N408FE

Cancelled 2013

Deregistered aircraft · 1983 Airbus Industrie A310-203 · GE CF6-80 series

Cancelled
March 27, 2013
Status when cancelled
Valid registration
Serial number
257
Year built
1983
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
August 4, 1995
Certificate issued
August 2, 2010
Last registry action
February 1, 2012
Mode S code
A4CADB
Owner when cancelled
Federal Express Corp
Location
Memphis, TN
Owner type
Corporation

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.

Service difficulty reports · 14

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

SDR 07FDEA05057Control Lever · failedGEAR LEVER WOULD NOT RETRACT PAST NEUTRAL POSITION IN SYS NR 1 OR SYS NR 2 INTERROGATED PROX BOX FOUND FAULT CODES 64 AND 60 INSTALLED TEST BOX IN A/C. REMOVED PROX BOX AND NOSE GEAR SWITCHES FOR TEST BOX HARNESS. TESTED SYSTEM PER MM TO GEAR MODULE STILL DDec 14, 2007 · N408FE · Airbus A310203 · Landing Gear Retraction/Extension SystemSDR 07FDEA01652Shear Tie · crackedA/C BAY AT RT SIDE OF KEEL BEAM AND ON TOP VERTICAL FLANGE OF FR 46 , 1 SHEAR TIE BRACKET HAS CRACK .51 LONG. REMOVED AND REPLACED SHEAR TIE IAW A310-200 SRM 51-72-10 AND EA 6-5320-110446.Apr 27, 2007 · N408FE · Airbus A310203 · Fuselage Internal Mounting StructureSDR 07FDEA01651Skin · debondedLT ELEVATOR LOWER SKIN IS DISBONDED AT RIB 13 ,5 IN FROM T/E 7.5 IN LONG. REPAIRED DAMAGED AREA IAW EA 6-5520-110453.Apr 27, 2007 · N408FE · Airbus A310203 · Elevator, Plate/SkinSDR 07FDEA01650Structure · corrodedAFT CARGO COMPT BILGE AREA BETWEEN FR 60-61 HAS CORROSION AROUND 18 EA RIVET BUCKTAILS ON S56R. REMOVED CORROSION IAW A310-200 SRM 51-74-10 CHECKED LIMITS IAW A310-200 SRM 53-10-00. FOUND STRG TO BE OUT OF LIMITS. REPAIRED STR IAW A310-200 SRM 53-10-14.Apr 27, 2007 · N408FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA01649Skin · crackedL-WING TE BOTTOM SKIN AT PANEL 581AB CUTOUT HAS CRACK ON LOWER SKIN RIB 11 WITH APPROX 0.75 IN LONG REF N00166 STOP DRILLED CRACK, DRILLED UP DOUBLER AND COLDWORKED AND INSTALLED IAW EA 6-5710-107726 AND SB A310-57-2066.Apr 27, 2007 · N408FE · Airbus A310203 · Wing, Plate/SkinSDR 04FDEA03192Uplock · failedAFTER TAKEOFF, NOSE GEAR AMBER "DOOR" WARNING LIGHTS (FWD AND OVERHEAD) REMAINED ON FOLLOWING GEAR RETRACTION. NO EXCESSIVE NOISE OR VIBRATION OBSERVED. WHEN GEAR WAS EXTENDED AGAIN, "DOOR" LIGHT REMAINED ON (BOTH FORWARD AND OVERHEAD INDICATIONS) RETURNED TNov 18, 2004 · N408FE · Airbus A310 · Landing Gear Position and WarningSDR 01FDEA00769Controller · malfunctionedPDIS WRI 26-12-5025 AT ABOUT 1500 AFT MAIN DECK CARGO LOOP-A ILLUMINATED, FOLLOWED BY LOOP-B AND RED SMOKE LIGHT & ECAM FIRE WARNING. DECLARED EMER AND RETURNED TO LAND. REMOVED AND REPLACED AFT UPPER CARGO SMOKE DETECTION CONTROLLER AND TESTED PER MM 26-19-Aug 24, 2001 · N408FE · Airbus A310 · Detection SystemSDR 01FDEA00026Smoke Warning · activatedON APR AT 1000 FT CONFIG TO LAND GOT CARGO SMOKE ALARM/WARN LIGHTS.Jan 18, 2001 · N408FE · Airbus A310203 · Smoke DetectionSDR 01FDEA00020Fire Warning · activatedCARGO SMOKE AND FIRE ON FINAL FIRE BOTTLES ON APU ENG DISCHARGED ON LAND. REPLACED NR 1 & 2 FIRE BOTTLES IN BOTH ENG 1 & 2 AS PER MM 26-22-12-4. AC OK FOR FLIGHT.Jan 12, 2001 · N408FE · Airbus A310203 · Fire DetectionSDR 99FDEA00509Warning System · activated99-292 - ON T/O YELLOW SYSTEM LOW PRESS ECAM WARNING. REJECTED TO AT 83 KTS. YELLOW SYS RECOVERED TO NORM CLEAR RUNWAY.Dec 22, 1999 · N408FE · Airbus A310203 · Hydraulic System, MainSDR 99FDEA00205Mec · malfunctionedNR 2 ENG SHUT DOWN DUE TO LOW OIL PRESS, NO RESTART. *S/D* REMOVED AND REPLACED NR 2 ENG MEC AND FUEL PUMP AS PER AIRBUS MM. CK GOOD. REMOVED AND REPLACED CIT SENSOR PER MM.Jun 3, 1999 · N408FE · Airbus A310203 · Fuel Control/Turbine EnginesSDR 98FDEA00763Switch · inopLANDING GEAR HANDLE WOULD NOT GO PAST THE MID POS. FOLLOW RED TAB AND USED OTHER SYS AS DIRECTED, PROBLEM REMAINED. JUST AFT SYS 2 USED, YELLOW SYS HYD ECAM CAME ON AMBER WITH MANY LIGHTS ON HYD PANEL. *S/D* REMOVED AND REPLACED LANDING GEAR CONTROL LEVER Dec 24, 1998 · N408FE · Airbus A310203 · Landing Gear Retraction/Extension SystemSDR 98FDEA00656Damper · inopT/O MEM COULD NOT RAISE GEAR HANDLE. TRIED BOTH POSITION DET SYSTEM 1 AND 2. RECYCLE HANDLE DOWN AND RETRIED. STILL NOT ABLE TO RETRACT. RETURNED TO MEM. REMOVED AND REPLACED LEFT MAIN LANDING GEAR PITCH DAMPER. PERFORMED GEAR SWING, OPS CHECK OK.Oct 18, 1998 · N408FE · Airbus A310203 · Landing Gear Retraction/Extension SystemSDR 97FDEA00834Retract Mech · malfunctionON FLAP RETRACTION FLAPS REMAINED AT 5 DEG. EXTENSION AND FLAPS SYSTEM NR 1 AND NR 2 FAULT ON, COMPLIED WITH QRH. RESET NR 1 AND NR 2 SFCC'S. CYCLED FLAPS AND SLATS SEVERAL TIMES, OPS CHECKED GOOD.Nov 13, 1997 · N408FE · Airbus A310203 · Leading Edge Slat Control System

Other aircraft with N408FE · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N408FE is registered now to the first aircraft listed.