# N802FD: 1990 Airbus Industrie A310-324, registration cancelled 2025-03-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 5, 2025 - Status when cancelled: Valid registration - Airframe: [Airbus Industrie A310-324](https://openairdocs.org/model/airbus-industrie-a310-324) (registry code 3930318) - Engine: [Pratt & Whitney PW4000 series](https://openairdocs.org/engine/pratt-whitney-pw4000-series) (registry code 52119) - Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (OpenAirDocs) - Serial number: 542 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 26, 2001 - Certificate issued: December 20, 2000 - Last registry action: July 18, 2023 - Mode S code: AAE9CC - Owner when cancelled: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP) - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Corporation - Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N802FD - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=802FD - Page: https://openairdocs.org/deregistered/N802FD-2025-03-05 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 A310-324: https://openairdocs.org/model/airbus-industrie-a310-324.md ## Service difficulty reports (25) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FDEA200908143019](https://openairdocs.org/sdr/FDEA200908143019), Aug 14, 2009: FLOOR SUPPORT. CORRODED. FWD CABIN FLOOR STRUCTURE - SUPPORT FLOOR AT Y730 BTW FR12A AND 13A FOUND CORRODED. SUPPORT FLOOR REPLACED IAW SRM 51-72-10. - [SDR FDEA200908133009](https://openairdocs.org/sdr/FDEA200908133009), Aug 13, 2009: FLOORBEAM. CORRODED. AFT CARGO BAY- FLOORBEAM CORROSION AT FR60 AT POSITION Y-140. BEAM REPLACED IAW SRM 51-40-21. - [SDR FDEA200908133008](https://openairdocs.org/sdr/FDEA200908133008), Aug 13, 2009: FLOORBEAM. CORRODED. AFT CARGO BAY- FLOORBEAM CORROSION AT FR60 AT POSITION Y1470. REPLACED IAW SRM 51-40-21. - [SDR FDEA200908073165](https://openairdocs.org/sdr/FDEA200908073165), Aug 7, 2009: SKIN. DELAMINATED. LT WING FLAP INBD WITH DEBONDING ON T/E. T/E WAS REPLACED IAW EA 6-5710-131046 AND SRM 51-72-10. - [SDR FDEA200908033100](https://openairdocs.org/sdr/FDEA200908033100), Aug 3, 2009: STRUCTURE. CRACKED. COCKPIT FLOOR STRUCTURE - UPPER PANEL AT RT TORSION BOX FOUND CRACKED BETWEEN FR1 AND FR2 AT Y1004. THE TORSION BOX WAS REPAIRED IAW EA 6-5310-131043. - [SDR FDEA200907303099](https://openairdocs.org/sdr/FDEA200907303099), Jul 30, 2009: STRUCTURE. CRACKED. COCKPIT FLOOR STRUCTURE - UPPER PANEL AT RT TORSION BOX FOUND CRACKED BETWEEN FR1 AND FR2 AT Y-1004. THE TORSION BOX WAS REPAIRED IAW EA 6-5310-131043. - [SDR FDEA200907293007](https://openairdocs.org/sdr/FDEA200907293007), Jul 29, 2009: FITTING. CORRODED. FWD CARGO COMPT - MANHOLE FITTING - CORROSION FOUND BTW FR38.1&FR38.2. CORROSION REMOVED IAW SRM 51-74-10. MANHOLE WAS REPAIRED IAW A310 SRM 53-14- 12 FIG.203. - [SDR FDEA200907292910](https://openairdocs.org/sdr/FDEA200907292910), Jul 29, 2009: SKIN. CORRODED. RIGHT WING - SPOTS OF CORROSION AT UPPER SKIN SURFACE AT REAR SPAR LOCATION, BTW RIBS 4 AND 5. CORROSION WAS BLENDED OUT AND REMAINING THICKNESS FOUND ACCEPTABL - [SDR FDEA200907273108](https://openairdocs.org/sdr/FDEA200907273108), Jul 27, 2009: BEAM. CORRODED. AFT CARGO COMPT, CORROSION ON BEAM OF CARGO COMPT FLOOR AT FRAME 63 BTW Y805 AND Y1740. THE BEAM WAS REPLACED IAW SRM 51-72-10. - [SDR FDEA200907233102](https://openairdocs.org/sdr/FDEA200907233102), Jul 23, 2009: TRUNNION. DAMAGED. LT WING - NR 3 EXTERIOR TRUNNION FOUND DAMAGED. TRUNNION NR 3LH WAS REPAIRED IAW CMM 57-53-12. - [SDR FDEA200907233101](https://openairdocs.org/sdr/FDEA200907233101), Jul 23, 2009: TRUNNION. DAMAGED. LT WING - NR 1 EXTERIOR TRUNNION FOUND DAMAGED. THE AFFECTED TRUNNION WAS REPAIRED IAW CMM 57-53-12. - [SDR FDEA200907032470](https://openairdocs.org/sdr/FDEA200907032470), Jul 3, 2009: BRAKE. BURNED. NR 8 BRAKE TAXING INTO GATE WENT ABOVE 300 DEGS WITH ALL OTHER TEMPS BETWN 50-75 DEGS. ON ARRIVAL, WERE INFORMED BY GRD CREW THE BRAKES WERE VERY HOT, SMOKING A - [SDR 08FDEA00047](https://openairdocs.org/sdr/08FDEA00047), Jan 6, 2008: WINDOW. CRACKED. CAPT FRONT COCKPIT WINDOW CRACKED REMOVED AND REPLACED WINDOW HEAT PROTECTION NR 1 IAW MM 30-42-11-4. PERFORMED OPS CHECK AS PER MM 30-42-00-5. ALL TEST PASSED. - [SDR 07FDEA04722](https://openairdocs.org/sdr/07FDEA04722), Oct 11, 2007: SKIN. DELAMINATED. LT WING, FLAP INBD W/ DBONDS AT THE T/E BETWEEN RIB 2 AND RIB 8 REPLACE TRAILING EDGE IAW FEDEX EA 6-5710-115293. - [SDR 07FDEA04735](https://openairdocs.org/sdr/07FDEA04735), Oct 10, 2007: ARM. CORRODED. NR 4 RUDDER HINGE ARM WITH CORROSION AT LUG BORES. REPAIR ACCOMPLISHED IN ACCORDANCE WITH 6-5510-115292. - [SDR 07FDEA04733](https://openairdocs.org/sdr/07FDEA04733), Oct 10, 2007: ARM. CORRODED. NR 3 RUDDER HINGE ARM WITH CORROSION AT LUG BORES. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA 6-5510-115292. - [SDR 07FDEA04732](https://openairdocs.org/sdr/07FDEA04732), Oct 10, 2007: ARM. CORRODED. NR 2 RUDDER HINGE ARM WITH CORROSION IN LUG BORE. REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5510-115292. - [SDR 07FDEA04723](https://openairdocs.org/sdr/07FDEA04723), Oct 9, 2007: SKIN. DEBONDED. RT WING INBD FLAP T/E W/ VARIOUS DEBONDS TRAILING EDGE WAS REPLACED IAW SRM 51-72-10 AND EA 6-5710-115293. - [SDR 06FDEA1027](https://openairdocs.org/sdr/06FDEA1027), Mar 13, 2006: SKIN. DAMAGED. ACCOMPLISH MAINTENANCE B-CHECK. NR 2 ENGINE CRK FOUND WITH ABOUT 4 INCHES ON AIR INLET INTERIOR SKIN SURFACE BETWEEN NR 5 AND NR 6 HOURS. REPAIRED PER CMM 71-11 - [SDR 06FDEA1026](https://openairdocs.org/sdr/06FDEA1026), Mar 13, 2006: SKIN. CRACKED. ACCOMPLISH MAINTENANCE B-CHECK. NR 2 ENG SMALL CRACKS FOUND ON AIR INLET EXTERIOR SKIN SURFACE AT ZONE BETWEEN NR 5 AND NR 6 HOURS (LIP INLET). REPAIRED PER CMM - [SDR 06FDEA0372](https://openairdocs.org/sdr/06FDEA0372), Jan 24, 2006: CONVERTER. NO TEST. REMOVED AND REPLACED SDAC IAW AMM 31-55-22-4. OPERATIONAL TEST FOUND SATISFACTORY. A/C OK TO CONTINUE. PREMATURE REMOVAL/INSTALLATION. - [SDR 05FDEA01221](https://openairdocs.org/sdr/05FDEA01221), May 6, 2005: SPOILER. DAMAGED. DURING C2 CHECK, FOUND AN EXISTING REPAIR ON LEFT WING NR 1 SPOILER TRAILING EDGE. REPAIRED PER SRM 57-70-00. - [SDR 05FDEA01220](https://openairdocs.org/sdr/05FDEA01220), May 6, 2005: SKIN. DAMAGED. DURING C2 CHECK, 2 EXISTING FLUSH COMPOSITE REPAIRS WHERE FOUND ON LEFT INBOARD FLAP TRAILING EDGE. REPAIRED IAW EA 6-5750-84119. - [SDR 05FDEA01219](https://openairdocs.org/sdr/05FDEA01219), May 6, 2005: SKIN. DAMAGED. DURING C2 CHECK, AN EXISTING REPAIR WAS FOUND ON LEFT ELEVATOR TOP SURFACE OUTBOARD OF RIB 17. NEW REPAIR ACCOMPLISHED PER SRM 55-20-00. - [SDR 05FDEA01218](https://openairdocs.org/sdr/05FDEA01218), May 6, 2005: FLAP. DAMAGED. DURING C2 CHECK, FOUND AN EXISTING REPAIR ON RIGHT INBOARD FLAP LOWER TRAILING EDGE. NEW REPAIR WAS PERFORMED IAW FEDEX EA 6-5710-84120. --- 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.