# N801FD: Airbus Industrie A310-324, registration cancelled 2024-02-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 6, 2024
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A310-324](https://openairdocs.org/model/airbus-industrie-a310-324) (registry code 3930318)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (OpenAirDocs)
- Serial number: 539
- Type of aircraft: Fixed wing multi engine
- Certificate issued: March 8, 2001
- Last registry action: September 22, 2023
- Mode S code: AAE615
- 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/N801FD
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=801FD
- Page: https://openairdocs.org/deregistered/N801FD-2024-02-06

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 (66, newest 50)

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

- [SDR FDEA201802220470](https://openairdocs.org/sdr/FDEA201802220470), Feb 22, 2018: SLAT SYSTEM. FAULTED. DURING APPROACH, SLATS SYSTEMS 1 & 2 FAULTED, SLATS STUCK IN THE RETRACTED POSITION, RAN THE QRH, PERFORMED A NO SLAT LANDING. NO TRIPPED INDICATIONS. COMPLIED 
- [SDR FDEA201802140400](https://openairdocs.org/sdr/FDEA201802140400), Feb 14, 2018: BUSHING. WORN. R1 DOOR HARD TO OPEN FROM THE INSIDE AND OUTSIDE. INSPECTED THE R1 DOOR, AND FOUND UPPER AND LOWER HINGE SUPPORT ARM HAT BUSHINGS MIGRATED. NO DAMAGE FOUND ON R
- [SDR FDEA201702080461](https://openairdocs.org/sdr/FDEA201702080461), Feb 8, 2017: GIRT BAR. DETACHED. R1 DOOR WILL NOT ARM. FOUND GIRT BAR DETACHED NOT ALLOWING PROPER OPERATION REINSTALLED GIRT BAR IAW MM 25-61-22-04-01.
- [SDR FDEA201611194116](https://openairdocs.org/sdr/FDEA201611194116), Nov 19, 2016: POWER SUPPLY. MALFUNCTIONED. COULD NOT GET RT SLIDE TO ARM. REMOVED AND REPLACED AUTONOMOUS STANDBY POWER SUPPLY UNIT 70WN AND BOTH BATTERIES ON ASPSU IAW AMM 52-73-18-04, BITE TEST OK. R1 
- [SDR FDEA201611123995](https://openairdocs.org/sdr/FDEA201611123995), Nov 12, 2016: WARNING MESSAGE. INTERMITTENT. BOTH ECAM SLIDE INDICATIONS ARE INTERMITTENT. RESET EMERGENCY SLIDE SYSTEM AND PERFORMED OPS CHECK SEVERAL TIMES IAW AMM 52-73-13-04. OPS CHECKED GOOD.
- [SDR FDEA201609273375](https://openairdocs.org/sdr/FDEA201609273375), Sep 27, 2016: INDICATION SYS. FAULTY. INFORMATION ONLY, REJECTED T/O 9L, PARKING BRAKE SET INDICATION, WE NEVER SET PARKING BRAKE. ONCE WE STARTED TAXI TO RUNWAY, CHECKED HANDLE DOWN POSITION, WE HA
- [SDR FDEA201602030435](https://openairdocs.org/sdr/FDEA201602030435), Feb 3, 2016: SENSOR. FAILED. DUAL SLATS FAULT 1 & 2 ON APPROACH, 3000' MSL 170 KTS, FLAPS STUCK AT 15'. R & R SLAT COMMAND SENSOR UNIT 51CV IAW AMM 27-51-17-04. R & R BOTH SFCC'S IAW AMM 27
- [SDR FDEA201404200759](https://openairdocs.org/sdr/FDEA201404200759), Apr 20, 2014: STRINGER. CORRODED. STRINGER 44L AT FRAMES 41 - 42 IN A/C BAY CORRODED. BLENED IAW SRM 51-74-10, PERFORMED DVI TO VERIFY NO CORROSION FOUND IAW NTM 51-70-00, PERFORMED ROTO TEST TO
- [SDR FDEA201404180749](https://openairdocs.org/sdr/FDEA201404180749), Apr 18, 2014: STRINGER. CORRODED. STRINGER 44L AT FRAMES 41 - 42 CORRODED.
- [SDR FDEA201404180750](https://openairdocs.org/sdr/FDEA201404180750), Apr 18, 2014: STRINGER. CORRODED. STRINGER 45L AT FRAMES 41 - 42 CORRODED. REPAIRED IAW SRM 51-74-10 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201401280212](https://openairdocs.org/sdr/FDEA201401280212), Jan 28, 2014: COMPUTER. FAILED. DURING FLAP EXTENSION, EXPERIENCED FLAP SYS 1 & 2 FAULT ILLUMINATION, FLAPS FAILED TO EXTEND. PERFORMED QRH PROCEDURE. WHEN FLAP HANDLE MOVED TO 40 DEGREES, FLA
- [SDR FDEA201204271661](https://openairdocs.org/sdr/FDEA201204271661), Apr 27, 2012: SLIDE. PARTIAL DEPLOY. INADVERTENT OPENING OF R1 CABIN DOOR STARTED INITIATION OF SLIDE DEPLOYMENT. INSTALLED R1 ESCAPE SLIDE IAW MM 25-61-20-02, AND ADJUSTMENT AND TEST IAW MM 25-61-
- [SDR FDEA201110154517](https://openairdocs.org/sdr/FDEA201110154517), Oct 15, 2011: SKIN. CORRODED. LEFT WING TOP SKIN CORRODED AT REAR SPAR RIB 4. ACCOMPLISHED REPAIR IAW EA 6-5730-149020. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
- [SDR FDEA201110154518](https://openairdocs.org/sdr/FDEA201110154518), Oct 15, 2011: SKIN. CORRODED. FORWARD CARGO COMPARTMENT BILGE AREA OF S45R, SKIN CORRODED BETWEEN FR 38.2 AND FR 39. CUT OUT THE DAMAGED AREA. REPAIRED WITH DOUBLER AND FASTENERS IAW SRM 53-
- [SDR FDEA201110154523](https://openairdocs.org/sdr/FDEA201110154523), Oct 15, 2011: FLOOR PANEL. DENTED. CARGO COMPARTMENT 162HF FLOOR PANEL DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 47 A532799620. R
- [SDR FDEA201110154522](https://openairdocs.org/sdr/FDEA201110154522), Oct 15, 2011: FLOOR PANEL. BROKEN. CARGO COMPARTMENT 161GF FLOOR PANEL BROKEN. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 48 A532799630. R
- [SDR FDEA201110154521](https://openairdocs.org/sdr/FDEA201110154521), Oct 15, 2011: FLOOR PANEL. DENTED. CARGO COMPARTMENT 161BF FLOOR PANEL DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 50 A532799650. R
- [SDR FDEA201110154520](https://openairdocs.org/sdr/FDEA201110154520), Oct 15, 2011: FLOOR PANEL. DAMAGED. BULK CARGO COMPARTMENT 162AF FLOOR PANEL UPPER SKIN DAMAGED. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING
- [SDR FDEA201110154516](https://openairdocs.org/sdr/FDEA201110154516), Oct 15, 2011: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT FLOOR PANEL 242UJ DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 27-R532B12
- [SDR FDEA201110154515](https://openairdocs.org/sdr/FDEA201110154515), Oct 15, 2011: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT FLOOR PANEL 242EK DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 85-R53
- [SDR FDEA201110154514](https://openairdocs.org/sdr/FDEA201110154514), Oct 15, 2011: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT FLOOR PANEL 252GF DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW PANEL IAW SRM 53-10-20, AND DRAWING 09-R532B1175
- [SDR FDEA201110154513](https://openairdocs.org/sdr/FDEA201110154513), Oct 15, 2011: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT FLOOR PANEL 252PH DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 21-B53
- [SDR FDEA201110154512](https://openairdocs.org/sdr/FDEA201110154512), Oct 15, 2011: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT FLOOR PANEL 252UH DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 34-R53
- [SDR FDEA201103222041](https://openairdocs.org/sdr/FDEA201103222041), Mar 22, 2011: POWER SUPPLY. FAILED. DURING PREFLIGHT CHECK, FOUND EMERGENCY LIGHT TEST FAILED. R & R EMERGENCY LIGHTS POWER SUPPLY UNIT 29WL IAW MM 33-51-14-04. ALSO, R & R EMERGENCY LIGHT BATTERY
- [SDR FDEA201011194431](https://openairdocs.org/sdr/FDEA201011194431), Nov 19, 2010: LIMITER. FAILED. SLATS SYS 1 AND SLATS SYS 2 FLAPS, REPEAT ITEM, NO SLATS LANDING. PERFORMED LGAV, T/S SYS IAW FIM 27-80-02, FIG 101, SHEET 1. FOUND TORQUE LIMITER POPED. R AND 
- [SDR FDEA200906292427](https://openairdocs.org/sdr/FDEA200906292427), Jun 29, 2009: FITTING. CORRODED. CORROSION WAS FOUND ON MANHOLE FITTING AT FR 23-24. REPAIR EVALUATED AND FOUND WITH CORROSION AT FWD MANHOLE INTEGRAL FITTING. MANHOLE REPLACEMENT PLUS REPAIR W
- [SDR FDEA200906232556](https://openairdocs.org/sdr/FDEA200906232556), Jun 23, 2009: CARGO TRACK. CRACKED. AFT CARGO COMPT - TRACK ROLLER NR 4 BTW FR55/58 AND 63 CRACKED AND WITH CORROSION AT DRAIN AREA. THE TRACK WAS REPAIRED IAW SRM 53-10-15 FIG 202.
- [SDR FDEA200906232436](https://openairdocs.org/sdr/FDEA200906232436), Jun 23, 2009: SKIN. DENTED. RIGHT WING FLAP OUTBOARD UPPER SKIN SURFACE WITH DEEP DENT AT FRICTION PLATE SEATING AREA BETWEEN RIB 2.5 AND RIB 3. REPAIRED IAW E.A. 6-5710-131025.
- [SDR FDEA200906222519](https://openairdocs.org/sdr/FDEA200906222519), Jun 22, 2009: FLOORBEAM. CORRODED. AFT CARGO COMPT- FR60 CROSSBEAM WITH CORROSION BTW Y1300 AND Y1390. BEAM REPAIRED IAW SRM 53-10-15 FIG 207.
- [SDR FDEA200906192472](https://openairdocs.org/sdr/FDEA200906192472), Jun 19, 2009: ARM. CORRODED. VERTICAL STABILIZER RUDDER HINGE ARM NR 4 FOUND WITH CORROSION AT VERTICAL STABILIZER CONNECTION. RUDDER HINGE ARM REPAIRED AS PER EA 6-5510-131027.
- [SDR FDEA200906192468](https://openairdocs.org/sdr/FDEA200906192468), Jun 19, 2009: SKIN. DAMAGED. RIGHT WING FLAP INBD LOWER SKIN SURFACE WITH DEBONDING AT T/E CARRIAGE NR 2 IT WAS REPAIRED IAW E.A.6-5710-131030
- [SDR FDEA200906162513](https://openairdocs.org/sdr/FDEA200906162513), Jun 16, 2009: TRACK. MISREPAIRED. PREVIOUS REPAIR FOUND LOCATED AT ROLLER TRACK LT, ON FWD CARGO COMPT BTW FR38- 38.1 AT STA Y140. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF
- [SDR FDEA200906162473](https://openairdocs.org/sdr/FDEA200906162473), Jun 16, 2009: SKIN. MISREPAIRED. PREVIOUS REPAIR FOUND LOCATED ON FUSELAGE BTW FR76-77 AT ATGR 23LH-25LH, NEXT TO AFT DOOR LT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF RE
- [SDR FDEA200906162459](https://openairdocs.org/sdr/FDEA200906162459), Jun 16, 2009: SKIN. MISREPAIRED. PREVIOUS REPAIR FOUND LOCATED ON FUSELAGE BTW FR25-26/32 AT STGR 41LH. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED U
- [SDR FDEA200906162439](https://openairdocs.org/sdr/FDEA200906162439), Jun 16, 2009: FLOORBEAM. MISREPAIRED. PREVIOUS REPAIR FOUND LOCATED ON FLOORBEAM RT BTW FR11A-12A AT STA Y-953. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPL
- [SDR FDEA200906092412](https://openairdocs.org/sdr/FDEA200906092412), Jun 9, 2009: FLOOR SUPPORT. CORRODED. CABIN - FLOOR TRACK WITH CORROSION BTW FRAMES 12A AND 13 AT Y730. TRACK WAS REPLACED AS PER SRM 51-72-10.
- [SDR FDEA200906082413](https://openairdocs.org/sdr/FDEA200906082413), Jun 8, 2009: SEAT TRACK. CORRODED. FWD CABIN SEAT TRACK Y-953 CORRODED BTW FRAMES 15B AND 19. THE TRACK WAS REPLACED AS PER SRM 51-72-10.
- [SDR FDEA200906082411](https://openairdocs.org/sdr/FDEA200906082411), Jun 8, 2009: SEAT TRACK. CORRODED. FWD CABIN SEAT TRACK AT Y-450 WITH CORROSION BTW FR14B AND FR19. TRACK WAS REPLACED AS PER SRM 51-72-10.
- [SDR FDEA200809063752](https://openairdocs.org/sdr/FDEA200809063752), Sep 6, 2008: TIRE. FAILED. ON DEPT TLV, ATC ADVISED COMPANY THAT RUBBER WAS FOUND ON RWY AFTER TAKEOFF. FRA CONFIRMED THAT A STARBOARD SIDE WAS DAMAGED. FOUND NR 8 TIRE LOST COMPLETE REIN
- [SDR 08FDEA03752](https://openairdocs.org/sdr/08FDEA03752), Sep 6, 2008: TIRE. FAILED. ON DEPT TLV, ATC ADVISED COMPANY THAT RUBBER WAS FOUND ON RWY AFTER T/O. FRA CONFIRMED THAT A STARBOARD SIDE WAS DAMAGED. FOUND NR 8 TIRE LOST COMPLETE REINFORC
- [SDR 07FDEA02560](https://openairdocs.org/sdr/07FDEA02560), Jul 19, 2007: PROXIMITY SENSOR. FAILED. ON DEPARTURE EDDF RWY 18 LDG GEAR WOULD NOT RETRACT. RETURNED TO LAND 10,000 BELOW MLW. NO FUTHER PROBLEMS. JACK A/C PER MM 07-11-00-0. REMOVED AND REPLACED BOG
- [SDR 07FDEA02559](https://openairdocs.org/sdr/07FDEA02559), Jul 19, 2007: PROXIMITY SENSOR. FAILED. ON DEPARTURE EDDF RWY 18 LDG GEAR WOULD NOT RETRACT. RETURNED TO LAND 10,000 BELOW MLW. NO FURTHER PROBLEMS. JACK A/C PER MM 07-11-00-0. REMOVED AND REPLACED BO
- [SDR 07FDEA01523](https://openairdocs.org/sdr/07FDEA01523), Apr 18, 2007: ATTACH FITTING. CORRODED. RT MLG RIB 5 FWD LUG, CORROSION FOUND IN LUG FACES AND BORE THE MLG RT. REPAIRED AS PER REPAIR INSTRUCTION R57249121. WORK COVERED BY RAS REF: RAS/BAC/1004683/2
- [SDR 07FDEA01522](https://openairdocs.org/sdr/07FDEA01522), Apr 18, 2007: ATTACH FITTING. CORRODED. LT MLG RIB 5 FWD LUG, CORROSION FOUND IN LUG FACES AND BORE THE MLG LT. REPAIRED AS PER REPAIR INSTRUCTION R57249121. WORK COVERED BY RAS/BAC/1004683/2007 ISSUE
- [SDR 07FDEA01507](https://openairdocs.org/sdr/07FDEA01507), Apr 16, 2007: SKIN. DENTED. THS - FRACTION 341BB AT L/E OF RT THS W/UPPER SKIN SURFACE W/DENT REPAIRED PER SRM 55-12-12 FIG 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".
- [SDR 07FDEA01506](https://openairdocs.org/sdr/07FDEA01506), Apr 16, 2007: SKIN. DENTED. THS-FRACTION 341BB AT L/E OF RT THS W/UPPER SKIN SURFACE W/DENT REPAIRED PER SRM 55-12-12 FIG 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".
- [SDR 07FDEA01444](https://openairdocs.org/sdr/07FDEA01444), Apr 11, 2007: STRUT. DAMAGED. RT MLG DOOR STRUT W/SKIN SURFACE DAMAGED REPAIRED PER FEDEX EA NR 6-5280-106709 AND SRM 51-77-12. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.
- [SDR 07FDEA01441](https://openairdocs.org/sdr/07FDEA01441), Apr 11, 2007: SKIN. CORRODED. CORROSION FOUND IN CWB UPPER SURFACE BETWEEN FR46/47 AND FR48 BETWEEN Y1555 AND Y1850. PERFORM NDT INSPECTION NTM 51-10-08, 51-10-01 AND 51-10-04. REPAIRED PER 
- [SDR 07FDEA01440](https://openairdocs.org/sdr/07FDEA01440), Apr 11, 2007: SKIN. CORRODED. LT WING OUTER SKIN SURFACE WITH CORROSION ON T/E AREA 591 RIB 27 REPAIRED PER FEDEX EA 6-5710-106708. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR
- [SDR 07FDEA01439](https://openairdocs.org/sdr/07FDEA01439), Apr 11, 2007: DOOR FRAME. WORN. FWD CARGO COMPARTMENT DOOR AFT FRAME FOUND WORN AT FRAME 25 REPAIRED PER FEDEX EA 6-5330-106703. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR.

All 66: https://openairdocs.org/deregistered/N801FD-2024-02-06/reports.md

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