# N506TA: 1982 Airbus Industrie A300 B4-203, registration cancelled 2009-10-20 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 20, 2009 - Status when cancelled: Valid registration - 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: 207 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 5, 2000 - Certificate issued: September 23, 2008 - Last registry action: September 23, 2008 - Mode S code: A651E4 - 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/N506TA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=506TA - Page: https://openairdocs.org/deregistered/N506TA-2009-10-20 From the FAA registry file of November 12, 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 (13) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR WRNA20080011](https://openairdocs.org/sdr/WRNA20080011), Apr 8, 2008: SLIDE. NO TEST. DURING OPERATIONAL TEST, THE R-1 DOOR ESCAPE SLIDE/RAFT FAILED TEST, DID NOT FULLY INFLATE. REPLACED ESCAPE SLIDE/RAFT CONTACTED MAINTENANCE STATION WERE TEST W - [SDR WRNA200700060](https://openairdocs.org/sdr/WRNA200700060), Oct 31, 2007: DUCT. BROKEN. DURING TAKE OFF, NR 2 ENGINE EGT EXCEEDED 960 C, POWER WAS REDUCED BELOW TAKEOFF SETTING, EGT DROPPED BELOW 945 C. DURING CLIMB, NR 2 ENGINE MANIFOLD PRESS 10 P - [SDR WRNA200700014](https://openairdocs.org/sdr/WRNA200700014), Mar 9, 2007: SERVO VALVE. FAILED. AFTER LANDING, NR 3 BRAKE TEMP, WENT TO 700C. INSPECTED IAW 05-51-16, FOUND HEAT DAMAGE REQUIRING BOGIE BEAM REPLACEMENT. TEST OF NR 3 SERVO VALVE INDICATED SER - [SDR WRNA200600042](https://openairdocs.org/sdr/WRNA200600042), Jan 12, 2007: ROD END. BROKEN. DURING HEAVY MAINTENANCE WHILE PERFORMING SB A300-27-189, ROD END ON RIGHT ELEVATOR BLUE SYSTEM SERVO SPRING ROD ASSEMBLY, WAS FOUND BROKEN. - [SDR WRNA200700021](https://openairdocs.org/sdr/WRNA200700021), Dec 26, 2006: FRAME. CORRODED. DURING M72 CHECK, CORROSION WAS FOUND, AFT FUSELAGE FRAME 58 AT STRINGER 39R. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS IAW DISPOSITION MSN 207/04 FROM FA - [SDR WRNA200700020](https://openairdocs.org/sdr/WRNA200700020), Dec 26, 2006: SKIN. CORRODED. DURING M72 CHECK, CORROSION WAS FOUND AT AFT EXTERNAL FUSELAGE AT FR 58 BETWEEN STR 24R AND 28R. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER IAW REPAIR DISPO - [SDR WRNA200600034](https://openairdocs.org/sdr/WRNA200600034), Aug 10, 2006: ENGINE. MAKING METAL. NR 1 ENGINE STALLED 3 TO 4 TIMES, EGT 909 C. REDUCED POWER TO IDLE AND RETURNED TO FIELD FOR SAFE LANDING. POST FLIGHT INSPECTION FOUND METAL IN TAIL PIPE, ENGI - [SDR WRNA200600016](https://openairdocs.org/sdr/WRNA200600016), Jun 2, 2006: ACTUATOR. UNSERVICEABLE. AFTER TAKEOFF, SEVERE VIBRATION FELT BELOW COCKPIT AFTER GEAR SELECTOR VALVE IN NEUTRAL. RECYCLED GEAR UP AND DOWN, VIBRATION REOCCURRED AFTER PLACING LEVER IN - [SDR WRNA20050030](https://openairdocs.org/sdr/WRNA20050030), Dec 13, 2005: OUTFLOW VALVE. UNSERVICEABLE. AFTER TAKEOFF USING SYSTEM NR1 NOTICED AFT OUTFLOW VALVE STAYED FULL OPEN. OPPOSITE SYSTEM SELECTED, NO HELP, UNABLE TO CLOSE MANUALLY. WITH BOTH PACKS ON COULD - [SDR DHL2003368002](https://openairdocs.org/sdr/DHL2003368002), Apr 8, 2003: PROXIMITY SWITCH. DIRTY. UNABLE TO RAISE LANDING GEAR LEVER PAST THE OFF POSITION FOR GEAR RETRACTION. TROUBLESHOT PER FIM 32-30-00. SYSTEM NR 1, SENSORS NR 4 & NR 7, FAIL BITE TEST. SY - [SDR DHL2003368001](https://openairdocs.org/sdr/DHL2003368001), Jan 14, 2003: SMOKE DETECTOR. MALFUNCTIONED. LAV SMOKE DETECTOR SOUNDED HAD TO BE DISCONNECTED. OPS CHECKED SMOKE DETECTOR IAW M/M 26-17-00. OPS CHECKED GOOD. - [SDR WRNA200200008](https://openairdocs.org/sdr/WRNA200200008), Oct 29, 2002: DAMPENER. UNSERVICEABLE. After Take off unable to retract landing gear with system 1 or 2. Followed abnormal procedures and returned to airport. Landing normal.Corrective Action: Found - [SDR 2001F00152](https://openairdocs.org/sdr/2001F00152), Jun 12, 2001: ACTUATOR. INOPERATIVE. GROUND AUXILIARY FAULT LIGHT REMAINED ON AFTER TAKEOFF AND DURING CLIMB. AIRCRAFT LANDED NORMAL. REMOVED AND REPLACED AUXILIARY VALVE ACTUATOR IAW 21-31-17. OPS --- 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, except the copies of manufacturers’ service documents, which belong to their rights holders.