# N412FE: 1985 Airbus Industrie A310-203, registration cancelled 2013-04-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 25, 2013
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A310-203](https://openairdocs.org/model/airbus-industrie-a310-203) (registry code 3930313)
- Engine: [GE CF6-6 series](https://openairdocs.org/engine/ge-cf6-6-series) (registry code 30020)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 360
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 10, 1994
- Certificate issued: November 23, 2009
- Last registry action: November 7, 2012
- Mode S code: A4DC10
- Owners when cancelled: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Attn: Michael Wilson](https://openairdocs.org/faa-owner/ATTN%3A%20MICHAEL%20WILSON)
- 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/N412FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=412FE
- Page: https://openairdocs.org/deregistered/N412FE-2013-04-25

From the FAA registry file of November 5, 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 A310-203: https://openairdocs.org/model/airbus-industrie-a310-203.md

## Service difficulty reports (34)

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

- [SDR 07FDEA04967](https://openairdocs.org/sdr/07FDEA04967), Nov 29, 2007: SWITCH. FAILED. RECEIVED AN AUDIBLE "TOO LOW-GEAR" WNG ON SHORT FINAL. ALL GEAR INDS SHOWED GREEN/DOWN, SWITCHED TO POS1, REATTEMPT LANDING ALL SYS WORK NORMAL. ACN RELEASED FO
- [SDR 07FDEA00908](https://openairdocs.org/sdr/07FDEA00908), Mar 15, 2007: SKIN. CORRODED. AVIONICS BAY, CORROSION BELOW FRAME 17 AT STR 44L REPAIRED IAW EA 6-5330-107691.
- [SDR 07FDEA00905](https://openairdocs.org/sdr/07FDEA00905), Mar 15, 2007: FLOORBEAM. MISREPAIRED. MDCC - FLOORBEAM FRAME 36 CRACKED (PREVIOUS REPAIR NOT PER SRM). REWORKED PREVIOUS REPAIR IAW EA 6-5321-29042.
- [SDR 07FDEA00902](https://openairdocs.org/sdr/07FDEA00902), Mar 15, 2007: SKIN. CORRODED. AVIONICS BAY CORROSION AROUND FASTENERS FS 16 TO 17, STR 44L TO 45L REPAIRED PER EA 6-5330-107691.
- [SDR 07FDEA00889](https://openairdocs.org/sdr/07FDEA00889), Mar 15, 2007: SKIN. CORRODED. FOUND CORROSION EXIST AT AVIONIC COMPARTMENT AT STA 1315/FR 16 AND 17 STGR 46 ON FUSELAGE SKIN TOTAL 2 BY 2 INCHES BELOW ACCESS PNL 121 PF ZONE 120 COMPLIED WIT
- [SDR 07FDEA00884](https://openairdocs.org/sdr/07FDEA00884), Mar 15, 2007: UNKNOWN. CORRODED. FOUND CORROSION EXIST AT AVIONICS COMPARTMENT STA 1315/ FR 17 STGR 45 LT 2' BY 2' INCHES BELOW ACCESS PNL 121 PF ZONE 120 COMPLIED WITH EA 6-5330-107691.
- [SDR 07FDEA00881](https://openairdocs.org/sdr/07FDEA00881), Mar 15, 2007: FRAME. CORRODED. FOUND CORROSION EXIST AT AVIONIC COMPARTMENT AT STA 1315/ FRAME 16 AND 17 BETWEEN S47 AND 48 BELOW ACCESS PNL 121 PF ZONE 120 COMPLIED WITH EA 6- 5330-107691.
- [SDR 07FDEA00876](https://openairdocs.org/sdr/07FDEA00876), Mar 15, 2007: SKIN. CRACKED. LT WING LOWER SKIN SURFACE HAS A CRACK OF APPROX 1 INCH LONG AT AFT END OF RIB 11, 4 INCHES AFT OF REAR SPAR, FWD INBD END OF CUTOUT FOR ACCESS PANEL 581AB. CRA
- [SDR 07FDEA00873](https://openairdocs.org/sdr/07FDEA00873), Mar 15, 2007: FLOORBEAM. CRACKED. FOUND CRACK FR 38 PROFILE MDCC FLOORBEAM LT FWD CARGO COMPARTMENT BETWEEN SEAT TRACKS L-4 & L-5, REF SRM 53-10-00 AND SRM 53-10-15. REPAIRED FR 38 MDCC FLOORBEA
- [SDR 07FDEA00845](https://openairdocs.org/sdr/07FDEA00845), Mar 14, 2007: FLOORBEAM. MISREPAIRED. PREVIOUS REPAIR ON CABIN FLOORBEAM FRAME 37 REPAIR ANGLES IMPROPERLY INSTALLED. CORRECTED REPAIR IAW EA 6-5310-107701.
- [SDR 07FDEA00844](https://openairdocs.org/sdr/07FDEA00844), Mar 14, 2007: FERRULE. CRACKED. NR 1 PYLON PRECOOLER FERRULE PAN CRACKED BETWEEN RIBS 4 AND 8. ACCOMPLISHED PERMANENT REPAIR IAW SB A310-54-2028.
- [SDR 07FDEA00843](https://openairdocs.org/sdr/07FDEA00843), Mar 14, 2007: SKIN. CORRODED. AVIONICS BAY HAD A 2.5" BY 1.5" AREA OF CORROSION BETWEEN FRAMES 17 AND 18 AND STRINGERS 50L AND 51L. CORROSION OUT OF LIMITS. COMPLIED WITH EA 6-5330-107691.
- [SDR 07FDEA00842](https://openairdocs.org/sdr/07FDEA00842), Mar 14, 2007: SKIN. CORRODED. AVIONICS BAY SKIN FWD OF FRAME 17 BETWEEN STRINGERS 48L AND 50L HAS 5" BY 5" AREA OF CORROSION AREA OUT OF LIMITS. COMPLIED WITH EA 6-5330-107691.
- [SDR 07FDEA00803](https://openairdocs.org/sdr/07FDEA00803), Mar 13, 2007: SEAT TRACK. GOUGED. MDCC SEAT TRACK 3L GOUGED CUT OUT AND REPLACED GOUGED SECTION OF SEAT TRACK. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
- [SDR 07FDEA00802](https://openairdocs.org/sdr/07FDEA00802), Mar 13, 2007: SEAT TRACK. GOUGED. MDCC SEAT TRACK 5L GOUGED BLENDED GOUGES IAW A310-200 SRM 51-74-10. FOUND TO BE IN LIMITS. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
- [SDR 05FDEA03547](https://openairdocs.org/sdr/05FDEA03547), Oct 27, 2005: WARNING LIGHT. FALSE ACTIVATION. SOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO DOOR NOT CLOSED. AFT CARGO SW FAULT AND AN AMBER DOOR LIGHT FOR AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE IAW M
- [SDR 05FDEA03546](https://openairdocs.org/sdr/05FDEA03546), Oct 27, 2005: WARNING LIGHT. FALSE ACTIVATION. SOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO NOT CLOSED AFT CRAGO SW FAULT AND AN AMBER DOOR LIGHT FOR AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE PER MEL/CDL
- [SDR 05FDEA03505](https://openairdocs.org/sdr/05FDEA03505), Oct 26, 2005: DOOR. MALFUNCTIONED. SOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO NOT CLOSED AFT CARGO SW FAULT AND AN AMBER DOOR LIGHT FO R AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE PER MEL/CD
- [SDR 04FDEA02835](https://openairdocs.org/sdr/04FDEA02835), Sep 28, 2004: PANEL. DAMAGED. PANEL LAND 650KB HAS 6EA ELONGATED HOLES (RT WING). REPAIRED HOLES IAW EA 6-5710-81998 AND A310 SRM 51-40-44 FIG 1.
- [SDR 04FDEA02834](https://openairdocs.org/sdr/04FDEA02834), Sep 28, 2004: PANEL. DAMAGED. PANEL LAND 550JB HAS 1EA ELONGATED HOLE (LT WING). REPAIRED HOLE IAW EA 6-5710-81998.
- [SDR 04FDEA02833](https://openairdocs.org/sdr/04FDEA02833), Sep 28, 2004: PANEL. DAMAGED. PANEL LAND 650JB HAS 2EA ELONGATED HOLES. REPAIRED 2EA ELONGATED HOLES IAW EA 6-5710-81998
- [SDR 04FDEA02441](https://openairdocs.org/sdr/04FDEA02441), Aug 11, 2004: SEAT TRACK. CORRODED. MAIN CABIN CARGO FLOOR 3 AREAS OF CORROSION ON SEAT TRACKS AT FR66 AND FR67 ZONE 251 TRACK F. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW SRM 53-10-16
- [SDR 04FDEA02440](https://openairdocs.org/sdr/04FDEA02440), Aug 11, 2004: PYLON. CRACKED. NR 1 ENGINE AFT UPPER PYLON HAS CRACKED UNDER PNL 473CL. STOP DRILLED CRACK AND INSTALLED U-CHANNEL IAW A310/200 SRM 54-50-00 AND 54-54-11 FIG 201 AND 54-54-51 
- [SDR 04FDEA02439](https://openairdocs.org/sdr/04FDEA02439), Aug 11, 2004: SEAT TRACK. CORRODED. MDC ON RT SEAT TRACK NR 3 FR53 NOTED CORROSION INSIDE SCALLOP HOLES AND ON FLANGE. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW A310/200 SRM 53-10-16.
- [SDR 04FDEA02438](https://openairdocs.org/sdr/04FDEA02438), Aug 11, 2004: DUMMY RAIL. CORRODED. UPPER MAIN CABIN FR48 BETWEEN TRACK D & E HAS 1EA DUMMY TRACK WITH CORROSION BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED DUMMY TRACK IAW A310 SRM 51-72-10.
- [SDR 04FDEA02437](https://openairdocs.org/sdr/04FDEA02437), Aug 11, 2004: DUMMY RAIL. CORRODED. UPPER MAIN CABIN BETWEEN D & E HAS 3EA DUMMY TRACK WITH CORROSION (LEVEL 2) AND 1EA DUMMY TRACK CRACKED (2 INCHES IN LENGTH) BETWEEN FR 52 AND 53. REMOVED AND R
- [SDR 04FDEA02338](https://openairdocs.org/sdr/04FDEA02338), Aug 1, 2004: TEE FITTING. CORRODED. REF. SNRM N00243 MDCC T-CAP JUST AFT OF COCKPIT DOOR HAS LEVEL 2 CORROSION REMOVED CORROED T-CAP SECTION INSTALLED A SPLICE IN SECTION IAW A310/200 SRM 53- 12-1
- [SDR 04FDEA00389](https://openairdocs.org/sdr/04FDEA00389), Feb 10, 2004: COALESCER BAG. DIRTY. ON TAKEOFF ROLL STRONG ODOR OF OIL OR AIR CONDITIONING SMOKE IN COCKPIT, REJECTED TAKEOFF. NO SIGN OF SMOKE COMING FROM VENTS, NO SMOKE WARNINGS, ALL INDICATION
- [SDR 03FDEA02008](https://openairdocs.org/sdr/03FDEA02008), Dec 2, 2003: THRUST REVERSER. MALFUNCTIONED. 1 ENG ON T/O, N1 DID NOT REACH T/O PWR. ENG N1 90 PRCT. ENG 2 N1 100 PRCT. TRIED TO MATCH N1 BY PUSHING UP 1 THROTTLE WHICH CAUSED 1 EGT TO RISE TO CAUTION RANG
- [SDR 02FDEA00384](https://openairdocs.org/sdr/02FDEA00384), Jun 8, 2002: CONTROLLER. FAILED. AIRCRAFT WOULD NOT PRESSURIZE. NR 1 FWD AND AFT OUTFLOW VALVE INDICATED FULL OPEN. PERFORMED FUNCTIONAL CHECK OF NR 1 AND NR 2 PRESSURIZATION CONTROLLERS. NR 1 
- [SDR 02FDEA00051](https://openairdocs.org/sdr/02FDEA00051), Jan 15, 2002: LIGHT. ILLUMINATED. 02-51 AFTER T/O MAIN DECK DOOR LIGHT CAME ON. A/C RELEASED PER MEL 52-9.
- [SDR 02FDEA00009](https://openairdocs.org/sdr/02FDEA00009), Jan 3, 2002: SYMBOL GENERATOR. INOPERATIVE. LOST F/O'S PRIMARY FLT AND NAV DISPLAY. EFIS SGU NR 2 INOP. RELEASED PER MEL 34-7.
- [SDR 00FDEA00002](https://openairdocs.org/sdr/00FDEA00002), Jan 4, 2000: SWITCH. FAILED. ON T/O, L/G WOULD NOT RETRACT DESPITE SEVERAL RECYCLES ON SYS 1 AND 2 C/B'S. RESET BOX AND FAULTED SAME UNITS. REMOVED AND REPLACED PROXIMITY DETECTOR UNIT PER 
- [SDR 99FDEA00510](https://openairdocs.org/sdr/99FDEA00510), Dec 22, 1999: RELAY. FAILED. 99-293 - ON DEPT GDL, F/O PITOT HEAT FAILED, THEN NR 1 ATS TRIPPED. WOULD NOT RESET. REMOVED AND REPLACED NOSE GEAR RELAY 153GB IAW MM. ALL CK GOOD, OK FOR SERV

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