# N455FE: Airbus Industrie A310-222, registration cancelled 2024-02-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 3, 2024
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A310-222](https://openairdocs.org/model/airbus-industrie-a310-222) (registry code 3930315)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (OpenAirDocs)
- Serial number: 331
- Type of aircraft: Fixed wing multi engine
- Certificate issued: January 30, 2003
- Last registry action: August 4, 2023
- Mode S code: A58531
- 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/N455FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=455FE
- Page: https://openairdocs.org/deregistered/N455FE-2024-02-03

From the FAA registry file of October 31, 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 (144, newest 50)

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

- [SDR FDEA201504101202](https://openairdocs.org/sdr/FDEA201504101202), Apr 10, 2015: COMPENSATOR. FAILED. DURING APPROACH, 2000 & 6 MILES, THE HOT BRAKE LIGHT IN THE CUBE ON THE LG TEST PANEL FLICKERED, FOLLOWED BY ECAM HOT BRAKE WARNINGS FOR ALL 4 WHEELS ON THE LT 
- [SDR FDEA201409102582](https://openairdocs.org/sdr/FDEA201409102582), Sep 10, 2014: ACTUATOR. FAILED. UPON GEAR RETRACTION, RECEIVED A LT MAIN GEAR RED UNLOCK INDICATION WITH AN AMBER LT DOOR LIGHT. COMPLIED WITH ECAM EXTENDED GEAR & LANDED. WE DID HAVE A LOUD W
- [SDR FDEA201408212293](https://openairdocs.org/sdr/FDEA201408212293), Aug 21, 2014: SEQUENCE VALVE. FAULTY. DURING CLIMB OUT AT GEAR RETRACTION, LT MAIN GEAR DID NOT APPEAR TO RETRACT & DOOR SHOWED OPEN. ECAM INDICATED LG RETRACTION INOPERATIVE. FUEL CONSUMPTION INCRE
- [SDR FDEA201405221136](https://openairdocs.org/sdr/FDEA201405221136), May 22, 2014: VALVE. FAILED. NR 1 SLAT SYS FAULT LIGHT DURING FINAL. RECYCLING DID NOT CORRECT, QRH PROCEDURES ACCOMPLISHED. SLAT FAULT LIGHT REMAINED ON, BUT SPFI SHOWED SLATS & FLAPS 30 &
- [SDR FDEA201403050452](https://openairdocs.org/sdr/FDEA201403050452), Mar 5, 2014: SWITCH. FAILED. ACCELERATING ABOVE 10,000 & 250 KTS, NR 1 ENGINE THRUST REVERSER UNLOCK ILLUMINATED STEADY. ALL OTHER INDICATIONS NORMAL. TROUBLESHOT IAW TSM 78-31-00, FOUND TH
- [SDR FDEA201305090953](https://openairdocs.org/sdr/FDEA201305090953), May 9, 2013: BRAKE SYS. MALFUNCTIONED. ACFT LOST BRAKES. THEY HAD WORKED NORMALLY ON INITIAL TAXI AND HOLD SHORT CROSSING RWY 27. APPROACHING 36C ON TAXIWAY D, GOT NO BRAKING WITH NORMAL. RELEASED BR
- [SDR FDEA201303130565](https://openairdocs.org/sdr/FDEA201303130565), Mar 13, 2013: VALVE. MALFUNCTIONED. LANDING GEAR FAILED TO EXTEND IN POSITION NR 1 OR NR 2. COMPLIED W/ QRH - MANUAL EXTENSION OK. EMERGENCY DECLARED. T/S IAW TSM 32-61-00. PREFORMED BITE TEST PRO
- [SDR FDEA201212044242](https://openairdocs.org/sdr/FDEA201212044242), Dec 4, 2012: SHUTOFF VALVE. MALFUNCTIONED. DURING CLIMBOUT PASSING 10000 FT, ECAM INDICATED THRUST REV NR 1 UNLOCKED. THIS INDICATION CYCLED IN AND OUT MULTIPLE TIMES. NO OTHER ENGINE INDICATIONS PRESENT
- [SDR FDEA201210133610](https://openairdocs.org/sdr/FDEA201210133610), Oct 13, 2012: HANDLE. STICKING. AS POWER WAS INCREASING AFTER TOGA ON TAKE OFF, RECEIVED A CRC FOR "PARKING BRAKE SET" EVEN THOUGH PARKING BRAKE HANDLE WAS DOWN. SECOND TAKE OFF ATTEMPT OK. IN
- [SDR FDEA201205312039](https://openairdocs.org/sdr/FDEA201205312039), May 31, 2012: PRESSURE SWITCH. FAILED. DESCENDING OUT OF FL310 WE GOT AN OIL CLOG LIGHT ON NR 1 ENGINE. COMPLIED WITH PROCEDURES, SHUTDOWN NR 1 ENGINE. ALL OIL PRESSURES INDICATED NORMAL BEFORE AFTER
- [SDR FDEA201112085220](https://openairdocs.org/sdr/FDEA201112085220), Dec 8, 2011: OIL SYSTEM. LOW PRESSURE. YELLOW OIL PRESSURE LIGHT ILLUMINATED DURING TAKE OFF ROLL AT 110 KTS. ABORTED TAKE OFF, COMPLIED WITH QRH. RAN ENGINES AT POWER, OIL PRESSURE STAYED AT 52 PSI 
- [SDR FDEA201110194576](https://openairdocs.org/sdr/FDEA201110194576), Oct 19, 2011: TRANSMITTER. INOPERATIVE. DURING T/O ROLL THE HIGH OIL PRESSURE (NR 1) ENG, CAME ON AT 80 KTS. R & R THE NR 1 ENG OIL PRESS TRANSMITER IAW MM 79-33-11-04, RAN ENG IAW JRH, CHECKS GOOD. A
- [SDR FDEA201110064343](https://openairdocs.org/sdr/FDEA201110064343), Oct 6, 2011: HMU. FAILED. ON TAKEOFF, NR 2 ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. R & R NR 2 ENGINE HMU IAW AMM 73-21-01-04. CHECKED GOOD. PERFORMED IDLE LEAK CHECK AND POWER TRI
- [SDR FDEA201109274156](https://openairdocs.org/sdr/FDEA201109274156), Sep 27, 2011: WIRE HARNESS. DAMAGED. REJECTED T/O, SET BOTH ENGINES TO 40 PERCENT N1, TOGA'D AND ENGINE NR1 IMMEDIATELY POWERED UP AND ENGINE 2 STOPPED ACCELERATING AT 50 PERCENT N1. MADE 2ND ATTEM
- [SDR FDEA201107012523](https://openairdocs.org/sdr/FDEA201107012523), Jul 1, 2011: SELECTOR VALVE. MALFUNCTIONED. LANDING GEAR WOULD NOT EXTEND NORMALLY AFTER GEAR HANDLE PLACED IN DOWN POSITION. MANUALLY EXTENDED GEAR. QRH COMPLIED WITH, UNEVENTFUL LANDING MADE. R & R LAND
- [SDR FDEA201105111801](https://openairdocs.org/sdr/FDEA201105111801), May 11, 2011: LATCH. MALFUNCTIONED. CLIMBING THRU FL 310 ECAM INDICATED "R FWD CABIN DOOR NOT CLOSED". CABIN PRESSURIZATION INCREASED RATE OF CLIMB FROM 300-400 FPM TO 800 FPM AND CABIN ALTITUDE W
- [SDR FDEA201102080502](https://openairdocs.org/sdr/FDEA201102080502), Feb 8, 2011: SELECTOR VALVE. INOPERATIVE. LANDING GEAR WOULD NOT EXTEND WHEN HANDLE WAS PLACED DOWN. PERFORMED "GRAVITY EXTENSION" IAW QRH. EMERGENCY DECLARED AND ACFT WAS STOPPED ON THE RUNWAY BECAUSE 
- [SDR FDEA201101250353](https://openairdocs.org/sdr/FDEA201101250353), Jan 25, 2011: FLAP SYSTEM. MALFUNCTIONED. GOT FLAP VANE JAM AND FLAP FAULT ECAM INDICATIONS WHILE EXTENDING FLAPS. THEY STUCK AT LESS THAN 15 DEGREE (APPROX 5 DEGREE). CYCLE TO NO AVAIL WENT AROUND AND 
- [SDR FDEA201101100184](https://openairdocs.org/sdr/FDEA201101100184), Jan 10, 2011: CABLE. GOUGED. NR1 PYLON LOWER SIDE OF NACELLE LT & RT THRUST REVERSER INTERLOCK CABLES GOUGED THRU CABLE INSULATION. MARKED, R & R NR1 PYLON LT INTERLOCK CABLE IAW AMM 76-11-
- [SDR FDEA201012174712](https://openairdocs.org/sdr/FDEA201012174712), Dec 17, 2010: DOOR FRAME. GOUGED. LT MLG DOOR TOP AFT INNER MATING SURFACE IS GOUGED. REMOVED GOUGE AND FOUND TO BE OUT OF LIMITS. MATERIAL LOSS 0.022 FROM 0.078., 0.056 MATERIAL REMAINING. FABB
- [SDR FDEA201012154690](https://openairdocs.org/sdr/FDEA201012154690), Dec 15, 2010: TEE FITTING. CRACKED. BULK CARGO DOOR TEE PROFILE IS CRACKED AT FRAME 68, BEAM 3. REMOVED TEE PROFILE REF SRM 51-40-21, PARA 6. MACHINED NEW TEE PROFILE REF DWG A52378044. LOCATED HO
- [SDR FDEA201012094623](https://openairdocs.org/sdr/FDEA201012094623), Dec 9, 2010: BRACKET. CRACKED. BULK CARGO DOOR STAY BRACKET IS CRACKED AT FRAME 68, BEAM 3. ACQUIRED MATERIAL ID FOR NEW STAY BRACKET IAW SRM 52-34-00, PO 680480.1. FORMED NEW STAY IAW SRM 51
- [SDR FDEA201011304517](https://openairdocs.org/sdr/FDEA201011304517), Nov 30, 2010: ANGLE. CRACKED. NR1 PYLON ACCESS PANEL 475 AL (STRINGER), RT SIDE, CTR SECTION OF PANEL "T" ANGLE IS CRACKED. REMOVED CRACKED FRAME AND FABBED NEW FRAME FROM 0.063, 2024-0, PO 
- [SDR FDEA201011294512](https://openairdocs.org/sdr/FDEA201011294512), Nov 29, 2010: STOP FITTING. CRACKED. RT AFT PAX / CREW DOOR STOP FITTING IS CRACKED AT THE INBD LOWER FASTENER; LOWER AFT DOOR FRAME STOP FITTING IN THE DOOR CUTOUT. REPLACED RT AFT PAX DOOR STOP F
- [SDR FDEA201011154367](https://openairdocs.org/sdr/FDEA201011154367), Nov 15, 2010: FLOOR SUPPORT. CRACKED. FWD PIT, AFT FLOOR SUPPORT, RT SIDE IS CRACKED BETWEEN FRAME 38.2 AND FRAME 39. REMOVED AND REPLACED AFT FLOOR SUPPORT, R/H SIDE AT FRAME 38.2 IAW SRM 51-40-21,
- [SDR FDEA201011124324](https://openairdocs.org/sdr/FDEA201011124324), Nov 12, 2010: PRESSURE PANEL. CORRODED. FWD CARGO COMPARTMENT HORIZ PRESSURE DECK UPPER SURFACE AT FRAME 40/41 IS CORRODED AT THE SPLICE. REPAIRED PER FEDEX EA 6-5310-136722, TITLE " FUSELAGE - PRESSU
- [SDR FDEA201011104306](https://openairdocs.org/sdr/FDEA201011104306), Nov 10, 2010: FITTING. CORRODED. NR1 ENGINE PYLON SPIGOT RECEPTICAL FITTING BALL JOINT FLANGE IS PITTED AT THE UPPER AND LOWER PLATES INCLUDING THE BEARING BORE. COMPLIED WITH EA 6-5450-136723;
- [SDR FDEA201011104305](https://openairdocs.org/sdr/FDEA201011104305), Nov 10, 2010: FITTING. CORRODED. NR 2 ENG PYLON SPIGOT RECEPTICAL FITTING BALL JOINT FLANGE IS PITTED AT THE UPPER AND LOWER FLANGE PLATES INCLUDING THE BEARING BORE. COMPLIED WITH EA 6-5450-13
- [SDR FDEA201011084276](https://openairdocs.org/sdr/FDEA201011084276), Nov 8, 2010: SIDEWALL PANEL. DENTED. BULK CARGP COMPARTMENT SIDEWALL PANEL 161 AW HAS MULTIPLE DENTS AND IS PUNCTURED ON THE FRONT. FABRICATED NEW SIDEWALL PANEL 161 AWIAW FEDEX DWG 25-005, REV "H"
- [SDR FDEA201011084281](https://openairdocs.org/sdr/FDEA201011084281), Nov 8, 2010: FLOORBOARD. DAMAGED. MAIN CABIN FLOORBOARD UPPER SKIN IS CRUSHED AND BROKEN FROM FRAME 60 TO FRAME 62, RBL 57 TO RBL 77. FABRICATED NEW FLOORBOARD 252 UF IAW DWG 25-005, REV "H".
- [SDR FDEA201011084280](https://openairdocs.org/sdr/FDEA201011084280), Nov 8, 2010: FLOORBOARD. DAMAGED. MAIN DECK FLOORBOARD BETWEEN FRAME 53 AND FRAME 54, LBL 78 AND LBL 98 IS BROKEN OFF AT THE AFT END. FABRICATED NEW FLOOR PANEL IAW DWG 25-005, REV "H".
- [SDR FDEA201011084279](https://openairdocs.org/sdr/FDEA201011084279), Nov 8, 2010: FLOORBOARD. DAMAGED. AFT CARGO FLOORBOARD 151 FF HAS A BROKEN CORNER. FABRICATED NEW FLOORBOARD 151 FF IAW DWG 25-005, REV "H".
- [SDR FDEA201011084278](https://openairdocs.org/sdr/FDEA201011084278), Nov 8, 2010: FLOORBOARD. TORN. FWD CARGO COMPARTMENT FLOORBOARD 132 QF IS TORN AND PUNCTURED. FABRICATED NEW FLOORBOARD 132 QF IAW DWG 25-005, REV "H".
- [SDR FDEA201011084277](https://openairdocs.org/sdr/FDEA201011084277), Nov 8, 2010: FLOOR PANEL. DENTED. BULK CARGO COMPARTMENT FLOOR PANEL 162 HF TOP SURFACE IS DENTED AND CRUSHED. FABRICATED NEW FLOOR PANEL 162 HF IAW DWG 25-005, REV "H" AND DWG 25-011, REV "C".
- [SDR FDEA201011084275](https://openairdocs.org/sdr/FDEA201011084275), Nov 8, 2010: PANEL. CORRODED. BULK CARGO COMPARTMENT SIDEWALL PANEL 162 AW BOTTOM SKIN IS CORRODED AND BOTH SKINS ARE DISBONDED. FABRICATED NEW SIDEWALL PANEL 162 AW IAW DWG 25-005, REV "H" 
- [SDR FDEA201011084274](https://openairdocs.org/sdr/FDEA201011084274), Nov 8, 2010: PANEL. DAMAGED. BULK CARGO COMPARTMENT SIDE WALL PANEL 162 CW HAS MULTIPLE DENTS ON THE TOP SURFACE. FABRICATED NEW SIDEWALL PANEL 162 CW IAW DWG 25-005, REV "H" AND DWG 25-011
- [SDR FDEA201011054263](https://openairdocs.org/sdr/FDEA201011054263), Nov 5, 2010: ATTACH FITTING. CORRODED. LT MLG DOOR ACTUATOR ATTACH FITTING IS CORRODED. REMOVED WORN JACK FITTING REF SRM 51-40-21, PAPR 7. INSTALLED NEW JACK FITTING REF SRM 51-40-21, PAPR 7. ALODIN
- [SDR FDEA201011044252](https://openairdocs.org/sdr/FDEA201011044252), Nov 4, 2010: SKIN. CORRODED. FUSELAGE INTERNAL STRUCTURE FWD CARGO COMPARTMENT AFT DOOR CUTOUT AT THE LOWER CORNER, THE SKIN IS CORRODED FROM FRAME 26 TO FRAME 27, STR 25R TO STR 26R.
- [SDR FDEA201011024207](https://openairdocs.org/sdr/FDEA201011024207), Nov 2, 2010: FLOOR PANEL. DELAMINATED. MLG BAY CTR OTBD FLOOR PANEL IS DELAMINATED AT THE EDGE. REMOVED OLD PANEL 148 BF REF SRM 51-40-21, PARA 5. FABBED NEW MLG OTBD FLOOR PANEL 148 BF IAW DWG SRZ 2
- [SDR FDEA201011024221](https://openairdocs.org/sdr/FDEA201011024221), Nov 2, 2010: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 252 PH IS CRACKED. FABRICATED NEW FLOOR PANEL 252 PH IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024220](https://openairdocs.org/sdr/FDEA201011024220), Nov 2, 2010: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 232 YH IS CRACKED. FABRICATED NEW FLOOR PANEL 232 YH IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024219](https://openairdocs.org/sdr/FDEA201011024219), Nov 2, 2010: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 252 BF IS CRACKED. FABRICATED NEW FLOOR PANEL 252 BF IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024218](https://openairdocs.org/sdr/FDEA201011024218), Nov 2, 2010: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 252 UH IS CRACKED. FABRICATED NEW FLOOR PANEL 252 UH IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024217](https://openairdocs.org/sdr/FDEA201011024217), Nov 2, 2010: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 252 GF IS CRACKED. FABRICATED NEW FLOOR PANEL 252 GF IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024216](https://openairdocs.org/sdr/FDEA201011024216), Nov 2, 2010: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 242 EK IS CRACKED. FABRICATED NEW FLOOR PANEL 242 EK IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024215](https://openairdocs.org/sdr/FDEA201011024215), Nov 2, 2010: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 242 ZJ IS CRACKED.
- [SDR FDEA201011024214](https://openairdocs.org/sdr/FDEA201011024214), Nov 2, 2010: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 242 UJ IS CRACKED. FABRICATED NEW FLOOR PANEL 242 UJ IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024213](https://openairdocs.org/sdr/FDEA201011024213), Nov 2, 2010: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 242 QJ IS CRACKED. FABRICATED NEW FLOOR PANEL 242 QJ IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024212](https://openairdocs.org/sdr/FDEA201011024212), Nov 2, 2010: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 231 BH IS CRACKED. FABRICATED NEW FLOOR PANEL 231 BH IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024211](https://openairdocs.org/sdr/FDEA201011024211), Nov 2, 2010: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 231 AH IS CRACKED. FABRICATED NEW FLOOR PANEL 231 AH IAW DWG SRZ 25-005, REV "H".

All 144: https://openairdocs.org/deregistered/N455FE-2024-02-03/reports.md

## 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 20130313005629I](https://openairdocs.org/incident/20130313005629I), Mar 13, 2013: Airbus Industrie A310-222 (N455FE), Omaha, NE, No damage. Landing gear could not be extended using number one or number two system. Emergency extension system used and uneventful landing completed.

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