# N810FD: Airbus Industrie A310-324, registration cancelled 2024-03-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 2, 2024 - Status when cancelled: Valid registration - Airframe: [Airbus Industrie A310-324](https://openairdocs.org/model/airbus-industrie-a310-324) (registry code 3930318) - Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (OpenAirDocs) - Serial number: 452 - Type of aircraft: Fixed wing multi engine - Certificate issued: January 18, 2005 - Last registry action: August 4, 2023 - Mode S code: AB09DD - 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/N810FD - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=810FD - Page: https://openairdocs.org/deregistered/N810FD-2024-03-02 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 (68, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FDEA201601200234](https://openairdocs.org/sdr/FDEA201601200234), Jan 20, 2016: GCU. FAILED. ON TAKEOFF AT 80 KNOTS GEN II FAILED, THEN FOLLOWED BY GEN 1, TOTAL ELEC FAILURE. REJECTED TAKEOFF, CLEARED RUNWAY & RAN QRH. REJECTED AT 100 KNOTS. INTERROGATE - [SDR FDEA201509172894](https://openairdocs.org/sdr/FDEA201509172894), Sep 17, 2015: SWITCH. FAILED. DURING TAKEOFF ROLL, RECEIVED A MOMENTARY NR 2 THRUST REVERSER UNLOCKED ALERT & INSTRUMENT CLUSTER TOP LIGHT. LIGHT EXTINGUISHED & TAKEOFF WAS CONTINUED. AFTER - [SDR FDEA201504081201](https://openairdocs.org/sdr/FDEA201504081201), Apr 8, 2015: ALTIMETER. MALFUNCTIONED. REPEAT WRITE UP, STBY ALTIMETER WITHIN 30' OF PRIMARY ALTIMETERS ON THE GND. AT FL 300 STBY ALTIMETER WAS 160 FT HIGHER, AT FL 148 STBY ALTIMETER WAS 250 FT HIG - [SDR FDEA201504071200](https://openairdocs.org/sdr/FDEA201504071200), Apr 7, 2015: ALTIMETER. MALFUNCTIONED. AT CRUISE ALTITUDE 35,000, STBY ALTIMETER INDICATES 250 HIGHER THAN BOTH CAPTAINS & COPILOTS ALTIMETERS. R & R THE STBY ALTIMETER IAW AMM 34-12-22-04. INTEGRAL - [SDR FDEA201503020625](https://openairdocs.org/sdr/FDEA201503020625), Mar 2, 2015: SEAT TRACK. DAMAGED. COMPLY WITH WRI 25-50/0216 & 0217, REPAIR THE SEAT TRACK ASSEMBLY OF MDC FRAME 54.2 - 58 RESTRAINT ID N1199. REPAIRED THE SEAT TRACK IAW SRM 53-10-16 FIGURE 202 - [SDR FDEA201401210149](https://openairdocs.org/sdr/FDEA201401210149), Jan 21, 2014: RELAY. FAILED. DURING DESCENT, RECEIVED AN INTERMITTENT CHIME, WITH NO ECAM ALERT, INVESTIGATION FOUND LOW FUEL TANK AT 1.5 & RO AT 1.7. THE CENTER TANK WAS FEEDING & TRIM TAN - [SDR FDEA201310012366](https://openairdocs.org/sdr/FDEA201310012366), Oct 1, 2013: SMOKE DETECTOR. FAILED. EQUIPMENT BAY SMOKE INDICATION, SEVERAL MINUTES AFTER, HEARD A LOUD BANG. UNKNOWN WHERE SOUND COME FROM. FIRE WARNING ILLUMINATED SEVERAL TIMES. DID NOT SMELL S - [SDR FDEA201309132202](https://openairdocs.org/sdr/FDEA201309132202), Sep 13, 2013: FITTING. CORRODED. RT WING MLG FITTING OF RIB 5 FORWARD LUG CORRODED, COMPLY WITH EA6-5710-T0302341A. - [SDR FDEA201309132201](https://openairdocs.org/sdr/FDEA201309132201), Sep 13, 2013: FITTING. CORRODED. LT WING MLG FITTING OF RIB 5 FORWARD LUG FOUND CORROSION, COMPLY WITH EA 6-5710-T0302340. - [SDR FDEA201206172253](https://openairdocs.org/sdr/FDEA201206172253), Jun 17, 2012: HYDRAULIC SYSTEM. WARNING MESSAGE. DURING CLIMB, HAD GREEN SYS OVERHEAT ECAM. COMPLIED WITH CHECKLIST, MANUALLY EXTENDED LANDING GEAR TOWED OFF RUNWAY. DRAINED AND SERVICED GREEN SYS HYD RESERVIO - [SDR FDEA201203301200](https://openairdocs.org/sdr/FDEA201203301200), Mar 30, 2012: HYDRAULIC SYSTEM. MULTIPLE FAIL. DURING CRUISE FLIGHT, HYD GREEN SYS RESERVOIR OVERHEAT ILLUMINATED ON ECAM. GREEN HYD PUMPS SECURED UNTIL APPROACH. TURNED BACK ON LOW POWER LIGHTS ILLUMINATED, - [SDR FDEA201102040472](https://openairdocs.org/sdr/FDEA201102040472), Feb 4, 2011: OUTFLOW VALVE. FAILED. 1 HR INTO FLIGHT, CABIN PRESSURE EXCEEDED TOLERANCE (AROUND 9.0 ON DEFFERENTIAL PRESSURE) AND BOTH CONTROLLERS FAILED. HAD TO SELECT MANUAL AGAIN TO BRING PRESS - [SDR FDEA200901140199](https://openairdocs.org/sdr/FDEA200901140199), Jan 14, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANELS ZONE 131, FLOOR PANEL 131QG HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 131QG PER SAMPLE IAW SRZ 25-005, ON TRAVELE - [SDR FDEA200901140198](https://openairdocs.org/sdr/FDEA200901140198), Jan 14, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANELS ZONE 132, FLOOR PANEL 132YF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 132YF PER SAMPLE IAW SRZ 25-005,ON TRAVELER - [SDR FDEA200901140197](https://openairdocs.org/sdr/FDEA200901140197), Jan 14, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANELS ZONE 132, FLOOR PANEL 132RF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 132RF PER SAMPLE IAW SRZ 25-005, ON TRAVELE - [SDR FDEA200901140196](https://openairdocs.org/sdr/FDEA200901140196), Jan 14, 2009: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT ZONE 232, FLOOR PANEL 323RG HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 232RG PER SAMPLE IAW SRZ 25-005, ON TRAVELER NR T8 - [SDR FDEA200901140195](https://openairdocs.org/sdr/FDEA200901140195), Jan 14, 2009: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT ZONE 231, FLOOR PANEL 231QG HAS STRUCTURAL DAMAGES. FABRICATED NEW PANEL NR 231QG PER SAMPLE IAW SRZ 25-005, ON TRAVELER NR T8/77343 - [SDR FDEA200901140194](https://openairdocs.org/sdr/FDEA200901140194), Jan 14, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANELS ZONE 132, FLOOR PANEL 132ZF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 132ZF PER SAMPLE IAW SRZ 25-005,ON TRAVELER - [SDR FDEA200901130185](https://openairdocs.org/sdr/FDEA200901130185), Jan 13, 2009: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT ZONE 231, FLOOR PANEL 231VH HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 231VH PER SAMPLE, ON TRAVELER NR T8 /773390. - [SDR FDEA200901130184](https://openairdocs.org/sdr/FDEA200901130184), Jan 13, 2009: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT ZONE 241, FLOOR PANEL 241WH HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 241WH PER SAMPLE IAW SRZ 25-005 ,ON TRAVELER NR T8/77 - [SDR FDEA200901130183](https://openairdocs.org/sdr/FDEA200901130183), Jan 13, 2009: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT ZONE 231, FLOOR PANEL 231LH HAS STRUCTURAL DAMAGES. FABRICATED NEW PANEL PER SAMPLE IAW SRZ 25-005,ON TRAVELER NR T8/773432. - [SDR FDEA200901130180](https://openairdocs.org/sdr/FDEA200901130180), Jan 13, 2009: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT ZONE 231, FLOOR PANEL 231NH HAS STRUCTURAL DAMAGES FABRICATED NEW PANEL PER SAMPLE IAW SRZ 25-005, ON TRAVELER 3 T8/773431. - [SDR FDEA200901130179](https://openairdocs.org/sdr/FDEA200901130179), Jan 13, 2009: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT ZONE 252, FLOOR PANEL 252UH HAS STRUCTURAL DAMAGES FABRICATED NEW FLOOR PANEL NR 252UH PER SAMPLE IAW SRZ 25-005 ON TRAVELER NR T8/7 - [SDR FDEA200901130178](https://openairdocs.org/sdr/FDEA200901130178), Jan 13, 2009: FLOOR PANEL. DAMAGED. MAIN CARGO COMPARTMENT ZONE 241, FLOOR PANEL NR 241BK HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL PER SAMPLE IAW SRZ 25-005 ON TRAVELER NR T8/773452. - [SDR FDEA200901130177](https://openairdocs.org/sdr/FDEA200901130177), Jan 13, 2009: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT ZONE 241, FLOOR PANEL 241QJ HAS STRUCTURAL DAMAGES. FABRICATED NEW CARGO PANEL NR 241QJ PER SAMPLE IAW SRZ 25-005 ON TRAVELER NR T8/ - [SDR FDEA200901130176](https://openairdocs.org/sdr/FDEA200901130176), Jan 13, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANELS ZONE 132, FLOOR PANEL 132QF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 132QF PER SAMPLE IAW SRZ 25-005 ON TRAVELER - [SDR FDEA200901130175](https://openairdocs.org/sdr/FDEA200901130175), Jan 13, 2009: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT ZONE 252, FLOOR PANEL 252CH HAS STRUCTURAL DAMAGES. FABRICATED NEW MAIN DECK PANEL NR 252CH PER SAMPLE IAW SRZ 25-005 ON TRAVELER NR - [SDR FDEA200901120167](https://openairdocs.org/sdr/FDEA200901120167), Jan 12, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANEL, ZONE 131 FLOOR PANEL 131 HG HAS STRUCTURAL DAMAGES FABRICATED NEW FWD CARGO COMPARTMENT FLOOR PANEL PER SAMPLE , PANEL 131 HG - [SDR FDEA200901120166](https://openairdocs.org/sdr/FDEA200901120166), Jan 12, 2009: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMARTMENT, ZONE 231 FLOOR PANEL 231 AJ HAS STRUCTURAL DAMAGES FABRICATED NEW MAIN CARGO DECK COMPARTMENT FLOOR PANEL 231 AJ PER SAMPLE IAW SRZ - [SDR FDEA200901120165](https://openairdocs.org/sdr/FDEA200901120165), Jan 12, 2009: FLOOR PANEL. DAMAGED. MAIN CARGO DECK COMPARTMENT, ZONE 231 FLOOR PANEL 231 XH HAS STRUCTURAL DAMAGES FABRICATED NEW MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231 XH PER SAMPLE IAW SRZ - [SDR FDEA200901120164](https://openairdocs.org/sdr/FDEA200901120164), Jan 12, 2009: FLOOR PANEL. DAMAGED. MAIN CARGO DECK COMPARTMENT, ZONE 231 FLOOR PANEL 231 XH HAS STRUCTURAL DAMAGES FABRICATED NEW MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231 XH PER SAMPLE IAW SRZ - [SDR FDEA200901120163](https://openairdocs.org/sdr/FDEA200901120163), Jan 12, 2009: FLOOR PANEL. DAMAGED. MANI DECK CARGO COMPARTMENT,ZONE 251 FLOOR PANEL 251 ZH HAS STRUCTURAL DAMAGES. FABRICATED NEW MAIN DECK CARGO COMPARTMENT FLOOR PANEL 251 ZH PER SAMPLE IAW SRZ - [SDR FDEA200901120162](https://openairdocs.org/sdr/FDEA200901120162), Jan 12, 2009: FLOOR PANEL. DAMAGED. BULK CARGO COMPARTMENT ZONE 161,FLOOR PANEL 161GF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 161GF PER SAMPLE IAW SRZ 25-011. - [SDR FDEA200901120160](https://openairdocs.org/sdr/FDEA200901120160), Jan 12, 2009: FLOOR PANEL. DAMAGED. BULK CARGO COMPARTMENT, ZONE 161 FLOOR PANEL 161BF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 161BF PER SAMPLE, IAW SRZ 25-011 ON TRAVELER. - [SDR FDEA200901120159](https://openairdocs.org/sdr/FDEA200901120159), Jan 12, 2009: FLOOR PANEL. DAMAGED. BULK CARGO COMPARTMENT ZONE 162, FLOOR PANEL 162HF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 162HF PER SAMPLE IAW SRZ 25-011 ON TRAVELER. - [SDR FDEA200901120156](https://openairdocs.org/sdr/FDEA200901120156), Jan 12, 2009: FLOOR PANEL. DAMAGED. AFT CARGO COMPARTMENT FLOOR PANELS ZONE 151, FLOOR PANEL 151AF HAS STRUCTURAL DAMAGE. FABRICATED NEW FLOOR PANEL 151AF PER SAMPLE IAW SRZ 25-005, ON TRAVELER NR - [SDR FDEA200901120151](https://openairdocs.org/sdr/FDEA200901120151), Jan 12, 2009: RIB. CRACKED. LEFT WING TIP RIB WY489 CRACKED REMOVED CRACKED RIB WY489.0 IAW SRM 51-40-21. FABRICATED NEW RIB ON TRAVELER NR T8/773917, BATCH NR 436186A1. INSTALLED RIB IAW - [SDR FDEA200901020002](https://openairdocs.org/sdr/FDEA200901020002), Jan 2, 2009: DOUBLER. DAMAGED. THE LT MAIN GEAR WHEEL WELL DOOR INNER AFT TIRE RECESS HAS A 1 INCH GROVE AT THE FWD OTBD SIDE BLENDED AREA ORIG MAT .063 REMAINING MAT IS OUT OF LIMITS, REMOVE - [SDR FDEA200812305320](https://openairdocs.org/sdr/FDEA200812305320), Dec 30, 2008: FLOOR PANEL. CRACKED. FWD CARGO COMPARTMENT FLOOR PANELS, ZONE 131, FLOOR PANEL 131 HG HAS STRUCTURAL DAMAGES FABRICATED NEW FWD CARGO COMPARTMENT FLOOR PANEL, IAW SAMPLE,PANEL 131 H - [SDR FDEA200812245272](https://openairdocs.org/sdr/FDEA200812245272), Dec 24, 2008: STRUCTURE. CORRODED. AIR CONDITIONING COMPT BETWEEN FR44 AND FR45, STR 38R AND 39R HAS SURFACE CORROSION. REMOVED LIGHT SURFACE CORROSION IAW SRM 51-74-10, MATERIAL LOSS .001 IN. TR - [SDR FDEA200812185224](https://openairdocs.org/sdr/FDEA200812185224), Dec 18, 2008: SEAT TRACK. CORRODED. MAIN CARGO DECK SEAT TRACK AT RBL 18 HAS EXFOLIATION FROM FR 19 TO FR 14B. REMOVED SEAT TRACK IAW SRM 51-40-21, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40 - [SDR 08FDEA03601](https://openairdocs.org/sdr/08FDEA03601), Aug 26, 2008: COMPUTER. FAILED. ON APPROACH TO KBUR APPROX 5000' MSL, WHEN SELECTING 20 DEGREES FLAP, T/E FLAPS STUCK AT 15 DEGREES WITH SYS 1 AND 2 FLAP FAULT LIGHTS ILLUMINATED. DIVERTED TO - [SDR 08FDEA02261](https://openairdocs.org/sdr/08FDEA02261), Jun 13, 2008: LINE. LEAKING. HYD GREEN SYSTEM LOW LEVEL IN FLIGHT. ECAM WARNING, MANUAL EXTENTION OF L/G. FOUND UPPER HYD LINE TO RT AILERON DROOP ACTUATOR LEAKING. REPAIRED SAME HYD LINE I - [SDR 07FDEA01500](https://openairdocs.org/sdr/07FDEA01500), Apr 13, 2007: SKIN. CORRODED. DUE TO REMOVAL OF SOME FASTENERS DURING REMOVAL OF CORROSION ON OUTER SKIN AT C80, P5-6 RHS IT WAS IMPOSSIBLE TO REINSTALL SOME FASTENERS WITHOUT DAMAGING THE A - [SDR 07FDEA01499](https://openairdocs.org/sdr/07FDEA01499), Apr 13, 2007: SHEAR TIE. CRACKED. FOUND CRACKED HOLES DURING ACCOMPLISHMENT OF EO 6-5310-7-5020 PT.1, LHS (C43 HOLE H2 CRACK LENGTH 9MM; C45 HOLE H22 CRACK LENGTH 7MM; C46 HOLE H29 CRACK LENGTH - [SDR 07FDEA01498](https://openairdocs.org/sdr/07FDEA01498), Apr 13, 2007: SKIN PANEL. CORRODED. FOUND CORROSION AT UPPER SKIN PANEL C91, P4 RT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5319-103315 AND RAS/DAHAM/4020861/2006 ISSUE "A". - [SDR 07FDEA01497](https://openairdocs.org/sdr/07FDEA01497), Apr 13, 2007: SKIN. DENTED. DENT IN OUTER SKIN AT C20, P24-25, RHS. REPAIR PERFORMED BY SMALL BLEND OUT IAW EA 6-5313-101308 AND RAS/DABRE/7006763/2006 ISSUE "A". - [SDR 07FDEA01496](https://openairdocs.org/sdr/07FDEA01496), Apr 13, 2007: VANE. CHAFED. CHAFING MARKS AT INBOARD FLAP VANE, RHS. REPAIR WAS PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5752-101309 AND RAS/DABRE/7006736/2006 ISSUE "A". - [SDR 07FDEA01495](https://openairdocs.org/sdr/07FDEA01495), Apr 13, 2007: BULKHEAD. DAMAGED. SCRATCH IN PRESSURE BULKHEAD AT C54, TR 4 LT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-101318 AND RAS/045121/010/2006 ISSUE "A". - [SDR 07FDEA01494](https://openairdocs.org/sdr/07FDEA01494), Apr 13, 2007: SKIN. CORRODED. CORROSION ON SEVERAL AREAS AT AIR CONDITIONING COMPARTMENT, C39-C47, P44-P54 LT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-101310 AND RAS/045255/008/2006 ISSU All 68: https://openairdocs.org/deregistered/N810FD-2024-03-02/reports.md --- 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.