# N418FE: 1985 Airbus Industrie A310-222, registration cancelled 2016-02-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 18, 2016 - Status when cancelled: Valid registration - Airframe: [Airbus Industrie A310-222](https://openairdocs.org/model/airbus-industrie-a310-222) (registry code 3930315) - Engine: [Pratt & Whitney JT9D-3A](https://openairdocs.org/engine/pratt-whitney-jt9d-3a) (registry code 52050) - Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU), [TCDS E20EA](https://openairdocs.org/tcds/E20EA) (OpenAirDocs) - Serial number: 343 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 14, 1999 - Certificate issued: July 28, 1995 - Last registry action: June 19, 2014 - Mode S code: A4F25A - 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/N418FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=418FE - Page: https://openairdocs.org/deregistered/N418FE-2016-02-18 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 (29) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FDEA201204131398](https://openairdocs.org/sdr/FDEA201204131398), Apr 13, 2012: VALVE. INOPERATIVE. PASSING 10000 FT, RECEIVED ECAM ALERT ROR EXCESS CABIN ALTITUDE, ALSO OBSERVED ECAM ADVISORY FOR EXCESS CABIN VERTICAL SPEED (APPROX 3800') CLIMB. TRIED CONTROL - [SDR FDEA201111235007](https://openairdocs.org/sdr/FDEA201111235007), Nov 23, 2011: LANDING GEAR. MALFUNCTIONED. NOSE GEAR WOULD NOT EXTEND USING NORMAL PROCEDURES, INDICATED UNLOCKED ON BOTH PRIMARY AND SECONDARY INDICATORS USED ALTERNATE PROCEDURE TO EXTEND. EMERGENCY WA - [SDR FDEA201010023862](https://openairdocs.org/sdr/FDEA201010023862), Oct 2, 2010: SKIN. CORRODED. RIGHT ELEVATOR UPPER SKIN AFT EDGE FOUND CORROSIN. REMOVE TOP SKIN UNTIL THE REAR SPAR. PERFORM SRM 55-21-11 CONG-1 FIG 209 WITH THE FOLLOWING PROVISIONS: INSTA - [SDR FDEA201009093324](https://openairdocs.org/sdr/FDEA201009093324), Sep 9, 2010: SLEEVE. OUT OF POSITION. ADVANCING THROTTLES FOR TAKEOFF, RECEIVED A ENG 2 BLEED LEAK. FACT OPEN NR 2 ENG COWLS AND INSPECTED FOUND NO EVIDENCE OF BLEED LEAK WITH APU AIR. REMOVED RT WI - [SDR FDEA201006222111](https://openairdocs.org/sdr/FDEA201006222111), Jun 22, 2010: UPLOCK. DAMAGED. AFTER TAKEOFF RECEIVED LANDING DOOR NOT CLOSED ECAM. CONFIRMED IT WAS THE NOSE FEAR DOOR (AMBER ON BOTH LANDING GEAR PANELS), IAW MX INSTRUCTION, RECYCLED GEAR, - [SDR 08FDEA04623](https://openairdocs.org/sdr/08FDEA04623), Oct 30, 2008: MOUNT. CORRODED. AFT MOUNTING MATING SURFACE ON NR 2 ENGINE PYLON RUSTED. PERFORMED REPAIR AS PER EA NR 6-5450-125471 PART 2. - [SDR 08FDEA04624](https://openairdocs.org/sdr/08FDEA04624), Oct 30, 2008: FITTING. CORRODED. AFT MOUNTING MATING SURFACE ON NR 1 ENGINE PYLON RUSTED. PERFORMED REPAIR AS PER EA 6-5450-125471 PART 2. - [SDR 08FDEA04465](https://openairdocs.org/sdr/08FDEA04465), Oct 21, 2008: ARM. CRACKED. EMPENNAGE, RT ELEV NR 5 HINGE ARM FOUND CRACKED/CORROSION AT UPPER END REPLACED RT ELEV NR 5 HINGE ARM AS PER AMM 55-16-45-4. - [SDR 08FDEA04464](https://openairdocs.org/sdr/08FDEA04464), Oct 21, 2008: SKIN. DELAMINATED. LT WING, INBD FLAP TRAILING EDGE UPPER SURFACE PREVIOUS REPAIR LOCATED 44.0 INCH FROM OTBD EDGE DELAMINATED APPROX 3.0 BY 3.0 IN SIZE. REMOVED EXISTING REPAIR B - [SDR 08FDEA04463](https://openairdocs.org/sdr/08FDEA04463), Oct 21, 2008: SKIN. DELAMINATED. RT WING, INBD FLAP TRAIL EDGE LWR SURFACE PREVIOUS REPAIR LOCATED 17.0 INCHES FROM INBD EDGE, DELAMINATED APPROX 22.0 BY 3.0 INCHES IN SIZE. REMOVED THE EXISTIN - [SDR 08FDEA04462](https://openairdocs.org/sdr/08FDEA04462), Oct 21, 2008: SKIN. DELAMINATED. LT WING, INBD FLAP TRAIL EDGE LWR SKIN PREVIOUS REPAIR LOCATED 54.5 INCHES FROM INBD EDGE DELAMINATED APPROX 3.0 BY 3.0 INCHES IN SIZE. REMOVED THE EXISTING REP - [SDR 08FDEA04449](https://openairdocs.org/sdr/08FDEA04449), Oct 20, 2008: LUG. CORRODED. WHILE COMPLYING WITH EO 6-5710-7-5010 CORROSION WAS FOUND ON BOTH LEFT AND RIGHT WING RIB 5 FORWARD LUG. COMPLIED WITH EA 6-5710-125482 IN THE REMOVAL OF CORROS - [SDR 07FDEA02433](https://openairdocs.org/sdr/07FDEA02433), Jul 10, 2007: REGULATOR VALVE. FAILED. ENG 1 REV UNLOCK LIGHTS ILLUMINATED ON T/O ROLL LESS THAN 80KTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C 11JUL SFS. REMOVED AND REPLACED ENG 1 PRSOV, P - [SDR 07FDEA02411](https://openairdocs.org/sdr/07FDEA02411), Jul 10, 2007: UNKNOWN. UNKNOWN. UNLOCK LIGHTS ILLUMINATED ON T/O ROLL, LESS THAN 80KTS. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 20JUL07 "MEL 78-30-01-C: ENGINE (ID - [SDR 06FDEA04174](https://openairdocs.org/sdr/06FDEA04174), Dec 5, 2006: SKIN. DAMAGED. R-WING NR 4 SPOILER PANEL CENTER I/B HINGE AND O/B HINGE HAS WORN BUSHING. EXCESSIVE PLAY DURING MOVEMENT OF PANEL REMOVED AND REPLACED NR 4 RT WING SPOILER BUS - [SDR 06FDEA04130](https://openairdocs.org/sdr/06FDEA04130), Nov 28, 2006: FRAME. DAMAGED. WHILE WORKING LT FS 12A DUE TO TOOLING MALFUNCTION DAMAGE TO FRAME 12A APPROX STR 29 COMPLIED WITH EA6-5310-105011. - [SDR 06FDEA04129](https://openairdocs.org/sdr/06FDEA04129), Nov 28, 2006: SKIN. UNKNOWN. PREVIOUS REPAIR, RT FUSELAGE SKIN HAS EXTERNAL REPAIR DOUBLER MEASURES 8.3 IN X 5.5 IN, LOCATED AT FS 77 BETWEEN STRINGERS 52RT AND 54R REMOVED EXISTING REPAIR - [SDR 06FDEA04091](https://openairdocs.org/sdr/06FDEA04091), Nov 22, 2006: RIB. CORRODED. VERTICAL STAB FRONT SPAR FWD FACE ENTIRE LENGTH OF RT VERT STAB L/E HAS CORROSION UNDER NUT PLATES AND FASTENER HOLES. REMOVED CORROSION FROM RIB12-26 RT CHORD - [SDR 06FDEA2855](https://openairdocs.org/sdr/06FDEA2855), Aug 6, 2006: ENGINE. BIRD INGESTION. FELT A JULT ON T/O. SUSPECT COMPRESSOR STALL. CHECKED PER MM 72-00-00-6 03 AND FOUND BIRD STRIKE AT NR 2 ENGINE. COMPLIED ITEM 13B. NOTED NO ABNORMALITIES. ENGI - [SDR 05FDEA02690](https://openairdocs.org/sdr/05FDEA02690), Aug 26, 2005: FIRE LOOP. MALFUNCTIONED. REPLACED FIRE DET ASSY (H2/H4) FOR BOTH LOOP A AND B, THIS ALSO CLEARED MEL ON "A" LOOP WRI 26-10/9082 PER MM 26-12-12-4. OPS CHECK SATIS AND PERFORMED ENG RUN - [SDR 04FDEA02875](https://openairdocs.org/sdr/04FDEA02875), Oct 5, 2004: FITTING. CRACKED. MOD TYPE H MOD NR C-CHECK REV NO, PS ACCOMPLISH MAINTENANCE C-CHECK NR 004. DURING C-CHECK WHILE ACCOMPLISHING EO 6-5710-7-3322 FOUND CRACK AT FWD FITTING FRAME - [SDR 04FDEA00390](https://openairdocs.org/sdr/04FDEA00390), Feb 10, 2004: THRUST REVERSER. OUT OF RIG. ON TAKEOFF ROLL, JUST AFTER TOGA AND BEFORE STANDARD PWR WAS SET NR 2 THRUST REVERSER UNLOCK LIGHT ILLUMINATED ON LEFT ECAM SCREEN. ABORTED T/O COMPLIED WITH QR - [SDR 01FDEA01040](https://openairdocs.org/sdr/01FDEA01040), Dec 7, 2001: CROSSBEAM. CRACKED. MAIN DECK CARGO FLOOR CROSSBEAM DAMAGED AT BS 37 BETWEEN LBL 26.5 & 37.5. R&R CROSSBEAM PER SRM 53-10-15 FIG 201. - [SDR 00FDEA00617](https://openairdocs.org/sdr/00FDEA00617), Sep 2, 2000: FLOORBEAM. CRACKED. FRAME 37 AT AXIS LHS Y + 1800, .5 INCH BELOW UPPER FLANGE, FOUND CRACK .5 INCH LONG. *S/D* REMOVED AND REPLACED PER FEDEX EA 6-5100-52045 & A310 SRM SUPL MANUAL - [SDR 00FDEA00463](https://openairdocs.org/sdr/00FDEA00463), Jul 18, 2000: SKIN. DENTED. THREE OFF DENTS IN FUSELAGE SKIN, RHS FWD OF BULK CARGO DOOR CUTOUT DURING C-CHECK. REPAIRED IN ACCORD WITH FEDEX EA REF EA 6-5330-49662. - [SDR 00FDEA00030](https://openairdocs.org/sdr/00FDEA00030), Jan 20, 2000: UNKNOWN. SMOKE. 00-17 - UPON TAXI OUT, ODOR OF SMOKE FILLED THE COCKPIT, RETURN TO RAMP. WHEN NR 2 ENGINE WAS SHUT DOWN, THE ODOR WAS GONE. PERF FAULT CONFIRM AND RESTARTED NR - [SDR 99FDEA00210](https://openairdocs.org/sdr/99FDEA00210), Jun 10, 1999: SMOKE DETECTOR. FAILED. 99-129 AT 17,000 MSL, LT ECAM RED/CRC AVIONICS SMOKE NOT NOTICABLE FUMES/ODORS. REMOVED AND REPLACED 13WA SMOKE DETECTOR PER MM 26-15-12. OPS CK GOOD MM A310-26 - [SDR 98FDEA00120](https://openairdocs.org/sdr/98FDEA00120), Feb 18, 1998: SMOKE DETECTOR. DEFECTIVE. APPROACHING LEVEL OFF AT FL 370, FWD CARGO COMPT SMOKE LIGHT AND ASSOC ECAM CAUTIONS ACTIVATED. NR 1 BOTTLE WAS DISCHARGED AND NR 2 BOTTLE WAS ACTIVATED ON APPR - [SDR 96FDEA01238](https://openairdocs.org/sdr/96FDEA01238), Jul 11, 1996: HYD LINE. LEAKING. STA KHH LOST GREEN HYD SYS DURING DESCENT PERFOMED ECAM ITEMS. WHEN A/C ARRIVED CK'D GREEN RSVR QTY AND FOUND LOWER THAN HAT ARC. T/S FOUND HYD FLUID LEAKING FR --- 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.