# N425FE: 1983 Airbus Industrie A310-203, registration cancelled 2016-02-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 18, 2016
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A310-203](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: 264
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 25, 1996
- Certificate issued: July 1, 1996
- Last registry action: June 19, 2014
- Mode S code: A50EB4
- 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/N425FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=425FE
- Page: https://openairdocs.org/deregistered/N425FE-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 A310-203: https://openairdocs.org/model/airbus-industrie-a310-203.md

## Service difficulty reports (303, newest 50)

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

- [SDR FDEA201203130922](https://openairdocs.org/sdr/FDEA201203130922), Mar 13, 2012: HANDLE. DIRTY. FLAP/SLAT HANDLE FAILED TO MOVE PAST 15/0 SETTING ON RETRACTION AND 20/20 SETTING ON LANDING. T/S SFCC FAULTED SUPPLY PSW. PARTS ID ARE FOR T/S, ADDITIONAL PART
- [SDR FDEA201202070508](https://openairdocs.org/sdr/FDEA201202070508), Feb 7, 2012: PIN. MISINSTALLED. AFTER TAKEOFF, FLAP LEVER WOULD NOT RETRACT BEYOND 15/0 POSITION. LEVER WOULD NOT DROP DOWN INTO GATE. SLAT/FLAP POSITION REMAINED AT 15/15. ON APPROACH, FLAPS 
- [SDR FDEA201201130164](https://openairdocs.org/sdr/FDEA201201130164), Jan 13, 2012: SKIN. FAILED. R1 DOOR AFT EXTERNAL SKIN PANEL REQUIRES REMOVAL TO SUPPORT FRAME 16A REPAIR. SKIN PANEL TO BE REPLACED AFTER FRAME 16A REPAIR. R & R R1 AFT EXTERNAL SKIN PANEL
- [SDR FDEA201201110098](https://openairdocs.org/sdr/FDEA201201110098), Jan 11, 2012: FAILSAFE. FAILED. R1 DOOR FAILSAFE RING REQUIRES REMOVAL TO FOM FARME 16A RT FRAME REPAIR. REMOVED FAIL SAFE RING IAW SRM 51-40-21 AND EA 6-5310-135257B. LOCATED AND DRILLED NEW 
- [SDR FDEA201201050027](https://openairdocs.org/sdr/FDEA201201050027), Jan 5, 2012: FRAME. DAMAGED. FRAME 16A RT DAMAED. REMOVED FRAME IAW SRM 51-40-21, PG 1 AND EA 6-5310-135257B. LOCATED AND DRILLED NEW FRAME IAW SRM 51-40-44, PG 9. INSTALLED NEW FRAME IAW S
- [SDR FDEA201201050026](https://openairdocs.org/sdr/FDEA201201050026), Jan 5, 2012: DEPRESSOR. DAMAGED. R1 DOOR FRAME 16A SEAL DEPRESSOR DAMAGED FRAME 16A. REPAIR REMOVED SEAL DEPRESSOR IAW SRM 51-72-10. LOCATED AND DRILLED NEW SEAL DEPRESSOR IAW A310 51-40-44. IN
- [SDR FDEA201107012552](https://openairdocs.org/sdr/FDEA201107012552), Jul 1, 2011: COMPUTER. MALFUNCTIONED. REJECTED TAKEOFF AT APPROX 78 KTS. NR1 ENGINE EXCEEDED THE SELECTED FLEX POWER SETTING N1(101.4). THE NR2 ENGINE ENGINE MOMENTARITLY STABLIZED AT 101.4 N1 THEN 
- [SDR FDEA201012304784](https://openairdocs.org/sdr/FDEA201012304784), Dec 30, 2010: SWITCH. INOPERATIVE. ECAM, FWD CARGO DOOR NOT CLOSED CAME ON AT FL 220 ON DEPARTURE, RAN QRH, CABIN ALT OK, RETURNED TO DEPARTURE, FWD CARGO SWITCH FAULT ECAM CAME ON LATER. R & R F
- [SDR FDEA201009173534](https://openairdocs.org/sdr/FDEA201009173534), Sep 17, 2010: SKIN. DAMAGED. LEFT WING OTBD FLAP LOWER SKIN DISBONDED 7.5 IN LENGTH X 1.5 IN WIDE AT T/E,48 IN INBD FROM OTBD EDGE. REPAIRED LT WING T/E SKIN IAW EA 6-5750-135278 - WINGS - 
- [SDR FDEA201009163513](https://openairdocs.org/sdr/FDEA201009163513), Sep 16, 2010: SEAT TRACK. BENT. SEAT TRACK SCALLOP 9 INCHES AFT OF FRAME 60 THE LOCKING TABS ARE CUT OUT AND 6 INCHES AFT OF FR60 THE LOCKING TABS ARE BENT UP. DAMAGED SEAT TRACK SCALLOPS WERE
- [SDR FDEA201009153424](https://openairdocs.org/sdr/FDEA201009153424), Sep 15, 2010: SKIN. MISREPAIRED. PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LT WING INBD FLAP UPPER SKIN AT RIB 10 TO 11 AND BETWEEEN THE REAR SPAR AND AUXILIARY SPAR ON STRINGERS 6 AND 7 MEAS
- [SDR FDEA201009153423](https://openairdocs.org/sdr/FDEA201009153423), Sep 15, 2010: FRAME. FAILED. PREVIOUS FRAME REPAIR LOCATED IN BULK CARGO COMPARTMENT UNDEFLOOR ON FRAME 67 BETWEEN STRINGERS 43 TO 46 RT HAS A REPAIR AGLE ON AFT SIDE OUTER FLANGE MEASURING
- [SDR FDEA201009113346](https://openairdocs.org/sdr/FDEA201009113346), Sep 11, 2010: SKIN. DENTED. L 2 DOOR EXTERIOR SKIN 20.5 INCHES FROM AFT END OF DOOR SKIN,12.5 INCHES FROM BOTTOM OF DOOR SKIN HAS SM DENT,10 MM W X .014 IN DEEP CUT OUT DAMAGED SECTION OF 
- [SDR FDEA201009113345](https://openairdocs.org/sdr/FDEA201009113345), Sep 11, 2010: CARGO TRACK. CRACKED. MAIN CARGO DECK FLOOR SUPPORT STRUCTURE FR 54.2 RT SIDE NR 5 SEAT TRACK HAS 3.5 INCH CRACK ON LOWER PART OF SEAT TRACK. REMOVED DAMAGED TRACK SECTION BETWEEN FR
- [SDR FDEA201009033253](https://openairdocs.org/sdr/FDEA201009033253), Sep 3, 2010: STRINGER. CORRODED. IN FWD CARGO AT FRONT FACE OF PRESSURE BULKHEAD FR 39 ALL THE WAY TO BOTTOM AND 24 " LT OF BOTTOM CTR THERE IS CORROSION APPROX 8 SQ INCHES AT STRINGER 50L. REM
- [SDR FDEA201009023250](https://openairdocs.org/sdr/FDEA201009023250), Sep 2, 2010: BEAM. CORRODED. LONGITUDENAL BEAM Y953 BETWEEN FR 12A AND FR 14 HAS EXFOLIATION CORROSION IN THE MAIN DECK. REMOVED CORROSION IAW SRM 51-74-10, CHECKED, FOUND OUT OF LIMIT. FAB
- [SDR FDEA201009023249](https://openairdocs.org/sdr/FDEA201009023249), Sep 2, 2010: FLOORBEAM. CRACKED. IN FWD CARGO MAIN DECK FLOORBEAM (FR 37) AT 27 INCHES RT OF CTR LINE. FWD FACE IS A CRACK IN THE UPPER SIDE OF THE BEAM APPROX .7500 INCH LONG REMOVED DAMAGE SE
- [SDR FDEA201008303199](https://openairdocs.org/sdr/FDEA201008303199), Aug 30, 2010: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO COMPT 10 IN AFT OF FR 14 , 57 IN. LT OF CTR LINE FLOOR SUPPORT CHANNEL HAS 4 SQ IN OF LEVEL 1 CORROSION ON UPPER SURFACE OF CHANNEL. REMOVED LEV
- [SDR FDEA201008283167](https://openairdocs.org/sdr/FDEA201008283167), Aug 28, 2010: SEAT TRACK. DAMAGED. MAIN FLOOR SUPPORT FLANGE UPPER SURFACE OF SEAT TRACK GOUGED .5 SQ IN. LOCATED 4 IN FWD OF FR 17 AND 37IN RT OF CTR LINE. BLENDED GOUGE IN MAIN FLOOR SUPPORT FL
- [SDR FDEA201008273165](https://openairdocs.org/sdr/FDEA201008273165), Aug 27, 2010: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO COMPARTMENT 10 IN AFT OF FR 14, 53 IN LT OF C/L FLOOR CHANNEL SUPPORT FOR COURIER SEAT HAS 3 SQ IN OF CORROSION AROUND ANCHOR NUTPLATES TOP SURF
- [SDR FDEA201008273164](https://openairdocs.org/sdr/FDEA201008273164), Aug 27, 2010: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO COMPARTMENT 5 IN AFT OF FR 14, 31 IN LT OF C/L FLOOR SUPPORT UPPER SURFACE HAS 3 SQ IN OF CORROSION. REMOVED LEVEL 1 CORROSION REMOVED DAMAGED F
- [SDR FDEA201008263154](https://openairdocs.org/sdr/FDEA201008263154), Aug 26, 2010: FLOORBEAM. CRACKED. MAIN CARGO DECK FLOOR STRUCTURE FR 54.3 BETWEEN SEAT TRACKS 2R AND 3R HAS 1 EA, .25 " CRACK IN STRUCTURE CROSSBEAM. CUT OUT DAMAGED AREA OF CROSSBEAM IAW SRM 53
- [SDR FDEA201008263153](https://openairdocs.org/sdr/FDEA201008263153), Aug 26, 2010: SEAT TRACK. CORRODED. UPPER DECK FLOOR STRUCTURE BETWEEN FR 18 AND FR19 AT SEATTRACK 2L (Y450) HAS LEVEL 1 CORROSION ON FLANGE UPPER SURFACE APPROX 6 SQ. INCHES, TOTAL CORROSION WAS 
- [SDR FDEA201008263152](https://openairdocs.org/sdr/FDEA201008263152), Aug 26, 2010: SEAT TRACK. DAMAGED. MAIN CARGO DECK FLOOR STRUCTURE FRAME 54.2 SEAT TRACK STRUCTURE 3R HAS 1 EA .1875" DRILL START (MISDRILL). R & R SEAT TRACK 3R IAW SRM 51-72-10 ON MAIN DECK FLO
- [SDR FDEA201008253135](https://openairdocs.org/sdr/FDEA201008253135), Aug 25, 2010: FLOOR SUPPORT. MISREPAIRED. PREVIOUS REPAIR LOCATED ON MAIN CABIN COURIER AREA FLOOR SUPPORT "T" CAP LONGERON RT SIDE BETWEEN FRAMES 12A TO 14, NR5 RT LONGERON FROM CTR- Y1959, HAS 2 EA RE
- [SDR FDEA201008253133](https://openairdocs.org/sdr/FDEA201008253133), Aug 25, 2010: STRINGER. MISREPAIRED. PREVIOUS STRINGER REPAIR LOCATED IN AFT CABIN UNDER FLOOR BEHIND BULK CARGO ON STRINGER 39 LT BETWEEN FRAMES 73 TO 74, HAS 1 EACH REPAIR ANGLE SPLICE 12.6" LONG
- [SDR FDEA201008253132](https://openairdocs.org/sdr/FDEA201008253132), Aug 25, 2010: SKIN. MISREPAIRED. PREVIOUS EXTERNAL LAP SEAM REPAIR LOCATED AT LT SIDE FUSELAGE SKIN AT FRAME 38 AND BETWEEN STRINGERS 42 TO 45 LT. THE REPAIR FILLER MEASURES 8.6" X 23.5" AND TH
- [SDR FDEA201008223089](https://openairdocs.org/sdr/FDEA201008223089), Aug 22, 2010: SKIN. DENTED. EXTERIOR SKIN JUST AFT OF AFT CARGO DOOR BETWEEN FRAMES 64 AND 65 AND STR 39R AND 44R HAS MULTIPLE DENTS. DEEPEST DENT MEASURED APROX .7500 IN WIDE,1IN LONG AND
- [SDR FDEA201008213078](https://openairdocs.org/sdr/FDEA201008213078), Aug 21, 2010: SKIN. MISREPAIRED. PREVIOUS FLUSH REPAIR LOCATED ON LT WING NR 2 SLAT NOSE SKIN BETWEEN RIB 13 AND 15 JUST BELOW UPPER GIRDER MEASURES 5.4 X 5.8 INCH PREVIOUS REPAIR WAS DETERMINE
- [SDR FDEA201008213077](https://openairdocs.org/sdr/FDEA201008213077), Aug 21, 2010: STRINGER. MISREPAIRED. PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 47 LT BETWEEN FR 59 AND FR 60 HAS 1EA STRINGER REPAIR SECTION FROM FR 55/58 TO 60 MEASURING 29.4IN LON
- [SDR FDEA201008213076](https://openairdocs.org/sdr/FDEA201008213076), Aug 21, 2010: STRINGER. MISREPAIRED. PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 45 LT BETWEEN FR 60 AND FR 61 HAS 1 EA STRINGER REPAIR SECTION FROM FR 55/58 TO 62 MEASURING 51IN LONG
- [SDR FDEA201008213075](https://openairdocs.org/sdr/FDEA201008213075), Aug 21, 2010: STRINGER. MISREPAIRED. PREVIOUS STR REPAIR LOCATED IN AFT CARGO ON STRINGER 52 LT BETWEEN FRAMES 62 TO 63 HAS 1 EACH STRINGER REPAIR SECTION FROM FR 60 TO 63 MEASURING 43IN LONG AND 1
- [SDR FDEA201008203074](https://openairdocs.org/sdr/FDEA201008203074), Aug 20, 2010: STRINGER. MISREPAIRED. PREVIOUS STR REPAIR LOCATED IN AFT CARGO ON STR 46 LT BETWEEN FRAMES 61 TO 62 HAS 1EA STR SECTION FROM FR 55/58 TO 62 MEASURING 71.7 INCH LONG AND 1EA REPAIR SP
- [SDR FDEA201008203073](https://openairdocs.org/sdr/FDEA201008203073), Aug 20, 2010: STRINGER. MISREPAIRED. PREVIOUS STR REPAIR LOCATED IN BULK CARGO ON STR 54 R BETWEEN FR 66 AND FR67 HAS 1 EA STR REPAIR SECTION FROM FR 65 TO FR 67 MEASURING 32 IN LONG AND 1EA REPAIR
- [SDR FDEA201008203072](https://openairdocs.org/sdr/FDEA201008203072), Aug 20, 2010: STRINGER. MISREPAIRED. PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 55 R/H BETWEEN FR66 AND FR67 HAS 1 EACH STRINGER REPAIR SECTION FROM FR 65 TO 67 MEASURING 32 INCH LO
- [SDR FDEA201008203071](https://openairdocs.org/sdr/FDEA201008203071), Aug 20, 2010: STRINGER. MISREPAIRED. PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 56 LT BETWEEN FRAMES 66 TO 67 HAS 1 EA STRINGER REPAIR SECTION FROM FR 65 TO 67 MEASURING 33.5 INCH L
- [SDR FDEA201008203070](https://openairdocs.org/sdr/FDEA201008203070), Aug 20, 2010: SEAT TRACK. MISREPAIRED. PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR1 Y0 BETWEEN FRAMES 61 TO 62, HAS 1 EA REPAIR ANGLE ON LT SIDE UPPER FLANGE MEASURING 9.3 INCHES LONG X 1.7 I
- [SDR FDEA201008203069](https://openairdocs.org/sdr/FDEA201008203069), Aug 20, 2010: STRINGER. MISREPAIRED. PREVIOUS STRINGER REPAIR LOCATED IN FWD CARGO ON STR 46 RT BETWEEN FRAME 38 AND FR 38.1 HAS 1 EACH REPAIR SPLICE 6.8 INCH LONG AND THE STRINGER SECTION WAS CUT 
- [SDR FDEA201008203068](https://openairdocs.org/sdr/FDEA201008203068), Aug 20, 2010: STRINGER. MISREPAIRED. PREVIOUS STRINGER REPAIR LOCATED IN FWD CARGO ON STR 47 RT BOTTOM FRAMES 38 AND FR 38.1 HAS 1 EACH REPAIR SPLICE 6.9 INCH LONG AND THE STRINGER SECTION WAS CUT 
- [SDR FDEA201008203065](https://openairdocs.org/sdr/FDEA201008203065), Aug 20, 2010: STRINGER. MISREPAIRED. PREVIOUS STRINGER REPAIR IN FWD CARGO ON STR 45 RT BETWEEN FR 38 AND FR 38.1 HAS 1 EACH REPAIR SPLICE 6.8 INCH LONG AND THE STR SECTION WAS CUT ONLY TO REMOVE F
- [SDR FDEA201008203064](https://openairdocs.org/sdr/FDEA201008203064), Aug 20, 2010: STRINGER. MISREPAIRED. PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 51 RT BETWEEN FRAMES 60 TO 62 HAS 1 EA, STRINGER REPAIR SECTION MEASURING 15.1 INCH LONG AND 2 EA. REP
- [SDR FDEA201008163008](https://openairdocs.org/sdr/FDEA201008163008), Aug 16, 2010: SKIN. MISREPAIRED. PREVIOUS EXTERNAL LAP SEAM REPAIR LOCATED AT LOWER FUSELAGE SKIN AT FRAME 66 AND BETWEEN STRINGERS 54 LT TO 56 RT. THE REPAIR FILLER MEASURES 19.3 IN X 11 IN AN
- [SDR FDEA201008122943](https://openairdocs.org/sdr/FDEA201008122943), Aug 12, 2010: SEAT TRACK. DAMAGED. MDCC SEAT TRACK 4L HAS 2 LOCK TABS GOUGED AT FRAMES 54.3-55. BLENDED GOUGES ON SEAT TRACK IAW SRM 51-74-10. CHECKED LIMITS IAW SRM 53-10-16, FIG 101 AND FOUND O
- [SDR FDEA201008112937](https://openairdocs.org/sdr/FDEA201008112937), Aug 11, 2010: SEAT TRACK. CORRODED. MAIN DECK CARGO COMPARTMENT SEAT TRACK 4 LT HAS 3 EA AREAS OF CORROSION ON SCALLOPS AND FLANGE, ABOUT 30 SQ IN BETWEEN FR 74 AND FR 76. REMOVED LEVEL 1 CORROSIO
- [SDR 08FDEA04423](https://openairdocs.org/sdr/08FDEA04423), Oct 11, 2008: UNKNOWN. UNKNOWN. LO TANK READ 1200 LBS LESS AFTER 1 HR T/O. GAUGE HAD DASH IN LAST DIGIT. DASH WENT AWAY. FQI CONTINUED TO DECREASE TO 1200 TOTAL. ON DESCENT FUEL INCREASED, AT 
- [SDR 08FDEA03275](https://openairdocs.org/sdr/08FDEA03275), Aug 6, 2008: CONNECTOR. INOPERATIVE. AFTER T/O FROM KIND, NR 2 ENG SHOWED ADVISORY FRO "NAC HEAT" OF 90. LEVELED OFF AT 15,000 FEET AND SLOWED TO 200 K. NAC HEAT DID NOT REDUCE. CONSULTED GOC AND R
- [SDR 08FDEA01560](https://openairdocs.org/sdr/08FDEA01560), Apr 25, 2008: SKIN. DAMAGED. FOUND 5 HOLES AT FRAME 16A TO HAVE PRE EXISTING TOOLING DAMAGE IN HOLES, FASTENERS MARKED AS A, B, C, D,AND E. COMPLIED WITH EA NR 6-5310-118477 TITLE: " FUSELA
- [SDR 08FDEA01467](https://openairdocs.org/sdr/08FDEA01467), Apr 21, 2008: SKIN. DAMAGED. RIGHT ELEVATOR UPPER SURFACE TRAILING EDGE; INBD SECTION HAD 2 DENTS AND A PUNCTURE ON THE INBD T/E WEDGE. REPAIRED DAMAGE TO RT ELEVATOR UPPER SURFACE BY, REMO
- [SDR 08FDEA01445](https://openairdocs.org/sdr/08FDEA01445), Apr 17, 2008: ATTACH ANGLE. CRACKED. LEFT WING ATTACHING ANGLE FOR L/E PANEL 523 HB IS CRACKED. FABRICATED A NEW REINFORCING PLATE IAW AIRBUS DWG 23-A-572-43292 ISSUE F. PRIMED IAW A310 SRM 51-21-1
- [SDR 08FDEA01421](https://openairdocs.org/sdr/08FDEA01421), Apr 16, 2008: DOOR FRAME. GOUGED. AFT PIT DOOR, LWR FWD CORNER, GOUGED. FOUND GOUGE TO BE OUT OF LIMITS IAW SRM 51-10-00. REMOVED AND REPLACED EDGE SECTION IAW SRM 51-40-21. FOR ADJUSTMENT AND C

All 303: https://openairdocs.org/deregistered/N425FE-2016-02-18/reports.md

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