# N403FE: 1983 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: 230
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 10, 1995
- Certificate issued: April 27, 2010
- Last registry action: October 20, 2023
- Mode S code: A4B848
- 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/N403FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=403FE
- Page: https://openairdocs.org/deregistered/N403FE-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 (218, newest 50)

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

- [SDR FDEA201402240394](https://openairdocs.org/sdr/FDEA201402240394), Feb 24, 2014: COALESCER BAG. DIRTY. AS TAKEOFF POWER WAS APPLIED ACRID SMELL DETECTED BY FIRST OFFICER THEN CAPTAIN, NOT VISIBLE, LOW SPEED REJECT AT 50 - 60 KTS. SHUTDOWN ON RWY & TUGGED TO GATE.
- [SDR FDEA201210303780](https://openairdocs.org/sdr/FDEA201210303780), Oct 30, 2012: HINGE FITTING. CRACKED. LEFT MLG UNSAFE DOOR INDICATION ON T/O. THEN UNSAFE MLG INDICATION ON APPROACH. FOUND LT MLG CENTER HINGE FITTINGS FRACTURED AT ACTUATOR ATTACHEMENT LUG, AND CR
- [SDR FDEA201208233144](https://openairdocs.org/sdr/FDEA201208233144), Aug 23, 2012: FILTER. CLOGGED. REJECTED TAKEOFF AT 70 KTS FOR NR 2 ENGINE FUEL FILTER CLOG ALERT ON ECAM. REPLACED NR 2 ENGINE MAIN FUEL FILTER IAW MM 73-12-03-02 IDLE LEAK CHECKED GOOD. RAN 
- [SDR FDEA201207152580](https://openairdocs.org/sdr/FDEA201207152580), Jul 15, 2012: SKIN. DAMAGED. DURING INSPECTION OF CIRCUMFERENTIAL SKIN JOINT AT FR 54 BETWEEN STGR 45 LT AND STGR 44 LT FASTENER HOLE 1EA WITH PRIOR BUSHING REPAIR IS ELONGATED. WORK IN CON
- [SDR FDEA201207122560](https://openairdocs.org/sdr/FDEA201207122560), Jul 12, 2012: SHOCK ABSORBER. GOUGED. LEFT MLG THRU HOLE FOR BOGIE BEAM PIN STRUT SIDE, LT INBD BUSHING GOUGED IN SEVERAL PLACES. DEEPEST GOUGE MEASURES .014" WITH MECHANICAL GAGE COMPLIED WITH EA 6
- [SDR FDEA201207122557](https://openairdocs.org/sdr/FDEA201207122557), Jul 12, 2012: WEB. CRACKED. NR 2 ENGINE PYLON OTBD LATERAL PANEL BETWEEN RIB 6 -7 HAS TWO CRACKS BOTH MEASURE .75 OF AN INCH. STOP DRILLED CRACKS IAW SRM 54-52-31, PG 212, 213, 214 CONFIG 
- [SDR FDEA201207032461](https://openairdocs.org/sdr/FDEA201207032461), Jul 3, 2012: FLOORBEAM. MISREPAIRED. FLOORBEAM MISREPAIRED. REPAIRED IAW EA 6-5310-161396 COMPLING WITH PART 1 OF EA AND RDAS REF 70563824/003/2012 ISSUE A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-1
- [SDR FDEA201207032460](https://openairdocs.org/sdr/FDEA201207032460), Jul 3, 2012: FLOORBEAM. FAILED. MAIN CABIN FLOORBEAM MISREPAIRED. REPAIRED IAW EA 6-5310-161396 COMPLING WITH PART 2 OF EA AND RDAS REF 70563824/003/2012 ISSUE A. REPAIR CLASSIFIED AS MAJOR IA
- [SDR FDEA201206272367](https://openairdocs.org/sdr/FDEA201206272367), Jun 27, 2012: FRAME. DAMAGED. FRAME 24 AT STRINGER 13R WAS FOUND WITH VISIBLE DISTORTION TO UNDERLYING FRAME SPLICES. FOUND FRAME SECTION DAMAGE BEYOND ECONOMICAL REPAIR AND R & R FRAME SECT
- [SDR FDEA201206222295](https://openairdocs.org/sdr/FDEA201206222295), Jun 22, 2012: FLOOR PANEL. CRACKED. DURING INSTALLATION, FOUND FLOOR PANEL 252BF CRACKED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201206202281](https://openairdocs.org/sdr/FDEA201206202281), Jun 20, 2012: WEDGE. DEBONDED. LEFT ELEVATOR T/E WEDGE AT RIB 11 AND 14 SPLICES UPPER AND LOWER SURFACES ARE DEBONDING AND CORRODED. REPAIRED IAW A300-600 SRM 55-21-11 C1 PARA. 5.I. FIG. 209.
- [SDR FDEA201206202282](https://openairdocs.org/sdr/FDEA201206202282), Jun 20, 2012: SKIN. DELAMINATED. RT ELEVATOR LOWER SKIN AT RIB 17 HAS 2EA AREAS OF DELAMINATION.
- [SDR FDEA201206192268](https://openairdocs.org/sdr/FDEA201206192268), Jun 19, 2012: SEAT TRACK. DAMAGED. FLOOR CLEVIS ADAPTER BETWEEN SEAT TRACK 2R AND 3R INSTALLED NOT ALIGN AND HAS 2 EA ELONGATED FASTENER HOLES. R & R DUMMY TRACK IAW SRM 51-72-10.
- [SDR FDEA201206192267](https://openairdocs.org/sdr/FDEA201206192267), Jun 19, 2012: SEAT TRACK. DAMAGED. FLOOR SEAT TRACK 2R HAS 5 EA ELONGATED HOLES FROM FRAME 54 TO 54.2 AT RT FLANGE. R & R SEAT TRACK 2R BETWEEN FRAMES 54 AND 54.2 IAW SRM 51-72-10.
- [SDR FDEA201206182256](https://openairdocs.org/sdr/FDEA201206182256), Jun 18, 2012: FLOORBEAM. BENT. FLOORBEAM TOP FLANGE IS BENT 10 SQUARE INCHES AT CLEVIS ADAPTER BETWEEN SEAT TRACKS 2L AND 3L AND FRAME 37. CUT, REMOVED DAMAGED SECTION & SPLICED IN NEW SECTIO
- [SDR FDEA201206182254](https://openairdocs.org/sdr/FDEA201206182254), Jun 18, 2012: FLOORBOARD. DELAMINATED. FLOORBOARD 231NG DELAMINATED IN MULTIPLE AREAS APPROX 30 SQUARE INCHES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201206092174](https://openairdocs.org/sdr/FDEA201206092174), Jun 9, 2012: SKIN. FAILED. RT WING NR 2 SLAT NOSE SKIN BETWEEN RIBS 35 TO 37 IS 4.3" X 2.8" MISREPAIRED. REPAIRED IAW SRM 57-43-11, FIG 202 SHEETS 6 AND 14 PAGES 219 AND 227. COMPLIED WIT
- [SDR FDEA201206092171](https://openairdocs.org/sdr/FDEA201206092171), Jun 9, 2012: STRINGER. FAILED. STRINGER 55 RIGHT MISREPAIRED. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201206082163](https://openairdocs.org/sdr/FDEA201206082163), Jun 8, 2012: STRINGER. MISREPAIRED. STRINGER 53 LEFT MISREPAIRED BETWEEN FRAMES 63 AND 64. REPAIRED IAW SRM 53-10-14, FIG 201 PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201206082155](https://openairdocs.org/sdr/FDEA201206082155), Jun 8, 2012: STRINGER. MISREPAIRED. STRINGER 53 LEFT MISREPAIRED BETWEEN FRAMES 61 TO 63. REPAIRED IAW SRM 53-10-14. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201206082165](https://openairdocs.org/sdr/FDEA201206082165), Jun 8, 2012: STRINGER. MISREPAIRED. STRINGER 54L BETWEEN FRAMES 65 AND 66 MISREPAIRED. REPAIRED SRM 53-10-14, FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201206082164](https://openairdocs.org/sdr/FDEA201206082164), Jun 8, 2012: STRINGER. MISREPAIRED. STRINGER 53L BETWEEN FRAMES 66 AND 69 MISREPAIRED. REPAIRED IAW SRM 53-10-14 FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201206082154](https://openairdocs.org/sdr/FDEA201206082154), Jun 8, 2012: STRINGER. MISREPAIRED. STRINGER 51 LEFT MISREPAIRED BETWEEN FRAMES 61 TO 63. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201206082166](https://openairdocs.org/sdr/FDEA201206082166), Jun 8, 2012: STRINGER. MISREPAIRED. STRINGER 56 LEFT MISREPAIRED. REPAIRED IAW SRM 53-10-14 FIG. 201 PGS. 205/206.
- [SDR FDEA201206082160](https://openairdocs.org/sdr/FDEA201206082160), Jun 8, 2012: STRINGER. MISREPAIRED. STRINGER 54 LEFT MISREPAIRED. REPAIRED IAW SRM 53-10-14 FIG. 201 PGS. 205/206
- [SDR FDEA201206082157](https://openairdocs.org/sdr/FDEA201206082157), Jun 8, 2012: STRINGER. MISREPAIRED. STRINGER 53 LEFT MISREPAIRED. REPAIRED IAW A310 SRM 53-10-14 FIG. 201 PGS. 205/206.
- [SDR FDEA201206082156](https://openairdocs.org/sdr/FDEA201206082156), Jun 8, 2012: STRINGER. MISREPAIRED. STRINGER 55 LEFT MISREPAIRED. REPAIRED IAW A310 SRM 53-10-14 FIG. 201 PGS. 205/206.
- [SDR FDEA201206082158](https://openairdocs.org/sdr/FDEA201206082158), Jun 8, 2012: FLOORBOARD. DAMAGED. FLOORBOARD 162HF HAS IMPACT DAMAGE OVER 50 PERCENT OF PANEL. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005 REV J, REF DWG SRZ 25-011.
- [SDR FDEA201206072136](https://openairdocs.org/sdr/FDEA201206072136), Jun 7, 2012: STRINGER. MISREPAIRED. STRINGER 53 LEFT, MISREPAIRED. REPAIRED PER SRM 53-10-14 FIG 201 PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA201206072132](https://openairdocs.org/sdr/FDEA201206072132), Jun 7, 2012: STRINGER. MISREPAIRED. STRINGER 50 LEFT MISREPAIRED, FRAMES 59 TO 60. REPAIRED PER SRM 53-10-14 FIG 201 PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA201206072131](https://openairdocs.org/sdr/FDEA201206072131), Jun 7, 2012: STRINGER. MISREPAIRED. STRINGER 47 LEFT MISREPAIRED, FRAMES 59 TO 60. REPAIRED PER SRM 53-10-14 FIG 201 PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA201206072120](https://openairdocs.org/sdr/FDEA201206072120), Jun 7, 2012: SEAT TRACK. CORRODED. SEAT TRACK 3R UPPER SURFACE BETWEEN SCALLOPS CORRODED 2 EA AREAS BET, FR 38.2 AND FR.40 MEASURED 6 SQ". REMOVED LEVEL 1 CORROSION ON SEAT TRACK 3R (AREA 1)BET 3
- [SDR FDEA201206062114](https://openairdocs.org/sdr/FDEA201206062114), Jun 6, 2012: STRINGER. MISREPAIRED. STRINGER 51 LEFT MISREPAIRED. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203-206.
- [SDR FDEA201206062112](https://openairdocs.org/sdr/FDEA201206062112), Jun 6, 2012: FLOORBOARD. DAMAGED. FWD CARGO FLOORBOARD 132RF DAMAGE ON THE EDGE ABOUT 3 FT. LONG. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201206062110](https://openairdocs.org/sdr/FDEA201206062110), Jun 6, 2012: FLOORBOARD. DELAMINATED. FLOORBOARD 242ZJ DELAMINATED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201206062109](https://openairdocs.org/sdr/FDEA201206062109), Jun 6, 2012: FLOORBOARD. DAMAGED. FLOORBOARD 231AH HAS FIVE CRUSHED AREAS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201206062108](https://openairdocs.org/sdr/FDEA201206062108), Jun 6, 2012: FLOORBOARD. DAMAGED. FLOORBOARD 231NH HAS THREE CRUSHED AREAS 5 INCHES LONG. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201206052096](https://openairdocs.org/sdr/FDEA201206052096), Jun 5, 2012: FLOORBEAM. MISREPAIRED. FLOORBEAM MISREPAIRED AT FRAME 36. REPAIRED IAW SRM 53-10-15, FIG 207, PAGES 237 TO 242. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201206052099](https://openairdocs.org/sdr/FDEA201206052099), Jun 5, 2012: STRINGER. MISREPAIRED. STRINGER 56 LEFT MISREPAIRED, FRAMES 73 TO 75. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206 FLAG NOTE 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201206052098](https://openairdocs.org/sdr/FDEA201206052098), Jun 5, 2012: STRINGER. MISREPAIRED. STRINGER 40 LEFT MISREPAIRED FRAMES 73 TO 74. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206 FLAG NOTE 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201206052094](https://openairdocs.org/sdr/FDEA201206052094), Jun 5, 2012: FLOORBEAM. MISREPAIRED. FLOORBEAM MISREPAIRED. REPAIRED IAW SRM 53-10-15, FIG 207, PG 241/242. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201206052097](https://openairdocs.org/sdr/FDEA201206052097), Jun 5, 2012: STRINGER. MISREPAIRED. STRINGER MISREPAIRED. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201206052095](https://openairdocs.org/sdr/FDEA201206052095), Jun 5, 2012: FLOORBOARD. DAMAGED. FLOORBOARD 241MK CRUSHED ON EDGE & FOUR SEPARATE DELAMINATION AREAS ON UPPER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201206052093](https://openairdocs.org/sdr/FDEA201206052093), Jun 5, 2012: FLOORBOARD. CORRODED. FLOORBOARD 251GH HAS CORROSION AT HONEYCOMB CORE OUTER EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW SRZ 25-005, REV J.
- [SDR FDEA201206052092](https://openairdocs.org/sdr/FDEA201206052092), Jun 5, 2012: FLOORBOARD. DELAMINATED. FLOORBOARD 242EK DELAMINATED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201206052091](https://openairdocs.org/sdr/FDEA201206052091), Jun 5, 2012: FLOORBOARD. DAMAGED. FLOORBOARD 162EF HAS COMPOSIT DAMAGE TO LOWER SURFACE AND HAS ONE DAMAGED HOLE GROMET, FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J & SRZ 25-011.
- [SDR FDEA201206052090](https://openairdocs.org/sdr/FDEA201206052090), Jun 5, 2012: THRUST PLATE. CORRODED. THRUST PLATE BETWEEN FRAME 34 AND 35 LOCATED BETWEEN SEAT TRACKS 5L AND 6L HAS 1 SQUARE INCH OF CORROSION. REMOVED CORROSION, ORIGINAL THICKNESS .094", 7EA AREA
- [SDR FDEA201206052089](https://openairdocs.org/sdr/FDEA201206052089), Jun 5, 2012: SHEAR PLATE. CRACKED. SHEAR PLATE LT SIDE WEB CRACKED BETWEEN FR79-FR80. R & R SHEAR PLATE WEB ON FLOOR LT SIDE BETWEEN FR79-FR80 IAW SRM 51-72-10, PG 1.
- [SDR FDEA201206042080](https://openairdocs.org/sdr/FDEA201206042080), Jun 4, 2012: FLOOR PANEL. CRACKED. FLOOR PANEL 242UJ HAS TWO, 10 INCH CRACKS. FABRICATED FLOOR PANEL 242 UJ IAW DWG NR SRZ 25-005, REV J.
- [SDR FDEA201206042079](https://openairdocs.org/sdr/FDEA201206042079), Jun 4, 2012: FLOORBOARD. DELAMINATED. FLOORBOARD 231HG UPPER SURFACE DISBONDED AT AFT OTBD CORNER 10 SQUARE INCHES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

All 218: https://openairdocs.org/deregistered/N403FE-2024-02-03/reports.md

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