# N423FE: 1984 Airbus Industrie A310-203, registration cancelled 2020-04-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 23, 2020
- 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: 281
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 20, 1996
- Certificate issued: November 2, 1995
- Last registry action: June 13, 2018
- Mode S code: A50746
- 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/N423FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=423FE
- Page: https://openairdocs.org/deregistered/N423FE-2020-04-23

From the FAA registry file of November 3, 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 (145, newest 50)

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

- [SDR FDEA201410042967](https://openairdocs.org/sdr/FDEA201410042967), Oct 4, 2014: WARNING LIGHT. FALSE ACTIVATION. AFTER TAKEOFF WITH LANDING GEAR RETRACTION, NOSE GEAR DOOR INDICATED UNSAFE, AMBER ON BOTH INDICATORS. FELT FLUTTER INDICATING DOOR WAS IN FACT STILL OPEN. AIR 
- [SDR FDEA201309212274](https://openairdocs.org/sdr/FDEA201309212274), Sep 21, 2013: JACKSCREW. WORN. ON APPLICATION OF SLATS 1 & 2, FAULT LIGHT CAME ON. SLATS LESS THAN 15- CYCLED HANDLE & NO CHANGE. RAN CHECKLIST & MADE NO SLAT LANDING. AFTER LANDING TRIED SLA
- [SDR FDEA201306181339](https://openairdocs.org/sdr/FDEA201306181339), Jun 18, 2013: SEAL. LEAKING. AFTER TAKE OFF, BLEED LEAK RT SIDE. REF QRH- LIGHT OUT IN FLIGHT. ON APPROACH LOWER ACCESS DOOR LIGHT CAME ON. FOUND LEAK TO BE COMING FROM THE UPPER RT CORNER 
- [SDR FDEA201306051198](https://openairdocs.org/sdr/FDEA201306051198), Jun 5, 2013: SKIN. CORRODED. RT ELEVATOR NR 2 T/E UPPER SURFACE CORRODED. REPAIRED THE DAMAGE IAW SRM 55-21-11/201 (C-1) FIG 209.
- [SDR FDEA201305150992](https://openairdocs.org/sdr/FDEA201305150992), May 15, 2013: CROSSBEAM. CORRODED. FWD CARGO FR 38.1 -Y140 CROSSBEAM CORRODED. REPAIRED CROSSBEAM IAW SRM 53-10-15, FIG 207.
- [SDR FDEA201107082612](https://openairdocs.org/sdr/FDEA201107082612), Jul 8, 2011: TRANSFER SYS. LEAKING. INFLIGHT YELLOW SYS RESERVOIR DECREASED TO RED DOT. FLUCTUATED SOME BUT NEVER WENT OUT OF YELLOW BAND. R & R GREEN/YELLOW POWER TRANSFER UNIT AS REQUIRED IAW MM
- [SDR FDEA201105061768](https://openairdocs.org/sdr/FDEA201105061768), May 6, 2011: GCU. FAILED. ON TAKEOFF ROLL AT APPROX 50 KNOTS, GEN NR2 FAILED. ABORTED TAKEOFF. INTEROGATED GPCU, SHOWS RT GENERATOR, UNDER FREQ TRIP, IDG /PMG / WIRING, GCU FAILED CODE 9
- [SDR FDEA201104201538](https://openairdocs.org/sdr/FDEA201104201538), Apr 20, 2011: TRANSCEIVER. INOPERATIVE. STATIC ON RADIOS AT 380 DOWN TO 120 WAS SO BAD AN EMERGENCY WAS DECLARED DUE TO NO RADIO CONDITION. INSTALLED NEW NR1 VHF RECEIVER AND CHECKED GOOD IAW MM 23-12
- [SDR FDEA201103082037](https://openairdocs.org/sdr/FDEA201103082037), Mar 8, 2011: BATTERY. FAILED. EMERGENCY LIGHTS WILL NOT TEST USING PUSH-BUTTON OR OVERHEAD PANEL LIGHT SWITCH. R & R EMERGENCY LIGHT BATTERY LOCATED ADJACENT LT PASSENGER ENTRY DOOR IAW MM 3
- [SDR FDEA201102010445](https://openairdocs.org/sdr/FDEA201102010445), Feb 1, 2011: FRAME. CORRODED. REAR FUSELAGE FRAME 87- 89, STR 16L, HORIZ STAB CUTOUT. INNER FWD STRAP HAS EXFOLIATION CORROSION APPROX 4 IN. R & R THS CUTOUT FWD UPPER FITTING IAW DWG A53985
- [SDR FDEA201101310424](https://openairdocs.org/sdr/FDEA201101310424), Jan 31, 2011: SKIN. DAMAGED. .5" X .5" SHALLOW PUNCTURE ON RUDDER LT OUTER SKIN ABOUT 22" AFT OF THE NR 4 ATTACH FITTING. REPAIRED RUDDER L/T OUTER SKIN ABOUT 22" AFT OF THE NR4 ATTACH FITT
- [SDR FDEA201101300418](https://openairdocs.org/sdr/FDEA201101300418), Jan 30, 2011: RIB. CORRODED. LT WING RIB 5 FWD LUG HAS CORROSION. REPAIRED IAW EA 6-5710-145518 WING-AD 2008-17-02 - WING GEAR RIB 5 FWD LUG BORE REWORK (LT SIDE), SB A310-57-2090, EO 6-571
- [SDR FDEA201101300417](https://openairdocs.org/sdr/FDEA201101300417), Jan 30, 2011: RIB. CORRODED. RT WING, RIB 5, FWD LUG HAS CORROSION REPAIRED IAW EA 6-5710-145517, WING-AD2008-17-02, WING GEAR, RIB5 FWD LUG BORE REWORK (RT SIDE), SB A310-57-2090, EO 6-571
- [SDR FDEA201101280401](https://openairdocs.org/sdr/FDEA201101280401), Jan 28, 2011: PROFILE. CRACKED. BULK CARGO LONGITUDINAL PROFILE CRACKED 1" PN A53974259202, FR64 - 65 24" LT OF CTR OF ACFT. R & R LONGITUDINAL PROFILE FR 64 TO FR65 Y805 IAW SRM 51-72-10, PGS
- [SDR FDEA201101270386](https://openairdocs.org/sdr/FDEA201101270386), Jan 27, 2011: SEAT TRACK. CORRODED. AFT SEAT TRACK 1 HAS CORROSION FR 71 TO FR 75 (ABOUT 70 SQUARE INCH). REMOVED CORROSION FROM SEAT TRACK IAW SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-16, PAGE 
- [SDR FDEA201101270385](https://openairdocs.org/sdr/FDEA201101270385), Jan 27, 2011: SKIN. DENTED. UPON REMOVAL OF RUBSTRIP ON NR N00391 RT WING OTBD FLAP UPPER MAIN SKIN BETWEEN RIBS 4 AND 5 ALSO BETWEEN THE MAIN SPAR CHORD AND REAR SPAR CORD HAS 8 DENTS WHI
- [SDR FDEA201101210330](https://openairdocs.org/sdr/FDEA201101210330), Jan 21, 2011: CHANNEL. CORRODED. FRAME LOCATION 87, BETWEEN STR 15 AND 16 FOUND CORROSION ON LT SIDE AFT UPPER "U" CHANNEL (CROSS STRUT). 1 AREA OF CORROSION ON UPPER FLANGE APPROX 1 SQ IN. R &
- [SDR FDEA201101200313](https://openairdocs.org/sdr/FDEA201101200313), Jan 20, 2011: FLOOR SUPPORT. DAMAGED. BULK CARGO FLOOR SUPPORT LONGITUDINAL PROFILE BROKEN BETWEEN FRAMES 65 AND 66 LT STR 52 LT. R & R PROFILE SECTION FR65 TO FR66 LT ABOVE STR52L IAW SRM 51-72-10.
- [SDR FDEA201101200312](https://openairdocs.org/sdr/FDEA201101200312), Jan 20, 2011: FLOORBEAM. CRACKED. MAIN CABIN FLOORBEAM CRACKED IN RADIUS FR36 BETWEEN L2 AND L3 SEAT TRACK. REPAIRED CROSSBEAM AT FR36 BETWEEN SEAT TRACKS 2L AND 3L IAW SRM 53-10-15.
- [SDR FDEA201101200303](https://openairdocs.org/sdr/FDEA201101200303), Jan 20, 2011: CROSSBEAM. CORRODED. REAR FUSELAGE FR 85 , APPROX 15 INCHES INBD OF STR16 RT, HORIZONTAL CROSSBEAM HAS EXFOLIATION CORROSION ON LOWER FLANGE REMOVED CORROSION FROM CROSSBEAM AT FR 8
- [SDR FDEA201101190290](https://openairdocs.org/sdr/FDEA201101190290), Jan 19, 2011: SEAT TRACK. CORRODED. AFT SEAT TRACK 1-R HAS CORROSION, FR78 - FR79, 20 SQUARE INCHES. R & R SEAT TRACK BETWEEN FR76 AND FR79 SEAT TRACK 1 IAW SRM 51-40-21, PG 24, 51-27-00, PG1, 51-
- [SDR FDEA201101120127](https://openairdocs.org/sdr/FDEA201101120127), Jan 12, 2011: SEAT TRACK. CORRODED. AFT SEAT TRACK 1 HAS CORROSION FR 75 TO FR 77 ABOUT 30 SQUARE INCHES, REMOVED, FABRICATED AND INSTALLED SEAT TRACK 1, FR75 TO FR79 ALL IAW SRM 51-40-21, PG 24 P
- [SDR FDEA201101100099](https://openairdocs.org/sdr/FDEA201101100099), Jan 10, 2011: FLOORBEAM. CORRODED. BULK CARGO COMPARTMENT UNDERFLOOR, FR69, 17" TO 19" RT OF ACFT CENTERLINE, AXIAL FLOOR PANEL SUPPORT ANGLE HAS CORROSION/SWELLING ABOUT 6 SQUARE INCHES. BULK CA
- [SDR FDEA201101100098](https://openairdocs.org/sdr/FDEA201101100098), Jan 10, 2011: BEAM. CORRODED. BULK CARGO, AFTER REMOVING LATERAL BEAM AT FR67 FOUND AXIAL BEAM CORRODED THROUGH 100 PERCENT PN A53974261202, BULK CARGO. R & R PROFILE BEAM FR66 - FR69 (Y535)
- [SDR FDEA201101100097](https://openairdocs.org/sdr/FDEA201101100097), Jan 10, 2011: FLOOR SUPPORT. DAMAGED. AFT CARGO FLOORBEAM RUNNING FWD AND AFT BETWEEN FR66 AND FR65 APPROX 2' RT OF ACFT CTR IS BROKEN. R & R PROFILE SECTION FR65 TO FR66, RBL18 TO RBL24 IAW SRM 51-
- [SDR FDEA201101090092](https://openairdocs.org/sdr/FDEA201101090092), Jan 9, 2011: FLOORBEAM. CORRODED. BULK CARGO UNDERFLOOR AXIAL FLOOR SUPPORT ANGLE HAS CORROSION/SWELLING, LT 4" TO 7" FR67 ABOUT 6 SQUARE INCHES. R & R PROFILE SECTION FR66 TO FR69 LT 4" TO 7" I
- [SDR FDEA201101090091](https://openairdocs.org/sdr/FDEA201101090091), Jan 9, 2011: FLOORBEAM. CRACKED. FWD CARGO COMPARTMENT FOUND 1EA CRACK (.1250" DEEP) IN RADIUS OF UPPER FLOORBEAM FR38, BETWEEN UPPER SEAT TRACK 4L AND 5L CROSSBEAM REPAIRED AT CRACKED STIFFENE
- [SDR FDEA201101080089](https://openairdocs.org/sdr/FDEA201101080089), Jan 8, 2011: FLOORBEAM. CORRODED. MAIN CABIN COURIER AREA UNDER FLOOR, CORROSION ON LONGITUDINAL MEMBER AT FLOOR SUPPORT ANGLE 7" FWD OF FLOORBEAM AT FR13, 40" TO LT FROM ACFT CENTERLINE. AMM 53
- [SDR FDEA201101080088](https://openairdocs.org/sdr/FDEA201101080088), Jan 8, 2011: SEAT TRACK. CORRODED. CORROSION IN CTR TOP OF SEAT TRACK 2L FRAME 51 ABOUT 5"X1". R & R DAMAGED SEAT TRACK 2L FR49.5 TO FR54 AND INSTALLED A SPLICE REPAIR ON SEAT TRACK 2L AT FR49.5 
- [SDR FDEA201101080087](https://openairdocs.org/sdr/FDEA201101080087), Jan 8, 2011: FLOORBEAM. CRACKED. FWD CARGO COMPARTMENT, UPPER FLOORBEAM FR33 HAS 1EA CRACK IN RADIUS BETWEEN SEAT TRACKS 2R AND 3R. CROSSBEAM REPAIRED AT FR33 BETWEEN SEAT TRACKS 2R AND 3R IAW 
- [SDR FDEA201101080086](https://openairdocs.org/sdr/FDEA201101080086), Jan 8, 2011: SEAT TRACK. CORRODED. MAIN CABIN CORROSION ON SEAT TRACK 5L APPROX 1"X 2" BETWEEN FRAME 35 AND 36. R & R SEAT TRACK 5L AT FR35-FR36 AND 4EA SEAT TRACK SPLICES IAW SRM 53-10-16, PG 24
- [SDR FDEA201101080085](https://openairdocs.org/sdr/FDEA201101080085), Jan 8, 2011: SEAT TRACK. CORRODED. CORROSION ON OTBD FLANGE OF SEAT TRACK 4R 2" AFT OF FRAME 34 1"X4 ". REMOVED DAMAGED SEAT TRACK 4R FR26 -FR36 IAW SRM 53-10-16, FIG 208. INSTALLED REPLACEMENT S
- [SDR FDEA201101080084](https://openairdocs.org/sdr/FDEA201101080084), Jan 8, 2011: FLOOR SUPPORT. CORRODED. BULK CARGO UNDERFLOOR FR69 10" LT FROM ACFT CENTERLINE, FLOOR SUPPORT ANGLE HAS CORROSION ABOUT 3 SQUARE INCHES. FABRICATED 1 EA FITTING IAW DWG A53974329. R & 
- [SDR FDEA201101080083](https://openairdocs.org/sdr/FDEA201101080083), Jan 8, 2011: FLOOR SUPPORT. CORRODED. BULK CARGO UNDERFLOOR, FR69 CORROSION ON CARGO NET CLEVIS SUPPORT ANGLE, (ABOUT 2 SQUARE INCHES) R & R BULK CARGO UNDERFLOOR CARGO NET CLEVIS SUPPORT FITTING, F
- [SDR FDEA201101080082](https://openairdocs.org/sdr/FDEA201101080082), Jan 8, 2011: SEAT TRACK. CORRODED. SEAT TRACK 4R HAS CORROSION AT 8" AFT OF FR51 (-1959) R & R SEAT TRACK SEGMENT AND SPLICE REPAIR AT FR51 TO FR52 SEAT TRACK 4R IAW SRM 51-72-10, PGS1-3 AND 53-1
- [SDR FDEA201101060054](https://openairdocs.org/sdr/FDEA201101060054), Jan 6, 2011: PROFILE. CORRODED. RT VERTICAL STABILIZER T/E HORIZ PANEL LANDING SUPPORT STRAP BETWEEN RIBS 21-22 HAS 8 INCH CORROSION IN AND AROUND 3 EA FASTENERS AND ALONG UPPER INTERIOR MATIN
- [SDR FDEA201101060058](https://openairdocs.org/sdr/FDEA201101060058), Jan 6, 2011: RIB. CORRODED. VERTICAL STABILIZER, RIB 1 TOP SURFACE HAS CORROSION (ABOUT 4 SQ INCHES) RT STRINGER 5 RT TO STR 7 RT. FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW SRM 53-3
- [SDR FDEA201101060056](https://openairdocs.org/sdr/FDEA201101060056), Jan 6, 2011: MOUNT. CORRODED. VERT STABILIZER AFT RT MOUNT LUG FITTING HAS CORROSION ON INTERIOR SURFACE BETWEEN STRINGER 1 RT AND STRINGER 2 RT,ABOUT 2 SQ INCHES. REPAIRED VERT STAB AFT RT 
- [SDR FDEA201101060055](https://openairdocs.org/sdr/FDEA201101060055), Jan 6, 2011: MOUNT. CORRODED. VERTICAL STABILIZER LT AFT MOUNT LUG HAS CORROSION FROM STR 1 LT TO STR 4 LT, ABOUT 70 SQ INCHES. REPAIRED VERT STAB LT AFT MOUNT LUG BETWEEN S1L TO S4L IAW EA 
- [SDR FDEA201101060053](https://openairdocs.org/sdr/FDEA201101060053), Jan 6, 2011: CROSSBEAM. CORRODED. REAR FUSELAGE FRAME 86, STR 16, LT TO THS DRIVE UNIT SUPPORT, FWD CROSSBEAM HAS EXFOILIATION CORROSION. REMOVED LEVEL 1 CORROSION. REWORKED CROSSBEAM ON FR 86 A
- [SDR FDEA201101060052](https://openairdocs.org/sdr/FDEA201101060052), Jan 6, 2011: SUPPORT BEAM. CORRODED. REAR FUSELAGE FRAME 87-88, STR 16, RT HORIZ STAB CUTOUT SUPPORT BEAM INBD FACE CORRODED AT 1 EA LOCK FASTENER APPROX 1 SQ INCH. REMOVED CORROSION IAW SRM 51-74-
- [SDR FDEA201101060051](https://openairdocs.org/sdr/FDEA201101060051), Jan 6, 2011: STRINGER. CORRODED. REAR FUSELAGE FRAME 87-89, STR 16, LT HORIZ STAB CUTOUT INNER FWD STRAP HAS EXFOILIATION CORROSION APPROX 4 SQ INCHES. R & R THS CUTOUT FWD FITTING IAW DWG A539
- [SDR FDEA201101060050](https://openairdocs.org/sdr/FDEA201101060050), Jan 6, 2011: FITTING. CORRODED. REAR FUSELAGE FRAME 87-89, STR 16 RT, THS CUTOUT INNER FWD STRAP HAS EXFOILIATION CORROSION APPROX 4 INCHES AT AFT ATTACH. R & R THS CUTOUT UPPER FWD CORNER FIT
- [SDR FDEA201101060049](https://openairdocs.org/sdr/FDEA201101060049), Jan 6, 2011: FRAME. CORRODED. REAR FUSELAGE FRAME 85, APPROX 15 INCHES INBD OF STR 16 RT HORIZ CROSSBEAM HAS EXFOILIATION CORROSION ON LOWER FLANGE. REMOVED LEVEL 1 CORROSION. FRAME R & R IA
- [SDR FDEA201101050015](https://openairdocs.org/sdr/FDEA201101050015), Jan 5, 2011: FLOORBEAM. CORRODED. BULK CARGO FLOOR SUPPORT LATERAL ANGLE AT FR66 HAS CORROSION AT NUT PLATE LOCATIONS, 10 PLACES, FROM RT 19" TO LT 48" FORM CTR LINE OF ACFT TOTALING 10 SQUARE I
- [SDR FDEA201101050014](https://openairdocs.org/sdr/FDEA201101050014), Jan 5, 2011: RIB. CORRODED. VERTICAL STABILIZER RIB 1 WEB TOP SURFACE HAS CORROSION ( ABOUT 4 - SQUARE INCHES) RT STRINGER 5R TO STRINGER 7R VERT STAB RT SIDE REMOVED CORRODED SECTION ON R
- [SDR FDEA201012244749](https://openairdocs.org/sdr/FDEA201012244749), Dec 24, 2010: SEAT TRACK. WORN. DUMMY SEAT TRACK RT NR6 AT FR 54.2 HAS GAP AT SLOTTED END. ATTACH BOLT OF .026". REMOVED, REPAIRED AND REINSTALLED DUMMY SEAT TRACK RT NR6 IAW EO 6-5310-7-3322,
- [SDR FDEA201012244748](https://openairdocs.org/sdr/FDEA201012244748), Dec 24, 2010: SEAT TRACK. WORN. DUMMY SEAT TRACK L3 AT FRAME 38.2 HAS A GAP AT SLOT OF 0.020 INCH. REMOVED DUMMY SEAT TRACK NR3L, AT FR 38.2. REPAIRED AND REINSTALLED IAW E0 6-5310-7-3322, P2 
- [SDR FDEA201012244747](https://openairdocs.org/sdr/FDEA201012244747), Dec 24, 2010: PLATE. CORRODED. MAIN DECK CARGO COMPARTMENT ZONE 230, FR 32 BETWEEN SEAT TRACK 5R AND 6R PAN CORRODED TOP SKIN APPROX 1 SQ INCH. REMOVED CORROSION FROM PAN AND CHECKED LIMITS I
- [SDR FDEA201012234744](https://openairdocs.org/sdr/FDEA201012234744), Dec 23, 2010: SEAT TRACK. WORN. DUMMY SEAT TRACK (ARTICULATED RAIL) L-4 AT FR 38.2 HAS A GAP AT THE SLOT OF .031" REMOVED, REPAIRED AND REINSTALLED THE DUMMY SEAT TRACK (ARTICULATED RAIL) L-4 

All 145: https://openairdocs.org/deregistered/N423FE-2020-04-23/reports.md

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