# N411FE: 1985 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: 359
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 4, 1995
- Certificate issued: January 13, 2010
- Last registry action: December 18, 2018
- Mode S code: A4D859
- 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/N411FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=411FE
- Page: https://openairdocs.org/deregistered/N411FE-2020-04-23

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 Industrie A310-203: https://openairdocs.org/model/airbus-industrie-a310-203.md

## Service difficulty reports (62, newest 50)

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

- [SDR FDEA201111225002](https://openairdocs.org/sdr/FDEA201111225002), Nov 22, 2011: DUCT. LEAKING. DURING CLIMB ECAM ALERT RECEIVED FOR NR 1 BLEED LEAK COMPLIED WITH ECAM QRH. DIVERTED TO AVOID ICING. REMOVED AND REPLACED NR 1 SYS ANTI-ICE DUCT IN PYLON PER A
- [SDR FDEA201111225003](https://openairdocs.org/sdr/FDEA201111225003), Nov 22, 2011: WARNING LIGHT. ILLUMINATED. DURING CLIMB, ECAM ALERT RECEIVED FOR NR 1 BLEED LEAK, COMPLIED WITH ECAM QRH. DIVERTED TO AVOID ICING. OPEN
- [SDR FDEA201108243464](https://openairdocs.org/sdr/FDEA201108243464), Aug 24, 2011: BELLCRANK. FAILED. DURING LANDING GEAR FREE FALL EXTENTION TEST PROCEDURES, THE LT AND RT MLG FAILED TO EXTEND AFTER HANDLE REACHED MAXIMUM ALLOWABLE TURNS OF 20.5. REMOVED AND RE
- [SDR FDEA201108243463](https://openairdocs.org/sdr/FDEA201108243463), Aug 24, 2011: SKIN. CORRODED. CENTER WING BOX LT FR 49 HAS OXIDATION AT UPPER SURFACE BETWEEN STR 27-28. BELOW SEAT TRACK 6L DEFECT MEASURES 8 SQ INCHED IN THE CORNER. CLEANED UPPER SURFACE 
- [SDR FDEA201108243458](https://openairdocs.org/sdr/FDEA201108243458), Aug 24, 2011: ATTACH FITTING. CORRODED. CTR WING BOX BETWEEN SEAT TRACK L5-L6 HYD LINES ATTACHMENT FITTING CORRODED FR 49-50. CLEANED 6 EA LINES AND FITTING FOUND TO BE OUT OF LIMIT IAW AMM 12-21-12-0
- [SDR FDEA201108153281](https://openairdocs.org/sdr/FDEA201108153281), Aug 15, 2011: FITTING. FAILED. NLG LEG DOOR LOWER RT ATTACHMENT FORK BROKEN. R & R NLG LEG DOOR RT FITTING AND ATTACHMENT FORK ,OPS CHECKED GOOD ALL IAW 32-22-15-04.
- [SDR FDEA201108133264](https://openairdocs.org/sdr/FDEA201108133264), Aug 13, 2011: FLOOR PANEL. DELAMINATED. FLOOR PANEL 242UJ HAS IMPACT DAMAGE. CUTOUT DAMAGE, & FABRICATED REPLACEMENT FLOOR PANEL 242UJ IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201108123247](https://openairdocs.org/sdr/FDEA201108123247), Aug 12, 2011: ADAPTER. FAILED. CLEVIS ADAPTOR AT FRAME 43 BETWEEN SEAT TRACKS 2R AND 3R BROKEN. REMOVED AND REPLACED CLEVIS ADAPTOR AT FRAME 43 BETWEEN SEAT TRACKS 2R AND 3R IAW SRM 51-40-21 
- [SDR FDEA201107273001](https://openairdocs.org/sdr/FDEA201107273001), Jul 27, 2011: SPRING. BENT. LT MLG 2 DOWNLOCK SPRINGS BENT. REPLACED BENT SPRINGS LT MAIN GEAR LOCK LINK IAW AMM 32-11-19-04.
- [SDR FDEA201107273000](https://openairdocs.org/sdr/FDEA201107273000), Jul 27, 2011: SPRING. BENT. RT MLG DOWNLOCK SPRINGS (2 EA) BENT. REPLACED BENT SPRINGS FOR RT MLG LOCK LINK IAW AMM 32-11-19-04.
- [SDR FDEA201011034246](https://openairdocs.org/sdr/FDEA201011034246), Nov 3, 2010: SWITCH. FAILED. ON DEPARTURE RECEIVED LANDING GEAR RETRACTION FAULT. DOWN AND LOCKED "GREEN" LIGHTS NEVER WENT OUT. FOUND ACFT IN SYS 2 ON ARRIVAL. TALKED TO CAPTAIN OF INBD FL
- [SDR FDEA201009303801](https://openairdocs.org/sdr/FDEA201009303801), Sep 30, 2010: FITTING. CORRODED. 134AR ACCESS DOOR SURROUNDING INTEGRAL FITTING FOUND CORROSION (FR23- 24, STGR49R-STGR54L) REMOVE CORROSION IAW SRM 51-74-10. MEASURE THE REMAINING THICKNESS IA
- [SDR FDEA201009293798](https://openairdocs.org/sdr/FDEA201009293798), Sep 29, 2010: FITTING. CORRODED. 136 AR ACCESS DOOR SURROUNDING INTEGRAL FITTING FOUND CORROSION (FR38.1- FR38.2, STGR49R-STGR54L) REMOVE CORROSION IAW SRM51-74-10. MEASURE THE REMAINING THICKN
- [SDR FDEA201009273730](https://openairdocs.org/sdr/FDEA201009273730), Sep 27, 2010: BEAM. CRACKED. LT AFT CREW DOOR FRAME FR73A TO FR75A, STRINGER 11 LONGITUDINAL BEAM NDT FOUND CRACK INDICATION FROM 5 FASTENER HOLES. REMOVE THE COVER PLATE AND DOOR FRAME BEA
- [SDR FDEA201009273729](https://openairdocs.org/sdr/FDEA201009273729), Sep 27, 2010: FRAME. DAMAGED. 2 DISTORTIONS FOUND ON FR54.2 FRAME BETWEEN STGR13L-15L 1.CUT OUT THE DAMAGED SECTION OF FRAME 54.1 BETWEEN STGR13L-15L AND MAKE THE REPAIR PART IAW SRM53-10-13
- [SDR FDEA201009273728](https://openairdocs.org/sdr/FDEA201009273728), Sep 27, 2010: FRAME. GOUGED. GOUGE FOUND ON FR54.1 FRAME BETWEEN STGR13L-14L 1.CUT OUT THE DAMAGED SECTION OF FRAME 54.1 BETWEEN STGR13L-15L AND MAKE THE REPAIR PART IAW SRM53-10-13-201, PA
- [SDR FDEA200811144882](https://openairdocs.org/sdr/FDEA200811144882), Nov 14, 2008: HOUSING. BROKEN. ON ARRIVAL INTO MEM, THE NOSE GEAR INDICATED UNSAFE ON BOTH SYSTEM 1 AND 2. COMPLIED WITH QRH AND USED THE MLG GRAVITY EXTEND CHECKLIST. WHEN THAT WAS COMPLETED
- [SDR 08FDEA04882](https://openairdocs.org/sdr/08FDEA04882), Nov 14, 2008: HOUSING. CRACKED. ON ARRIVAL, NOSE GEAR INDICATED UNSAFE ON BOTH SYSTEM 1 AND 2. COMPLIED WITH QRH AND USED MLG GRAVITY EXTEND CHECKLIST. WHEN COMPLETED UNSAFE WARNING REMAINED, 
- [SDR 07FDEA03423](https://openairdocs.org/sdr/07FDEA03423), Sep 5, 2007: TRANSMITTER. MALFUNCTIONED. DURING CRUISE, GREEN HYDRAULICS SHOWED "0" PRESSURE AND "LO RSVR QUANTITY" ON ECAM. QUANTITY CONFIRMED ON OVERHEAD PANEL. DIVERTED TO ATL. DURING MANUAL GEAR EX
- [SDR 07FDEA03392](https://openairdocs.org/sdr/07FDEA03392), Sep 5, 2007: TRANSMITTER. LEAKING. DURING CRUISE, GREEN HYDRAULICS SHOWED "0" PRESSURE AND "LO RSVR QUANTITY" ON ECAM. QUANTITY CONFIRMED ON OVERHEAD PANEL. DURING MANUAL GEAR EXTENSION, QUANTITY
- [SDR 07FDEA01653](https://openairdocs.org/sdr/07FDEA01653), Apr 27, 2007: SKIN. MISREPAIRED. PREVIOUS REPAIR LOCATED ON R/SIDE FUSELAGE SKIN BETWEEN FR 66 TO 67 BETWEEN STR 35TO 38 RT HAS AN EXTERNAL REPAIR DOUBLER MEASURING 8.8 BY 11.9. REPAIR REVIEWED
- [SDR 07FDEA01655](https://openairdocs.org/sdr/07FDEA01655), Apr 27, 2007: SKIN. MISREPAIRED. PREVIOUS REPAIR LOCATED ON L-SIDE FUSELAGE SKIN BETWEEN FR 21-22 BETWEEN STR 34-36 LT AT LAP SEAM HAS AN EXTERNAL DOUBLER MEASURING 6.25 BY 9 IN REPAIR DETERMIN
- [SDR 07FDEA01241](https://openairdocs.org/sdr/07FDEA01241), Apr 2, 2007: FLOORBEAM. CRACKED. 1 CRACK EXIST IN FLOORBEAM VERTICAL STIFFENER AT FR 36 BETWEEN SEAT TRACK L4 AND L5, MEASURING 0.450" P/N 537B1041000 A310-200 AMM 53-10-15-6. REMOVED 1 CRACK I
- [SDR 07FDEA01185](https://openairdocs.org/sdr/07FDEA01185), Mar 29, 2007: FLOORBEAM. CRACKED. 1 CRACK EXIST IN FLOORBEAM VERTICAL STIFFENER AT FRAME 36 BETWEEN SEAT TRACK L2 AND L3 MEASURING .5" REF R537B1041000 A310-200 AMM 53-10-15-6. REMOVED CRACK PER
- [SDR 07FDEA01184](https://openairdocs.org/sdr/07FDEA01184), Mar 29, 2007: FLOORBEAM. CRACKED. 1 CRACK FOUND .75" IN UPPER SUPPORT LEG ON AFT SIDE OF FLOORBEAM FR 58 BETWEEN SEAT TRACK 4L AND 5L EXTENDING INTO FLOORBEAM WEBBING UNDER CLS ADAPTER IAW A310-
- [SDR 07FDEA01080](https://openairdocs.org/sdr/07FDEA01080), Mar 22, 2007: FLOORBEAM. CRACKED. FORWARD CARGO COMPARTMENT, FLOORBEAM (C25) FORWARD FACE OF BEAM LOCATED BETWEEN R2 AND R3 SEAT TRACK HAS A .400 INCH CRACK IN VERTICAL STIFFENER. REPAIRED FLOOR
- [SDR 07FDEA01078](https://openairdocs.org/sdr/07FDEA01078), Mar 22, 2007: FLOORBEAM. CRACKED. FWD CARGO COMPARTMENT, OVER HEAD FLOORBEAM [ C34 ] FWD FACE OF BEAM , LOCATED BETWEEN L4 AND L5 SEAT TRACK HAS A 0.425 INCH CRACK IN VERTICAL STIFFENER. REMOVED
- [SDR 07FDEA01076](https://openairdocs.org/sdr/07FDEA01076), Mar 22, 2007: TRACK. MISREPAIRED. PREVIOUS REPAIR LOCATED ON AFT CARGO ROLLER TRACK LEFT NR 2 HAS A 9 INCH LONG REPAIR SECTION WITH 2 REPAIR ANGLES ON THE OUTBD SIDE MEASURING 7 INCH LONG EACH B
- [SDR 06FDEA04243](https://openairdocs.org/sdr/06FDEA04243), Dec 14, 2006: CONTROL UNIT. MALFUNCTIONED. ON CLIMB-OUT, AUTO BRAKE FAIL LIGHT CAME ON, LIGHT STAYED ON UNTIL LEVEL OFF AND THEN AFTER A PERIOD OF TIME THE LIGHT WENT OUT. LIGHT THEN CAME ON AFTER A PERI
- [SDR 06FDEA2663](https://openairdocs.org/sdr/06FDEA2663), Jul 23, 2006: PITOT TUBE. DIRTY. RIGHT AFTER ROTATION BOTH ATS LEVERS DROPPED OFF. ADC FAILED ON CAPT SIDE SWITCHED OVER TO OTHER SYSTEM REENGAGED ATS LEVERS AS PER ECAM THROTTLE RETARDED TO ID
- [SDR 06FDEA2659](https://openairdocs.org/sdr/06FDEA2659), Jul 22, 2006: ADC. FAILED. JUST AFTER ROTATION BOTH ATS LEVERS DROPPED OFFLINE AND WOULD NOT RESET. YAW DAMP DROPPED OFF, WOULD NOT RESET. CAPTS PFD, ADC FAILED. SWITCHED OVER TO F/O SYST
- [SDR 06FDEA1782](https://openairdocs.org/sdr/06FDEA1782), May 11, 2006: COMPUTER. FAULTED. ON T/O AT LAX, DID A RTO AT 90 KTS THE ECAM ALERT WAS BOTH PITCH 1/2 AND BOTH RUDDERS 1/2 FAULTED. REMOVED AND REPLACED NR 1 AND NR 2 FEEL LIMITATION COMPUTERS 
- [SDR 05FDEA04399](https://openairdocs.org/sdr/05FDEA04399), Dec 22, 2005: INDICATOR. SMOKE. N CRUISE BURNING SMELL IN COCKPIT, DIVERTED AND LANDED. STRONGEST SMELL FROM THROTTLE QUADRANT AREA, FIRE CREW TEMP DETECTOR SHOWED HIGHEST HEAT IN THAT LOCATIO
- [SDR 05FDEA01899](https://openairdocs.org/sdr/05FDEA01899), Jul 12, 2005: ACCESS PANEL. DAMAGED. ACCESS PANEL 650GB HAS 1 ELONGATED HOLE, COMPLIED WITH EA6-5710-90863.
- [SDR 05FDEA01898](https://openairdocs.org/sdr/05FDEA01898), Jul 12, 2005: ACCESS PANEL. DAMAGED. ACCESS PANEL 650 FB HAS 1 ELONGATED HOLE, COMPLIED WITH EA6-5710-90863.
- [SDR 04FDEA02798](https://openairdocs.org/sdr/04FDEA02798), Sep 21, 2004: ANGLE. CORRODED. BULK CARGO COMPT FLOOR STRUCTURE FS 67 2EA AREAS OF CORROSION NOTED ON TOP AND BOTTOM SURFACES. REMOVED AND REPLACED PROFILE ANGLE IAW A310 SRM 51-40-21.
- [SDR 04FDEA02797](https://openairdocs.org/sdr/04FDEA02797), Sep 21, 2004: FLOORBEAM. CORRODED. BULK CARGO COMPT FLOOR STRUCTURE FS 65 ON LT SIDE, MID AND RT SIDE AREA NOTED CORROSION ON TOP AND UNDERNEATH SURFACES. REMOVED AND REPLACED BEAM IAW A310 SRM 5
- [SDR 04FDEA02796](https://openairdocs.org/sdr/04FDEA02796), Sep 21, 2004: SEAT TRACK. CORRODED. MDCC SEAT TRACK L4 FRAME 74-80 HAS 5EA CORRODED AREAS. REPAIRED SEAT TRACK BY SPLICING IAW A310 SRM 51-22-00, 51-40-21 AND 53-10-16.
- [SDR 04FDEA02795](https://openairdocs.org/sdr/04FDEA02795), Sep 21, 2004: FLOORBEAM. CORRODED. AFT CARGO COMPT FS 63 FLOOR STRUCTURE, ON LEFT SIDE 3EA AREAS OF CORROSION ON TOP SURFACE AND UNDERNEATH FLOOR STRUCTURE. REMOVED AND REPLACED FLOOR STRUCTURE B
- [SDR 04FDEA02794](https://openairdocs.org/sdr/04FDEA02794), Sep 21, 2004: STRUCTURE. CORRODED. AFT CARGO COMPT FWD OF FS 54.2 BILGE AREA NOTED SPOT OF CORROSION AROUND THE HOLE PLUG. REPAIRED BILGE AREA IAW EA 6-5330-55370.
- [SDR 04FDEA02793](https://openairdocs.org/sdr/04FDEA02793), Sep 21, 2004: SEAT TRACK. CORRODED. MDCC SEAT TRACK R1 BETWEEN FRAME 73-80 HAS 7EA DISCREPANT AREAS 5EA AREAS THAT ARE CORRODED AND GOUGED AND 2EA AREAS THAT ARE GOUGED. REMOVED AND REPLACED R1 SE
- [SDR 04FDEA02724](https://openairdocs.org/sdr/04FDEA02724), Sep 17, 2004: SEAT TRACK. CRACKED. MDCC SEAT TRACK SECTION AT R2, BETWEEN FR54 TO 8 INCHES AFT OF FR54.1 HAS DAMAGE TO THE SCALLOP LUGS. (ON EDGES AND BENEATH LUGS) REMOVED DAMAGE AND FOUND TO BE
- [SDR 04FDEA02698](https://openairdocs.org/sdr/04FDEA02698), Sep 16, 2004: FLOORBEAM. CRACKED. FWD CARGO FLOORBEAM STRUCTURE FR33 NOTED INDICATION OF CRACK. REMOVED DAMAGED AREA IAW A310 SRM 53-10-15, AND REPAIRED BY INSTALLING A DOUBLER IAW A310 SRM 53-1
- [SDR 04FDEA02697](https://openairdocs.org/sdr/04FDEA02697), Sep 16, 2004: ADAPTER. CRACKED. TRACK ADAPTER AT FR61 Y-450 IS CRACKED APPROX 6 INCHES LONG. REMOVED AND REPLACED TRACK ADAPTER IAW A310 SRM 51-40-21.
- [SDR 04FDEA02696](https://openairdocs.org/sdr/04FDEA02696), Sep 16, 2004: ADAPTER. CRACKED. TRACK ADAPTER AT FR61 Y-450 IS CRACKED APPROX 6 INCHES LONG. REMOVED AND REPLACED TRACK ADAPTER IAW A310 SRM 51-40-21.
- [SDR 04FDEA02695](https://openairdocs.org/sdr/04FDEA02695), Sep 16, 2004: SEAT TRACK. GOUGED. SEAT TRACK AT FR 36 AFT APPROX 8 INCHES IS GOUGED. BLENDED AREA PER A310 SRM 51-22-00 AND FOUND TO BE OUT OF LIMITS PER A310 SRM 53-10-16. REPAIRED BY REMOVING 
- [SDR 04FDEA02694](https://openairdocs.org/sdr/04FDEA02694), Sep 16, 2004: SEAT TRACK. CORRODED. SEAT TRACK 0, SECTION BETWEEN FR73 TO FR80 HAS TWO DISCREPANT AREAS. TRACK 0 AT APPROX 12 INCHES AFT FROM FR 77 HAS 2 GOUGES INSIDE OF SCALLOPED AREA. TRACK 0 A
- [SDR 04FDEA02693](https://openairdocs.org/sdr/04FDEA02693), Sep 16, 2004: FLOORBEAM. CRACKED. BULK CARGO COMPT FLOOR STRUCTURE ON FR67 AT RT SIDE CORNER UNDERNEATH NOTED CRACK. REMOVED AND REPLACED BEAM IAW A310 SRM 51-40-21.
- [SDR 04FDEA02692](https://openairdocs.org/sdr/04FDEA02692), Sep 16, 2004: FLOOR SUPPORT. CORRODED. BULK CARGO COMPT. FLOOR STRUCTURE FR66 LT SIDE , MID AND RT SIDE AREA NOTED CORROSION ON TOP AND UNDERNEATH SURFACE. REMOVED CORROSION IAW SRM 51-74-10, AND FOU
- [SDR 04FDEA02691](https://openairdocs.org/sdr/04FDEA02691), Sep 16, 2004: FLOOR SUPPORT. CORRODED. BULK CARGO COMPT. FLOOR STRUCTURE, ON RT SIDE FR 66 TO FR 63 CORROSION ON TOP AND BENEATH SURFACE. REMOVED CORROSION IAW SRM 51-70-10 AND FOUND TO BE OUT OF LIM

All 62: https://openairdocs.org/deregistered/N411FE-2020-04-23/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 20000727027679I](https://openairdocs.org/incident/20000727027679I), Jul 27, 2000: Airbus A310203 (N411FE), Indianapolis, IN. (-23)On July 27, 2000 flight 151 declared an emergency due to a flight control problem. In cruise noticed amber light on green hydraulic servo control jam…

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