# N415FE: 1984 Airbus Industrie A310-203, registration cancelled 2009-10-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 26, 2009
- Status when cancelled: Triennial form not returned
- 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: 349
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 26, 1996
- Certificate issued: November 24, 1995
- Last registry action: December 18, 2007
- Mode S code: A4E735
- Owner when cancelled: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION)
- 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/N415FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=415FE
- Page: https://openairdocs.org/deregistered/N415FE-2009-10-26

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 (13)

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

- [SDR 08FDEA01609](https://openairdocs.org/sdr/08FDEA01609), Apr 25, 2008: PRESSURE SWITCH. FAILED. AFTER DEPARTURE GOT A FLAP FAULT, FOUND FAULT CODE ON SFCC 1 LT WING HIGH SPEED PRESS SWITCH. PERFORMED TEST PER AMM 27-51-00-5, ALL PASSED. SWITCHED SFCC NR 1 
- [SDR 08FDEA00688](https://openairdocs.org/sdr/08FDEA00688), Mar 4, 2008: ADC. UNKNOWN. ON TAKEOFF ROLL, CAPT/FO AIRSPEED DIFFERENCE OF 40 KNOTS (120/80) REJECTED TAKEOFF. PERFORMED ADS SYSTEM CHECK IAW TSM 34-10-00. NO FAULTS NOTED. NO FAULTS ON A
- [SDR 07FDEA01760](https://openairdocs.org/sdr/07FDEA01760), May 11, 2007: WIRE. SHORTED. CAPT WINDOW HEAT SIDE SLIDING WINDOW WIRING SHORTED OUT AND MOMENTARY CAUGHT FIRE PULLED ASSOCIATED CB H86. WIRING CAPPED AND STOWED AND ASSOCIATED ITEMS, SLIDI
- [SDR 07FDEA01761](https://openairdocs.org/sdr/07FDEA01761), May 11, 2007: WIRE. SHORTED. CAPT WINDOW HEAT SIDE SLIDING WINDOW WIRING SHORTED OUT AND MOMENTARY CAUGHT FIRE PULLED ASSOCIATED CB H86. ACCOMPLISHED EA 6-3040-111404, DISCONNECT, CAP AND S
- [SDR 04FDEA02872](https://openairdocs.org/sdr/04FDEA02872), Oct 5, 2004: PROXIMITY SENSOR. MALFUNCTIONED. GEAR WOULD NOT RETRACT AFTER TAKEOFF IN EITHER SYSTEM. PERFORMED BITE TEST OF PROX DETECT UNIT 54GB. NO MEMORIZED FAULTS. PERFORMED SYS TEST WITH THE FOLLOWING 
- [SDR 04FDEA02394](https://openairdocs.org/sdr/04FDEA02394), Aug 6, 2004: OUTFLOW VALVE. INOPERATIVE. PDIS 415 21-30 0007170 FWD NR 1 OUTFLOW VALVE STUCK IN THE OPEN POSITION (AMBERARROW ON ECAM). NR 1 PRESS REGULATOR IN USE-ECAM SHOWED 0 V/S AND CABIN ALT. AT 2
- [SDR 03FDEA02236](https://openairdocs.org/sdr/03FDEA02236), Dec 23, 2003: COMPUTER. FAULTY. LEFT INNER TANK QUANTITY WENT TO ZERO READING IN LESS THAN A MINUTE. AFTER THE FQI CHAN SUPPLY 1 AND 2 C/B'S WERE RESET IAW QRH FUEL LEAK PROCEDURE ECAM SHOWED 
- [SDR 03FDEA01230](https://openairdocs.org/sdr/03FDEA01230), Aug 9, 2003: STRUCTURE. VIBRATION. AIRFRAME VIBRATION STARTED CLIMBING OUT AT FL22.5 2CD A330 KIAS. ENGINE DATA N1-104.1 2C104.23A EGT 832 2C 841 3A VIBES 0.62C+0.2 3A N2 VIBES 2.0 2C0.4. VIBRATI
- [SDR 02FDEA00294](https://openairdocs.org/sdr/02FDEA00294), Apr 26, 2002: LANDING GEAR. MALFUNCTIONED. 02-105 AFTER TAKE OFF, ALL 3 LANDING GEAR WOULD NOT RETRACT, GEAR NOT UP AND LOCKED DISPLAYED ON ECAM. ALL 3 RED GEAR DISAGREE ARROW LIGHTS DISPLAYED. LG SYS NR
- [SDR 00FDEA00458](https://openairdocs.org/sdr/00FDEA00458), Jul 18, 2000: PITOT TUBE. BLOCKED. ON T/O ROLL, CAPT''S AIRSPEED IND ON PFD NEVER GAVE ANY A/S IND. DISCONNECTED LINE FROM ADC NR 1 BLEW THRU PITOT TUBE, GOT BIG BUG. PERFORMED LEAK TEST PER AMM 
- [SDR 99FDEA00002](https://openairdocs.org/sdr/99FDEA00002), Jan 5, 1999: PITCH DAMPER. LEAKING. AIR TURNBACK, CREW CALLED GEAR AND GEAR WOULD NOT RETRACT. *S/D* REMOVED AND REPLACED LT BOGIE PITCH DAMPER PER MM 32-11-15. LEAK CK C/W, NO LEAKS NOTED.
- [SDR 98FDEA00264](https://openairdocs.org/sdr/98FDEA00264), Apr 11, 1998: CONTROL UNIT. MALFUNCTIONED. 98-0100, AT FL290 CREW RECEIVED AN ECAM WARNING OF MAIN DECK SMOKE WARNING. CREW DONNED 02 MASK AND FOLLOWED AFM PROCEDURES. NEVER DID SMELL SMOKE. DECLARED PRE
- [SDR 98FDEA00024](https://openairdocs.org/sdr/98FDEA00024), Jan 8, 1998: RETRACT MECH. MALFUNCTIONED. FLAPS STUCK AT APPROX 5 DEG ON RETRACTION. FLAPS SYS 1 AND 2 FAULT ILLUMINATED. FLAPS WOULD NOT EXTEND BEYOND 5 DEG ON LANDING. SLATS OPERATED NORMALLY. SFPI FL

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20020426019039I](https://openairdocs.org/incident/20020426019039I), Apr 26, 2002: Airbus A310203 (N415FE), Rochester, NY. (-23) On Friday, April 26, 2002, the crew of an A-320-203 aircraft, N415FE, operated by federal express, selected the landing gear "up" position after takeoff,…

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