# N449FE: 1983 Airbus Industrie A310-222, registration cancelled 2010-05-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 10, 2010
- Status when cancelled: Triennial form not returned
- Airframe: [Airbus Industrie A310-222](https://openairdocs.org/model/airbus-industrie-a310-222) (registry code 3930315)
- Engine: [Pratt & Whitney JT9D series](https://openairdocs.org/engine/pratt-whitney-jt9d-series) (registry code 52054)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (OpenAirDocs)
- Serial number: 217
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 30, 1997
- Certificate issued: February 22, 1997
- Last registry action: September 15, 2009
- Mode S code: A56C8E
- Owners when cancelled: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION), [Attn  Al Garcia](https://openairdocs.org/faa-owner/ATTN%20%20AL%20GARCIA)
- 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/N449FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=449FE
- Page: https://openairdocs.org/deregistered/N449FE-2010-05-10

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 A310-222: https://openairdocs.org/model/airbus-industrie-a310-222.md

## Service difficulty reports (40)

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

- [SDR FDEA200812095113](https://openairdocs.org/sdr/FDEA200812095113), Dec 9, 2008: WARNING SYSTEM. ILLUMINATED. NR 2 ENGINE REVERSER UNLOCK ECAM AT ABOUT 60 KTS ON TAKEOFF. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 14 DEC 08. FOUND NR 2 ENGI
- [SDR 07FDEA02865](https://openairdocs.org/sdr/07FDEA02865), Aug 14, 2007: SHUTOFF VALVE. INOPERATIVE. AFTER LIFTOFF (KATL) ENG NR 1 THRUST REVERSER SHOWED "UNLOCKED". ON TAKEOFF ROLL LIGHT FLICKERED MOMENTARILY THEN WENT OUT. FOLLOWED QRH AND ECAM PROCEDURE AND 
- [SDR 07FDEA02872](https://openairdocs.org/sdr/07FDEA02872), Aug 14, 2007: SHUTOFF VALVE. INOPERATIVE. AFTER LIFTOFF(KATL) ENG1 THRUST REVERSER SHOWED "UNLOCKED". ON T/O ROLL, LIGHT FLICKERED MOMENTARILY THEN WENT OUT. FOLLOWED QRH AND ECAM PROC AND DECLARED EMER
- [SDR 07FDEA02375](https://openairdocs.org/sdr/07FDEA02375), Jul 5, 2007: RECTIFIER. FAILED. FOUND NR 1 TRANSFORMER RECTIFIER FAULTED ON MAINT PANE (MULTIPLE FAULTS IN FLT- TRANSPONDER, AUTO-THROTTLE, PITCH TRIM). REMOVED AND REPLACED NR 1 TRANSFORMER R
- [SDR 07FDEA02296](https://openairdocs.org/sdr/07FDEA02296), Jun 27, 2007: CONNECTOR. LOOSE. ON TAKEOFF REC'D NR 1 REVERSER UNLOCKED LIGHT AT 2 SEPARATE TIMES. ONCE DURING ENG OVERTEMP AND AFTER THROTTLE WAS REDUCED. ON TAKEOFF, ECAM NR 1 ENG OVERTEMP, 
- [SDR 07FDEA02033](https://openairdocs.org/sdr/07FDEA02033), May 31, 2007: UNKNOWN. UNKNOWN. SHORTLY AFTER T/O A/C ACTED AS IF THERE WAS GROUND SENSING PROBLEM, MALFUNCTIONS TO INCLUDE; ATS 1, PITCH TRIM 1, ALL THREE PITOT PROBE, CAPT TAT, BOTH PRESS CO
- [SDR 07FDEA01348](https://openairdocs.org/sdr/07FDEA01348), Apr 3, 2007: OUTFLOW VALVE. MALFUNCTIONED. NR 2 AUTO PRESSURIZATION SYSTEM FWD AND AFT VALVES WOULD NOT CLOSE. NR 1 SYSTEM COULD NOT CONTROL AIRCRAFT PRESSURE. ATTEMPTED TO CONTROL PRESSURIZATION MANUALL
- [SDR 07FDEA00327](https://openairdocs.org/sdr/07FDEA00327), Feb 5, 2007: UNKNOWN. UNKNOWN. IN FLIGHT AIRCRAFT WANTED TO TURN RIGHT. REQUIRED 3 UNITS AILERON DEFLECTION TO FLY STRAIGHT. REQUIRED 14 UNITS OF RIGHT RUDDER TRIM TO LEVEL OUT AILERONS. NO C
- [SDR 06FDEA04099](https://openairdocs.org/sdr/06FDEA04099), Nov 23, 2006: FRAME. UNKNOWN. UPON DETAILED SPECIAL INSP (SDET) OF CENTER WING BOX LOWER SKIN BETWEEN FRAME 40/41AND 47/48 LT SIDE AT FRAME 44.2 OB MOST FWD HOLE SHOWS POSITIVE INDICATION DU
- [SDR 06FDEA04044](https://openairdocs.org/sdr/06FDEA04044), Nov 19, 2006: STRINGER. DAMAGED. PREVIOUS REPAIR BULK CARGO UNDER FLOOR STRINGER 55 LT HAS A STRG REPAIR BETWEEN FS 66 AND 70 WITH 4 STRINGER SECTIONS AND 4 REPAIR SPLICES REPAIRED PER FEDEX EA
- [SDR 06FDEA04043](https://openairdocs.org/sdr/06FDEA04043), Nov 19, 2006: SUPPORT. CORRODED. 4 AREAS OF CORROSION AROUND FASTENERS ON HORIZONTAL LOWER SURFACE OF STRINGER SUPPORT STRAP AT FS 40 STRG 1 C/W FEDEX EA6-5730-105024.
- [SDR 06FDEA04042](https://openairdocs.org/sdr/06FDEA04042), Nov 19, 2006: SUPPORT. CORRODED. 13 AREAS OF CORROSION AROUND FASTENERS ON HORIZONTAL LOWER SURFACE OF STRINGER SUPPORT STRAP AT FRAME 40 STRINGER 3R C/W FEDEX EA6-5730-105024.
- [SDR 06FDEA04040](https://openairdocs.org/sdr/06FDEA04040), Nov 19, 2006: SPAR. CORRODED. 33 AREAS OF CORROSION AROUND FASTENERS ALONG FS 40 AT CTR WING TANK LOWER SPAR CHORD BETWEEN STRINGER 1 AND 5R (EXTERNAL OF TANK) C/W FEDEX EA6-5730-105024.
- [SDR 06FDEA04039](https://openairdocs.org/sdr/06FDEA04039), Nov 19, 2006: SUPPORT. CORRODED. 4 AREAS OF CORROSION AROUND FASTENERS ON HORIZONTAL LOWER SURFACE OF STRINGER SUPPORT STRAP AT FS 40 5L. REPAIRED PER FEDEX EA6-5730-105024.
- [SDR 06FDEA04038](https://openairdocs.org/sdr/06FDEA04038), Nov 19, 2006: SUPPORT. CORRODED. SEVEN AREAS OF CORROSION AROUND FASTENERS ON HORIZONTIAL LOWER SUFACE OF STRINGER SUPPORT AT FS 40 STRINGER 2L. REPAIRED IAW FEDEX EA6-5730-105024.
- [SDR 06FDEA04037](https://openairdocs.org/sdr/06FDEA04037), Nov 19, 2006: STRAP. CORRODED. 12 AREAS OF CORROSION AROUND FASTENERS ON HORIZONTAL LOWER SURFACE OF STRINGER SUPPORT STRAP AT FS 40 STRINGER 3L. REPAIRED IAW WITH FEDEX EA6-5730-105024.
- [SDR 06FDEA04036](https://openairdocs.org/sdr/06FDEA04036), Nov 19, 2006: SPAR. CORRODED. 29 AREAS OF CORROSION AROUND FASTENERS ALONG FRAME 40 AT CTR WING TANK LOWER SPAR CHORD BETWEEN STGR 3L AND 5L (EXTERNAL OF TANK) REPAIRED PER FEDEX EA6-5730-10
- [SDR 06FDEA04035](https://openairdocs.org/sdr/06FDEA04035), Nov 19, 2006: STRINGER. CORRODED. 22 AREAS OF CORROSION AROUND FASTENERS ALONG STIFFENER 3 AFR43 BETWEEN CENTER WING TANK LOWER SKIN STRINGERS 2L AND 5L (EXTERNAL OF TANK). REPAIRED IAW FEDEX EA
- [SDR 06FDEA04034](https://openairdocs.org/sdr/06FDEA04034), Nov 19, 2006: STRINGER. MISREPAIRED. PREVIOUS REPAIR BULK CARGO UNDER FLOOR STRG 53 LT HAS A STGR REPAIR BETWEEN FS 66/70 WITH 4 STGR SECTIONS AND 4 REPAIR SPLICES PREVIOUSLY INSTALLED REPAIR FOUND
- [SDR 06FDEA04033](https://openairdocs.org/sdr/06FDEA04033), Nov 19, 2006: STRINGER. MISREPAIRED. PREVIOUS REPAIR BULK CARGO UNDER FLOOR STGR 50 LT HAS A STGR REPAIR BETWEEN FS 65 AND 66 WITH 1EA STGR SECTION AND 1EA REPAIR SPLICE. PREVIOUSLY INSTALLED REPAI
- [SDR 06FDEA04032](https://openairdocs.org/sdr/06FDEA04032), Nov 19, 2006: STRINGER. MISREPAIRED. PREVIOUS REPAIR AFT CARGO UNDER FLOOR STRINGER 49 LT HAS A STRINGER REPAIR BETWEEN FS 59/60 WITH 1 EA STRINGER SECTION AND 1 EA REPAIR SPLICE PREVIOUSLY INSTALL
- [SDR 06FDEA04031](https://openairdocs.org/sdr/06FDEA04031), Nov 19, 2006: SPAR. MISREPAIRED. PREVIOUS REPAIR, RT REAR UPPER SPAR CHORD HAS A STRAP REPAIR 13.5" LONG BETWEEN RIB 21 TO THE END OF THE SPAR CHORD. PREVIOUSLY INSTALLED REPAIR LOCATED AT RT T
- [SDR 06FDEA04030](https://openairdocs.org/sdr/06FDEA04030), Nov 19, 2006: STRINGER. MISREPAIRED. PREVIOUS REPAIR BULK CARGO UNDER FLOOR STRINGER 49 LT HAS A STRINGER REPAIR BETWEEN FRAMES 65 AND 66 WITH 1 STRINGER SECTION AND 1 REPAIR SPLICE PREVIOUSLY INST
- [SDR 06FDEA04029](https://openairdocs.org/sdr/06FDEA04029), Nov 19, 2006: SKIN. MISREPAIRED. PREVIOUS REPAIR BULK CARGO DOOR EXTERIOR SKIN HAS AN EXTERNAL REPAIR DOUBLER MEASURING 6.25" BY 15.1" AT THE LOWER AFT CORNER PREVIOUSLY INSTALLED REPAIR LOCATE
- [SDR 06FDEA04028](https://openairdocs.org/sdr/06FDEA04028), Nov 19, 2006: FRAME. DAMAGED. UPON REMOVAL OF WEB RT BETWEEN FS 12 AND FS 13 3 HOLES ARE ELONGATED DOUBLE DRILLED FLOOR LEVEL AT FS 13 REPAIRED FRAME AT FS 13 RT IAW A310SRM 53-12-13 FIG 201
- [SDR 06FDEA04027](https://openairdocs.org/sdr/06FDEA04027), Nov 19, 2006: FRAME. DAMAGED. UPON REMOVAL OF WEB BETWEEN FS 12 - FS 13 FOUND 3 HOLES ELONGATED DOUBLE DRILLED FLOOR LEVEL LT SIDE AT FS 13 REPAIRED FRAME AT FS-13, IAW A310 SRM 53-12-31 FIG
- [SDR 06FDEA03902](https://openairdocs.org/sdr/06FDEA03902), Nov 6, 2006: SPAR. CORRODED. AFTER REMOVAL OF LEADING EDGE OF LT HORIZONTAL STAB, FOUND CORROSION ON UPPER CHORD OF FORWARD SPAR NEAR RIB 10 REMOVED CORROSION IAW A310 SRM 51-74-10, CHECKED
- [SDR 06FDEA02276](https://openairdocs.org/sdr/06FDEA02276), Jun 8, 2006: TRUNNION. CRACKED. FOUND LT GEAR AFT TRUNNION FWD SUPPORT FITTING CRACKED WHILE PERFORMING GEAR LUBE DURING B CHECK. AIRBUS FIELD TEAM REMOVED AND REPLACED LT GEAR TRUNNION.
- [SDR 06FDEA2276](https://openairdocs.org/sdr/06FDEA2276), Jun 8, 2006: SUPPORT FITTING. CRACKED. FOUND LEFT GEAR AFT TRUNNION FWD SUPPORT FITTING CRACKED WHILE PERFORMING GEAR LUBE DURING B-CHECK.
- [SDR 04FDEA02081](https://openairdocs.org/sdr/04FDEA02081), Jul 15, 2004: PANEL. DAMAGED. PANEL 550HB HAS 2 EA ELONGATED HOLES. REPAIRED 1 EA HOLE IAW A310/200 SRM 51-40-44 FIG 1 CHAMBER CODE-J, COMPLIED WITH EA 6-5730-55328A PT 1 ON 1EA HOLE.
- [SDR 04FDEA02080](https://openairdocs.org/sdr/04FDEA02080), Jul 15, 2004: PANEL. DAMAGED. PANEL LAND 650 KB HAS 1 EA ELONGATED HOLE. COMPLIED WITH EA 6-5730-55328A PT1.
- [SDR 01FDEA00057](https://openairdocs.org/sdr/01FDEA00057), Jan 31, 2001: IDG. INOPERATIVE. DURING CLIMBOUT, NR 2 IDG TEMP CONT TO CLIMB. VERIFIED NR 2 IDG DEFERRED CORRECTLY. VERIFIED PROPER SERVICE ACCOMPLISH. NO FAULTS NOTED. IDG TEMP WITHIN LIMITS 
- [SDR 00FDEA00794](https://openairdocs.org/sdr/00FDEA00794), Nov 29, 2000: INDICATOR. ILLUMINATED. REJECTED T/O DUE TO AN OIL PRESSURE LIGHT ILLUMINATED ON NR 1 ENGINE.
- [SDR 00FDEA00724](https://openairdocs.org/sdr/00FDEA00724), Oct 19, 2000: CONTROLLER. FAILED. NR 1 CABIN PRESSURE FAILED AFT T/O, SEL NR 2 CABIN PRESSURE AC FAILED TO PRESSURIZE.
- [SDR 00FDEA00236](https://openairdocs.org/sdr/00FDEA00236), Apr 12, 2000: DAMPER. FAILED. AFT TO LANDING GEAR WOULD NOT RETRACT IN SYS 1 OR 2. RECYCLED TWICE EACH SYS. REMOVED AND REPLACED RT MLG PITCH DAMPER IAW AMM 32-11-15. OPS CK PER IAW AMM 32-3
- [SDR 00FDEA00214](https://openairdocs.org/sdr/00FDEA00214), Apr 9, 2000: LANDING GEAR. MALFUNCTIONED. LANDING GEAR WON''T RETRACT. SERVICE RT PITCH DAMPER AND REPLACED PRESSURE DROP IND PER FEDEX AC MX WORK CARD NR 47B402.
- [SDR 99FDEA00514](https://openairdocs.org/sdr/99FDEA00514), Dec 29, 1999: COMPUTER. INOPERATIVE. 99-297 - ECAM AND MASTER SHOW CHECK FUEL MGMT. REMOVED AND REPLACED FUEL QTY COMPUTER PERFORM BITE CK.
- [SDR 99FDEA00439](https://openairdocs.org/sdr/99FDEA00439), Oct 21, 1999: SWITCH. OUT OF ADJUST. NR 1 ENG REV UNLOCK LIGHT CAME ON AT APPROX 55 KTS ON T/O ROLL. ABORTED T/O. NR 1 THRUST REVERSER WAS DEFERRED MEL 78-1 CTRL NR 61783. ADJUSTED STOW SWITCHES PE
- [SDR 99FDEA00367](https://openairdocs.org/sdr/99FDEA00367), Sep 7, 1999: FITTING. CRACKED. TWO MAIN CROSSBEAMS THAT RUN ACROSS THE LANDING GEAR BAY AND HOLD BOTH MLG DOOR ACTUATORS UPPER ATTACH ARE BROKEN. RT MLG DOOR ACTUATOR ATTACH FITTING WAS PULLE
- [SDR 98FDEA00048](https://openairdocs.org/sdr/98FDEA00048), Jan 26, 1998: HYD ELEC PUMP. SHORTED. BURNT 101 VU WIRING CAUSED BY GREEN HYDRAULIC PUMP INTERNALLY SHORTED. C/B DID NOT POP. THIS CAUSED WIRING BEHIND 101 VU PANEL TO SMOKE AND BURN UP. REPLACED GR

## FAA accident and incident reports (2)

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 20040213002429I](https://openairdocs.org/incident/20040213002429I), Feb 13, 2004: Airbus A310222 (N449FE), Indianapolis, IN, Minor damage. (-23) On landing roll out between approx 60-80 knots crew observed a flash on l/h side of a/c. after exiting runway they were informed by the tower that the #1…
- [Incident 20020926026599I](https://openairdocs.org/incident/20020926026599I), Sep 26, 2002: Airbus A310222 (N449FE), Burbank, CA. (-23) Federal express flight 1417 landed at Burbank airport on 9/26/02. On rollout the Burbank tower reported to the aircrew that the number one engine was on…

## Other aircraft with N449FE

- [Cancelled 2022-05-14](https://openairdocs.org/deregistered/N449FE-2022-05-14): Dehavilland DHC-8-102, S/N 128. First renewal notice. Owner: [Dynamic Avlease Inc](https://openairdocs.org/faa-owner/DYNAMIC%20AVLEASE%20INC), [Bridgewater, VA](https://openairdocs.org/faa-place/VA/Bridgewater)

---
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.