# N804FD: 1990 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)
- 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: 549
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 16, 2005
- Certificate issued: September 14, 2004
- Last registry action: January 8, 2024
- Mode S code: AAF13A
- 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/N804FD
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=804FD
- Page: https://openairdocs.org/deregistered/N804FD-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 (119, newest 50)

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

- [SDR FDEA201609153243](https://openairdocs.org/sdr/FDEA201609153243), Sep 15, 2016: COALESCER BAG. ODOR. AFTER PARKING, THE AVIONICS SMOKE WARNING SOUNDED. PULLED CIRCUIT BREAKERS, TURNED ON OVERRIDE NR 1 AND 2 AND OPEN THE AVIONICS HATCH, SMELLED SMOKE. POWERED DO
- [SDR FDEA201607192536](https://openairdocs.org/sdr/FDEA201607192536), Jul 19, 2016: SMOKE DETECTOR. FAULTY. "AVIONICS SMOKE" DISPLAYED ON ELECTRICAL PANEL AFTER ENGINE SHUTDOWN AT GATE. NO SMOKE WAS EMITTED ON THE SNIFFER FAN. R & R SMOKE DETECTOR.
- [SDR FDEA201511193714](https://openairdocs.org/sdr/FDEA201511193714), Nov 19, 2015: BRACKET. DAMAGED. ON POST FLIGHT FOUND FUELING DOOR 144DR MISSING WITH DAMAGE TO RT PACK INLET FAIRING. REPLACED BROKEN COOLING DUCT SUPPORT BRACKET IAW SRM 51-72-10. REMOVED AND
- [SDR FDEA201510313432](https://openairdocs.org/sdr/FDEA201510313432), Oct 31, 2015: ACTUATOR. LEAKING. BLUE RESERVOIR LO LEVEL ECAM WITH ASSOCIATED SPOILERS FAULTS. FOLLOWED ECAM & QRH, RETURNED FOR UNEVENTFUL LANDING. FOUND NR 3 RT SPOILER ACTUATOR, SIDE CAP BLO
- [SDR FDEA201510303445](https://openairdocs.org/sdr/FDEA201510303445), Oct 30, 2015: COMPUTER. FAILED. DURING LANDING, GEAR EXTENSIONS WITH POSITION DETECTOR, SYS NR 2 SELECTED, GOT ECAM, LG DOOR SYS INOPERATIVE UNTIL ALL GEARS WERE DOWN & LOCKED. SYS NR 1 MEL'D,
- [SDR FDEA201503060700](https://openairdocs.org/sdr/FDEA201503060700), Mar 6, 2015: SLIDE. UNWANTED DEPLOY. DOOR R1 SLIDE DEPLOYED ACCIDENTALLY AT BLOCK. REMOVED AND REPLACED THE R1 SLIDE IAW MM 25-61-22-04-02, ARMED THE R1 SLIDE OPS TEST IAW MM 52-73-00-05. REMOVED A
- [SDR FDEA201409112578](https://openairdocs.org/sdr/FDEA201409112578), Sep 11, 2014: SKIN. CORRODED. AV COMPARTMENT FUSELAGE SKIN FRAME 16A - 17 STRINGER 44 - 45 RT INNER SURFACE FOUND CORROSION. COMPLIED WITH EA 6-5310-T0310792 P1 EA TITLE FUSELAGE MAIN FRAME 
- [SDR FDEA201409012391](https://openairdocs.org/sdr/FDEA201409012391), Sep 1, 2014: REPAIR. DEBONDED. AGING INSPECTION - EXISTING REPAIR ON LT WING I/B FLAP TRAILING EDGE RIB8-10 UPR & LWR SURFACE. REPAIR PATCH DISBONDED. REPORTED TO ENGINEER. REMOVED THE OLD RE
- [SDR FDEA201408222288](https://openairdocs.org/sdr/FDEA201408222288), Aug 22, 2014: FASTENER. MISSING. AGING INSPECTION EXISTING REPAIR ON AFT CARGO DOOR SILL BEAM BETWEEN FRAME 59 & 64 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALVATED AND FOUND THE RE
- [SDR FDEA201408202239](https://openairdocs.org/sdr/FDEA201408202239), Aug 20, 2014: REPAIR. DEBONDED. AGING INSPECTION EXISTING REPAIR ON RT WING INBD FLAP TE RIB 5 - 7 LOWER SURFACE, REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR PATCH DISBONDED REMOVED OLD REP
- [SDR FDEA201408202238](https://openairdocs.org/sdr/FDEA201408202238), Aug 20, 2014: REPAIR. DEBONDED. AGING INSPECTION EXISTING REPAIR ON RT WING INBD FLAP TE RIB 3 - 5 LOWER SURFACE, REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED AND FOUND THE OLD
- [SDR FDEA201408202242](https://openairdocs.org/sdr/FDEA201408202242), Aug 20, 2014: REPAIR. CORRODED. AGING INSPECTION EXISTING REPAIR ON AV COMPARTMENT STRINGER 44 RT BETWEEN FRAME 16 & 17 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS FOUND CORRODED HEVAIL
- [SDR FDEA201408202241](https://openairdocs.org/sdr/FDEA201408202241), Aug 20, 2014: STRINGER. CORRODED. AGING INSPECTION EXISTING REPAIR ON AV COMPARTMENT STRINGER 44 RT BETWEEN FRAME 15A & 16 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALVATED AND FOUND 
- [SDR FDEA201408072106](https://openairdocs.org/sdr/FDEA201408072106), Aug 7, 2014: STRINGER. CORRODED. AV COMPARTMENT STRINGER 44 RT FOUND HEAVY CORROSION AT FRAME 16 LOCATION. COMPLIED WITH EA 6-5310-T0310620 PART 1 TITLE :FUSELAGE MAINFRAME SECTION 12. CORROSIO
- [SDR FDEA201407281996](https://openairdocs.org/sdr/FDEA201407281996), Jul 28, 2014: COMPUTER. FAILED. PASSING 10000 FT TRIM TANK PUMPS ECAM MSG FUEL QTY SHOWED 34K TOTAL, 64.2 TAKEOFF FUEL. ECAM MSG SELF-CLEARED & FUEL SLOWLY ROSE AGAIN, FUEL WAS GOOD. AFTER TAK
- [SDR FDEA201406281576](https://openairdocs.org/sdr/FDEA201406281576), Jun 28, 2014: PULLEY. DEFECTIVE. ON DEPARTURE CLIMB WITH AUTO PILOT NR 2 ON WHEN THE SLATS WERE RETRACTED THE ACFT GAVE VERY HARD TO THE RT. THE AILERONS COMPENSATED BY GOING LT 6 UNITS. AT THI
- [SDR FDEA201405110982](https://openairdocs.org/sdr/FDEA201405110982), May 11, 2014: RIB. CORRODED. LEFT RIB 5 FWD LUG HAS CORROSION IN BORE, FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0307941 P-1. MAJOR REPAIR.
- [SDR FDEA201405110981](https://openairdocs.org/sdr/FDEA201405110981), May 11, 2014: RIB. CORRODED. RIGHT RIB 5 FWD LUG HAS CORROSION IN BORE, FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0307941 P-2, WING BASIC WING STRUCTURE, LT & RT RIB 5 FWD LUG CORROSION. MA
- [SDR FDEA201402140320](https://openairdocs.org/sdr/FDEA201402140320), Feb 14, 2014: TRU. FAULTED. ESS TR INDICATED 4A NUMEROUS TIMES IN CRUISE. FOUND ONLY 4A ON ESS TR & I ESS TRANSFORMER RECTIFIER IAW MM 24-32-11-04. OPERATIONS CHECK SATISFACTORY RUN NR 2 E
- [SDR FDEA201202160589](https://openairdocs.org/sdr/FDEA201202160589), Feb 16, 2012: SPAR. DAMAGED. RT PYLON SPIGOT RECEPTACLE FITTING FOUND A MISDRILLED BOLT HOLE. REPAIRED IAW AMM 54-50-00 AND AMM 20-21-12
- [SDR FDEA201202100542](https://openairdocs.org/sdr/FDEA201202100542), Feb 10, 2012: SKIN. CONTAMINATED. TWO WATER TRAPPED AREAS WERE FOUND AT RT RUDDER NR 27 SCREW (5.5" X 5") AND NR 38 SCREW (3" X 1.5") (EO 6-5530-7-5004, PART 2) NDT INSPECT L/E AND T/E. THE OUTE
- [SDR FDEA201202100543](https://openairdocs.org/sdr/FDEA201202100543), Feb 10, 2012: SKIN. CORRODED. RIGHT WING UPPER SKIN NEAR REAR SPAR FOUND CORROSION POSITION BETWEEN RIB 4 AND RIB 6. PERFORMED THE REPAIR IAW EA 6-5730-1490. REPAIR EVALUATED IAW GMM 6-2-100
- [SDR FDEA201202100541](https://openairdocs.org/sdr/FDEA201202100541), Feb 10, 2012: SKIN. CORRODED. LEFT WING BOTTOM SKIN UPPER SURFACE CORRODED AT RIB 5 REINFORCING BEHIND REAR SPAR AREA. REMOVED CORROSION IAW EA 6-5730-149035. REPAIR CLASSIFIED AS MINOR IAW 
- [SDR FDEA201202040470](https://openairdocs.org/sdr/FDEA201202040470), Feb 4, 2012: SKIN. DENTED. NOSE SECTION RT LOWER HALT SKIN PLATE EXTERNAL HAS A DENT JUST BELOW COCKPIT FLOOR LEVEL LOCATION BETWEEN FR2 AND FR3 POSITION 1. PAIN REMOVED IAW SRM 51-75-20.
- [SDR FDEA201201110095](https://openairdocs.org/sdr/FDEA201201110095), Jan 11, 2012: SKIN. CORRODED. RIGHT WING UPPER SKIN NEAR FRONT SPAR FOUND CORROSION POSITION BETWEEN RIB 8 AND RIB 9. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE DAMAGE AND FOUND WI
- [SDR FDEA201201110094](https://openairdocs.org/sdr/FDEA201201110094), Jan 11, 2012: SKIN. CORRODED. RIGHT WING UPPER SKIN NEAR MIDDLE SPAR FOUND CORROSION POSITION BETWEEN RIB 8 AND RIB 9. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE THE DAMAGE AND FOU
- [SDR FDEA201201110096](https://openairdocs.org/sdr/FDEA201201110096), Jan 11, 2012: FLOOR SUPPORT. CORRODED. FWD MAIN DECK COURIER FLOOR AREA FOUND FLOOR SUPPORT CORRODED FROM FR 12 TO FR 14 BETWEEN Y 383 AND Y 953. REPLACED WITH NEW SUPPORT IAW SRM 51-40-21 AND 51-72-
- [SDR FDEA201201110093](https://openairdocs.org/sdr/FDEA201201110093), Jan 11, 2012: SKIN. CORRODED. RIGHT WING UPPER SKIN NEAR REAR SPAR FOUND CORROSION POSITION AT RIB 7. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE THE DAMAGE AND FOUND WITHIN ALLOWAB
- [SDR FDEA201201110091](https://openairdocs.org/sdr/FDEA201201110091), Jan 11, 2012: SKIN. CORRODED. RIGHT WING UPPERSKIN NEAR FRONT SPAR FOUND CORRODED, POSITION BETWEEN RIBS 16 AND 17. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE THE DAMAGE AND FOUND 
- [SDR FDEA201201110090](https://openairdocs.org/sdr/FDEA201201110090), Jan 11, 2012: SKIN. CORRODED. RIGHT WING UPPER SKIN NEAR FRONT SPAR FOUND CORROSION POSITION BETWEEN RIB 20 AND RIB 21. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE THE DAMAGE AND FO
- [SDR FDEA201201110089](https://openairdocs.org/sdr/FDEA201201110089), Jan 11, 2012: SKIN. CORRODED. RIGHT WING UPPER SKIN NEAR REAR SPAR FOUND CORROSION POSITION BETWEEN RIB 25 AND RIB 26. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURE DAMAGE AND FOUND W
- [SDR FDEA201201110088](https://openairdocs.org/sdr/FDEA201201110088), Jan 11, 2012: SKIN. CORRODED. RT WING UPPER SKIN FOUND CORROSION POSITION ABOUT RIB 27 BESIDE THE OTBD JET FUEL PANEL. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURED THE DAMAGE AND FO
- [SDR FDEA201201110086](https://openairdocs.org/sdr/FDEA201201110086), Jan 11, 2012: SKIN. CORRODED. RT WING UPPER SKIN NEAR REAR SPAR FOUND CORROSION POSITION BETWEEN RIB 28 AND RIB 29. BLENDED OUT TO A SMOOTH POLISHED PROFILE AND MEASURED THE DAMAGE AND FOUND
- [SDR FDEA201201080046](https://openairdocs.org/sdr/FDEA201201080046), Jan 8, 2012: SEAT TRACK. CHAFED. MAIN DECK SEAT TRACK CHAFED BETWEEN FR 54.2 AND FR 54.3, Y0. FABRICATED THE SEAT TRACK IAW SRM 51-40-21 AND DWG NR 16 A53274256. REPAIR CLASSIFIED AS MAJOR IAW 
- [SDR FDEA201201080045](https://openairdocs.org/sdr/FDEA201201080045), Jan 8, 2012: SEAT TRACK. CHAFED. MAIN DECK SEAT TRACK CHAFED BETWEEN FR 54.2 AND FR 54.3, Y1456. FABRICATED THE SEAT TRACK IAW SRM 51-40-21 AND DWG NR 16, A53274256. REPAIR CLASSIFIED AS MAJOR 
- [SDR FDEA201110174555](https://openairdocs.org/sdr/FDEA201110174555), Oct 17, 2011: ENGINE. FAILED. CLIMBING THRU FL300 F/O FELT SLIGHT VIBRATION, BUT NO INDICATIOINS OR ECAM AT FL 355, THERE WAS A YAW AND LOUD BANGING, EPR HAD DROPPED TO BELOW 1, OTHER ENGINE
- [SDR FDEA201010093981](https://openairdocs.org/sdr/FDEA201010093981), Oct 9, 2010: DAMPER. LEAKING. LANDING GEAR WOULD NOT RETRACT ON DEPARTURE, RETURNED TO RPVM, HAD LANDING GEAR RETRACTION FAULT PROX. DETECTION BOX FAULTED TO "BR" - BOGIE RIGHT FAIL. ON INSP
- [SDR FDEA201010073974](https://openairdocs.org/sdr/FDEA201010073974), Oct 7, 2010: SELECTOR VALVE. FAILED. LOWERED MLG HANDLE (WITH SYS 2, POSITION DET SELECTED) GOT UNLOCK LIGHTS BUT NO MLG DOWN, SELECTED SYS 1, NO CHANGE, RAISED MLG HANDLE, LIGHTS WENT OUT, LOWERED
- [SDR FDEA201009263715](https://openairdocs.org/sdr/FDEA201009263715), Sep 26, 2010: CONNECTOR. DIRTY. CLIMBING THROUGH FL330 GOT RT R1 DOOR NOT CLOSED COMPLIED WITH QRH AND DESCENTED BELOW 10,000. GOING THROUGH FL200 THE WARNING WENT AWAY. ATC WOULD NOT LET US C
- [SDR FDEA201008263146](https://openairdocs.org/sdr/FDEA201008263146), Aug 26, 2010: PITOT HEAD. CONTAMINATED. F/O A/S INOP DURING T/O ROLL ABORTED T/O. PVG U CHECKED F/O PITOT TUBE FOUND A BUG INSIDE, CLEARED PITOT TUBE AND PERFORMED THE PITOT TUBE INSP ALL OK IAW AMM 3
- [SDR FDEA200912104401](https://openairdocs.org/sdr/FDEA200912104401), Dec 10, 2009: SKIN. MISREPAIRED. PREVIOUS FLUSH REPAIR LOCATED ON LT WING NR 2 SLAT UPPER NOSE SKIN BETWEEN RIBS 14 TO 17 MEASURES 11.7 INCHES X 9.8 INCHES. PREVIOUSLY INSTALLED REPAIR LOCATED 
- [SDR FDEA200912104400](https://openairdocs.org/sdr/FDEA200912104400), Dec 10, 2009: SKIN. MISREPAIRED. PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT RT SIDE FUSELAGE SKIN AT FRAME 74 AND BETWEEN STRINGERS 39 TO 41 RT MEASURES 9 INCHES X 7.2 INCHES, WITH A SKIN CUTO
- [SDR FDEA200912074364](https://openairdocs.org/sdr/FDEA200912074364), Dec 7, 2009: SKIN. CORRODED. LT WING UPPER SURFACE GRAVITY FUEL PORT INBD HAS LEVEL 1 CORROSION AROUND CUT-OUT EXTENDING UNDER SKIN APROX 1" TO 1.5" REPAIRED UPPER WING SKIN AROUND LT UPPER
- [SDR FDEA200812315322](https://openairdocs.org/sdr/FDEA200812315322), Dec 31, 2008: SENSOR. MALFUNCTIONED. AFTER T/O LANDING GEAR FAILED TO RETRACT. ECAM DISPLAYED L/G RETRACTION INOP. ACFT LOST AUTO-THROTTLES. FOUND TARGET SENSORS 9GA AND 11GA LOS SE AND OUT OF "C" 
- [SDR 08FDEA03529](https://openairdocs.org/sdr/08FDEA03529), Aug 21, 2008: SELECTOR VALVE. FAILED. LDG GEAR DID NOT EXTEND WITH GEAR HANDLE, GRAVITY EXTENSION OK PER CREW DEBRIEF, WHEN GEAR HANDLE CYCLED THERE WAS NO ASSOCIATED AUDIABLE SOUND NORMALLY HEARD D
- [SDR 07FDEA03926](https://openairdocs.org/sdr/07FDEA03926), Sep 18, 2007: STRINGER. CORRODED. FOUND PITTING CORROSION ON FOLLOWING MILLED STRINGER: 52, 53 AND 54 RT AND STRG 52, 53, 54 AND 56 LT, BETWEEN FRAME 54.1-55/58. REPAIR PERFORMED BY REPLACEMENT 
- [SDR 07FDEA03924](https://openairdocs.org/sdr/07FDEA03924), Sep 18, 2007: STRINGER. CORRODED. FOUND PITTING CORROSION ON FOLLOWING STRINGER: 48 AND 50 RT AND STRG 46, 47, 48, 50 AND 51 LT, BETWEEN FRAME 54-55/58. REPAIR PERFORMED BY REPLACEMENT OF STRING
- [SDR 07FDEA03923](https://openairdocs.org/sdr/07FDEA03923), Sep 18, 2007: STRINGER. CORRODED. FOUND PITTING CORROSION ON STRINGER 44 RT, BETWEEN FRAME 54-55/58. REPAIR PERFORMED BY REPLACEMENT OF STRINGER PORTION AS LONG AS POSSIBLE BY USING ADDITIONAL C
- [SDR 07FDEA03922](https://openairdocs.org/sdr/07FDEA03922), Sep 18, 2007: STRINGER SPLICE. CORRODED. FOUND CORRODED STRINGER COUPLING AT FRAME 55/58, STRG 50 RT. REPLACEMENT OF COUPLING IAW SRM 51-72-10.
- [SDR 07FDEA03921](https://openairdocs.org/sdr/07FDEA03921), Sep 18, 2007: STRINGER SPLICE. CORRODED. FOUND TWO CORRODED STRINGER COUPLINGS AT FRAME 55/58, STRG 48 AND 49 RT. REPLACEMENT OF BOTH COUPLINGS IAW SRM 51-72-10.

All 119: https://openairdocs.org/deregistered/N804FD-2024-03-02/reports.md

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