# N813FD: 1989 Airbus A310-324, registration cancelled 2024-02-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 3, 2024
- Status when cancelled: Valid registration
- Airframe: [Airbus A310-324](https://openairdocs.org/model/airbus-a310-324) (registry code 3940014)
- Engine: [Pratt & Whitney PW4152](https://openairdocs.org/engine/pratt-whitney-pw4152) (registry code 51668)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU), [TCDS E24NE](https://openairdocs.org/tcds/E24NE) (OpenAirDocs)
- Serial number: 500
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 10, 2007
- Certificate issued: July 31, 2006
- Last registry action: April 1, 2023
- Mode S code: AB1502
- 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/N813FD
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=813FD
- Page: https://openairdocs.org/deregistered/N813FD-2024-02-03

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 A310-324: https://openairdocs.org/model/airbus-a310-324.md

## Service difficulty reports (130, newest 50)

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

- [SDR FDEA201310252617](https://openairdocs.org/sdr/FDEA201310252617), Oct 25, 2013: CONTROLLER. MALFUNCTIONED. CABIN NR 2 PRESSURE REGULATOR INITIALLY ROUGH DURING TAKEOFF AND CLIMBOUT, EVENTUALLY SMOOTHED OUT. FAULTED AT FL 310. HAD TO TURN BOTH NR 1 & NR 2 OFF & USE MA
- [SDR FDEA201308131865](https://openairdocs.org/sdr/FDEA201308131865), Aug 13, 2013: WINDSCREEN. CRACKED. DURING CRUISE AT FL340, CAPT'S WINDSCREEN CRACKED. ARCING NOTED TOP RT CORNER AFTER CRACKING. COMPLIED WITH QRH, PROCEED TO DESTINATION IAW GOC GUIDANCE. ENTERE
- [SDR FDEA201308131864](https://openairdocs.org/sdr/FDEA201308131864), Aug 13, 2013: WINDSCREEN. CRACKED. DURING CRUISE AT FL340, CAPTAIN'S WINDSCREEN CRACKED. ARCING NOTED TOP RT CORNER AFTER CRACKING. COMPLIED WITH QRH, PROCEED TO DESTINATION IAW GOC GUIDANCE. TEX
- [SDR FDEA201307041476](https://openairdocs.org/sdr/FDEA201307041476), Jul 4, 2013: DRAIN. OBSTRUCTED. STANDBY AIRSPEED INDICATORS INOPERATIVE. AT 250 KTS ON BOTH PFD'S BOTH STANDBY AIRSPEED INDICATORS SHOWED 180 KTS, THIS WAS AT 10,000 FT, BOTH STANDBY AIRSPEED 
- [SDR FDEA201110094389](https://openairdocs.org/sdr/FDEA201110094389), Oct 9, 2011: SKIN. PUNCTURED. LT WING INBD FLAP LWR SKIN JUST AFT OF THE CARRIAGE FOUND PUNCTURED. CUT OUT THE DAMAGED LOWER SKIN PER SRM 57-52-12/201 FIG205.
- [SDR FDEA201109284176](https://openairdocs.org/sdr/FDEA201109284176), Sep 28, 2011: SKIN. CHAFED. FLUSH DOUBLER REPAIR ON L/E OF D-NOSE SKIN CHAFED AT TRACK NR 1. REPAIRED IAW EA6-5741-103419
- [SDR FDEA201109274146](https://openairdocs.org/sdr/FDEA201109274146), Sep 27, 2011: FITTING. CORRODED. NR 1 ENG PYLON SPIGOT RECEPTACLE UPPER AND LOWER FITTING CORRODED. REMOVED THE SPIGOT FITTINGS PER SRM51-40-21 MACHINE THE MATING SURFACE OF THE NEW SPIGOT LOWE
- [SDR FDEA201109244113](https://openairdocs.org/sdr/FDEA201109244113), Sep 24, 2011: ANGLE. CRACKED. CENTER WING FUEL TANK REAR SPAR INNER ANGLE FOUND CRACKED. REPAIRED IAW SRM 51-40-44, EO 6-5710-7-3322 &SRM 51-40-21. NO CRACK FOUND IAW NTM51-10-18.
- [SDR FDEA201109193958](https://openairdocs.org/sdr/FDEA201109193958), Sep 19, 2011: ANGLE. CRACKED. CENTER WING FUEL TANK REAR SPAR INTERNAL ANGLE FOUND CRACKED. COMPLIED WITH EA 6-5710-153425. REAMED HOLE IAW EA:6-5710-7-3322, B1, PART 1.
- [SDR FDEA201109163902](https://openairdocs.org/sdr/FDEA201109163902), Sep 16, 2011: SLAT TRACK. DAMAGED. LEFT WING SLAT NR 3, NR 9 TRACK BLEND OUT AREA EXCEEDED THE LIMITS (WIDTH=56.21MM). COMPLIED WITH EA 6-5741-103381, PART 3. REPLACED SLAT TRACK IAW AMM27-80-14-
- [SDR FDEA201102010448](https://openairdocs.org/sdr/FDEA201102010448), Feb 1, 2011: FLUID. ODOR. ON TAKEOFF AT 4000FT. ECAM ALERT OF MAIN DECK CARGO SMOKE. FOLLOWED QRH AND RETURNED TO DEPARTURE. WE HAD EXTENSIVE ICE ON ACFT WHICH REQUIRED 1 HR 45 MIN OF DE
- [SDR FDEA201006252142](https://openairdocs.org/sdr/FDEA201006252142), Jun 25, 2010: UPLOCK. FAILED. ON TAKEOFF WITH GEAR HANDLE SELECTED UP- HEARD LOUD NOISE FROM UNDER ACFT AND NOSE GEAR DOOR LIGHT ON BOTH MAIN INDICATOR AND OVERHEAD INDICATOR. DURING AFTER T
- [SDR FDEA200904081217](https://openairdocs.org/sdr/FDEA200904081217), Apr 8, 2009: ANGLE. CRACKED. AFT LOWER CARGO, FRAME 63A, LOWER CLOSE OUT ANGLE IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-72-10.
- [SDR FDEA200904061204](https://openairdocs.org/sdr/FDEA200904061204), Apr 6, 2009: SUPPORT BRACKET. CHAFED. NR 1 ENGINE OUTBD FAN COWL; FORWARD EDGE ALIGNMENT PIN SUPPORT BRACKET IS CHAFED AT THE BOTTOM SURFACE. REMOVED DAMAGE IAW EA 6-7110-127946. FOUND TO BE WITHIN 
- [SDR FDEA200904061200](https://openairdocs.org/sdr/FDEA200904061200), Apr 6, 2009: FLOOR SUPPORT. CORRODED. FUSELAGE INTERNAL STRUCTURE BELOW THE CARGO COMPARTMENT FLOOR HAS CORROSION ON A SUPPORT ANGLE AT FRAME 35 LBL 55. REMOVED CORROSION & FOUND TO OUT OF LIMITS IA
- [SDR FDEA200904061199](https://openairdocs.org/sdr/FDEA200904061199), Apr 6, 2009: FLOOR SUPPORT. CORRODED. FUSELAGE INTERNAL STRUCTURE & CARGO COMPARTMENT FLOOR FLANGE IS CORRODED UNDER & AROUND THE NUTPLATES AND NUTS FROM FRAMES 38-38.1 RBL 55. REMOVED CORROSION & F
- [SDR FDEA200904061205](https://openairdocs.org/sdr/FDEA200904061205), Apr 6, 2009: SKIN. DELAMINATED. NR 1 PYLON PANEL 474 BR INNER SKIN IS DELAMINATED. REPAIRED NR 1 PYLON PANEL 474 BR BY REMOVING DAMAGE; CLEANING; PREPARING AREA AND APPLYING FIBERGLASS WET LAY
- [SDR FDEA200904021159](https://openairdocs.org/sdr/FDEA200904021159), Apr 2, 2009: FLOOR SUPPORT. CORRODED. BULK CARGO COMPARTMENT, FLOOR SUPPORT ANGLE BETWEEN FRAME 69 AND FRAME 70; AT STRINGER 42R THRU STRINGER 44R HAS CORROSION AROUND 2 FASTENER HOLES. ANGLE FOUND 
- [SDR FDEA200904011135](https://openairdocs.org/sdr/FDEA200904011135), Apr 1, 2009: SKIN. DENTED. FUSELAGE SKIN FWD EDGE OF THE CARGO DOOR CUTOUT, 12 INCHES FROM THE LOWER FWD CORNER IS DENTED. REMOVED FASTENERS IAW SRM 51-40-21. REMOVED DAMAGE IAW SRM 53-13
- [SDR FDEA200903311114](https://openairdocs.org/sdr/FDEA200903311114), Mar 31, 2009: BEAM. CORRODED. THE BULK CARGO DOOR LOWER SUPPORT WEB IS CORRODED AROUND THE NUTPLATES AND SKIN BETWEEN FRAMES C-67 AND C-69. REMOVED AND INSTALLED NUTPLATES REF SRM 51-40-21. 
- [SDR FDEA200903311113](https://openairdocs.org/sdr/FDEA200903311113), Mar 31, 2009: PANEL. CRACKED. NR 1 PYLON PANEL 413 BL IS CRACKED IN THE CORNER UNDER THE SEAL. REMOVED SEAL RETAINERS AND SEALS IAW SRM 51-40-21; PG 5. STOP DRILLED CRACKS IAW SRM 54-52-51; 
- [SDR FDEA200903301107](https://openairdocs.org/sdr/FDEA200903301107), Mar 30, 2009: RIB. CRACKED. LEFT HORIZONTAL STABILIZER LEADING EDGE 341 AB CENTER RIB IS CRACKED. REMOVED FASTENERS IAW A310 ARM 51-40-21. STOP DRILED CRACK IAW SRM 55-12-19. FABRICATED RE
- [SDR FDEA200903261051](https://openairdocs.org/sdr/FDEA200903261051), Mar 26, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANEL 131 QF HAS MULTIPLE PUNCTURES ON THE BACK. REPAIRED PANEL 131 QF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A 
- [SDR FDEA200903261075](https://openairdocs.org/sdr/FDEA200903261075), Mar 26, 2009: FLOOR PANEL. DAMAGED. CABIN FLOOR PANEL 241 LK. REPAIRED PNL 241LK WITH FABRICATION OF NEW PANEL. USING OLD PNL AS TEMPLATE IAW SRZ 25-005 REV H.
- [SDR FDEA200903261074](https://openairdocs.org/sdr/FDEA200903261074), Mar 26, 2009: FLOOR PANEL. DAMAGED. CABIN FLOOR PANEL 242 LK IS BROKEN. REPAIRED PANEL 242 LK WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".
- [SDR FDEA200903261073](https://openairdocs.org/sdr/FDEA200903261073), Mar 26, 2009: FLOOR PANEL. CRACKED. CABIN FLOOR BOARD 282 KF IS CRACKED. REPAIRED PANEL 282 KF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H".
- [SDR FDEA200903261058](https://openairdocs.org/sdr/FDEA200903261058), Mar 26, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANEL 132 YF IS CRUSHED ALONG THE EDGE AND HAS A BROKEN INSERT. REPAIRED PANEL 132 YF WITH THE FABRICATION OF A NEW PANEL USING THE 
- [SDR FDEA200903261056](https://openairdocs.org/sdr/FDEA200903261056), Mar 26, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANEL 132 RF IS CRACKED AT THE PDU CUTOUT. REPAIRED PANEL 132 RF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLA
- [SDR FDEA200903261055](https://openairdocs.org/sdr/FDEA200903261055), Mar 26, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANEL 132 ZF HAS MULTIPLE PUNCTURES ON THE BACK AND IS CRACKED AT THE CORNER OF THE PDU CUTOUT. REPAIRED PANEL 132 ZF WITH THE FABRI
- [SDR FDEA200903261054](https://openairdocs.org/sdr/FDEA200903261054), Mar 26, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANEL 131 YF IS BROKEN ALONG THE EDGE OF THE PANEL. REPAIRED PANEL 131 YF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS
- [SDR FDEA200903261053](https://openairdocs.org/sdr/FDEA200903261053), Mar 26, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANEL 131 ZF IS CRUSHED AT THE CORNERS OF THE PDU CUTOUT. REPAIRED PANEL 131 ZF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PA
- [SDR FDEA200903261052](https://openairdocs.org/sdr/FDEA200903261052), Mar 26, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANEL 131 RF IS BROKEN AT THE PDU CUTOUT. REPAIRED PANEL 131 RF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLAT
- [SDR FDEA200903261070](https://openairdocs.org/sdr/FDEA200903261070), Mar 26, 2009: SILL. CORRODED. MAIN DECK, R-2 DOOR SILL AREA HAS A STRINGER ANGLE CORRODED AT FRAME 74, BS 3998 THRU 4005; STRINGER 26R. REMOVED CORROSION IN REF TO SRM 51-74-40. ORIGINAL MAT
- [SDR FDEA200903261069](https://openairdocs.org/sdr/FDEA200903261069), Mar 26, 2009: FLOOR PANEL. PUNCTURED. AFT CARGO COMPARTMENT FLOOR PANEL 152 AF HAS MULTIPLE PUNCTURES ON THE BACK. REPAIRED PANEL 152 AF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A 
- [SDR FDEA200903261068](https://openairdocs.org/sdr/FDEA200903261068), Mar 26, 2009: FLOOR PANEL. DELAMINATED. AFT CARGO COMPARTMENT FLOOR PANEL 152 FF HAS DELAMINATION AND EDGE DAMAGE. REPAIRED PANEL 152 FF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TE
- [SDR FDEA200903261067](https://openairdocs.org/sdr/FDEA200903261067), Mar 26, 2009: FLOOR PANEL. PUNCTURED. AFT CARGO COMPARTMENT FLOOR PANEL 152 BF HAS MULTIPLE PUNCTURES ON THE BACK. REPAIRED PANEL 152 BF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A 
- [SDR FDEA200903261066](https://openairdocs.org/sdr/FDEA200903261066), Mar 26, 2009: FLOOR PANEL. DAMAGED. AFT CARGO COMPARTMENT FLOOR PANEL 152 EF HAS A BROKEN CORNER AND IS MISSING AN INSERT. REPAIRED PANEL 152 EF WITH THE FABRICATION OF A NEW PANEL USING THE OLD P
- [SDR FDEA200903261065](https://openairdocs.org/sdr/FDEA200903261065), Mar 26, 2009: FLOOR PANEL. DAMAGED. BULK CARGO COMPARTMENT FLOOR PANEL 162 HF IS CRACKED AND CORRODED ON THE BACK OF THE PANEL. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & S
- [SDR FDEA200903261064](https://openairdocs.org/sdr/FDEA200903261064), Mar 26, 2009: FLOOR PANEL. PUNCTURED. BULK CARGO COMPARTMENT FLOOR PANEL 162 DF IS PUNCTURED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".
- [SDR FDEA200903261063](https://openairdocs.org/sdr/FDEA200903261063), Mar 26, 2009: FLOOR PANEL. DAMAGED. BULK PIT FLOOR PANEL 161 GF IS PUNCTURED AND DENTED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".
- [SDR FDEA200903261062](https://openairdocs.org/sdr/FDEA200903261062), Mar 26, 2009: FLOOR PANEL. PUNCTURED. BULK PIT FLOOR PANEL 161 HF IS PUNCTURED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".
- [SDR FDEA200903261061](https://openairdocs.org/sdr/FDEA200903261061), Mar 26, 2009: FLOOR PANEL. DAMAGED. BULK PIT FLOOR PANEL 161 GF IS PUNCTURED AND CORRODED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".
- [SDR FDEA200903261060](https://openairdocs.org/sdr/FDEA200903261060), Mar 26, 2009: FLOOR PANEL. DAMAGED. BULK PIT FLOOR PANEL 161 AF IS PUNCTURED AND CORRODED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".
- [SDR FDEA200903261059](https://openairdocs.org/sdr/FDEA200903261059), Mar 26, 2009: FLOOR PANEL. DAMAGED. BULK PIT FLOOR PANEL 161 BF IS PUNCTURED AND DENTED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C".
- [SDR FDEA200903261057](https://openairdocs.org/sdr/FDEA200903261057), Mar 26, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANEL 132 QF IS BROKEN INTO MULTIPLE PIECES. REPAIRED FLOOR PANEL 132 QF WITH FABRICATION OF NEW FLOOR PANEL USING THE OLD PANEL AS 
- [SDR FDEA200903261050](https://openairdocs.org/sdr/FDEA200903261050), Mar 26, 2009: FLOOR PANEL. PUNCTURED. AFT CARGO PIT SLANT PANEL 161 CW HAS SEVERAL PUNCTURES. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW DWG SRZ 25-005, REV "H" & DWG SRZ 25-011, REV "C".
- [SDR FDEA200903251037](https://openairdocs.org/sdr/FDEA200903251037), Mar 25, 2009: FLOORBEAM. CORRODED. THE MAIN DECK FLOORBEAMS ARE CORRODED AT FRAME C-14; RBL 36. REMOVED CORROSION IN REF TO SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-12-15. REMOVED FLOOR
- [SDR FDEA200902260741](https://openairdocs.org/sdr/FDEA200902260741), Feb 26, 2009: CONTROL UNIT. SMOKE. AT FL 330, ATS LEVER DROPPED OFF, NR 1 A/P DROPPED OFF ALONG WITH A PUFF OF SMOKE VISIBLE BE GLARESHIELD FLOOD LIGHTS. ATS RE-ENGAGED AS DID THE NR 1 A/P. NO FU
- [SDR FDEA200811154892](https://openairdocs.org/sdr/FDEA200811154892), Nov 15, 2008: ADC. FAILED. ON TAKEOFF ROLL, F/O HAD NO AIRSPEED INDICATION, PERFORMED REJECT (70KTS). PERFORMED ALL OTHER PARAMETERS THAT COME FROM ADC ARE NORMAL. THE ON ISSUE IS THE SEE
- [SDR 08FDEA04892](https://openairdocs.org/sdr/08FDEA04892), Nov 15, 2008: ADC. FAILED. ON TAKEOFF ROLL, F/O HAD NO AIRSPEED INDICATION, PERFORMED REJECT (70KTS). PERFORMED ALL OTHER PARAMETERS THAT COME FROM ADC ARE NORMAL. THE ON ISSUE IS THE SEE

All 130: https://openairdocs.org/deregistered/N813FD-2024-02-03/reports.md

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