdr/WRNA200700052), Jul 6, 2007: TRUNNION. CORRODED. DURING M-96 CHECK, CORROSION WAS FOUND IN LT MAIN LANDING GEAR AFT TRUNNION FORWARD LUG FITTING BORE AND FACE. REMOVED CORROSION BY OVERSIZING BORE AND SPOT FAC - [SDR WRNA200700055](https://openairdocs.org/sdr/WRNA200700055), Jun 29, 2007: RIB. UNSERVICEABLE. DURING M96 COMPLY WITH S/B A300-57-0245, REPLACEMENT OF LT INBOARD FLAP RIB NR 7. REMOVED LEFT WING INBOARD FLAP, RIB NR 7, PERFORMED HFEC INSPECTION IAW A300-5 - [SDR WRNA200700056](https://openairdocs.org/sdr/WRNA200700056), Jun 25, 2007: FLOORBEAM. CRACKED. DURING M-96 CHECK, FOUND LOWER CROSS BEAM OF FLOORBEAM AT FRAME 57 BL 0 CRACKED. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-30. - [SDR RNA200700054](https://openairdocs.org/sdr/RNA200700054), Jun 24, 2007: FLOORBEAM. CORRODED. DURING M-96 CHECK, FLOOR SUPPORT BEAM IN AFT CARGO AT FRAME 63 WAS FOUND CORRODED AND HAD A 5 INCH CRACK BETWEEN STR 41L AND 43L. CUT OUT DAMAGED SECTION OF FLO - [SDR WRNA200700054](https://openairdocs.org/sdr/WRNA200700054), Jun 24, 2007: FLOORBEAM. CORRODED. DURING M-96 CHECK, FLOOR SUPPORT BEAM IN AFT CARGO A7 FRAME 63 WAS FOUND CORRODED AND HAD A 5 INCH CRACK BETWEEN STR 41L AND 43L. CUT OUT DAMAGED SECTION OF FLO - [SDR WRNA200700028](https://openairdocs.org/sdr/WRNA200700028), Jun 5, 2007: SLIDE. DEPLOYED. ON GROUND, CREW OPENED LEFT HAND DOOR WITH DOOR ARMED, SLIDE WAS DEPLOYED. SLIDE WAS PLACED ON MEL 52-61-01 AND AIRCRAFT RELEASED FOR SERVICE. SLIDE WAS REPLACE - [SDR WRNA200600026](https://openairdocs.org/sdr/WRNA200600026), Jun 20, 2006: SLIDE. WILL NOT ARM. R2 DOOR SLIDE WILL NOT ARM. REPLACED DOOR SLIDE IAW A300 25-61-11. RETURNED TO SERVICE. - [SDR WRNA200500007](https://openairdocs.org/sdr/WRNA200500007), Mar 24, 2005: ADC. UNSERVICEABLE. AFTER TAKEOFF, CAPTAINS AIRSPEED INDICATOR DECREASED TO ZERO (0). CAPTIANS ALTIMETER REMAINED AT 300 FT. DURING CLIMB OUT. AIRCRAFT RETURNED TO AIRPORT, LANDING ## Other aircraft with N510TA - [Registered now](https://openairdocs.org/aircraft/N510TA): Taus MK-5B, S/N MK-5B-002 - [Cancelled 1998-09-14](https://openairdocs.org/deregistered/N510TA-1998-09-14): North American T-39A, S/N 603482. Exported to Mexico. Owner: [Jett Racing And Sales Inc](https://openairdocs.org/faa-owner/JETT%20RACING%20AND%20SALES%20INC), [Laredo, TX](https://openairdocs.org/faa-place/TX/Laredo) --- 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.