# N435FE: 1985 Airbus Industrie A310-203, registration cancelled 2024-02-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 3, 2024
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A310-203](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: 369
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 26, 2004
- Certificate issued: February 20, 2002
- Last registry action: August 25, 2023
- Mode S code: A53633
- 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/N435FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=435FE
- Page: https://openairdocs.org/deregistered/N435FE-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 A310-203: https://openairdocs.org/model/airbus-industrie-a310-203.md

## Service difficulty reports (94, newest 50)

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

- [SDR FDEA201309042115](https://openairdocs.org/sdr/FDEA201309042115), Sep 4, 2013: SELECTOR VALVE. FAILED. ON LANDING, NOSE TILLER COULD NOT BE MOVED. DIFFERENTIAL BRAKING USED TO CLEAR RWY. TROUBLESHOT IAW TSM 32-51-00 FIG 103 TO STEP 4. NOSE GEAR DOORS WILL NOT RAI
- [SDR FDEA201210313788](https://openairdocs.org/sdr/FDEA201210313788), Oct 31, 2012: JACKSCREW. FAILED. DURING DESCENT AT MEM TO 36R, SLATS WOULD NOT EXTEND AT 210 KTS. EXECUTED QRH PROCEDURES, DECLARED EMERGENCY AND REMAINDER OF APPROACH AND LANDING NORMAL. CREW 
- [SDR FDEA201108193388](https://openairdocs.org/sdr/FDEA201108193388), Aug 19, 2011: PANEL. CORRODED. RT ELEVATOR, L/E PANEL 345DT, OTBD LANDING HAS 1 EA CORRODED FASTNER HOLE, 2EA MISDRILLED HOLES, AND CORROSION ON THE WEB ATTACHMENT STRAP. REMOVED LEVEL 1 CORR
- [SDR FDEA201108183365](https://openairdocs.org/sdr/FDEA201108183365), Aug 18, 2011: SKIN. GOUGED. RT WING FIX L/E IS GOUGED APPROX 6" LONG BETWEEN SLAT TRACK 5 AND 6, FROM CONTACT WITH NR 2 SLAT LOWER SKIN FASTENERS. SMOOTHED AND BLENDED AREA IAW SRM 51-75-1
- [SDR FDEA201108183356](https://openairdocs.org/sdr/FDEA201108183356), Aug 18, 2011: SKIN. GOUGED. RT HORIZONTAL STAB L/E PANEL 341AB, EXTERNAL SKIN SCRATCHED AND GOUGED, ENTIRE LENGTH OF INBD EDGE. BLENDED OUT AREAS (4EA) ON RT HORIZONTAL STAB L/E PANEL 341A
- [SDR FDEA201108173303](https://openairdocs.org/sdr/FDEA201108173303), Aug 17, 2011: ATTACH FITTING. CORRODED. LT WING RIB 5 FWD LUG BORE DIAMETER HAS CORROSION THAT HAS EXCEEDED MAX ALLOWABLE REWORK DIMENSIONS "4.8405 IN". REMOVED LEVEL 1 CORROSION FROM LT WING RIB 5 BY
- [SDR FDEA201108163289](https://openairdocs.org/sdr/FDEA201108163289), Aug 16, 2011: ADAPTER. CRACKED. CLEVIS ADAPTER AT FR 46 BETWEEN SEAT TRACKS 2R & 3R IS CRACKED APPROX.2" LONG AT FWD & AFT FLANGE. R & R CLEVIS ADAPTER AT FR 46, BETWEEN TRACKS 2R AND 3R IAW S
- [SDR FDEA201108153280](https://openairdocs.org/sdr/FDEA201108153280), Aug 15, 2011: CHANNEL. BENT. INNER FUSELAGE "U" CHANNEL IS BENT STR 33L BETWEEN FR 83 TO FR 84. R & R CHANNEL AT STR 33L BETWEEN FR 83 TO FR 84 IAW SRM 51-40-21. PARAGRAPH 7.
- [SDR FDEA201108143274](https://openairdocs.org/sdr/FDEA201108143274), Aug 14, 2011: INTERCOSTAL. BENT. INTERCOSTAL AND UPPER ANGLE ARE BENT STR 33R. INNER FUSELAGE BETWEEN FRAME 85 AND FRAME 86. REMOVED AND FAB AND INSTALLED INTERCOSTAL ANGLE ON FR 85 TO 86 RT ST
- [SDR FDEA201108113220](https://openairdocs.org/sdr/FDEA201108113220), Aug 11, 2011: SKIN. GOUGED. UPPER AFT AREA OF AFT CARGO DOOR CUTOUT, EXT SURFACE, HAS MULTIPLE SCRATCHES EXTENDING 10" AFT OF CUTOUT (FR63) BETWEEN STRINGERS 27R & 28R. SMOOTHED AND BLENDE
- [SDR FDEA201108113219](https://openairdocs.org/sdr/FDEA201108113219), Aug 11, 2011: PANEL. CRACKED. RT HORIZ L/E PANEL 341AB, INTERNAL STIFFENER CRACKED AT AFT END, FROM FASTENER TO EDGE OF PART, .3125" LONG, UPPER AFT CORNER OF PANEL. REMOVED FASTENERS HORZ L
- [SDR FDEA201108113200](https://openairdocs.org/sdr/FDEA201108113200), Aug 11, 2011: FRAME. CORRODED. AFT CARGO DOOR AFT EDGE SEAL LANDING STRIP GOUGED AT MULTIPLE PLACES ON FUSELAGE CUTOUT FR 63A R & R 3EA AFT CARGO DOOR AFT EDGE SEAL LANDINGS IAW SRM 51-72-10.
- [SDR FDEA201108083139](https://openairdocs.org/sdr/FDEA201108083139), Aug 8, 2011: ACCESS DOOR. CRACKED. APU RT ACCESS DOOR 316AR AFT MATING FLANGE ON TAILCONE ASSY DEFORMED BELOW LATCH RECEPTACLE, MEASURED 4 IN LENGTH. REMOVED MATING FLANGE IAW SRM 51-40-21. INSTA
- [SDR FDEA201108083138](https://openairdocs.org/sdr/FDEA201108083138), Aug 8, 2011: TRAY. CORRODED. AFT CARGO COMPARTMENT LT FWD PDU TRAY FLANGE IS BENT BETWEEN FR55 AND 56 AND NR 2L AND NR 3L TRACK ROLLERS. R & R PDU TRAY IAW SRM 51-40-21, DUE TO CORROSION FO
- [SDR FDEA201108083133](https://openairdocs.org/sdr/FDEA201108083133), Aug 8, 2011: HINGE. CRACKED. BOTTOM EXT FUSE EXT ELECTRICAL POWER PLUG ACCESS DOOR INNER DOUBLER CRACKED .2" IN LENGTH. REMOVED ELECTRICAL POWER PLUG ACCESS DOOR, R & R DAMAGED INNER DOUBLE
- [SDR FDEA201108073130](https://openairdocs.org/sdr/FDEA201108073130), Aug 7, 2011: RETAINER. CRACKED. RT WING NR1 SPOILER T/E RETAINER STRAP IS CRACKED APPROX 1" LONG INBD END. R & R RETAINER STRIP IAW CMM 57-71-11.
- [SDR FDEA201108073132](https://openairdocs.org/sdr/FDEA201108073132), Aug 7, 2011: ACCESS PANEL. CRACKED. RT WING L/E ACCESS PANEL NR 624EB CUT OUT LANDING IS CRACKED APPROX 1" LONG. R & R CUT OUT LANDING FOR ACCESS PANEL 624EB IAW SRM 51-40-01, PAR 6 & 7 AND SRM 51
- [SDR FDEA201108063117](https://openairdocs.org/sdr/FDEA201108063117), Aug 6, 2011: ADAPTER. CRACKED. CLEVIS ADAPTER AT FR 45 BETWEEN SEAT TRACK 2 & 3 RT IS CRACKED APPROX 1" LONG AT FWD FLANGE. R & R CLEVIS ADAPTER IN MDCC AT FR 45 BETWEEN SEAT TRACKS NR 2 AND 
- [SDR FDEA201108053112](https://openairdocs.org/sdr/FDEA201108053112), Aug 5, 2011: SUPPORT BRACKET. CRACKED. NR1 ENGINE THRUST REVERSER TRANSLATING COWL UPPER GUIDE SUPPORT SLIDER BRACKET CRACKED. REMOVED NR 1 ENG O/B TRANSLATING SLEEVE IAW A310-200 AMM 78-32-11-04. RE
- [SDR FDEA201108033081](https://openairdocs.org/sdr/FDEA201108033081), Aug 3, 2011: STRINGER. CRACKED. RT SIDE STRINGER 9R BETWEEN FR 98 TO 100 HAS 2 PIECES BROKEN OFF. R & R STRINGER 9R FROM FR 95 TO 102 IAW SRM 51-72-10, PARA 5A & 6A. FABRICATED NEW STRINGER IA
- [SDR FDEA201108033083](https://openairdocs.org/sdr/FDEA201108033083), Aug 3, 2011: INTERCOSTAL. BENT. INNER FUSELAGE INTERCOSTAL IS BENT STR 33L BETWEEN FR85 TO FR84. REMOVED INTERCOSTAL STR 33L BETWEEN FR85 TO FR84 IAW SRM51-40-21, PARA 6, B/S FABRICATED STIFFE
- [SDR FDEA201108013058](https://openairdocs.org/sdr/FDEA201108013058), Aug 1, 2011: INTERCOSTAL. BENT. INTERCOSTAL IS BENT STR 35R INNER FUSELAGE BETWEEN FR86 TO FR87. REMOVED DAMAGED INTERCOSTAL, REPLACED WITH NEW INTERCOSTAL AND STRIP AT STR 35R BETWEEN FR 86 A
- [SDR FDEA201107313046](https://openairdocs.org/sdr/FDEA201107313046), Jul 31, 2011: STRUCTURE. GOUGED. RT WING SPOILER NR 7 LOWER T/E IS GOUGED APPROX .500" WIDE. R & R T/E OF RT WING NR 7 SPOILER IAW SRM 51-72-10.
- [SDR FDEA201107303040](https://openairdocs.org/sdr/FDEA201107303040), Jul 30, 2011: SEAT TRACK. DAMAGED. FLOOR TRACK L3 HAS DAMAGED RECEPTICLES LOCATED BETWEEN FLOORBEAM 61 AND 60. REMOVED DAMAGED SECTION FROM BETWEEN FRAMES 58 AND FRAMES 62 AND INSTALLED SPLICE RE
- [SDR FDEA201107303038](https://openairdocs.org/sdr/FDEA201107303038), Jul 30, 2011: MOUNT BRACKET. CRACKED. AFT UPPER PYLON RIB 21, 3 INCH CRACK AT WING TO PYLON MOUNT BRACKET. R & R TEE PICK-UP ANGLE IAW SRM 51-72-10, PGS 1-3 AND SRM 51-40-21, PGS 31-36.
- [SDR FDEA201107303037](https://openairdocs.org/sdr/FDEA201107303037), Jul 30, 2011: ACCESS PANEL. CRACKED. LT EXTERNAL PACK AREA INBD LANDING FOR PANEL 143FL HAS .250. CRACK REMOVED LANDING FOR PANEL 143FL, INSTALLED NUTPLATES ON NEW LANDING IAW SRM 51-40-21. INSTALL
- [SDR FDEA201107293031](https://openairdocs.org/sdr/FDEA201107293031), Jul 29, 2011: SEAL. WORN. PANEL 475CL FWD FINGER SEAL IS WORN APPROX 20 PERCENT ACROSS THE RT SIDE. REMOVED SEAL , FABRICATED NEW SEAL IAW SRM 51-40-44. INSTALLED NEW SEAL IAW SRM 51-40-
- [SDR FDEA201107293021](https://openairdocs.org/sdr/FDEA201107293021), Jul 29, 2011: BRACKET. BENT. FR 33, STGR 15L, 2 EA ISOLATOR BRACKET BENT. REMOVED 2 EA BRACKETS IAW SRM 51-40-21. FABBED 2 EA BRACKETS IAW DWG A53771078. ALODINED BRACKETS IAW SRM 51-21-10.
- [SDR FDEA201107293020](https://openairdocs.org/sdr/FDEA201107293020), Jul 29, 2011: FRAME. CORRODED. AFT PRESSURE BULKHEAD LWR FWD SIDE CIRCUMFERENCE STRAP CORRODED 2 INCHES LENGTH X 3 INCHES WIDTH BETWEEN STGR 44L AND 46L. REMOVED AND REAPPLIED SEALANT ON AFT 
- [SDR FDEA201107293019](https://openairdocs.org/sdr/FDEA201107293019), Jul 29, 2011: INTERCOSTAL. BENT. INTERCOSTAL IS BENT STR 33R INNER FUSELAGE BETWEEN FR'S 86 AND 87 FABRICATED. REPLACEMENT INTERCOSTAL, LOCATED, DRILLED, INSTALLED AND REPROTECTED IAW SRM 51-40
- [SDR FDEA201107252942](https://openairdocs.org/sdr/FDEA201107252942), Jul 25, 2011: ROLLER TRAY. CORRODED. INSIDE AFT CARGO COMPT AT THE BOTTOM SURFACE OF 2R ROLLER TRACK, CORROSION 2.5" X 3" AT 10" FWD OF FR62. AFTER REMOVAL OF BALL MATS FOUND 1EA AREA ON ROLLER TRA
- [SDR FDEA201107252941](https://openairdocs.org/sdr/FDEA201107252941), Jul 25, 2011: SEAT TRACK. CRACKED. CLS ADAPTER AT FS 43 BETWEEN SEAT TRACKS 2R & 3R IS CRACKED APPROX 1 INCH LONG AT FWD FLANGE. R & R CLS ADAPTER AT FR 43 BETWEEN SEAT TRACK 2 & 3 IAW SRM 51-40-
- [SDR FDEA201107252937](https://openairdocs.org/sdr/FDEA201107252937), Jul 25, 2011: ADAPTER. CRACKED. CLS ADAPTER AT FS 42 BETWEEN SEAT TRACK 2R AND 3R IS CRACKED APPROX 1.5" LONG AT FWD FLANGE. R & R CLS ADAPTER AT FR42 BETWEEN SEAT TRACKS 2 AND 3RT IAW SRM 51-
- [SDR FDEA201107252931](https://openairdocs.org/sdr/FDEA201107252931), Jul 25, 2011: STRINGER SPLICE. CORRODED. STRINGER 26R SPLICE AT FRAME 54 HAS A 1 SQ IN AREA OF CORROSION, AFT SIDE OF FRAME. REMOVED CORROSION AT SPLICE PLATE AND FOUND LEVEL 1 CORROSION TO BE OUT OF L
- [SDR FDEA201107242925](https://openairdocs.org/sdr/FDEA201107242925), Jul 24, 2011: STRAP. CORRODED. RUDDER L/E ATTACH LANDING , RT SIDE , INTERNAL STRAP CORRODED, 2SQ IN , 6 INCHES ABOVE NR1 HINGE FITTING. REMOVED NUT PLATE STRAP IAW SRM 51-72-10, PAR 5, FABRI
- [SDR FDEA201107242929](https://openairdocs.org/sdr/FDEA201107242929), Jul 24, 2011: RIB. CRACKED. LT PYLON AT RIB 22 UPPER AFT SIDE HAS A 2 IN LONG CRACK. R & R TEE PICKUP ON LT NR1 PYLON AT RIB 22 IAW SRM 51-72-10.
- [SDR FDEA201107242924](https://openairdocs.org/sdr/FDEA201107242924), Jul 24, 2011: STRAP. CORRODED. RUDDER L/E ATTACH LANDING, RT SIDE INTERNAL STRAP CORRODED 2SQ IN, 8" ABOVE NR4 HINGE FITTING. REMOVED NUT PLATE STRAP IAW SRM 51-72-10: FABRICATED PLATE IAW DW
- [SDR FDEA201107242923](https://openairdocs.org/sdr/FDEA201107242923), Jul 24, 2011: BRACKET. CRACKED. FR26, STR 15 LT ISOLATOR BRACKET BROKEN IAW AMM 25-50-00-06. R & R ISOLATOR BRACKET AT FR 26 STR 15 LT IAW SRM 51-72-10 & 51-40-21, PARA 6.
- [SDR FDEA201107222908](https://openairdocs.org/sdr/FDEA201107222908), Jul 22, 2011: FLOORBOARD. DAMAGED. AFT CARGO FLOORBOARD 152EF MISSING EDGE FILLER DEFCT MEASURES 2 SQ INCHES. FABRICATED REPLACEMENT FLOORBOARD 152EF IAW DWG SR2 25-005, REV J.
- [SDR FDEA201107222907](https://openairdocs.org/sdr/FDEA201107222907), Jul 22, 2011: FLOOR PANEL. CRACKED. FLOOR PANEL 252GF HAS 1EA 12" CRACK FABRICATED REPLACEMENT FLOOR PANEL 262GF IAW DWG SR2 25-005, REV J.
- [SDR FDEA201107222906](https://openairdocs.org/sdr/FDEA201107222906), Jul 22, 2011: FLOORBOARD. DAMAGED. FLOORBOARD 251GF HAS PUNCTURE. FABRICATED REPLACEMENT FLOORBOARD 251GF IAW DWG SRZ-25-005, REV J.
- [SDR FDEA201107222905](https://openairdocs.org/sdr/FDEA201107222905), Jul 22, 2011: FLOOR PANEL. CRACKED. FLOOR PANEL 251WH HAS 12 IN CRACK FABRICATED REPLACEMENT PANEL 251WH IAW DWG SRZ-25-005, REV J.
- [SDR FDEA201107222904](https://openairdocs.org/sdr/FDEA201107222904), Jul 22, 2011: FLOOR PANEL. CONTAMINATED. FLOOR PANEL 147BF IS OIL SOAKED. FABRICATED REPLACEMENT PANEL 147BF IAW DWG SRZ-25-005, REV J.
- [SDR FDEA201107222902](https://openairdocs.org/sdr/FDEA201107222902), Jul 22, 2011: FLOOR PANEL. DAMAGED. AVIONICS COMPT FLOOR PANEL 121JF HAS 1 EA CORNER BROKEN AND 1 EA CORNER PLIES WORN THRU. FABRICATED REPLACEMENT FLOOR PANEL 121JF IAW DWG SRZ-25-005, REV J.
- [SDR FDEA201107212888](https://openairdocs.org/sdr/FDEA201107212888), Jul 21, 2011: SPAR. CORRODED. LEFT HORIZONTAL STAB UPPER REAR SPAR TOP FLANGE BOTTOM SIDE CORRODED AT 4EA NUTPLATE HOLES LOCATED 6 TO 18 INCHES OTBD OF FUSELAGE BETWEEN RIBS 3 AND 5 MEASURED
- [SDR FDEA201107192817](https://openairdocs.org/sdr/FDEA201107192817), Jul 19, 2011: FLOORBEAM. CRACKED. FWD CARGO MAIN DECK FLOORBEAM AT FRAME 34 CRACKED AT STIFFENER, BETWEEN SEAT TRACKS 2 & 3 RT SIDE. CUTOUT DAMAGE AT FLOORBEAM IN FWD CARGO COMPARTMENT SUPPORT F
- [SDR FDEA201107192816](https://openairdocs.org/sdr/FDEA201107192816), Jul 19, 2011: SKIN. CRACKED. APU EXHAUST DOOR 317AL RT LOWER LATCH CUTOUT SKIN HAS A .10 INCH CRACK. ROUTED OUT CRACK, NDT FOUND NO CRACKS, REPROTECTED AREA IAW SRM 52-41-18, PAGE 203 AND S
- [SDR FDEA201107192798](https://openairdocs.org/sdr/FDEA201107192798), Jul 19, 2011: CLEVIS. BENT. MDCC AT FS 54.1 BETWEEN SEAT TRACKS 2 & 3 RT CLEVIS ADAPTER FWD FLANGE IS BENT IN 2 EA PLACES. R & R ADAPTER AT FR 54.1 MDCC BETWEEN TRACKS 2 & 3 ON RT SIDE IAW
- [SDR FDEA201107192793](https://openairdocs.org/sdr/FDEA201107192793), Jul 19, 2011: CLEVIS. CRACKED. MDCC AT FS 54.1 AT SEAT TRACK 3RT CLEVIS ADAPTER MOUNT FITTING CRACK APPROX 2" LONG. R & R CLEVIS IN MDCC AT FR 54.1 ON RT NR 3 TRACK IAW SRM 51-72-10 PARA 5A &
- [SDR FDEA201107182783](https://openairdocs.org/sdr/FDEA201107182783), Jul 18, 2011: FLOOR PANEL. CRACKED. FLOOR PANEL 147 AF HAS A 1" INCH CRACK AND IS OIL SOAKED. FABRICATED REPLACEMENT FLOOR PANEL 147 AF USING DWG SRZ 25-005, REV J.

All 94: https://openairdocs.org/deregistered/N435FE-2024-02-03/reports.md

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