# N432FE: 1984 Airbus A310-203, registration cancelled 2010-05-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 10, 2010
- Status when cancelled: Triennial form not returned
- Airframe: [Airbus A310-203](https://openairdocs.org/model/airbus-a310-203) (registry code 3940008)
- 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: 326
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 20, 2004
- Certificate issued: April 11, 2002
- Last registry action: March 18, 2008
- Mode S code: A52B0E
- 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/N432FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=432FE
- Page: https://openairdocs.org/deregistered/N432FE-2010-05-10

From the FAA registry file of November 5, 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 A310-203: https://openairdocs.org/model/airbus-a310-203.md

## Service difficulty reports (95, newest 50)

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

- [SDR FDEA200805221955](https://openairdocs.org/sdr/FDEA200805221955), May 22, 2008: ENGINE. FAILED. ON TAKEOFF ROLL SERIES OF POPS OR BANGS, SPEED LESS THAN 40 KTS, EXPERIENCED LT SWERVE, LOW SPEED REJECT. SOUNDED LIKE POSSIBLE COMPRESSOR STALL. GVI OF NR 1 EN
- [SDR 08FDEA01955](https://openairdocs.org/sdr/08FDEA01955), May 22, 2008: ENGINE. FAILED. ON TAKEOFF ROLL SERIES OF POPS OR BANGS, SPEED LESS THAN 40 KTS, EXPERIENCED LEFT SWERVE, LOW SPEED REJECT. SOUNDED LIKE POSSIBLE COMPRESSOR STALL. GVI OF NR 1 
- [SDR 07FDEA03773](https://openairdocs.org/sdr/07FDEA03773), Sep 14, 2007: COUPLING. CORRODED. FOUND CORROSION AT COUPLING, C 65, P 56 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03771](https://openairdocs.org/sdr/07FDEA03771), Sep 14, 2007: COUPLING. CORRODED. FOUND CORROSION AT COUPLING, C 70, P 37RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03770](https://openairdocs.org/sdr/07FDEA03770), Sep 14, 2007: COUPLING. CORRODED. FOUND CORROSION AT COUPLING, C 65, P 56 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03769](https://openairdocs.org/sdr/07FDEA03769), Sep 14, 2007: PLATE. CORRODED. FOUND CORROSION AT GROUND VALVE PLATE C 24-25 , P52-55 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03767](https://openairdocs.org/sdr/07FDEA03767), Sep 14, 2007: COUPLING. CORRODED. FOUND CORROSION AT COUPLING P 55RH, C 65. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03766](https://openairdocs.org/sdr/07FDEA03766), Sep 14, 2007: COUPLING. CORRODED. FOUND CORROSION AT COUPLING P 53LT, C 55/58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03765](https://openairdocs.org/sdr/07FDEA03765), Sep 14, 2007: FITTING. CORRODED. FOUND CORROSION AF FITTING C 54.2, P 45-46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03764](https://openairdocs.org/sdr/07FDEA03764), Sep 14, 2007: FITTING. CORRODED. FOUND CORROSION AF FITTING C 54.2, P 45-46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03756](https://openairdocs.org/sdr/07FDEA03756), Sep 14, 2007: COUPLING. CORRODED. FOUND CORROSION ON COUPLING P 50 RH, C 69. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03754](https://openairdocs.org/sdr/07FDEA03754), Sep 14, 2007: STRINGER. CORRODED. FOUND CORROSION ON STRINGER P 54 RT, C 68-69 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.
- [SDR 07FDEA03751](https://openairdocs.org/sdr/07FDEA03751), Sep 14, 2007: COUPLING. CORRODED. CORROSION FOUND AT COUPLING AT C 65, P 57 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03750](https://openairdocs.org/sdr/07FDEA03750), Sep 14, 2007: COUPLING. CORRODED. CORROSION FOUND AT COUPLING AT C 65, P 55 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03747](https://openairdocs.org/sdr/07FDEA03747), Sep 14, 2007: COUPLING. CORRODED. CORROSION FOUND AT COUPLING AT C 26/32, P 45 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03746](https://openairdocs.org/sdr/07FDEA03746), Sep 14, 2007: ANGLE. CORRODED. CORROSION FOUND ON REINFORCING ANGLE AT C38-39, P 48 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03672](https://openairdocs.org/sdr/07FDEA03672), Sep 13, 2007: PANEL. CORRODED. FOUND CRACK ON PYLON NR 2 AT RIB 8 INBOARD AND OUTBOARD SIDE AT PANEL (ABOUT 8MM) DOUBLER REPAIR ON SIDEWALL PANELS PERFORMED IAW SRM 5451-31 FIG 201.
- [SDR 07FDEA03646](https://openairdocs.org/sdr/07FDEA03646), Sep 13, 2007: BEAM. CRACKED. FOUND CRACK ON LONGITUDINBAL BEAM C 74-76, P 11 LT/RT, (LT: 8MM, RT 15MM). REPAIR PERFORMED BY INSTALLING REPAIR ANGLES IAW SRM 53-181-18 FIG 204.
- [SDR 07FDEA03684](https://openairdocs.org/sdr/07FDEA03684), Sep 13, 2007: SKIN. DAMAGED. DURING FUNCTION PHASE, THE RT INBOARD FLAP TRAILING EDGE WAS DAMAGED REPAIR PERFORMED IAW SRM 57-53-12 PARA 13 (FIG 209).
- [SDR 07FDEA03707](https://openairdocs.org/sdr/07FDEA03707), Sep 13, 2007: FLANGE. DAMAGED. FOUR MISDRILLED HOLES AT UPPER FLANGE (BEAM) AT C 33 LT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.
- [SDR 07FDEA03705](https://openairdocs.org/sdr/07FDEA03705), Sep 13, 2007: FLANGE. DAMAGED. TWO MISDRILLED HOLES AT UPPER FLANGE (BEAM) AT C 33 LT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.
- [SDR 07FDEA03704](https://openairdocs.org/sdr/07FDEA03704), Sep 13, 2007: FRAME. CORRODED. FOUND CORROSION AT MILLING FRAME C60, P 22RT REPAIR PERFORMED BY BLEND OUT CORROSION IAW RAS/DATLS/0001942/2004.
- [SDR 07FDEA03703](https://openairdocs.org/sdr/07FDEA03703), Sep 13, 2007: FLANGE. CORRODED. CORROSION FOUND ON UPPER FLANGE C25. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10
- [SDR 07FDEA03701](https://openairdocs.org/sdr/07FDEA03701), Sep 13, 2007: SPLICE. CORRODED. FOUND CORROSION AT SPLICE C20, P50 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03700](https://openairdocs.org/sdr/07FDEA03700), Sep 13, 2007: SPLICE. CRACKED. FOUND CORROSION AT SPLICE C20, P46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03697](https://openairdocs.org/sdr/07FDEA03697), Sep 13, 2007: RIB. CORRODED. FOUND ON LT MLG FWD LUG INNER BORE RIB 5 THE BUSHING TO BE OUT OF ROUND, AFTER REMOVAL OF BUSHING FOUND CORROSION ON THE LUG REPAIR PERFORMED BY CORROSION REMOV
- [SDR 07FDEA03696](https://openairdocs.org/sdr/07FDEA03696), Sep 13, 2007: RIB. CORRODED. FOUND ON RT MLG FWD LUG INNER BORE RIB 5 THE BUSHING TO BE OUT OF ROUND, AFTER REMOVAL OF BUSHING FOUND CORROSION ON THE LUG REPAIR PERFORMED BY CORROSION REMOV
- [SDR 07FDEA03690](https://openairdocs.org/sdr/07FDEA03690), Sep 13, 2007: SKIN PANEL. WORN. ELONGATED HOLES FOUND ON RT WING TO PYLON HYDRAULIC FITTING RIB 8 REPAIR PERFORMED BY REAM UP AND BUSH INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-572
- [SDR 07FDEA03688](https://openairdocs.org/sdr/07FDEA03688), Sep 13, 2007: SKIN PANEL. WORN. FOUND ELONGATED HOLES ON LT WING TO PYLON HYDRAULIC FITTING HOLES RIB 8 REPAIR PERFORMED BY REAM UP AND INSTALL BUSHINGS IAW DRAWING R572-49184 , APPROVED BY EA
- [SDR 07FDEA03686](https://openairdocs.org/sdr/07FDEA03686), Sep 13, 2007: VANE. DENTED. FOUND DENT ON LT INBOARD FLAP VANE NOSE SKIN, RIB 7-8 REPAIR PERFORMED BY CUTTING THE DAMAGED AREA AND INSTALLING A NEW SKIN WITH INNER STRAPS IAW EA 6-5752-810
- [SDR 07FDEA03682](https://openairdocs.org/sdr/07FDEA03682), Sep 13, 2007: SKIN. DELAMINATED. FOUND ON LT INBOARD FLAP LOWER SKIN AT TRAILING EDGE, RIB 3-4, DELAMINATION. IN THIS AREA FOUND ON UPPER SKIN AN OLD DOUBLER INSTALLED. REPAIR PERFORMED BY REMO
- [SDR 07FDEA03681](https://openairdocs.org/sdr/07FDEA03681), Sep 13, 2007: SKIN. CORRODED. DURING REMOVAL OF BOLT 642, NOTED IN SB A310-57-2028 FOUND CORROSION INSIDE THE FITTING BORE, LT WING AREA OF RIB 5 REPAIR PERFORMED BY OVERSIZING THE HOLE IAW 
- [SDR 07FDEA03679](https://openairdocs.org/sdr/07FDEA03679), Sep 13, 2007: SPAR. CORRODED. CORROSION FOUND ON RT ELEVATOR FRONT SPAR WEB NEAR RIB 2A AROUND ONE BONDING POINT REPAIR PERFORMED BY BLENDOUT UNTIL CORROSION REMOVAL IAW EA 6-5520-79603 AND 
- [SDR 07FDEA03675](https://openairdocs.org/sdr/07FDEA03675), Sep 13, 2007: SKIN. WORN. FOUND ON PYLON NR 1 AT RIB 8 INBOARD AND OUTBOARD SIDE THE HOLE FOR SUPPORT WORN DOUBLER REPAIR PERFORMED IAW SRM 54-51-31 FIG 201.
- [SDR 07FDEA03673](https://openairdocs.org/sdr/07FDEA03673), Sep 13, 2007: FITTING. WORN. AT RT SPIGOT FITTING FWD OUTBOARD SIDE FOUND WEAR MARKS REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5720-79605 AND RAS/BAE/0818/2004 ISS A.
- [SDR 07FDEA03671](https://openairdocs.org/sdr/07FDEA03671), Sep 13, 2007: ATTACH FITTING. CHAFED. FOUND CHAFING MARKS, ENLARGED HOLES AND NOT CORRECT INSTALLED BUSHINGS AT PYLON NR 2 PYLON TO WING ATTACH FITTING LUGS AT RIB 12. REPAIR PERFORMED BY OVERSIZING
- [SDR 07FDEA03667](https://openairdocs.org/sdr/07FDEA03667), Sep 13, 2007: FITTING. CORRODED. FOUND CORROSION AT RUN OUT FITTING AT P 44, C16A-17A LT. REPAIR PERFORMED BY REPLACEMENT OF RUNOUT FITTING IAW DRAWING R536-10440.
- [SDR 07FDEA03666](https://openairdocs.org/sdr/07FDEA03666), Sep 13, 2007: SKIN PANEL. DENTED. FOUND DENT ON SKIN C 94-95, P3-4 RT OUT OF LIMIT. DOUBLER REPAIR PERFORMED IAW SRM 53-19-12 FIG 201.
- [SDR 07FDEA03661](https://openairdocs.org/sdr/07FDEA03661), Sep 13, 2007: STRINGER. CORRODED. FOUND CORROSION ON STRINGER P 56 RT, C 64-65 OUT OF LIMIT STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.
- [SDR 07FDEA03660](https://openairdocs.org/sdr/07FDEA03660), Sep 13, 2007: FLOORBEAM. CORRODED. FOUND CORROSION AT CROSSBEAM C 67, C66. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15 FIG 207 .
- [SDR 07FDEA03657](https://openairdocs.org/sdr/07FDEA03657), Sep 13, 2007: STRINGER. CORRODED. FOUND CORROSION ON STRINGER P50 AT C80, LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.
- [SDR 07FDEA03654](https://openairdocs.org/sdr/07FDEA03654), Sep 13, 2007: BEAM. CORRODED. CORROSION FOUND ON LOWER SILL BEAM OF AFT CARGO DOOR AT C59A. REPAIR PREFORMED BY TRIM OUT THE AFFECTED AREA AND FABRICATE A STRAP IAW EA 6-5310-79580 AND RAS/D
- [SDR 07FDEA03652](https://openairdocs.org/sdr/07FDEA03652), Sep 13, 2007: SKIN PANEL. CORRODED. CORROSION FOUND ON SKIN PANEL C78/80, P 45-50 RT, IN SERVICE PANEL AREA. REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION REMOVAL AND REPLACING THE TOILET SERVICE 
- [SDR 07FDEA03649](https://openairdocs.org/sdr/07FDEA03649), Sep 13, 2007: ANGLE. CORRODED. FOUND CORROSION AFT PRESSURE BULKHEAD CIRCUMFERENTIAL STRAP, INNER RIM ANGLE AND FRAME COUPLING AT C80/82, P25LH TO 36RH. REPAIR PERFORMED BY CUT OUT OF DAMAGED
- [SDR 07FDEA03643](https://openairdocs.org/sdr/07FDEA03643), Sep 13, 2007: STRINGER. CORRODED. FOUND CORROSION ON STRINGER P 57 LT, C 69-70 OUT OF LIMIT. STRINGER REPAIR PERFORMED SRM 53-10-14 FIG 201.
- [SDR 07FDEA03639](https://openairdocs.org/sdr/07FDEA03639), Sep 13, 2007: STRINGER. CORRODED. FOUND CORROSION ON STRINGER CONNECTION AT C80, P 38 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA03638](https://openairdocs.org/sdr/07FDEA03638), Sep 13, 2007: STRINGER. CORRODED. CORROSION FOUND AT STRINGER P38, C79-80. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201
- [SDR 07FDEA03636](https://openairdocs.org/sdr/07FDEA03636), Sep 13, 2007: SKIN PANEL. CORRODED. CORROSION FOUND ON INTERNAL SKIN C-37-38, P55LT-55RT DOUBLER REPAIR PERFORMED IAW SRM 53-10-12 FIG 221 AND 203.
- [SDR 07FDEA03635](https://openairdocs.org/sdr/07FDEA03635), Sep 13, 2007: STRINGER. CORRODED. FOUND CORROSION AT STRINGER P 37 RT, C37 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.
- [SDR 07FDEA03584](https://openairdocs.org/sdr/07FDEA03584), Sep 11, 2007: STRINGER. CORRODED. FOUND CORROSION ON CLIP AT C 71, P57-56RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

All 95: https://openairdocs.org/deregistered/N432FE-2010-05-10/reports.md

## Other aircraft with N432FE

- [Cancelled 2024-04-02](https://openairdocs.org/deregistered/N432FE-2024-04-02): Dehavilland DHC-8-102, S/N 237, built 1990. Exported to Canada. Owner: [Dynamic Avlease Inc](https://openairdocs.org/faa-owner/DYNAMIC%20AVLEASE%20INC), [Bridgewater, VA](https://openairdocs.org/faa-place/VA/Bridgewater)

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