# N805FD: 1988 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: 456 - Year built: 1988 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 9, 2005 - Certificate issued: November 19, 2004 - Last registry action: June 23, 2023 - Mode S code: AAF4F1 - 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/N805FD - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=805FD - Page: https://openairdocs.org/deregistered/N805FD-2024-03-02 From the FAA registry file of October 31, 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 (70, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FDEA201609133211](https://openairdocs.org/sdr/FDEA201609133211), Sep 13, 2016: SLAT. LACK OF LUBE. DURING APPROACH, SLATS WOULD NOT EXTEND, COMPLIED WITH PHASE 1, ECAM & QRH - SLATS CONFIRMED STUCK. DID NO SLAT/FULL FLAP LANDING IAW QRH. CREW CALLED IN FIRETR - [SDR FDEA201606131980](https://openairdocs.org/sdr/FDEA201606131980), Jun 13, 2016: COMPUTER. FAULTY. APPROX 60 NM FROM DESTINATION, GOT FUEL ADV ON ECAM. LT OUTER 6K, LT INNER 11.0, CTR WAS 0, TRIM TANK WAS 0, RT INNER STARTED AT 11, THEN 10, THEN 9, THEN 8, AL - [SDR FDEA201407191860](https://openairdocs.org/sdr/FDEA201407191860), Jul 19, 2014: STRINGER. CORRODED. AFT CARGO STRINGER 46R FRAME 63 - 64 STRINGER CORRODED. REPAIRED THE STRINGER PER A310 SRM 53-10-14 PB201 FIG201H - [SDR FDEA201207262710](https://openairdocs.org/sdr/FDEA201207262710), Jul 26, 2012: ENGINE. FAILED. UPASSING 3000 ON T/O, FELT ABNORMAL VIBRATION WITH UNUSUAL NOISE. NOTICED N1 VIB AT 1.4 AND N2 VIB AT 2.4 ON ENG 1. WHILE TROUBLESHOOTING RECEIVED ENG 1 EPR MOD - [SDR FDEA201204051259](https://openairdocs.org/sdr/FDEA201204051259), Apr 5, 2012: FUEL CELL. LEAKING. LEFT WING INNER TANK LOWER SURFACE 1 EA BOLT FUEL SEEPING NEAR REAR SPAR RIB 8 POSITION. USED OPTIONAL INSP METHOD WITH HIGH LEVEL FUEL SENSING. TORQUED NUT WIT - [SDR FDEA201204051258](https://openairdocs.org/sdr/FDEA201204051258), Apr 5, 2012: FUEL CELL. LEAKING. RIGHT OUTER TANK REAR SPAR, FUEL SEEPING AT NR 6 SPOILER BLOCK VALVE SUPPORT FITTING LWR RT FITTING FASTENERS. USED OPTIONAL INSPECTION METHOD WITH HIGH LEVEL F - [SDR FDEA201203190997](https://openairdocs.org/sdr/FDEA201203190997), Mar 19, 2012: FLOOR SUPPORT. CORRODED. FWD MAIN DECK, COURIER FLOOR AREA, FOUND FLOOR SUPPORT CORRODED LOCATION FROM FR 11 TO 13A AND Y-724. R & R THE FLOOR SUPPORT IAW SRM 51-72-10. REPAIR CLASSIFIE - [SDR FDEA201203160965](https://openairdocs.org/sdr/FDEA201203160965), Mar 16, 2012: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 241NK DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. - [SDR FDEA201203130909](https://openairdocs.org/sdr/FDEA201203130909), Mar 13, 2012: SKIN. DENTED. NOSE SECTION RT LOWER HALF SKIN PLATE EXTERNAL GOT A DENT JUST BELOW COCKPIT FLOOR LEVEL LOCATION BETWEEN FR 2 AND FR 3 POSITION. - [SDR FDEA201109264124](https://openairdocs.org/sdr/FDEA201109264124), Sep 26, 2011: SKIN. SCRATCHED. LEFT WING OTBD FLAP UPPER SURFACE NEAR FLAP TRACK NR 3, FOUND SURFACE WITH 8" SCRATCH MARK UNDER RUBSTRIP. REPLACED THE O/B FLAP PER AMM 27-50-12-04-0 - [SDR FDEA201106122214](https://openairdocs.org/sdr/FDEA201106122214), Jun 12, 2011: THRUST REVERSER. MALFUNCTIONED. AT APPRX 70KTS, NR 2 THRUST REVERSER UNLOCK AMBER LIGHT ON. REJECTED T/O, AFTER STOWING THRUST REVERSER, LIGHT OUT. REVERSER APPEARED TO OPERATE NORMAL. RELEASE - [SDR FDEA201007082423](https://openairdocs.org/sdr/FDEA201007082423), Jul 8, 2010: PRIORITY VALVE. FAILED. ON START OF T/O ROLL, RECEIVED ECAM FOR BLUE RSVR LO LEVEL, BLUE RSVR INDICATES EMPTY. TURNED OFF BLUE HYD ENG PUMP APPROX, 2 MINUTES AFTER ECAM ALERT. T/S AND - [SDR FDEA201001130093](https://openairdocs.org/sdr/FDEA201001130093), Jan 13, 2010: STRINGER. MISREPAIRED. PREVIOUS STR REPAIR LOCATED IN AFT CABIN UNDER FLOOR BEHIND BULK CARGO ON STR 51 LT BETWEEN FRAMES 72 TO 74 HAS 2 EACH REPAIR ANGLES AND 1 EACH STR REPAIR SECTI - [SDR FDEA201001110078](https://openairdocs.org/sdr/FDEA201001110078), Jan 11, 2010: FAIRING. SHEARED. NR 2 PYLON FAIRING 485AL INBD AFT SECTION MOUNTING RIVETS SHEARED NOT GOING THROUGH REINFORCING STRINGER REMOVED REINFORCING ANGLE. REPAIRED SKIN USING SPLICING - [SDR FDEA200912294540](https://openairdocs.org/sdr/FDEA200912294540), Dec 29, 2009: SKIN. DENTED. LT SIDE LWR FUSELAGE SKIN AT FRAME 67 STR 50L DENT MEASURING 12 INCHES X 1 INCH X .188 DEEP. REPAIRED SKIN PN A53974208200 AT FRAME 67 BETWEEN STRINGERS 49L AND - [SDR FDEA200912234512](https://openairdocs.org/sdr/FDEA200912234512), Dec 23, 2009: STRINGER. MISREPAIRED. PREVIOUS STRINGER REPAIR LOCATED IN FWD CARGO ON STRINGER 36 LT BETWEEN FRAMES 20 TO 22 HAS 1 EACH REPAIR SPLICE MEASURING 7.2" LONG AND 1 EACH STRINGER REPAIR - [SDR FDEA200808263598](https://openairdocs.org/sdr/FDEA200808263598), Aug 26, 2008: COMPUTER. FAILED. DURING APPROACH WITH THE LANDING GEAR DOWN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT LIGHTS ON O/H. DISCONTI - [SDR FDEA200808263597](https://openairdocs.org/sdr/FDEA200808263597), Aug 26, 2008: COMPUTER. MALFUNCTIONED. DURING APPROACH WITH THE LDG GEAR DN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT LIGHTS ON O/H. DISCONTINUED A - [SDR FDEA200808263602](https://openairdocs.org/sdr/FDEA200808263602), Aug 26, 2008: LIMITER. FAILED. DURING APPROACH WITH LANDING GEAR DOWN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT O/H. SLATS/FLAPS CYCLED PER - [SDR 08FDEA03602](https://openairdocs.org/sdr/08FDEA03602), Aug 26, 2008: LIMITER. MALFUNCTIONED. DURING APPROACH WITH LANDING GEAR DOWN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT O/H. SLATS/FLAPS CYCLED PER - [SDR 08FDEA03598](https://openairdocs.org/sdr/08FDEA03598), Aug 26, 2008: SLAT SYSTEM. FAILED. DURING APPROACH WITH THE LDG GEAR DN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT LIGHTS ON O/H. DISCONTINUED A - [SDR 08FDEA03597](https://openairdocs.org/sdr/08FDEA03597), Aug 26, 2008: SLAT SYSTEM. MALFUNCTIONED. DURING APPROACH WITH THE LDG GEAR DN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT LIGHTS ON O/H. DISCONTINUED A - [SDR FDEA200807122844](https://openairdocs.org/sdr/FDEA200807122844), Jul 12, 2008: JACKSCREW. LEAKING. SLATS STUCK AT 0 DEG, C/W QRH. EMERGENCY DECLARED, LANDED UNEVENTFULLY AT SYR. REMOVED AND REPLACED RIGHT NR 2 JACKSCREW ASSY PER A310-300MM ATA 27-84-22-4. - [SDR 08FDEA02844](https://openairdocs.org/sdr/08FDEA02844), Jul 12, 2008: JACKSCREW. STUCK. SLATS STUCK AT O DEG, C/W QRH, EMERGENCY DECLARED, LANDED UNEVENTFULLY AT SYR. REMOVED AND REPLACED RIGHT NR 2 JACKSCREW ASSY PER A310-300MM ATA 27-84-22-4. - [SDR 07FDEA05026](https://openairdocs.org/sdr/07FDEA05026), Dec 11, 2007: STRINGER. CORRODED. FWD PIT BETWEEN FR 39 AND FR 38.2 STGR 53 LT HAS CORROSION REMOVED CORROSION FOUND TO BE OUT OF LIMIT IAW SRM 53-10-14. FAB`D STRINGER DOUBLER IN T7/711755. REM - [SDR 07FDEA04854](https://openairdocs.org/sdr/07FDEA04854), Nov 19, 2007: STRINGER. CORRODED. FWD CARGO BETWEEN FR 38.1 AND FR 38.2 STGR 48 RT HAS CORROSION. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-14. CUT OUT DAMAGE AREA STR 48 RT FR 3 - [SDR 07FDEA04488](https://openairdocs.org/sdr/07FDEA04488), Oct 4, 2007: SKIN. CORRODED. FOUND CORROSION AT WEDGE C 70, P56-57 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04485](https://openairdocs.org/sdr/07FDEA04485), Oct 4, 2007: STRINGER. CORRODED. FOUND CORROSION AT STRINGER SEGMENT C 65, P 54 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04483](https://openairdocs.org/sdr/07FDEA04483), Oct 4, 2007: STRINGER. CORRODED. FOUND CORROSION AT STRINGER SEGMENT P48, C 68-69 AND C 70-71. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04451](https://openairdocs.org/sdr/07FDEA04451), Oct 2, 2007: SKIN. DENTED. FOUND DENT AT SLAT NR 2 LT OUT OF LIMIT. NOSE SKIN REPAIR PERFORMED IAW SRM 57-43-11 FIG 202. - [SDR 07FDEA04446](https://openairdocs.org/sdr/07FDEA04446), Oct 2, 2007: LUG. CORRODED. FOUND CORROSION ONE BEARING BORE OF RT WING PYLON OUTBOARD MOUNTING LUG REPAIR PERFORMED BY BLEND OUT CORROSION, NDT FOR DAMAGE FREE IAW EA 6-5720- 81124 AND RA - [SDR 07FDEA04467](https://openairdocs.org/sdr/07FDEA04467), Oct 2, 2007: STRINGER. CORRODED. FOUND CORROSION AT STRINGER SEGMENT P 56, C55/58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04466](https://openairdocs.org/sdr/07FDEA04466), Oct 2, 2007: STRINGER. CORRODED. FOUND CORROSION AT STRINGER P 48 LT, C 69-70 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04465](https://openairdocs.org/sdr/07FDEA04465), Oct 2, 2007: FITTING. CORRODED. FOUND CORROSION AT CORNER FITTING P 44 LT, C64 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04464](https://openairdocs.org/sdr/07FDEA04464), Oct 2, 2007: FRAME. DAMAGED. FOUND ENLARGED HOLES AT C 26/32 BETWEEN P 13-22 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04463](https://openairdocs.org/sdr/07FDEA04463), Oct 2, 2007: FITTING. CORRODED. FOUND CORROSION AT CORNER FITTING C 33 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04462](https://openairdocs.org/sdr/07FDEA04462), Oct 2, 2007: CHANNEL. DENTED. LT AFT CREW DOOR LOWER CHANNEL HAS A NOTCH OUT OF LIMIT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04461](https://openairdocs.org/sdr/07FDEA04461), Oct 2, 2007: STRINGER. CORRODED. FOUND CORROSION AT STRINGER SEGMENT P 56 LT, C 80 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04460](https://openairdocs.org/sdr/07FDEA04460), Oct 2, 2007: SKIN. MISREPAIRED. FOUND OLD POCKET REPAIRS AT RIB 21 INBOARD FLAP LT NOT CONFORM TO SRM. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SB 57-2055. - [SDR 07FDEA04459](https://openairdocs.org/sdr/07FDEA04459), Oct 2, 2007: STRINGER. CORRODED. FOUND CORROSION AT STRINGER SEGMENT C 72, P 48 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04458](https://openairdocs.org/sdr/07FDEA04458), Oct 2, 2007: STRINGER. CORRODED. FOUND CORROSION AT STRINGER SEGMENT C 72, 45 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04457](https://openairdocs.org/sdr/07FDEA04457), Oct 2, 2007: FLANGE. CORRODED. FOUND FLANGE C61-62, AD CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04456](https://openairdocs.org/sdr/07FDEA04456), Oct 2, 2007: FITTING. CORRODED. FOUND CORROSION AT RUN OUT FITTING P44 LT/RT, C17 REPAIR PERFORMED BY REPLACEMENT OF PART IAW DRAWING R536-10440. - [SDR 07FDEA04455](https://openairdocs.org/sdr/07FDEA04455), Oct 2, 2007: FITTING. CORRODED. FOUND FITTING AT C13-13A, P26 LT CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04454](https://openairdocs.org/sdr/07FDEA04454), Oct 2, 2007: SEAT TRACK. CORRODED. FOUND SEAT TRACK C 15A-19, Y-953 CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04453](https://openairdocs.org/sdr/07FDEA04453), Oct 2, 2007: SKIN PANEL. CORRODED. FOUND CORROSION AT CENTER TANK TOP SKIN C 44-48, TRACK 3-5, LT/RT REPAIR PERFORMED BY REMOVAL OF CORROSION AND INSTALLING OF TWO DOUBLERS IAW DRAWING R573-10011 - [SDR 07FDEA04452](https://openairdocs.org/sdr/07FDEA04452), Oct 2, 2007: RIB. DAMAGED. FOUND OLD REPAIRS ON INBOARD FLAP RIB 21 (POCKET REPAIRS) NOT CONFORM TO SRM REPAIR PERFORMED BY REPLACEMENT OF END RIB 21 IAW SRM 57-2055. - [SDR 07FDEA04450](https://openairdocs.org/sdr/07FDEA04450), Oct 2, 2007: SKIN. WORN. FOUND ON RT WING ON PYLON NR 2 ELONGATED HOLE AT WING TO PYLON BOTTOM SKIN ON AREA OF HYDRAULIC LINES. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW - [SDR 07FDEA04449](https://openairdocs.org/sdr/07FDEA04449), Oct 2, 2007: SKIN. WORN. FOUND ON LT WING ON PYLON NR 1 ELONGATED HOLE AT WING TO PYLON BOTTOM SKIN ON AREA OF HYDRAULIC LINES. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW - [SDR 07FDEA04448](https://openairdocs.org/sdr/07FDEA04448), Oct 2, 2007: SKIN. DAMAGED. RT INNER FLAP WITH SEVERAL DAMAGES, LIMITED TO 5 FLIGHTS IAW RAS/DABRE/7002673/2003. REPAIR PERFORMED IN WORKSHOP AND RELEASED IAW FAA FORM 8130-3 NR 05/1145. All 70: https://openairdocs.org/deregistered/N805FD-2024-03-02/reports.md ## Other aircraft with N805FD - [Cancelled 2004-11-19](https://openairdocs.org/deregistered/N805FD-2004-11-19): Airbus A310-324, S/N 456. N-number assigned (import), not yet registered --- 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.