# N807FD: 1989 Airbus 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 A310-324](https://openairdocs.org/model/airbus-a310-324) (registry code 3940014) - 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: 492 - Year built: 1989 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 1, 2005 - Certificate issued: August 26, 2004 - Last registry action: January 8, 2024 - Mode S code: AAFC5F - 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/N807FD - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=807FD - Page: https://openairdocs.org/deregistered/N807FD-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 A310-324: https://openairdocs.org/model/airbus-a310-324.md ## Service difficulty reports (79, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FDEA2019060311203](https://openairdocs.org/sdr/FDEA2019060311203), May 31, 2019: SEQUENCE VALVE. MISALIGNED. 6685 ON GEAR EXTENSION RECEIVED UNSAFE INDICATION FOR RT MLG ON SYS 1 SYS 2. COMPLIED WITH QRH PROCEDURES AND LG GRAVITY EXTENSION CHECKLIST. GEAR DOORS REMAINE - [SDR FDEA2018042601120](https://openairdocs.org/sdr/FDEA2018042601120), Apr 25, 2018: POWER SUPPLY. FAILED. EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY 29WLI IAW AMM 33-51-14-04-09. OPS CHECKED GOOD. - [SDR FDEA201705031343](https://openairdocs.org/sdr/FDEA201705031343), May 3, 2017: JACKSCREW. LACK OF LUBE. WHEN SELECTING FLAPS TO 15, NOTICE BINDING LEAVING THE SLATS/FLAPS 15/0 GATE AT FLAPS 15 RECEIVED FLAP FAULT SYS 1 AND 2. CYCLED THE FLAP HANDLE, NO CHANGE. QRH - [SDR FDEA201612134398](https://openairdocs.org/sdr/FDEA201612134398), Dec 13, 2016: FLOOR SUPPORT. CORRODED. MAIN DECK FRAMES 12A - 14, Y953 FLOOR SUPPORT FOUND CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201612134397](https://openairdocs.org/sdr/FDEA201612134397), Dec 13, 2016: SKIN. DENTED. FUSELAGE SKIN FOUND A DENTED BETWEEN FRAMES 65 - 66, STRINGER 36 - 37R. REPAIRED IAW SRM 53-10-12- 201 PARA 6 FIG225 SHEET 2 . MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201612094367](https://openairdocs.org/sdr/FDEA201612094367), Dec 9, 2016: ANGLE. CRACKED. FRAME 47 RT INTERNAL ANGLE\ FOUND CRACKED. REPAIRED THE ANGLE IAW EA 6-5710-T0312253 C P3. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201612094366](https://openairdocs.org/sdr/FDEA201612094366), Dec 9, 2016: ANGLE. CRACKED. ANGLE AT FRAME 47 LT SIDE FOUND CRACKED. REPAIRED IAW EA 6-5710-T0312253 C P3. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201612094369](https://openairdocs.org/sdr/FDEA201612094369), Dec 9, 2016: ANGLE. CRACKED. TEE ANGLE AT STIFFENER 8 RT FOUND CRACKED. REPAIRED IAW EA 6-5710-T0330412 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201612094368](https://openairdocs.org/sdr/FDEA201612094368), Dec 9, 2016: ANGLE. CRACKED. TEE ANGLE AT STIFFENER 8 LT FOUND CRACK. REPAIRED THE TEE ANGLE IAW EA 6-5710-T0330412 P1. MAJOR REPAIR IAW GMM 6-2-100 - [SDR FDEA201612074345](https://openairdocs.org/sdr/FDEA201612074345), Dec 7, 2016: ATTACH FITTING. CRACKED. AFT CARGO DOOR ACTUATOR ATTACH FITTING FOUND CRACK BY HFEC INSPECTION. REPLACED THE ATTACH FITTING IAW SRM 51-40-21. - [SDR FDEA201612074344](https://openairdocs.org/sdr/FDEA201612074344), Dec 7, 2016: FLOOR SUPPORT. CORRODED. MAIN DECK FR11-FR14 Y770 FLOOR SUPPORT CORRODED. - [SDR FDEA201612074343](https://openairdocs.org/sdr/FDEA201612074343), Dec 7, 2016: ATTACH FITTING. CRACKED. FWD CARGO DOOR ACTUATOR ATTACH FITTING WITH CRACK SIGNAL. REPLACED THE ATTACH FITTING IAW SRM 51-40-21. - [SDR FDEA201612074342](https://openairdocs.org/sdr/FDEA201612074342), Dec 7, 2016: SKIN. CRACKED. LEFT WING BOTTOM SKIN FOUND CRACKED AT 581AB CUTOUT. REPAIRED IAW EA 6-5730-T0330205 P1 AND DWG R57249152. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201605021440](https://openairdocs.org/sdr/FDEA201605021440), May 2, 2016: WINDSHIELD. CRACKED. DURING CRUISE FLIGHT AT FL 360, BEGAN TO SEE AN ORANGE GLOW IN LOWER LT CORNER OF CAPTAINS FWD WIND SCREEN. TURNED OUT TO BE WINDSHIELD HEAT ARCING, SO TURNED O - [SDR FDEA201601240289](https://openairdocs.org/sdr/FDEA201601240289), Jan 24, 2016: WINDSHIELD. CRACKED. CRACK ON CAPTAINS' OUTER FRONT WINDSHIELD. WINDOW HEAT WAS ON, BUT TURNED OFF ONCE CRACK DEVELOPED. R & R CAPTAINS WINDSHIELD. R & R LT WINDOW TEMP CONTROLLER - - [SDR FDEA201410123118](https://openairdocs.org/sdr/FDEA201410123118), Oct 12, 2014: SKIN. CORRODED. LEFT WING UPPER SURFACE SKIN FOUND CORROSION AT THE FRONT OF NR 2 SPOILER. REPAIRED LT WING UPPER SURFACE SKIN IAW EA 6-5730-T0311884 P1. TITLE WING PLATES & SK - [SDR FDEA201410113111](https://openairdocs.org/sdr/FDEA201410113111), Oct 11, 2014: TEE FITTING. CRACKED. CENTER WING INSP REAR SPAR INTERNAL ANGLE & TEE FITTING RT NR 10 FASTENER HOLE WITH CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0312253 TITLE WINGS BASIC WING STRUCTU - [SDR FDEA201410062974](https://openairdocs.org/sdr/FDEA201410062974), Oct 6, 2014: BRACKET. CRACKED. LEFT AILERON OTBD HINGE PANEL BRACKET CRACKED REPAIRED LT AILERON OTBD HINGE PANEL BRACKET IAW EA 6-5750-T0312135. WINGS FLIGHT SURFACES FRONT SPAR LOWER DOUBLE - [SDR FDEA201410032930](https://openairdocs.org/sdr/FDEA201410032930), Oct 3, 2014: FITTING. CRACKED. ANGLE & TEE FITTING CRACKED FRAME 47. REPAIRED IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201410032929](https://openairdocs.org/sdr/FDEA201410032929), Oct 3, 2014: ANGLE. CRACKED. ANGLE & TEE FITTING CRACKED FRAME 47. REPAIRED IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201410032928](https://openairdocs.org/sdr/FDEA201410032928), Oct 3, 2014: ANGLE. CRACKED. ANGLE & TEE FITTING CRACKED FRAME 47. REPAIRED IAW IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201410032927](https://openairdocs.org/sdr/FDEA201410032927), Oct 3, 2014: ANGLE. CRACKED. REAR SPAR INTERNAL ANGLE & TEE FITTING RT NR 1 FASTENER HOLE WITH A CRACK SIGNAL. REPAIREDSPAR ANGLE & TEE FITTING IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM - [SDR FDEA201409302860](https://openairdocs.org/sdr/FDEA201409302860), Sep 30, 2014: FLOORBEAM. CORRODED. FORWARD CARGO COMPARTMENT FLOORBEAM TEE CORRODED AT FRAME 37, Y140 - Y805. REPAIRED THE FLOORBEAM IAW EA 6-5310-T0311889. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201409272822](https://openairdocs.org/sdr/FDEA201409272822), Sep 27, 2014: FLOORBEAM. DELAMINATED. AFT CARGO BAY FLOORBEAM TEE FOUND DELAMINATION AT FRAME 60 Y-805 - Y-1470. CUT THE DELAMINATED BEAM IAW SRM 53-10-15 FIG 207 CHECKED THE CRACKS TO CUTOUT PER NT - [SDR FDEA201409242751](https://openairdocs.org/sdr/FDEA201409242751), Sep 24, 2014: FITTING. CRACKED. CENTER WING INSP REAR SPAR INTERNAL ANGLE & TEE FITTING LT NR 10 FASTENER HOLE WITH CRACK SIGNAL. REPAIRED CENTER WING INSP REAR SPAR INTERNAL ANGLE & TEE FITTI - [SDR FDEA201404010608](https://openairdocs.org/sdr/FDEA201404010608), Apr 1, 2014: RIB. CORRODED. RT RIB 5 BORE & AFT FACE HAVE CORROSION. COMPLIED WITH EA 6-5710-T0307063 P 1 WINGS & BASIC WING STRUCTURE, RT RIB 5 LUG CORROSION. - [SDR FDEA201404010606](https://openairdocs.org/sdr/FDEA201404010606), Apr 1, 2014: RIB. CORRODED. LT RIB 5 HAS CORROSION IN BORE & FACE. COMPLIED WITH EA 6-5710-T0307003 WINGS & BASIC STRUCTURE, LT RIB 5 LUG CORROSION. - [SDR FDEA201402070285](https://openairdocs.org/sdr/FDEA201402070285), Feb 7, 2014: FUEL. CONTAMINATED. EN ROUTE LT OUTER PUMP 1 & PUMP 2 FAILED IN FLIGHT. BOTH PUMPS SHOWED LOW PRESS. FOLLOWED ECAM TO TURNOFF. THAWED LO FUEL PUMPS & TANK WITH 3 COLD BUSTERS FOR 5 - [SDR FDEA201311302913](https://openairdocs.org/sdr/FDEA201311302913), Nov 30, 2013: FLOOR SUPPORT. CRACKED. MDIS 807 53-00 0008007 30NOV13 BQN CLOSE R FOUND FWD FUSELAGE FLOOR SUPPORT MEMBER BETWEEN C9 & C10, ONE FRAME LT 09 88 WITH SEVERAL CRACKS. A536 11977200 ID WE - [SDR FDEA201204241547](https://openairdocs.org/sdr/FDEA201204241547), Apr 24, 2012: FITTING. CRACKED. PERFORMED NDT IAW E6-5710-7-3324 A PT2 , CRACKS WERE FOUND AT HOLE NR 1 AND HOLE NR 2 OF FRAME 40 RT UPPER CORNER FITTING. - [SDR FDEA201204241546](https://openairdocs.org/sdr/FDEA201204241546), Apr 24, 2012: FITTING. CRACKED. PERFORMED NDT IAW E6-5710-7-3324 A PT1, CRACKS WERE FOUND AT HOLE NR 1 AND HOLE NR 2 OF FRAME 40 LT UPPER CORNER FITTING. - [SDR FDEA201108273530](https://openairdocs.org/sdr/FDEA201108273530), Aug 27, 2011: POWER SUPPLY. FAILED. L1 & R1 DOORS ESCAPE SLIDE RELEASE WARNING LIGHTS SYSTEM INOPERATIVE. R & R AUTONOMOUS STANDBY POWER SUPPLY UNIT (70WN). OPS CHECKED GOOD REF MM 52-73-18-04. OK - [SDR FDEA201104182042](https://openairdocs.org/sdr/FDEA201104182042), Apr 18, 2011: BATTERY. FAILED. ON PREDISPATCH CK, FOUND ON COURIER COMPARTMENT EMERGENCY LT TEST INOP. REMOVED AND REPLACED EMG POWER SUPPLY UNIT AND EMERGENCY SUPPLY BATTERY, REF MM 33-51-14 - [SDR 2011FA0000222](https://openairdocs.org/sdr/2011FA0000222), Feb 18, 2011: JACKSCREW. OUT OF POSITION. DURING O/H, MX PERFORMED ON THE SCREW JACK ASSY, FE140 SN 125, IDENTIFICATION OF THE WRONG POSITIONING OF THE RATCHET WHEEL (ITEM 3-620 OF CMM 27-44-13), ASSEMB - [SDR FDEA200910213626](https://openairdocs.org/sdr/FDEA200910213626), Oct 21, 2009: SKIN. DAMAGED. ACCOMPLISH TERMINATING ACTION REPAIR OF RUDDER. NEW REVISION "C" PART 2 OF EA 6-5540-118407 ACCOMPLISHED TERMINATING ACTION REPAIR OF RUDDER IAW EA NR 6-5540-11 - [SDR 07FDEA04039](https://openairdocs.org/sdr/07FDEA04039), Sep 19, 2007: SKIN. MISREPAIRED. OLD EXTERNAL DOUBLER REPAIR ON INBOARD FLAP RT ON LOWER SIDE BETWEEN RIB 10-11, NOT CONFORM TO OLD RECORDS AS PER SRM 57-52-12/FIG 204: EXTERNAL DOUBLER IS ON L - [SDR 07FDEA04037](https://openairdocs.org/sdr/07FDEA04037), Sep 19, 2007: DOOR FRAME. DAMAGED. DURING LT FWD PAX DOOR FRAMING AFT PANEL REPLACEMENT, A DOUBLE HOLE WAS PERFORMED AT FRAME 18, STRG 26 IN LOWER BEAM WEB AT ITS REAR END AND IN STRG 26 COUPLING - [SDR 07FDEA04036](https://openairdocs.org/sdr/07FDEA04036), Sep 19, 2007: DOOR FRAME. DAMAGED. DURING LT FWD PAX DOOR FRAMING AFT PANEL REPLACEMENT, A DOUBLE HOLE WAS PERFORMED AT FRAME 18, STRG 26 IN LOWER BEAM WEB AT ITS REAR END AND IN STRG 26 COUPLING - [SDR 07FDEA04034](https://openairdocs.org/sdr/07FDEA04034), Sep 19, 2007: SKIN PANEL. MISREPAIRED. FOUND OLD DOUBLER REPAIR BETWEEN FRAME 11-11A, STRG 27-28 LT, NOT CONFORM TO REPAIR REFERENCE AS PER SRM 53-12-12/FIG 201. DOUBLER REPAIR RENEWED IAW SRM 53-12- - [SDR 07FDEA04033](https://openairdocs.org/sdr/07FDEA04033), Sep 19, 2007: RIB. NONE. OLD REPAIR ON RT INBOARD FLAP AT END RIB 21. CUSTOMER DECISION TO FINAL REPAIR PER SB A310-57-2055, REPLACEMENT OF END RIB 21. - [SDR 07FDEA04032](https://openairdocs.org/sdr/07FDEA04032), Sep 19, 2007: RIB. NONE. OLD REPAIR ON LT INBOARD FLAP AT END RIB 21. CUSTOMER DECISION TO FINAL REPAIR PER SB A310-57-2055, REPLACEMENT OF END RIB 21. - [SDR 07FDEA04029](https://openairdocs.org/sdr/07FDEA04029), Sep 19, 2007: STRINGER. CORRODED. DURING NON ROUTINE DR0115, FOUND CORROSION ON STRINGER 51 LT, BETWEEN FRAME 54.1-54.2. PARTIAL STRINGER REPLACEMENT WITH SPLICE REPAIR PERFORMED, BETWEEN FRAME - [SDR 07FDEA04026](https://openairdocs.org/sdr/07FDEA04026), Sep 19, 2007: STRINGER SPLICE. CORRODED. CORROSION ON CONNECTING SEGMENT STRG 51 LT, BETWEEN FRAME 54.2-54.3. REPLACEMENT OF CONNECTING SEGMENT IAW SRM 51-72-10. - [SDR 07FDEA04024](https://openairdocs.org/sdr/07FDEA04024), Sep 19, 2007: FLOORBEAM. CORRODED. HEAVY CORROSION ON CROSSBEAM AT FRAME 63 RT, CARGO COMP FLOOR STRUCTURE. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15. - [SDR 07FDEA04022](https://openairdocs.org/sdr/07FDEA04022), Sep 19, 2007: FLOOR SUPPORT. CORRODED. HEAVY CORROSION ON LONGITUDINAL PROFILE (LONGERON) BETWEEN FRAME 66-69 AD, BULK CARGO COMP FLOOR STRUCTURE. REPLACEMENT OF LONGERON IAW SRM 51-72-10. - [SDR 07FDEA04021](https://openairdocs.org/sdr/07FDEA04021), Sep 19, 2007: FLOORBEAM. CORRODED. HEAVY CORROSION ON CROSSBEAM AT FRAME 69 LT, BULK CARGO COMP FLOOR STRUCTURE. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15. - [SDR 07FDEA04019](https://openairdocs.org/sdr/07FDEA04019), Sep 19, 2007: FRAME. DAMAGED. OLD REPAIR ON FRAME 13, STRG 14 LT, FUSELAGE NOSE SECTION. THE REINFORCEMENT REPAIR ANGLE AT FRAME SEGMENT WAS CHAFED AND AFTER REWORK OUT OF LIMIT. REPAIR PERF - [SDR 07FDEA04015](https://openairdocs.org/sdr/07FDEA04015), Sep 19, 2007: SHEAR PLATE. CRACKED. CRACKED SHEAR PLATE AT STR 26 LT, BETWEEN FRAME 79-80. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10. - [SDR 07FDEA04014](https://openairdocs.org/sdr/07FDEA04014), Sep 19, 2007: STRINGER. CORRODED. CORROSION ON STRINGER 42 RT, BETWEEN FRAME 72-73. STRINGER SPLICE REPAIR IAW SRM 53-10-14/FIG 201. - [SDR 07FDEA04013](https://openairdocs.org/sdr/07FDEA04013), Sep 19, 2007: STRINGER. DAMAGED. OLD DAMAGE ON STRINGER 30 RT, BETWEEN FRAME 54.2-54.3. STRINGER SPLICE REPAIR IAW SRM 53-10-14/FIG 201. All 79: https://openairdocs.org/deregistered/N807FD-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.