# N817FD: Airbus Industrie A310-304, registration cancelled 2024-03-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 2, 2024
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A310-304](https://openairdocs.org/model/airbus-industrie-a310-304) (registry code 3930339)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (OpenAirDocs)
- Serial number: 552
- Type of aircraft: Fixed wing multi engine
- Certificate issued: May 31, 2006
- Last registry action: January 22, 2023
- Mode S code: AB23DE
- 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/N817FD
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=817FD
- Page: https://openairdocs.org/deregistered/N817FD-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 A310-304: https://openairdocs.org/model/airbus-industrie-a310-304.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 FDEA201405211117](https://openairdocs.org/sdr/FDEA201405211117), May 21, 2014: FITTING. DAMAGED. LEFT RIB 5 FWD LUG BORE OUT OF ROUND REPAIRED LT RIB 5 FWD LUG BORE OUT OF ROUND IAW DWG R57249389 & COMPLIED WITH EA 6-5710-T0308275.
- [SDR FDEA201401030015](https://openairdocs.org/sdr/FDEA201401030015), Jan 3, 2014: SWITCH. MALFUNCTIONED. LEFT CABIN DOOR SHOWED UNLOCKED AT FL 240. LEVELED OFF, PERFORMED QRH & PUSHED ON THE HANDLE. DOOR SHOWED LOCKED. CONTINUED TO CLIMB & DOOR SHOWED UNLOCKED AT F
- [SDR FDEA201312122966](https://openairdocs.org/sdr/FDEA201312122966), Dec 12, 2013: HINGE FITTING. NICKED. NOSE LANDING GEAR, RT AFT DOOR HINGE FITTING, BEARING HOLE FOUND TWO NICKS. REPAIRED IAW EA 6-5310-99725B PART 2.
- [SDR FDEA201304240855](https://openairdocs.org/sdr/FDEA201304240855), Apr 24, 2013: WIRE HARNESS. FAILED. AFTER TOUCHDOWN, DURING ROLLOUT NR 5 AND NR 6 TIRES BLEW. ACFT REMAINED ON CENTERLINE. REMOVED AND INSTALLED AND ROUTED LT MLG HARNESS LOOM THRU NR 5 AND NR 6 B
- [SDR FDEA201203160978](https://openairdocs.org/sdr/FDEA201203160978), Mar 16, 2012: SHEAR PLATE. CORRODED. FWD END SHEAR PLATE FOUND CORRODED AT SEVERAL LOCATIONS FROM BS 410 TO 440, BL 0 TO LBL 24.75 FWD END SHEAR PLATE REPAIRED IAW EA F-5310-157901.
- [SDR FDEA201202160591](https://openairdocs.org/sdr/FDEA201202160591), Feb 16, 2012: COMPUTER. MALFUNCTIONED. APPROX 1.5 HRS INTO FLIGHT, RT OTBD FUEL TANK QTY BEGAN TO DECREASE RAPIDLY. TANK WENT TO EMPTY, XX, AND REMAINED UNTIL IN DESCENT AT 16,000 FT, THEN QTY RETURN
- [SDR FDEA201107032558](https://openairdocs.org/sdr/FDEA201107032558), Jul 3, 2011: FLOORBEAM. DAMAGED. BULK CARGO COMPARTMENT, FR 63 FLOORBEAM BOTTOM CEILING PANEL ATTACHMENT BETWEEN SEAT TRACK 1 AND 2L HAS A DRILL START. COMPLIED WITH EA 6-5310-145342 PT1.
- [SDR FDEA201107012531](https://openairdocs.org/sdr/FDEA201107012531), Jul 1, 2011: STRINGER. GOUGED. AFT CARGO COMPARTMENT LT SIDE FWD OF FR 54.1, STR 37 HAS GOUGE. REMOVED, REPAIRED AND RE-INSTALLED STRINGER SECTION IAW SRM 53-10-14, PGS 201 THROUGH 231 SRM 51
- [SDR FDEA201107012532](https://openairdocs.org/sdr/FDEA201107012532), Jul 1, 2011: SEAL. CRACKED. METALLIC VAPOR SEAL CRACKED ON LT SIDE AT FR 42-43, R & R METALLIC VAPOR SEAL ON LT SIDE FR 42-43.
- [SDR FDEA201106142246](https://openairdocs.org/sdr/FDEA201106142246), Jun 14, 2011: WEB. DAMAGED. AFT PIT FR 69 RBL 26 VERTICAL WEB PUNCTURED AT CARGO FLOOR LEVEL REMOVED AND REPLACED VERTICAL WEB AT FR 69 RBL 26 IAW SRM 51-40-21
- [SDR FDEA201106122211](https://openairdocs.org/sdr/FDEA201106122211), Jun 12, 2011: SEAT TRACK. CRACKED. SEAT TRACK NR 3 LT CORRODED AT FR 19. REMOVED CORROISON FROM NR 3 SEAT TRACK AT FR 19 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED NR 3 
- [SDR FDEA201106122212](https://openairdocs.org/sdr/FDEA201106122212), Jun 12, 2011: SEAT TRACK. CORRODED. MDCC SEAT TRACK, NR 6, RT CORRODED INSIDE TRACK. REMOVED LEVEL 1 CORROSION ON SEAT TRACK NR 6 AT FR 19 AND FOUND TO BE OUT OF LIMITS IAW AIRBUS SRM 53-10-16. RE
- [SDR FDEA201106122210](https://openairdocs.org/sdr/FDEA201106122210), Jun 12, 2011: SEAT TRACK. CORRODED. RIGHT SEAT TRACK NR6 BETWEEN FRAME 19 & 20 HAS CORRSION 1 SQ INCH. REMOVED LEVEL 1 CORROSION FROM RT NR 6 SEAT TRACK BETWEEN FRAME 19 & 20 AND FOUND BEYOND LIMI
- [SDR FDEA201106122213](https://openairdocs.org/sdr/FDEA201106122213), Jun 12, 2011: FLOORBEAM. CORRODED. MDC UNDERFLOOR TEE HAS 1 SQ INCH OF CORROSION FWD OF SEAT TRACK NR LT AT FR 12A. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED AND R
- [SDR FDEA201106102204](https://openairdocs.org/sdr/FDEA201106102204), Jun 10, 2011: SEAT TRACK. DAMAGED. SEAT TRACK 4L AT FRAME 54.3 HAS DAMAGE TO TACK AND SCALLOPS. BLENDED DAMAGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 4L SECTION AT
- [SDR FDEA201106102201](https://openairdocs.org/sdr/FDEA201106102201), Jun 10, 2011: SEAT TRACK. DAMAGED. MDC SEAT TRACK 5R HAS 2 GOUGES AT SCALLOPS, 1 AT 54.2 AND 1 7 INCHES AFT OF 54.2. BLENDED DAMAGED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SE
- [SDR FDEA201106102203](https://openairdocs.org/sdr/FDEA201106102203), Jun 10, 2011: SEAT TRACK. DAMAGED. 2 EA GOUGES ON SEAT TRACK 3R FROM FRAME 54.2 TO FRAME 55/58. BLENDED GOUGED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 3R SECTION AT
- [SDR FDEA201106102202](https://openairdocs.org/sdr/FDEA201106102202), Jun 10, 2011: SEAT TRACK. DAMAGED. SEAT TRACK 2R AT FRAME 54.2 HAS GOUGE AT SCALLOP. BLENDED GOUGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 2R SECTION AT AT FR 54.2 
- [SDR FDEA201106052123](https://openairdocs.org/sdr/FDEA201106052123), Jun 5, 2011: FITTING. CORRODED. NR2 PYLON SPIGOT RECEPTACLE FITTING HAS PITTING CORROSION ON UPPER PLATE. REMOVED NR 2 PYLON IAW AMM 54-50-00-4 REMOVED AND REPLACED UPPER AND LOWER SPIGOT FITT
- [SDR FDEA201106052121](https://openairdocs.org/sdr/FDEA201106052121), Jun 5, 2011: FITTING. CORRODED. NR 1 PYLON SPIGOT RECEPTACLE FITTING HAS PITTING CORROSION ON UPPER PLATE. REMOVED NR 1 PYLON IAW AMM 54-50-00-4. REMOVED AND REPLACED UPPER AND LOWER SPIGOT FI
- [SDR FDEA201106012083](https://openairdocs.org/sdr/FDEA201106012083), Jun 1, 2011: SEAT TRACK. MISINSTALLED. MAIN CABIN SEAT TRACK NR 2 LT Y450 BETWEEN FRAMES 47/48 TO 49 HAS AN EXISTING REPAIR WITH INCORRECT FASTENERS INSTALLED ON TOP FLANGE. REMOVED AND REPLACED 20 E
- [SDR FDEA201002090367](https://openairdocs.org/sdr/FDEA201002090367), Feb 9, 2010: BELLCRANK. DIRTY. LT MAIN GEAR DOOR WOULD NOT CLOSE ON T/O. RETURNED TO DEPARTURE. OPS CHECKED LT MLG DOOR IAW MM 32-12-11-5. OPS CHECKS NORMAL. DURING TROUBLESHOOTING, WERE ABLE
- [SDR FDEA200907012422](https://openairdocs.org/sdr/FDEA200907012422), Jul 1, 2009: IDG. UNDERSERVICED. ON T/O ROLL AT APPROX 80 KNOTS RECEIVED ECAM ALERT, NR 1 IDG OIL PRESS W/ GEN 1 FAULT. RTO AND RETURNED TO BLOCKS. GEN 1 FAULT CLEARED BUT IDG NR1 FAULT KEPT FL
- [SDR FDEA200812065096](https://openairdocs.org/sdr/FDEA200812065096), Dec 6, 2008: BUSHING. DAMAGED. MAIN FRAME RT NOSE LANDING GEAR BEARING FITTING INSPECTION PER EA T6-5310-99725A, REQUIRES REMOVAL OF REPAIR BUSHING FOR INSPECTION. REMOVED REPAIR BUSHING, FAB
- [SDR 08FDEA04961](https://openairdocs.org/sdr/08FDEA04961), Nov 22, 2008: SEAT TRACK. DAMAGED. MAIN DECK CARGO COMPT SEAT TRACK NR 2 RT, 12 IN AFT OF FR 43 HAS 2 DAMAGED SCALLOPS. REMOVED DAMAGED SECTION OF SEAT TRACK NR 2 RT. FABRICATED REPLACEMENT SECTI
- [SDR 08FDEA01724](https://openairdocs.org/sdr/08FDEA01724), May 1, 2008: TRANSMITTER. INOPERATIVE. ON FINAL APPROACH, RECEIVED SLAT SYS 1 AND 2 FAULT FOLLOWED UP SHORTLY W/GREEN HYD ECAM COMMAND TO TURN OFF BOTH GREEN HYD PUMPS. FAULTS ON OVERHEAD WERE AS FOL
- [SDR 08FDEA00192](https://openairdocs.org/sdr/08FDEA00192), Jan 18, 2008: HYDRAULIC SYSTEM. LOW. REJECT T/O DUE TO ECAM: GREEN SYSTEM HYD QTY LOW. VERY COLD OUTSIDE AIR TEMP. PERFORMED VISUAL INSPECTION AND NO LEAKS FOUND. SERVICED GREEN HYD SYS PER SMP AND
- [SDR 07FDEA00151](https://openairdocs.org/sdr/07FDEA00151), Jan 22, 2007: SLIDE. LOW. R1 DOOR ESCAPE SLIDE PRESSURE INDICATOR NOT IN GREEN BAND REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE IAW A310-300 AMM 25-61-22-4-01 AND A310 - 300 AMM 52-10-00-3
- [SDR 06FDEA03588](https://openairdocs.org/sdr/06FDEA03588), Oct 4, 2006: FITTING. CORRODED. COMPLY WITH AGING 9-AGING-INSP, FOUND CORROSION AND WEAR LOCATED IN RT FITTING BETWEEN FS 16A/ FS 17 IN HOLE AT ATTACHMENT FITTING OF AFT DOOR.
- [SDR 06FDEA03400](https://openairdocs.org/sdr/06FDEA03400), Sep 22, 2006: SKIN. DAMAGED. RT MLG-STRUT DOOR W/SKIN SURFACE DAMAGED AND REPAIR AT LOWER AREA THE STRUT DOOR WAS REPAIRED PER FEDEX EA 6-5280-99721 EVALUATED PER GMM 6-2-100 AND CLASSIFIED
- [SDR 06FDEA03054](https://openairdocs.org/sdr/06FDEA03054), Aug 22, 2006: SKIN. DAMAGED. FOUND REPAIR LOCATED RT OUTBD FLAP AT INNER LOWER SKIN SURFACE AND UPPER SKIN SURFACE OF T/E RIB 11/RIB 12. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINAT
- [SDR 06FDEA03053](https://openairdocs.org/sdr/06FDEA03053), Aug 22, 2006: SKIN. DAMAGED. FOUND REPAIR LOCATED MLG RT W/W DOOR AT INNER LOWER SKIN SURFACE AT OUTBD LOWER PART. REPAIR REQUIRE EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR 
- [SDR 06FDEA03052](https://openairdocs.org/sdr/06FDEA03052), Aug 22, 2006: SKIN. DAMAGED. FOUND REPAIR LOCATED AT RT ELEVATOR AT INNER LOWER SKIN SURFACE STA 833/ER 38 AND STA 791/ ER36. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF 
- [SDR 06FDEA03051](https://openairdocs.org/sdr/06FDEA03051), Aug 22, 2006: SKIN. DAMAGED. FOUND REPAIR LOCATED RT ELEVATOR AT INNER LOWER SKIN STA 604/ER26 AND STA 566/ER 24. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR A
- [SDR 06FDEA03050](https://openairdocs.org/sdr/06FDEA03050), Aug 22, 2006: SKIN. DAMAGED. FOUND REPAIR LOCATED ON LT NR 2 SLAT SKIN SURFACE OF L/E BETWEEN RIB 44/45 (NEXT JACK RIB 4). REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF T
- [SDR 06FDEA03049](https://openairdocs.org/sdr/06FDEA03049), Aug 22, 2006: SKIN. DAMAGED. FOUND REPAIR LOCATED INBD FLAP LT AT LOWER SURFACE AT RIB 8/ RIB 10. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USI
- [SDR 06FDEA03048](https://openairdocs.org/sdr/06FDEA03048), Aug 22, 2006: SKIN. DAMAGED. FOUND REPAIR LOCATED LT INB FLAP AT T/E UPPER AND LOWER SKIN SURFACE BETWEEN RIB 5 AND RIB 8. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE
- [SDR 06FDEA03047](https://openairdocs.org/sdr/06FDEA03047), Aug 22, 2006: SKIN. DAMAGED. FOUND REPAIR LOCATED RT OUTB FLAP AT INNER LOWER SKIN SURFACE AT T/E OF INDB OF RIB 3. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR
- [SDR 06FDEA03046](https://openairdocs.org/sdr/06FDEA03046), Aug 22, 2006: SKIN. DAMAGED. FOUND REPAIR LOCATED RT INB FLAP AT INNER LOWER AND UPPER SKIN SURFACE AT T/E OF FLAP RIB 19. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE
- [SDR 06FDEA03045](https://openairdocs.org/sdr/06FDEA03045), Aug 22, 2006: STRUCTURE. UNKNOWN. FOUND REPAIR LOCATED ON RT WING T/E WS 1625, RIB 26-27 BETWEEN OUTB FLAP AND WING TIP. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WA
- [SDR 06FDEA03044](https://openairdocs.org/sdr/06FDEA03044), Aug 22, 2006: DOOR. MISREPAIRED. FOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 5055/5065 FS 100/100. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING
- [SDR 06FDEA03043](https://openairdocs.org/sdr/06FDEA03043), Aug 22, 2006: DOOR. MISREPAIRED. FOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 4986/5003 FR 98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA
- [SDR 06FDEA03042](https://openairdocs.org/sdr/06FDEA03042), Aug 22, 2006: DOOR. MISREPAIRED. FOUND REPAIR RT APU DOOR BETWEEN STA 4969/5001 FS 97/98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPR
- [SDR 06FDEA03041](https://openairdocs.org/sdr/06FDEA03041), Aug 22, 2006: DOOR. MISREPAIRED. FOUND REPAIR RT APU DOOR BETWEEN STA 4937/4969 FR 96/97 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPRO
- [SDR 06FDEA03040](https://openairdocs.org/sdr/06FDEA03040), Aug 22, 2006: DOOR. MISREPAIRED. FOUND REPAIR LOCATED LT APU DOOR BETWEEN STA 5033/5045 FS 99/99. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING 
- [SDR 06FDEA03039](https://openairdocs.org/sdr/06FDEA03039), Aug 22, 2006: SKIN. DAMAGED. PREVIOUS REPAIR FOUND AT BULK COMP´T DOOR SKIN LOCATED AT BEAM 5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR ACCOMPLISHED USING FAA 
- [SDR 06FDEA3035](https://openairdocs.org/sdr/06FDEA3035), Aug 22, 2006: NONE. NONE. NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT
- [SDR 06FDEA3036](https://openairdocs.org/sdr/06FDEA3036), Aug 22, 2006: NONE. NONE. NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT
- [SDR 06FDEA3037](https://openairdocs.org/sdr/06FDEA3037), Aug 22, 2006: NONE. NONE. NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT
- [SDR 06FDEA3038](https://openairdocs.org/sdr/06FDEA3038), Aug 22, 2006: NONE. NONE. NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED LT 

All 66: https://openairdocs.org/deregistered/N817FD-2024-03-02/reports.md

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