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N411FE

Cancelled 2020

Deregistered aircraft · 1985 Airbus Industrie A310-203 · GE CF6-80 series

Open in FAA registry

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Cancelled: April 23, 2020
Status when cancelled: Valid registration
Serial number: 359
Year built: 1985
Type: Fixed wing multi engine
Engine: 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
Location: Memphis, TN
Owner type: Corporation

Airframe modelAirbus Industrie A310-203TCDS A35EU · ADs, bulletins and aircraft registered now Engine modelGE CF6-80 seriesTCDS E13NE · Turbo-fan

From the FAA registry file of November 3, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N411FE and the event date: up to this one’s cancellation.

Incident 20000727027679INormal Cruise · 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 illuminated. No ecam warning. Followed abnormal procedures, turned green servo switch off. The flight…Jul 27, 2000

Service difficulty reports · 62

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

SDR FDEA201111225002Duct · leakingDURING 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 AMM 20-26-00-000. PERFORMED LEAK CHECK WITH APU AIR, FOUND NO LEAKS AT DUCT. ACFT OK FOR SERVICENov 22, 2011 · N411FE · Airbus A310203 · Air Intake Anti/De-Ice System SDR FDEA201111225003Warning Light · illuminatedDURING CLIMB, ECAM ALERT RECEIVED FOR NR 1 BLEED LEAK, COMPLIED WITH ECAM QRH. DIVERTED TO AVOID ICING. OPENNov 22, 2011 · N411FE · Airbus A310203 · Pneumatic Distribution System SDR FDEA201108243464Bellcrank · failedDURING 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 REINSTALLED FLOOR PANELS FOR ACCESS IAW AMM 53-23-04. R & R FREE FALL CONTROL BELL CRANK IAW SRM 51-Aug 24, 2011 · N411FE · Airbus A310203 · Landing Gear Retraction/Extension System

See all 62 reports