# N408FE: 1983 Airbus Industrie A310-203, registration cancelled 2013-03-27 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 27, 2013 - Status when cancelled: Valid registration - Airframe: [Airbus Industrie A310-203](https://openairdocs.org/model/airbus-industrie-a310-203) (registry code 3930313) - Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025) - Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs) - Serial number: 257 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 4, 1995 - Certificate issued: August 2, 2010 - Last registry action: February 1, 2012 - Mode S code: A4CADB - 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/N408FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=408FE - Page: https://openairdocs.org/deregistered/N408FE-2013-03-27 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 Industrie A310-203: https://openairdocs.org/model/airbus-industrie-a310-203.md ## Service difficulty reports (14) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 07FDEA05057](https://openairdocs.org/sdr/07FDEA05057), Dec 14, 2007: CONTROL LEVER. FAILED. GEAR LEVER WOULD NOT RETRACT PAST NEUTRAL POSITION IN SYS NR 1 OR SYS NR 2 INTERROGATED PROX BOX FOUND FAULT CODES 64 AND 60 INSTALLED TEST BOX IN A/C. REMOVED - [SDR 07FDEA01652](https://openairdocs.org/sdr/07FDEA01652), Apr 27, 2007: SHEAR TIE. CRACKED. A/C BAY AT RT SIDE OF KEEL BEAM AND ON TOP VERTICAL FLANGE OF FR 46 , 1 SHEAR TIE BRACKET HAS CRACK .51 LONG. REMOVED AND REPLACED SHEAR TIE IAW A310-200 SRM 51 - [SDR 07FDEA01651](https://openairdocs.org/sdr/07FDEA01651), Apr 27, 2007: SKIN. DEBONDED. LT ELEVATOR LOWER SKIN IS DISBONDED AT RIB 13 ,5 IN FROM T/E 7.5 IN LONG. REPAIRED DAMAGED AREA IAW EA 6-5520-110453. - [SDR 07FDEA01650](https://openairdocs.org/sdr/07FDEA01650), Apr 27, 2007: STRUCTURE. CORRODED. AFT CARGO COMPT BILGE AREA BETWEEN FR 60-61 HAS CORROSION AROUND 18 EA RIVET BUCKTAILS ON S56R. REMOVED CORROSION IAW A310-200 SRM 51-74-10 CHECKED LIMITS IAW A - [SDR 07FDEA01649](https://openairdocs.org/sdr/07FDEA01649), Apr 27, 2007: SKIN. CRACKED. L-WING TE BOTTOM SKIN AT PANEL 581AB CUTOUT HAS CRACK ON LOWER SKIN RIB 11 WITH APPROX 0.75 IN LONG REF N00166 STOP DRILLED CRACK, DRILLED UP DOUBLER AND COLDWO - [SDR 04FDEA03192](https://openairdocs.org/sdr/04FDEA03192), Nov 18, 2004: UPLOCK. FAILED. AFTER TAKEOFF, NOSE GEAR AMBER "DOOR" WARNING LIGHTS (FWD AND OVERHEAD) REMAINED ON FOLLOWING GEAR RETRACTION. NO EXCESSIVE NOISE OR VIBRATION OBSERVED. WHEN GE - [SDR 01FDEA00769](https://openairdocs.org/sdr/01FDEA00769), Aug 24, 2001: CONTROLLER. MALFUNCTIONED. PDIS WRI 26-12-5025 AT ABOUT 1500 AFT MAIN DECK CARGO LOOP-A ILLUMINATED, FOLLOWED BY LOOP-B AND RED SMOKE LIGHT & ECAM FIRE WARNING. DECLARED EMER AND RETURNED - [SDR 01FDEA00026](https://openairdocs.org/sdr/01FDEA00026), Jan 18, 2001: SMOKE WARNING. ACTIVATED. ON APR AT 1000 FT CONFIG TO LAND GOT CARGO SMOKE ALARM/WARN LIGHTS. - [SDR 01FDEA00020](https://openairdocs.org/sdr/01FDEA00020), Jan 12, 2001: FIRE WARNING. ACTIVATED. CARGO SMOKE AND FIRE ON FINAL FIRE BOTTLES ON APU ENG DISCHARGED ON LAND. REPLACED NR 1 & 2 FIRE BOTTLES IN BOTH ENG 1 & 2 AS PER MM 26-22-12-4. AC OK FOR FLIGH - [SDR 99FDEA00509](https://openairdocs.org/sdr/99FDEA00509), Dec 22, 1999: WARNING SYSTEM. ACTIVATED. 99-292 - ON T/O YELLOW SYSTEM LOW PRESS ECAM WARNING. REJECTED TO AT 83 KTS. YELLOW SYS RECOVERED TO NORM CLEAR RUNWAY. - [SDR 99FDEA00205](https://openairdocs.org/sdr/99FDEA00205), Jun 3, 1999: MEC. MALFUNCTIONED. NR 2 ENG SHUT DOWN DUE TO LOW OIL PRESS, NO RESTART. *S/D* REMOVED AND REPLACED NR 2 ENG MEC AND FUEL PUMP AS PER AIRBUS MM. CK GOOD. REMOVED AND REPLACED CIT S - [SDR 98FDEA00763](https://openairdocs.org/sdr/98FDEA00763), Dec 24, 1998: SWITCH. INOP. LANDING GEAR HANDLE WOULD NOT GO PAST THE MID POS. FOLLOW RED TAB AND USED OTHER SYS AS DIRECTED, PROBLEM REMAINED. JUST AFT SYS 2 USED, YELLOW SYS HYD ECAM CAM - [SDR 98FDEA00656](https://openairdocs.org/sdr/98FDEA00656), Oct 18, 1998: DAMPER. INOP. T/O MEM COULD NOT RAISE GEAR HANDLE. TRIED BOTH POSITION DET SYSTEM 1 AND 2. RECYCLE HANDLE DOWN AND RETRIED. STILL NOT ABLE TO RETRACT. RETURNED TO MEM. REMOVE - [SDR 97FDEA00834](https://openairdocs.org/sdr/97FDEA00834), Nov 13, 1997: RETRACT MECH. MALFUNCTION. ON FLAP RETRACTION FLAPS REMAINED AT 5 DEG. EXTENSION AND FLAPS SYSTEM NR 1 AND NR 2 FAULT ON, COMPLIED WITH QRH. RESET NR 1 AND NR 2 SFCC'S. CYCLED FLAPS AND S ## Other aircraft with N408FE - [Registered now](https://openairdocs.org/aircraft/N408FE): Textron 408, S/N 408-0003, built 2022 --- 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.