# N402FE: 1983 Airbus Industrie A310-203, registration cancelled 2016-01-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 25, 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: 201
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 10, 1995
- Certificate issued: April 5, 2010
- Last registry action: February 4, 2014
- Mode S code: A4B491
- 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/N402FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=402FE
- Page: https://openairdocs.org/deregistered/N402FE-2016-01-25

From the FAA registry file of October 28, 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 (181, newest 50)

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

- [SDR FDEA201007162570](https://openairdocs.org/sdr/FDEA201007162570), Jul 16, 2010: SKIN. CORRODED. RT WING UPPER SKIN SURFACE 8 INCH AFT OF REAR SPAR AND RIB 4 HAS 4 SQ INCH OF CORROSION COMMON TO FASTNER HEAD. REPAIR ACCOMPLISHED IAW EA 6-5730-135225 IAW APP
- [SDR FDEA201007132499](https://openairdocs.org/sdr/FDEA201007132499), Jul 13, 2010: FRAME. DENTED. FUSELAGE INTERNAL STRUCTURE AT FR 54.2 HAS (2 EA) AREAS DENTED. AREA NR1=.0781 IN.D X .7500 IN W . AREA NR2 =.0469 IN D X .5 IN W BETWEEN STRINGER 12-15 LT SIDE
- [SDR FDEA201007122480](https://openairdocs.org/sdr/FDEA201007122480), Jul 12, 2010: FITTING. CORRODED. NR 2 PYLON PYRAMID FITTING BASE PLATE UPPER SURFACE HAS CORROSION AROUND 4 EA MOUNT HOLES (APPROX 6 SQ IN TOTAL) REMOVED CORROSION FROM NR 2 PYLON PYRAMID FITTI
- [SDR FDEA201007112475](https://openairdocs.org/sdr/FDEA201007112475), Jul 11, 2010: FRAME. DENTED. FUSELAGE INTERNAL STRUCTURE FR 54.3 L HAS A DENT APPROX 3/32 INCH DEEP AND 1.5 IN DIAM. BETWEEN STR 14-13 LT MEASURED DENT ON FR 54.3 AT STR. 13L-14L FOUND TO B
- [SDR FDEA201007082425](https://openairdocs.org/sdr/FDEA201007082425), Jul 8, 2010: RIB. GOUGED. LT WING L/E KRUEGER FLAP LOWER LIP OTBD L/E GOUGED, 2 SQ INCHES FOUND DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-41-11. REMOVED DAMAGED END CAP AND FABRICATED RE
- [SDR FDEA201007082424](https://openairdocs.org/sdr/FDEA201007082424), Jul 8, 2010: SHEAR TIE. CRACKED. FWD CARGO DOOR STRUCTURE SKIN SUPPORT ANGLE AFT OF ACTUATOR HINGE FITTING LOWER END HAS 1 IN CRACK REMOVED DAMAGED ANGLE AND STRINGER CLIPS, FABRICATED REPLACEM
- [SDR FDEA201007082422](https://openairdocs.org/sdr/FDEA201007082422), Jul 8, 2010: SKIN. DAMAGED. FWD CARGO DOOR HAS DAMAGE STRUCTURE WEB AND HOLE BETWEEN FR 22A AND FR 23 AT BEAM 2. REMOVED DAMAGED AREA OF DOOR SKIN BY CUT OUT OF APPROX 2 IN X 3 IN AND INST
- [SDR FDEA201007082421](https://openairdocs.org/sdr/FDEA201007082421), Jul 8, 2010: RIB. DAMAGED. RT WING KRUEGER FLAP FWD OTBD CORNER HAS IMPACT DAMAGE TO THE EXTERIOR SKIN & CLOSE OUT RIB. FOUND DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-41-11. REMOVED DAMA
- [SDR FDEA201007082406](https://openairdocs.org/sdr/FDEA201007082406), Jul 8, 2010: SPAR. CORRODED. VERTICAL STAB T/E PANEL ATTACH ANGLEAT RT SIDE HAS APPROX 2 SQ INCH OF VISIBLE CORROSION BETWEEN RIB 9 AND AT RIB 10 AT STA 286 AND 309 (2 EA LOCATIONS) BETWEEN
- [SDR FDEA201007072398](https://openairdocs.org/sdr/FDEA201007072398), Jul 7, 2010: CROSSBEAM. CRACKED. CLS AT FR 36 BETWEEN SEAT TRACKS 3 RT AND 2 RT FWD SIDE LWR SURFACE REPAIR ANGLE CRACKED ON RADIUS, APPROX 1.5 IN LONG REMOVED EXISTING REPAIR ANGLE AT FRAME 36
- [SDR FDEA201007072396](https://openairdocs.org/sdr/FDEA201007072396), Jul 7, 2010: SEAT TRACK. CORRODED. SEAT TRACK 5 RT AT FR 34 TO FR 36 HAS CORROSION AT 3 EA LOCATIONS UPPER SURFACE, APPROX 3 SQ IN REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF TRACK, FAB
- [SDR FDEA201007072395](https://openairdocs.org/sdr/FDEA201007072395), Jul 7, 2010: FLOORBEAM. CORRODED. MAIN DECK CARGO COMPT FLOORBEAM CORRODED ON UPPER SURFACE,FR 14 AT SEAT TRACK 3 LT REMOVED LEVEL 1CORROSION. REMOVED, FABRICATED REPLACEMENT TRACK SECTION AND R
- [SDR FDEA201007072394](https://openairdocs.org/sdr/FDEA201007072394), Jul 7, 2010: FLOOR PANEL. CORRODED. FRAME 26 SEAT TRACK 4 LT OTBD JUST AFT OF CLS, FOUND CORROSION IN FLOOR PANEL, APPROX 1 SQ INCH REMOVED LEVEL 1 CORROSION. MATERIAL LOSS OUT OF LIMITS IAW SRM 5
- [SDR FDEA201007072393](https://openairdocs.org/sdr/FDEA201007072393), Jul 7, 2010: SEAT TRACK. CORRODED. SEAT TRACK 6LT INBD SIDE UPPER SURFACE IS CORRODED JUST FWD OF FR 33, APPROX 1 SQ IN REMOVED LEVEL 1 CORROSION. CUT OUT DAMAGED SECTION OF SEAT TRACK 6 LT BETWE
- [SDR FDEA201007022330](https://openairdocs.org/sdr/FDEA201007022330), Jul 2, 2010: WEB. DAMAGED. WEB BETWEEN FR 14 AND FR 15 BENEATH TRACK 3 LT IS DAMAGED REMOVED DAMAGED WEB, FABRICATED REPLACEMENT WEB IAW DWG A53610800 AND INSTALLED REPLACEMENT WEB BETWEE
- [SDR FDEA201007022329](https://openairdocs.org/sdr/FDEA201007022329), Jul 2, 2010: WEB. DAMAGED. WEB HAS DAMAGED HOLES AT FR 10 AND FR 12A SEAT TRACK 3 LT REMOVED DAMAGED WEB, FABRICATED REPLACEMENT WEB IAW DWG A53610800 AND INSTALLED REPLACEMENT WEB BETWEE
- [SDR FDEA201007022328](https://openairdocs.org/sdr/FDEA201007022328), Jul 2, 2010: WEB. DAMAGED. WEB BETWEEN FRAME 12A AND 14, BENEATH TRACK 3 LT, IS DAMAGED. REMOVED DAMAGED WEB, FABRICATED REPLACEMENT WEB IAW DWG A53610800 AND INSTALLED REPLACEMENT WEB BE
- [SDR FDEA201007022327](https://openairdocs.org/sdr/FDEA201007022327), Jul 2, 2010: FLOORBEAM. CORRODED. MAIN DECK CARGO COMPT CROSSOVER BEAM HAS CORROSION ON UPPER SURFACE FR 14, BETWEEN SEAT TRACKS 3 LT AND 4 LT. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED BEAM, F
- [SDR FDEA201007022324](https://openairdocs.org/sdr/FDEA201007022324), Jul 2, 2010: PLATE. CORRODED. SUB FLOOR CORRODED APPROX 1 SQ IN AFT OF FR 25 BETWEEN SEAT TRACKS 4 LT AND TRACK 3 LT REMOVED LEVEL 1 CORROSION. R & R SUB FLOOR THRUST PLATE BETWEEN FR 25 AND
- [SDR FDEA201007022323](https://openairdocs.org/sdr/FDEA201007022323), Jul 2, 2010: STRINGER. CORRODED. AFT CARGO COMPT BILGE AREA, STR 44 LT HAS CORROSION ON VERTCAL LEG FROM FR 62 TO FR 63,APPROX 10 SQ IN. REMOVED LEVEL 1 CORROSION. CUT OUT DAMAGED SECTION OF ST
- [SDR FDEA201007012313](https://openairdocs.org/sdr/FDEA201007012313), Jul 1, 2010: SKIN. CORRODED. RT ELEVATOR LWR SURFACE SKIN HAS CORROSION 56 INCHES FROM OTBD END, 6 INCHES FWD OF AFT EDGE APPROX 5 SQ IN TOTAL , APPROX ER 34 REMOVED LEVEL 1 CORROSION IAW S
- [SDR FDEA201007012312](https://openairdocs.org/sdr/FDEA201007012312), Jul 1, 2010: FLOOR SUPPORT. CORRODED. MDCC SEAT TRACK 5L HAS A 4 SQ INCH AREA OF CORROSION BENEATH FLOOR PANEL FR 16A. REMOVED CORROSION IAW SRM 51-74-10 , CHECKED LIMITS IAW SRM 53-10-15 FIG 101 FO
- [SDR FDEA201007012311](https://openairdocs.org/sdr/FDEA201007012311), Jul 1, 2010: FLOORBEAM. CRACKED. MAIN DECK FLOORBEAM FWD FACE HAS 0.188 INCH CRACK , ON FR 38 , 67 INCHES FROM CTR LINE, LT SIDE. TRIMMED OUT DAMAGE AREA IAW SRM 53-10-15, FIG 201, NDT CHECK IA
- [SDR FDEA201007012305](https://openairdocs.org/sdr/FDEA201007012305), Jul 1, 2010: FLOORBEAM. CORRODED. MDCC FLOORBEAM HAS CORROSION ON UPPER SURFACE AT FR 14 6IN. BETWEEN SEAT TRACK 3L AND 4L. REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND CROSSBEAM SE
- [SDR FDEA201007012304](https://openairdocs.org/sdr/FDEA201007012304), Jul 1, 2010: FLOORBEAM. DAMAGED. BULK CARGO COMPT FLOOR STRUCTURE FRAME 69 RBL 20 FLOORBEAM SUPPORT HAS MISDRILLED HOLE THRU UPPER CHORD FWD SIDE. REMOVED DAMAGE AND FABRICATED SPLICE IAW SRM 5
- [SDR FDEA201007012303](https://openairdocs.org/sdr/FDEA201007012303), Jul 1, 2010: SKIN. CORRODED. RT ELEVATOR UPPER SURFACE HAS APPROX 1.5 SQ IN OF CORROSION AT APPROX. ER36 1 IN. FWD OF AFT EDGE REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND UPPE
- [SDR FDEA201007012302](https://openairdocs.org/sdr/FDEA201007012302), Jul 1, 2010: SKIN. CORRODED. RT ELEVATOR LWR SURFACE CTR SPLICE HAS CORROSION 8 IN FWD FROM AFT EDGE APPROX 1.5 SQ IN APPROX STA ER21. REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FO
- [SDR FDEA201006302296](https://openairdocs.org/sdr/FDEA201006302296), Jun 30, 2010: SUPPORT FITTING. CRACKED. AFT CARGO BILGE AREA- FR 54 BULKHEAD SUPPORT FITTING AT STR 53R HAS A 1 IN. CRACK ON OTBD. SIDE ABOUT 3 IN AFT OF BULKHEAD. REMOVED SPLICE AND 2 EA ATTACH FITTI
- [SDR FDEA201006302295](https://openairdocs.org/sdr/FDEA201006302295), Jun 30, 2010: SEAT TRACK. CORRODED. SEAT TRACK 6R HAS 5EA AREAS CORRODED APPROX 6 SQ IN FROM FR 34 TO FR 39 REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM
- [SDR FDEA201006302294](https://openairdocs.org/sdr/FDEA201006302294), Jun 30, 2010: SEAT TRACK. CORRODED. 5L SEAT TRACK HAS CORROSION AT 7 EA. LOCATIONS BETWEEN FR 33 AND FR38.1 APPROX 15 SQ INCH REMOVED CORROSION IAW SRM 51-74-10, PAGE 205, CHECKED FOUND TO BE OUT 
- [SDR FDEA201006302293](https://openairdocs.org/sdr/FDEA201006302293), Jun 30, 2010: SEAT TRACK. CORRODED. SEAT TRACK 6L HAS 7 AREAS OF CORROSION BETWEEN FR 35 TO FR38 APPROX 10 SQ INCH. REMOVED CORROSION IAW SRM 51-74-10, CHECKED FOUND TO BE OUT OF LIMITS IAW SRM 53
- [SDR FDEA201006302292](https://openairdocs.org/sdr/FDEA201006302292), Jun 30, 2010: STRINGER. CORRODED. AFT CARGO COMPARTMENT BILGE AREA STR. 45L HAS CORROSION AT FR60 TO FR60 2 INCHES APPROX TOTAL 2 SQ INCHES. REMOVED CORROSION IAW SRM 51-74-10, CHECKED FOUND OUT
- [SDR FDEA201006302290](https://openairdocs.org/sdr/FDEA201006302290), Jun 30, 2010: SEAT TRACK. CORRODED. MDCC SEAT TRACK HAS CORROSION 4 EA AREAS ON UPPER SURFACE BETWEEN FR 15 AND FR 16A AT 4L. REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS AND FOUND TO BE OUT
- [SDR FDEA201006302285](https://openairdocs.org/sdr/FDEA201006302285), Jun 30, 2010: FLOORBEAM. CORRODED. AFT CARGO COMPT FLOORBEAM FR63, RBL 45, PRODUCTION SPLICE HAS CORROSION BETWEEN IT AND T-CHORD APPROX. 5" LONG (EXFOLIATION) REMOVED CORROSION ON AFT CARGO COMP
- [SDR FDEA201006302283](https://openairdocs.org/sdr/FDEA201006302283), Jun 30, 2010: SEAT TRACK. CORRODED. SEAT TRACK 4L IS CORRODED AT 4 EA LOCATIONS FROM FR 33 TO FR 38.1 APPROX 6 SQ IN. REMOVED CORROSION IAW SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-16, FIG 101, 
- [SDR FDEA201006302280](https://openairdocs.org/sdr/FDEA201006302280), Jun 30, 2010: SEAT TRACK. CORRODED. SEAT TRACK 2R INBD SIDE CORRODED AT 4 EA LOCATIONS FROM APPROX 16 IN FWD OF FR33 TO 10 INCHES AFT OF FR 33 APPROX 5 SQ INCH TOTAL. REMOVED CORROSION IAW SRM 51-
- [SDR FDEA201006302279](https://openairdocs.org/sdr/FDEA201006302279), Jun 30, 2010: SEAT TRACK. CORRODED. SEAT TRACK 2L APPROX 18 IN FWD OF FR33 IS CORRODED APPROX 1 SQ IN REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS IAW SRM 53-10-16, FIG 101, FOUND TO BE OUT 
- [SDR FDEA201006302278](https://openairdocs.org/sdr/FDEA201006302278), Jun 30, 2010: SEAT TRACK. CORRODED. SEAT TRACK 2R HAS 2EA. LOCATIONS CORRODED BETWEEN FR49 TO FR46. CORROSION IS ON THE OTBD UPPER AND LOWER SURFACE APPROX. 4SQ IN. REMOVED CORROSION IAW SRM 51-74
- [SDR FDEA201006302268](https://openairdocs.org/sdr/FDEA201006302268), Jun 30, 2010: SKIN. DAMAGED. LT WING INBD FLAP LWR T/E SURFACE HAS IMPACT DAMAGE MEASURING 6 IN. X 6 IN. X .32 IN. D REPAIRED IMPACT DAMAGE ON LT WING INBD FLAP LWR T/E SURFACE USING COR RE
- [SDR FDEA201006302267](https://openairdocs.org/sdr/FDEA201006302267), Jun 30, 2010: SEAT TRACK. CORRODED. SEAT TRACK NR1 HAS 2EA LOCATIONS THAT ARE CORRODED FR 33 TO APPROX 18 IN FWD OF FR 33 REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND TRACK SECTION OU
- [SDR FDEA201006292225](https://openairdocs.org/sdr/FDEA201006292225), Jun 29, 2010: FLOOR SUPPORT. CORRODED. FLOORBOARD SUPPORT STRUCTURE THAT TURNS INTO THE 5L SEAT TRACK IS CORRODED, FR 14 TO FR 15 APPROX 72 IN LONG. REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVA
- [SDR FDEA201006242141](https://openairdocs.org/sdr/FDEA201006242141), Jun 24, 2010: SEAT TRACK. CORRODED. MDCC SEAT TRACK 3R , AT FR 54.2 HAS 1 SQ INCH OF CORROSION. REMOVED CORROSION IAW SRM 51-74-10 , CHECKED SEAT TRACK 3R AT FR 54.2 FOUND OUT OF LIMITS IAW SRM 53
- [SDR FDEA201006242140](https://openairdocs.org/sdr/FDEA201006242140), Jun 24, 2010: SEAT TRACK. CORRODED. MDCC SEAT TRACK 4R BETWEEN FRAMES 18 & 19 HAS 5 SQ. INCH OF CORROSION. REMOVED CORROSION IAW SRM 51-74-10, PAGE 205 , CHECKED FOUND TO BE OUT OF LIMITS IAW SRM 
- [SDR FDEA201006192080](https://openairdocs.org/sdr/FDEA201006192080), Jun 19, 2010: SKIN. DENTED. RAMP REPORTED 3 SMALL DENTS 10 IN AFT OF AFT LOWER CARGO COMPT DOOR. REF WRITE UP WRI 53-30 1790. CUT OUT DAMAGE AREA IAW SRM 53-17-12, FIG 205, NDT VERIFIED NO
- [SDR FDEA201006192079](https://openairdocs.org/sdr/FDEA201006192079), Jun 19, 2010: STRINGER. CORRODED. AFT CARGO COMPT HAS CORROSION AT STRINGER 31 RT FROM FRAME 54.1 TO FRAME 54.1, 12 IN TOTAL AREA APPROX 13 SQ IN. REMOVE CORROSION IAW SRM 51-74-10, CHECK FOUND 
- [SDR FDEA201006192078](https://openairdocs.org/sdr/FDEA201006192078), Jun 19, 2010: SEAT TRACK. CORRODED. MAIN CABIN FR 54 SEAT TRACK 3R CORROSION ON A FLANGE UPPER SURFACE. REMOVED CORROSION IAW SRM 51-74-10 CHECK LIMIT FOUND OUT OF LIMIT IAW SRM 53-10-16, FIG 101.
- [SDR FDEA201006192077](https://openairdocs.org/sdr/FDEA201006192077), Jun 19, 2010: FLOORBEAM. CORRODED. AFT CARGO COMPT FRAME 58 LT SIDE FLOOR SUPPORT BEAM, LBL 44 UNDER SIDE HAD EXFOLIATION CORROSION APROX 4SQ IN IN TOTAL. REMOVED CORROSION IAW SRM 51-74-10 CHECK
- [SDR FDEA201006192076](https://openairdocs.org/sdr/FDEA201006192076), Jun 19, 2010: FLOOR SUPPORT. CORRODED. BULK CARGO COMPT FLOOR STRUCTURE LONGITUDINAL SUPPORT BETWEEN FRAME 65-66, LBL 5. UPPER AND LOWER SURFACES HAVE CORROSION IN AND AROUND FASTENER HOLES, APPROX 1
- [SDR FDEA201006192072](https://openairdocs.org/sdr/FDEA201006192072), Jun 19, 2010: STRINGER. CORRODED. FUSELAGE SKIN STRINGER HAS 1" X 1" CORROSION FWD OF AFT PRESSURE BULK HEAD 10" FWD OF FR 80/82 STR 56R REMOVED CORROSION IAW SRM 51-74-10, PAGE 205, FIG 201. CH
- [SDR FDEA201006192071](https://openairdocs.org/sdr/FDEA201006192071), Jun 19, 2010: STRINGER. CORRODED. FUSELAGE SKIN STRINGER HAS 1" X 1" CORROSION FWD OF AFT PRESSURE BULKHEAD 10" FWD OF FR 80/82 STR 56L. REMOVED CORROSION IAW SRM 51-74-10, PAGE 205, FIG 201, CH

All 181: https://openairdocs.org/deregistered/N402FE-2016-01-25/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 20050527010369I](https://openairdocs.org/incident/20050527010369I), May 27, 2005: Airbus A310203 (N402FE), Omaha, NE. (-23) N402FE, A310, was being operated as federal express flight 1475 from memphis, TN, to Omaha, NE. At FL340 the crew received a fluid low level alert,…

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.