# N806FD: 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: 458 - Year built: 1988 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 18, 2005 - Certificate issued: November 19, 2004 - Last registry action: June 23, 2023 - Mode S code: AAF8A8 - 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/N806FD - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=806FD - Page: https://openairdocs.org/deregistered/N806FD-2024-03-02 From the FAA registry file of November 3, 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 (65, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FDEA201401030016](https://openairdocs.org/sdr/FDEA201401030016), Jan 3, 2014: SEQUENCE VALVE. FAILED. RIGHT MLG WOULD NOT GO DOWN. UTILIZED CRANK HANDLE & RT MLG LOWERED. RT MLG SEQUENCE VLV LOCKED UP & WOULD NOT MOVE. R & R RT MLG SEQUENCE VLV IAW AMM A310-300 - [SDR FDEA201312253039](https://openairdocs.org/sdr/FDEA201312253039), Dec 25, 2013: SEQUENCE VALVE. OUT OF RIG. GEAR LEVER RAISED, RT MAIN GEAR DID NOT RETRACT. GREEN DOWN INDICATION, GEAR DOOR AMBER. PUT GEAR HANDLE BACK DOWN ALL INDICATIONS BACK TO NORMAL FOR DOWN & LOC - [SDR FDEA201206272374](https://openairdocs.org/sdr/FDEA201206272374), Jun 27, 2012: ACTUATOR. FAULTED. PRIOR TO THRUST SET FOR TAKEOFF, RECEIVED NR 1 ENGINE FADEC CHANNEL A FAULT AND FADEC CHANNEL B FAULT. REJECTED TAKEOFF AT 45-50 KNOTS. FOLLOWED QRH PROCEDURES. - [SDR FDEA201205041733](https://openairdocs.org/sdr/FDEA201205041733), May 4, 2012: SKIN. CRACKED. NR 1 ENGINE PYLON LT SIDE LOWER SKIN PANEL CRACKED POSITION NEAR AFT ENGINE MOUNT. REPAIRED IAW SRM 51-40-21 AND SRM 54-56-10 C2. THE REPAIR CLASSIFIED AS MINOR - [SDR FDEA201205041732](https://openairdocs.org/sdr/FDEA201205041732), May 4, 2012: SKIN. CRACKED. NR 1 ENGINE PYLON RT SIDE LOWER SKIN PANEL CRACKED POSITION NEAR AFT ENGINE MOUNT. REPAIRED IAW SRM 51-40-21 AND SRM 54-56-10 C2. THE REPAIR CLASSIFIED AS MINOR - [SDR FDEA201205011687](https://openairdocs.org/sdr/FDEA201205011687), May 1, 2012: SKIN. CRACKED. ONE CRACK FOUND, LENGTH 13MM AT RT WING BOTTOM SKIN LANDING PLATE AREA. REPAIRED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. - [SDR FDEA201204271627](https://openairdocs.org/sdr/FDEA201204271627), Apr 27, 2012: FLOOR SUPPORT. CORRODED. FWD MAIN DECK COURIER FLOOR AREA FOUND FLOOR SUPPORT CORROSION LOCATION FROM FR 11 TO FR 13A AND Y-724. R & R FLOOR SUPPORT WITH NEW IAW SRM 51-72-10. THE REPAI - [SDR FDEA201204181477](https://openairdocs.org/sdr/FDEA201204181477), Apr 18, 2012: FLOOR PANEL. DAMAGED. AVIONICS BAY FLOOR PANEL 122PF HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-27- 04. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 12 A53210216. R - [SDR FDEA201204181476](https://openairdocs.org/sdr/FDEA201204181476), Apr 18, 2012: FLOOR PANEL. DAMAGED. BULK CARGO BAY FLOOR PANEL 162HF HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 17 A53279962. - [SDR FDEA201204181475](https://openairdocs.org/sdr/FDEA201204181475), Apr 18, 2012: FLOOR PANEL. DAMAGED. BULK CARGO BAY FLOOR PANEL 161JF HAS IMPACT DAMAGED. REMOVED FLOOR PANEL IAW AMM 53-10-35- 04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20 AND DWG 17 A5327996 - [SDR FDEA201204181474](https://openairdocs.org/sdr/FDEA201204181474), Apr 18, 2012: FLOOR PANEL. DAMAGED. AFT CARGO COMPARTMENT FOUND FLOOR PANEL 151AF HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-33- 04. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG - [SDR FDEA201204181473](https://openairdocs.org/sdr/FDEA201204181473), Apr 18, 2012: FLOOR PANEL. DAMAGED. FWD CARGO BAY FLOOR PANEL 132RF HAS IMPACT DAMAGED. REMOVED FLOOR PANEL, FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG A53272792. REPAIR EVALUATED PER - [SDR FDEA201105171851](https://openairdocs.org/sdr/FDEA201105171851), May 17, 2011: TRANSMITTER. LEAKING. LOST YELLOW SYS HYD ENROUTE. COMPLIED WITH ECAM & QRH. HYD FLUID LEAKING FROM YELLOW HYD SYS PRESSURE TRANSMITTER 16WV HSG CAP & CGO DOOR HYD SELECTOR VALVE 10M - [SDR FDEA201007062366](https://openairdocs.org/sdr/FDEA201007062366), Jul 6, 2010: SKIN. MISREPAIRED. AN EXISTING FUSELAGE SKIN REPAIR IS AT FR52-53, BELOW STRINGER 18L. THERE ARE 5 ROWS OF 11 RIVETS ATTACHING THE SKIN (A53870003220) TO THE PLATE (A53870004218). - [SDR 08FDEA00830](https://openairdocs.org/sdr/08FDEA00830), Mar 10, 2008: SEAT TRACK. DAMAGED. MAIN DECK CARGO FLOOR SEAT TRACK NR 1 RT SIDE, FR 61 HAS DAMAGE ON LOWER SURFACE, .545 IN ROUND BY .045 IN DEEP. REMOVED DAMAGED SEAT TRACK SECTION FROM FR 60.5 - [SDR 07FDEA04991](https://openairdocs.org/sdr/07FDEA04991), Dec 4, 2007: WINDSHIELD. CRACKED. A/C HAS DIVERTED INTO CUN DUE F/O WINDSHIELD HAS SHATTERED. REMOVED AND REPLACED F/O WINDSHIELD A310-300 M/M 56-11-11-4, OPN CHECK IS GOOD. OK FOR SVC. REPLACED - [SDR 07FDEA04407](https://openairdocs.org/sdr/07FDEA04407), Oct 1, 2007: SKIN PANEL. DAMAGED. FOUND DURING P TO F CONVERSION A CUT (10MM) AT SKIN PANEL C 35, P 35 LT REPAIR PERFORMED BY CUT OUT THE SKIN AND INSTALLING A FLUSH REPAIR WITH NEW STRAP AND CO - [SDR 07FDEA04406](https://openairdocs.org/sdr/07FDEA04406), Oct 1, 2007: FITTING. CHAFED. FOUND CHAFING MARKS AT PYLON TO WING FITTING RIB 18, PYLON NR 2 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04405](https://openairdocs.org/sdr/07FDEA04405), Oct 1, 2007: SKIN PANEL. DENTED. FOUND NICK ON SKIN PANEL NR 3 C 18-19, P 33 RT REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5313-82859 AND RAS/DABRE/7005143/2005 ISS A. - [SDR 07FDEA04404](https://openairdocs.org/sdr/07FDEA04404), Oct 1, 2007: SKIN. DELAMINATED. FOUND AT RUDDER TRAILING EDGE LOWER CORNER DELAMINTION NEAR RIB 0 REPAIR PERFORMED IAW SRM 55-41-12 FIG 208A. - [SDR 07FDEA04403](https://openairdocs.org/sdr/07FDEA04403), Oct 1, 2007: FITTING. DAMAGED. FOUND MISDRILLED HOLES IN CORNER FITTING C59, P 44 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04402](https://openairdocs.org/sdr/07FDEA04402), Oct 1, 2007: DOUBLER. CORRODED. FOUND CORROSION AT DOUBLER C71-72, P 47-48 LT REPAIR PERFORMED BYREWORK OF CORROSION, NDT FOR CRACK FREE AND FLAP PEENING IAW EA 6-5317-82856 AND RAS/DATLS/0002 - [SDR 07FDEA04401](https://openairdocs.org/sdr/07FDEA04401), Oct 1, 2007: STRINGER. CORRODED. FOUND CORROSION AT STRINGER P52 LT, C70-71. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. - [SDR 07FDEA04400](https://openairdocs.org/sdr/07FDEA04400), Oct 1, 2007: FITTING. CRACKED. FITTING AT P 48, C78 LT CRACKED (ABOUT 8MM). REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04399](https://openairdocs.org/sdr/07FDEA04399), Oct 1, 2007: FITTING. CORRODED. FOUND CORROSION AT FITTING C 63, P44-46 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04398](https://openairdocs.org/sdr/07FDEA04398), Oct 1, 2007: SPAR. DAMAGED. SHOULDERED BOLTS FOUND DURING EMBODIMENT OF SB A310-57-2079 AT HOLE NR 21 AND NR 14 RT REAR SPAR AREA OF SPOILER NR 3 RT REPAIR PERFORMED BY REPLACEMENT OF BUSH - [SDR 07FDEA04397](https://openairdocs.org/sdr/07FDEA04397), Oct 1, 2007: FLOORBEAM. DAMAGED. FOUND OLD MISDRILLED HOLE AT CROSSBEAM C 64 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04396](https://openairdocs.org/sdr/07FDEA04396), Oct 1, 2007: STRINGER. DAMAGED. FOUND MISDRILLED HOLES AT STRINGER 41 LT, C33-34 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. - [SDR 07FDEA04395](https://openairdocs.org/sdr/07FDEA04395), Oct 1, 2007: STRINGER. CORRODED. FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 - [SDR 07FDEA04394](https://openairdocs.org/sdr/07FDEA04394), Oct 1, 2007: STRINGER. CORRODED. FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 - [SDR 07FDEA04393](https://openairdocs.org/sdr/07FDEA04393), Oct 1, 2007: STRINGER. CORRODED. FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 - [SDR 07FDEA04392](https://openairdocs.org/sdr/07FDEA04392), Oct 1, 2007: STRINGER. CORRODED. FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 - [SDR 07FDEA04391](https://openairdocs.org/sdr/07FDEA04391), Oct 1, 2007: STRINGER. CORRODED. FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 - [SDR 07FDEA04390](https://openairdocs.org/sdr/07FDEA04390), Oct 1, 2007: STRINGER. CORRODED. FOUND CORRODED STRINGER SEGMENT P 57 AT C 72 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04389](https://openairdocs.org/sdr/07FDEA04389), Oct 1, 2007: FLOORBEAM. CORRODED. FOUND CROSSBEAM C 63 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04388](https://openairdocs.org/sdr/07FDEA04388), Oct 1, 2007: FLANGE. CORRODED. FOUND CORRODED FLANGE AT C61-62, P 56 RT-56 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04387](https://openairdocs.org/sdr/07FDEA04387), Oct 1, 2007: STRINGER. CORRODED. FOUND CORRODED STRINGER P 21 LT, BETWEEN 55/58-60 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. - [SDR 07FDEA04386](https://openairdocs.org/sdr/07FDEA04386), Oct 1, 2007: PANEL. CRACKED. FOUND CRACK (ABOUT 6MM) AT PYLON NR 2 RIB 8 OUTBOARD SIDE WALL DOUBLER REPAIR PERFORMED IAW SRM 54-51-31 FIG 201. - [SDR 07FDEA04370](https://openairdocs.org/sdr/07FDEA04370), Sep 28, 2007: PLATE. DAMAGED. DAMAGED WEB PLATES BETWEEN FRAME 86-87, STGR. 33 LT REPLACEMENT OF WEB PLATE IAW SRM 51-72-10. - [SDR 07FDEA04369](https://openairdocs.org/sdr/07FDEA04369), Sep 28, 2007: PLATE. DAMAGED. DAMAGED WEB PLATES BETWEEN FRAME 86-87, STGR 39 LT AND RT. REPLACEMENT OF WEB PLATES LT AND RT IAW SRM 51-72-10 - [SDR 07FDEA04368](https://openairdocs.org/sdr/07FDEA04368), Sep 28, 2007: FITTING. CORRODED. CORROSION ON UPPER RUN OUT FITTING BETWEEN FRAME 16A-17, STRG 44 RT, AFTER REWORK NO REMAINING THICKNESS WAS EXISTED. REPLACEMENT OF UPPER RUN OUT FITTING IAW. - [SDR 07FDEA04367](https://openairdocs.org/sdr/07FDEA04367), Sep 28, 2007: SKIN. CHAFED. FOUND SCRATCHES ON NOSE SKIN OF SLAT NR 2 RT WING, RIB 24-27. NOSE SKIN REPAIR PERFORMED IAW SRM 57-43-11/FIG 202/SHEET 11. REFER TO NON ROUTINE DR0399, AT RIB - [SDR 07FDEA04365](https://openairdocs.org/sdr/07FDEA04365), Sep 28, 2007: SKIN. CHAFED. FOUND CHAFING MARKS BETWEEN SLAT TRACK 6 AND JACK 4, LEADING EDGE SKIN, RT WING. REPAIR PERFORMED BY INSTALLATION OF NEW SKIN INSERT IAW SRM 57-41-12/FIG 203, 2 - [SDR 07FDEA04364](https://openairdocs.org/sdr/07FDEA04364), Sep 28, 2007: SKIN. CHAFED. FOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 203, 204, CHAFING MARKS BETWEEN SLAT TRACK 5 AND SLAT TRACK 6, LEADING EDGE SKIN, RT WING. NEW REPAIR SKIN IN - [SDR 07FDEA04363](https://openairdocs.org/sdr/07FDEA04363), Sep 28, 2007: SKIN. CHAFED. FOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 204, CHAFING MARKS BETWEEN JACK 3 AND SLAT TRACK 5, LEADING EDGE SKIN, RT WING. NEW REPAIR SKIN INSERT INSTAL - [SDR 07FDEA04362](https://openairdocs.org/sdr/07FDEA04362), Sep 28, 2007: SKIN. CHAFED. FOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 203, 204, CHAFING MARKS BETWEEN SLAT TRACK 1 AND SLAT TRACK 2, LEADING EDGE SKIN, RT WING. NOSE SKIN REPAIR R - [SDR 07FDEA04360](https://openairdocs.org/sdr/07FDEA04360), Sep 28, 2007: SKIN. CHAFED. FOUND CHAFING MARKS BETWEEN JACK 3 AND SLAT TRACK 5, LEADING EDGE SKIN, LT WING. NOSE SKIN REPAIR PERFORMED SRM 57-41-12/FIG 203, 204. - [SDR 07FDEA04359](https://openairdocs.org/sdr/07FDEA04359), Sep 28, 2007: SKIN. CHAFED. FOUND CHAFING MARKS BETWEEN SLAT TRACK 5 AND SLAT TRACK 6, LEADING EDGE SKIN, LT WING. REPLACEMENT OF CHAFED NOSE SKIN IAW SRM 51-72-10. - [SDR 07FDEA04358](https://openairdocs.org/sdr/07FDEA04358), Sep 28, 2007: PLATE. CRACKED. FOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 7, FWD OF FRONT SPAR, UPPER SKIN, RT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 7 RT IAW SRM 51-72-10. - [SDR 07FDEA04357](https://openairdocs.org/sdr/07FDEA04357), Sep 28, 2007: PLATE. CRACKED. FOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 7, FWD OF FRONT SPAR, UPPER SKIN, LT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 7 LT IAW SRM 51-72-10. All 65: https://openairdocs.org/deregistered/N806FD-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.