# N808FD: 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: 439
- Type of aircraft: Fixed wing multi engine
- Certificate issued: January 3, 2005
- Last registry action: August 4, 2023
- Mode S code: AB0016
- 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/N808FD
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=808FD
- Page: https://openairdocs.org/deregistered/N808FD-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 (104, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR FDEA201902120385](https://openairdocs.org/sdr/FDEA201902120385), Feb 12, 2019: STRUT. INOPERATIVE. ON APPROACH INITIAL GEAR EXTENSION DID NOT SHOW NOSE GEAR GREEN LOCKED INDICATION BUT RED UNLOCKED. RAN QRH AND ATTEMPTED MANUAL GEAR EXTENSION. ON FIRST ATTEMP
- [SDR FDEA2019020870269](https://openairdocs.org/sdr/FDEA2019020870269), Feb 7, 2019: SEQUENCE VALVE. MALFUNCTIONED. ON APPR FOR 20 YEG, GEAR DOWN SELECTED, GOT AN UNSAFE GEAR INDICATION ON NOSE GEAR. FOLLOWED ECAM & QRH. EXTENDED GEAR W/GRAVITY PROCEDURE. TUG TO GATE. CARRIED
- [SDR FDEA2018040853507](https://openairdocs.org/sdr/FDEA2018040853507), Dec 15, 2018: ARM. FAILED. AFTER EXTENDING THE LANDING GEAR, THE NOSE GEAR INDICATED UNLOCKED ON SYSTEM 1 AND 2. AFTER ABOUT 3 MINUTES,, SHOWED LOCKED ON SYSTEM 1 AND 2. REMOVED AND REPLA
- [SDR FDEA201812153507](https://openairdocs.org/sdr/FDEA201812153507), Dec 15, 2018: WARNING SYSTEM. MALFUNCTIONED. AFTER EXTENDING THE LANDING GEAR, THE NOSE GEAR INDICATED UNLOCKED ON SYSTEM 1 AND 2. AFTER ABOUT 3 MINUTES, SHOWED LOCKED ON SYSTEM 1 AND 2.
- [SDR FDEA201710193010](https://openairdocs.org/sdr/FDEA201710193010), Oct 19, 2017: SLIDE. INOPERATIVE. L1 DOOR SLIDE IS INOPERATIVE.
- [SDR FDEA201707151956](https://openairdocs.org/sdr/FDEA201707151956), Jul 15, 2017: SPAR. CRACKED. RIGHT WING REAR SPAR INTERNAL ANGLE NR 60 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201707151951](https://openairdocs.org/sdr/FDEA201707151951), Jul 15, 2017: SPAR. CRACKED. RIGHT WING REAR SPAR INTERNAL ANGLE NR 16 HOLE, NDT INSPECTION FOUND CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201707151950](https://openairdocs.org/sdr/FDEA201707151950), Jul 15, 2017: SPAR. CRACKED. RIGHT WING REAR SPAR INTERNAL ANGLE NR 12 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW IAW GMM 6-2-100.
- [SDR FDEA201707151949](https://openairdocs.org/sdr/FDEA201707151949), Jul 15, 2017: SPAR. CRACKED. RIGHT REAR SPAR INTERNAL ANGLE NR 7 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201707151948](https://openairdocs.org/sdr/FDEA201707151948), Jul 15, 2017: ANGLE. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 61 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201707151947](https://openairdocs.org/sdr/FDEA201707151947), Jul 15, 2017: SPAR. CRACKED. LEFT WING REAR SPAR INTERNAL ANGLE NR 13 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201707151959](https://openairdocs.org/sdr/FDEA201707151959), Jul 15, 2017: SKIN. CRACKED. RIGHT WING RIB 11, CRACKED ON LOWER SKIN ACROSS A FASTENER HOLE APPROX 1.0 INCH IN LENGTH NEAR ACCESS PANEL 681AB. COMPLIED WITH EA 6-5730-T0334254 P1. MAJOR RE
- [SDR FDEA201707151958](https://openairdocs.org/sdr/FDEA201707151958), Jul 15, 2017: SKIN. CRACKED. LEFT WING RIB 11, CRACKED ON THE LOWER SKIN ACCROSS A FASTENER HOLE APPROX 1.5 INCH IN LENGTH, NEAR ACCESS PANEL 581AB. COMPLIED WITH EA 6-5730-T0334254, P1. MA
- [SDR FDEA201707151946](https://openairdocs.org/sdr/FDEA201707151946), Jul 15, 2017: ANGLE. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 53 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAM THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51
- [SDR FDEA201707151957](https://openairdocs.org/sdr/FDEA201707151957), Jul 15, 2017: SPAR. CRACKED. RIGHT REAR SPAR INTERNAL ANGLE NR 63 HOLE NDT INSPECTION FOUND CRACK SIGNAL. RIGHT REAR SPAR INTERNAL ANGLE 63 HOLE NDT INSPECTION FOUND CRACK SIGNAL. REAM THE 
- [SDR FDEA201707151955](https://openairdocs.org/sdr/FDEA201707151955), Jul 15, 2017: SPAR. CRACKED. RIGHT WING REAR SPAR INTERNAL ANGLE NR 38 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION IAW NTM 51-10
- [SDR FDEA201707151954](https://openairdocs.org/sdr/FDEA201707151954), Jul 15, 2017: SPAR. CRACKED. RIGHT WING REAR SPAR INTERNAL ANGLE NR 35 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION IAW NTM 51-10
- [SDR FDEA201707151953](https://openairdocs.org/sdr/FDEA201707151953), Jul 15, 2017: SPAR. CRACKED. RIGHT WING REAR SPAR INTERNAL ANGLE NR 33 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE I
- [SDR FDEA201707151952](https://openairdocs.org/sdr/FDEA201707151952), Jul 15, 2017: SPAR. CRACKED. RIGHT REAR SPAR INTERNAL ANGLE NR 30 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAM THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM5
- [SDR FDEA201707151945](https://openairdocs.org/sdr/FDEA201707151945), Jul 15, 2017: SPAR. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 35 HOLE NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE AFFECTED HOLE THROUGH ALL LAYERS IAW SRM 51-40-44, PERFORM ROTOTEST INS
- [SDR FDEA201707111907](https://openairdocs.org/sdr/FDEA201707111907), Jul 11, 2017: ANGLE. CRACKED. LEFT WING REAR SPAR INERNAL ANGLE 16 HOLE FOUND CRACKED. REPAIRED IAW EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201707051852](https://openairdocs.org/sdr/FDEA201707051852), Jul 5, 2017: SKIN. CORRODED. FWD TOILET SERVICE PANEL LOWER CUTOUT SKIN DELAMINATED. INSPECTED FOUND SKIN INNER STIFFENER CORRODED AND OUT OF LIMITS IAW SRM 51-40-21, & SRM 53-12-18, FIG 2,
- [SDR FDEA201705011301](https://openairdocs.org/sdr/FDEA201705011301), May 1, 2017: PUMP. INOPERATIVE. IN CRUISE FL360 GOT GREEN HYD SYSTEM OVERHEAT. ECAM ADVISED TO TURN OFF GREEN ENGINE PUMPS 1 AND 2. ENG HYD 1 PUMP SHUT OFF NORMALLY. ENG HYD 2 GREEN PUMP TURNE
- [SDR FDEA201602150560](https://openairdocs.org/sdr/FDEA201602150560), Feb 15, 2016: SKIN PANEL. CORRODED. CORROSION ON UPPER RT WING SKIN, APPROX 83.5" FROM WTB. CORROSION FORMED AROUND FASTENER HEAD & EXTENDS AFT, APPROX 2"X4". REMOVED VISIBLE CORROSION ON RT WING 
- [SDR FDEA201512284090](https://openairdocs.org/sdr/FDEA201512284090), Dec 28, 2015: ENGINE. POWER LOSS. DURING DESCENT BELOW PROFILE THRUST WAS APPROX 75 - 77% N1. AT PROFILE THROTTLES REDUCED TO IDLE & APPROX 60% N1, A THUMPING SOUND WAS HEARD & FELT. SUSPECT COM
- [SDR FDEA201506171831](https://openairdocs.org/sdr/FDEA201506171831), Jun 17, 2015: WINDSHIELD. CRACKED. AT FL 370 CAPTAIN`S OUTER WINDSCREEN SHATTERED. PRESSURIZATION HELD OK, DIVERTED. R & R CAPTAIN`S WINDSHIELD PANEL IAW AMM 56-11-11-04. WINDSHIELD PANEL ANTI-IC
- [SDR FDEA201504301331](https://openairdocs.org/sdr/FDEA201504301331), Apr 30, 2015: WINDOW. FAILED. AFTER TAKEOFF GOT RT WINDOW HEAT FAULT. FOLLOWED QRH & RESET RT WINDOW HEAT. LATER CLIMBING THROUGH FL 280, THE LT WINDSHIELD COMPLETELY SHATTERED ON THE OUTSID
- [SDR FDEA201502220573](https://openairdocs.org/sdr/FDEA201502220573), Feb 22, 2015: SKIN. DAMAGED. FOUND ONE LIGHTNING STRIKE AT THE TRAILING EDGE OF THE LT WING TIP UPPER INBD SURFACE. REPLACED THE SKIN IAW SRM 57-30-11.
- [SDR FDEA201502160536](https://openairdocs.org/sdr/FDEA201502160536), Feb 16, 2015: FITTING. CRACKED. AFT CARGO COMPARTMENT DOOR ACTUATOR FITTING CRACKED. REMOVED THE AFT CARGO DOOR ASSEMBLY IAW AMM 52-32-11-04. REPLACED THE FRAME HEAD IAW SRM 51-40-21. INSTALLE
- [SDR FDEA201502130527](https://openairdocs.org/sdr/FDEA201502130527), Feb 13, 2015: CROSSBEAM. CORRODED. AFT CARGO FLOOR FRAME 63 CROSSBEAM CORRODED BETWEEN Y140 & Y805. REPAIRED THE CROSSBEAM PER SRM 53-10-15 FIG.209.SHT.1
- [SDR FDEA201502130526](https://openairdocs.org/sdr/FDEA201502130526), Feb 13, 2015: CROSSBEAM. CORRODED. AFT CARGO FLOOR FRAME 61 CROSSBEAM CORRODED BETWEEN -Y805 & Y805. REPAIR THE CROSSBEAM PER SRM 53-10-15 FIG.209 SHT.1
- [SDR FDEA201501070049](https://openairdocs.org/sdr/FDEA201501070049), Jan 7, 2015: BLEED VALVE. MALFUNCTIONED. FLIGHT DEPARTED WITH MEL 36-11-06-1A, NR 1 BLEED AIR VLV INOPERATIVE. DURING CLIMB OUT, WE DEVELOPED A NR 2 HP BLEED FAULT. FOLLOWED ECAM & QRH PROCEDURES. PROC
- [SDR FDEA201303120549](https://openairdocs.org/sdr/FDEA201303120549), Mar 12, 2013: RIB. CRACKED. LT WING T/E AT 284.85, SUPPORT RIB CRACKED, JUST BETWEEN SPOILER NR 5 AND SPOILER NR 6.
- [SDR FDEA201205011689](https://openairdocs.org/sdr/FDEA201205011689), May 1, 2012: ANGLE. CRACKED. LEFT FRAME40 PICK UP ANGLE FOUND CRACK EXTENDED FURTHER THAN STOP HOLE (EXTENDED CRACK LENGTH:0.2INCHES) COMPLY WITH EA 6-5310-161218, PART 1.
- [SDR FDEA201112295456](https://openairdocs.org/sdr/FDEA201112295456), Dec 29, 2011: OIL SYSTEM. OVERTEMP. NR 2 ENG, HIGH OIL TEMP - ABOVE 180 DEG - SHUT ENG DOWN. ALL OTHER ENG PARAMETERS OK. INSPECTED NR2 ENG INLET & EXHAUST AREA; NIL ABNORMALTIES NOTED. VISUAL CK 
- [SDR FDEA201109203976](https://openairdocs.org/sdr/FDEA201109203976), Sep 20, 2011: CABIN PRESSURE. MALFUNCTIONED. RED CABIN ALTITUDE WARNING, PERFORMED DESCENT TO 10,000 FT ON CABIN PRESSURE SYS PAGE, BOTH OUTFLOW VALVES SHOW AMBER & FULL OPEN - NO ECAM MESSAGE, CABIN ALTIT
- [SDR FDEA200912084382](https://openairdocs.org/sdr/FDEA200912084382), Dec 8, 2009: COMPUTER. MALFUNCTIONED. ON CLIMB OUT, FLAPS AND SLATS UP, CAPT MAX SPEED INDICATOR (ZIPPER) REMAINED AT 245 KTS. F/O SPD LIMIT REMAINED "ON". R & R NR 2 SFCC DUE TO FAULT AND R & R NR 
- [SDR FDEA200904011132](https://openairdocs.org/sdr/FDEA200904011132), Apr 1, 2009: WIRE. FAULTED. AFTER T/O FLAPS STUCK AT ABOUT 5 DEGREES, COMPLIED WITH QRH. NO LUCK, RETURNED TO IND FLAPS CAME DOWN OK FOUND SAME FAULT CODES AS BEFORE SFCC 1 AND 2 LT VANE O
- [SDR FDEA200812315323](https://openairdocs.org/sdr/FDEA200812315323), Dec 31, 2008: DAMPER. MALFUNCTIONED. LANDING GEAR WOULD NOT RETRACT ON TAKEOFF ALTHOUGH AUTO THROTTLES WAS ENGAGED IT WAS INOP IN THE INITIAL CLIMB AUTO THROTTLE WORKED AGAIN ONCE SLATS WERE EXTEND
- [SDR 08FDEA04005](https://openairdocs.org/sdr/08FDEA04005), Sep 23, 2008: SEAT TRACK. DAMAGED. MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE HAS SCRATCH AT FR 40 LT, BELOW FLOOR PANEL 231QH, AFT SIDE REMOVED DAMAGED SEAT TRACK AND FABRICATED AND INSTALLED R
- [SDR 08FDEA03938](https://openairdocs.org/sdr/08FDEA03938), Sep 18, 2008: SEAT TRACK. CORRODED. MDCC SEAT TRACK 4R CORRODED 2 AREAS FRAME 42 AND 44 4 SQ INCH. REMOVED LEVEL 1 CORROSION. REMOVED AND REPLACED SEAT TRACK FROM FR 40 TO 44.5 RT AT Y-1456 IAW SR
- [SDR 08FDEA03937](https://openairdocs.org/sdr/08FDEA03937), Sep 18, 2008: FLOORBEAM. CRACKED. MDCC FLOOR FRAME 30 HAS 1 INCH CRACK BETWEEN SEAT TRACK 2L AND 3L REMOVED CRACK AND INSTALLED FLOORBEAM REPAIR BETWEEN SEAT TRACK 2L AND 3L AT FR 30 IAW SRM 53-
- [SDR 08FDEA03936](https://openairdocs.org/sdr/08FDEA03936), Sep 18, 2008: SEAT TRACK. CORRODED. MDCC SEAT TRACK NR 1 CORRODED AT FRAME 71 2 SQ IN REMOVED LEVEL 1 CORROSION. REMOVED AND REPLACED SEAT TRACK SECTION AT FR71 TO 74 AND INSTALLED NEW SECTION IAW
- [SDR 08FDEA03935](https://openairdocs.org/sdr/08FDEA03935), Sep 18, 2008: SKIN. DAMAGED. RIGHT SIDE FUSELAGE FR 37 STRINGER 30 1 LIGHTNING STRIKE REMOVED DAMAGED AREA AT FR37 RT SIDE STR 30 AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-12 FIG 224 SHEET
- [SDR 08FDEA03934](https://openairdocs.org/sdr/08FDEA03934), Sep 18, 2008: SEAT TRACK. CORRODED. MDCC SEAT TRACK 3R CORRODED 2 AREAS AT FRAME 46 4 INCH SQ IN REMOVED LEVEL 1 CORROSION ON SEAT TRACK SECTION AND INSTALLED NEW SEAT TRACK 3R FROM FRAME 44 TO 49
- [SDR 08FDEA03910](https://openairdocs.org/sdr/08FDEA03910), Sep 17, 2008: SEAT TRACK. DAMAGED. MAIN DECK CARGO SEAT TRACK NR 4LT BETWEEN FR 59.2 AND FR 59.3 HAS 2 AREAS OF DAMAGED SCALLOPS REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED REPLACEMENT TR
- [SDR 08FDEA00544](https://openairdocs.org/sdr/08FDEA00544), Feb 21, 2008: WIRE. DAMAGED. AFTER START GOT OVERBOARD VALVE FAULT COMPLIED WITH ECAM QRH AND CHECKED MEL. DURING CLIMB-OUT, AIRCRAFT WOULD NOT PRESSURIZE. REMOVED AVIONICS EXTRACT VALVE TO
- [SDR 07FDEA03455](https://openairdocs.org/sdr/07FDEA03455), Sep 7, 2007: STRINGER. CORRODED. FOUND CORROSION ON STRINGER 50, BETWEEN FRAME 55/58-59 LHS, OUT OF LIMIT. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.
- [SDR 07FDEA03463](https://openairdocs.org/sdr/07FDEA03463), Sep 7, 2007: SKIN PANEL. CORRODED. HEAVY CORROSION FOUND ON CENTER WING BOX TOP SKIN AT TR5 AND TR6 RT/LT, FRAME 43-46.2. REPAIR PERFORMED IAW SRM 57-10-12/FIG 201 AND RAS/042817/015/2006 ISSUE A
- [SDR 07FDEA03462](https://openairdocs.org/sdr/07FDEA03462), Sep 7, 2007: STRINGER. CORRODED. FOUND CORROSION ON STRINGER 43 RT BETWEEN FRAME 47-48, OUT OF LIMIT. REPAIR PERFORMED BY BLEND OUT THE CORRODED AREAS IAW EA 6-5315-99192 AND RAS/043644/008/200

All 104: https://openairdocs.org/deregistered/N808FD-2024-03-02/reports.md

## FAA accident and incident reports (1)

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 20171017021719I](https://openairdocs.org/incident/20171017021719I), Oct 17, 2017: Airbus Industrie A310-324 (N808FD), Lubbock, TX, No damage, 1 fatal. At approximately 1434 hours (CDT), the fedex chief inspector called to notify this office that fedex had an aircraft maintenance technician involved in a fatal…

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