FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N415FE and the event date: up to this one’s cancellation.
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 08FDEA01609Pressure Switch · failedAFTER DEPARTURE GOT A FLAP FAULT, FOUND FAULT CODE ON SFCC 1 LT WING HIGH SPEED PRESS SWITCH. PERFORMED TEST PER AMM 27-51-00-5, ALL PASSED. SWITCHED SFCC NR 1 AND 2 NO FAULTS FOUND. SWITCHED BACK TO ORG PLACES. STARTED T/S PER PER A310 TSM 27-50-0 6. SESDR 08FDEA00688Adc · unknownON TAKEOFF ROLL, CAPT/FO AIRSPEED DIFFERENCE OF 40 KNOTS (120/80) REJECTED TAKEOFF. PERFORMED ADS SYSTEM CHECK IAW TSM 34-10-00. NO FAULTS NOTED. NO FAULTS ON ADC NR 1 OR NR 2. PERFORMED VISUAL INSPECTION OF ALL PITOT PROBES, NO BLOCKAGE FOUND. PERFORMEDSDR 07FDEA01760Wire · shortedCAPT WINDOW HEAT SIDE SLIDING WINDOW WIRING SHORTED OUT AND MOMENTARY CAUGHT FIRE PULLED ASSOCIATED CB H86. WIRING CAPPED AND STOWED AND ASSOCIATED ITEMS, SLIDING WINDOW HEAT, SEVERAL LIGHTS ON THE CAPT'S SIDE PLACED ON MEL.SDR 07FDEA01761Wire · shortedCAPT WINDOW HEAT SIDE SLIDING WINDOW WIRING SHORTED OUT AND MOMENTARY CAUGHT FIRE PULLED ASSOCIATED CB H86. ACCOMPLISHED EA 6-3040-111404, DISCONNECT, CAP AND STOW OF FIVE EACH WIRES AT TERMINAL STRIP 195VT. MEL PROCEDURES STILL NEED TO BE ACCOMPLISHED. RESDR 04FDEA02872Proximity Sensor · malfunctionedGEAR WOULD NOT RETRACT AFTER TAKEOFF IN EITHER SYSTEM. PERFORMED BITE TEST OF PROX DETECT UNIT 54GB. NO MEMORIZED FAULTS. PERFORMED SYS TEST WITH THE FOLLOWING SENSOR FAULTS, 03 (LT BOGIE SYS 1), 04 (RT BOGIE SYS 1), 05 (NOSE CENTERED SYS 1), 06 (LT MLGSDR 04FDEA02394Outflow Valve · inoperativePDIS 415 21-30 0007170 FWD NR 1 OUTFLOW VALVE STUCK IN THE OPEN POSITION (AMBERARROW ON ECAM). NR 1 PRESS REGULATOR IN USE-ECAM SHOWED 0 V/S AND CABIN ALT. AT 260 FT. WHEN SWITCHED TO NR 2 REG. ECAM SHOWED ACTUAL V/S MATCHED A/C CLIMB RATE AND CABIN SDR 03FDEA02236Computer · faultyLEFT INNER TANK QUANTITY WENT TO ZERO READING IN LESS THAN A MINUTE. AFTER THE FQI CHAN SUPPLY 1 AND 2 C/B'S WERE RESET IAW QRH FUEL LEAK PROCEDURE ECAM SHOWED XX'S IN LT INNER AND TOTAL. FUEL QUANTITY READING RETURNED PASSING 12,700 FT. ON THE DESCENT. RESDR 03FDEA01230Structure · vibrationAIRFRAME VIBRATION STARTED CLIMBING OUT AT FL22.5 2CD A330 KIAS. ENGINE DATA N1-104.1 2C104.23A EGT 832 2C 841 3A VIBES 0.62C+0.2 3A N2 VIBES 2.0 2C0.4. VIBRATION REMAINED THROUGHOUT FLIGHT UNTIL DESCENDING PAST FT.VIBRATION WOULD DECREASE AS POWER WAS REMOSDR 02FDEA00294Landing Gear · malfunctioned02-105 AFTER TAKE OFF, ALL 3 LANDING GEAR WOULD NOT RETRACT, GEAR NOT UP AND LOCKED DISPLAYED ON ECAM. ALL 3 RED GEAR DISAGREE ARROW LIGHTS DISPLAYED. LG SYS NR 2 SEL CYCLED GEAR TWICE NO HELP. NR 1 GEN COOLER VALVE CIRCUIT BREAKER POPPED. ** S/D ** COSDR 00FDEA00458Pitot Tube · blockedON T/O ROLL, CAPT''S AIRSPEED IND ON PFD NEVER GAVE ANY A/S IND. DISCONNECTED LINE FROM ADC NR 1 BLEW THRU PITOT TUBE, GOT BIG BUG. PERFORMED LEAK TEST PER AMM 34-10-00-5-01 CONFIG 1. OPS CHECK GOOD. AC OK FOR SERVICE.SDR 99FDEA00002Pitch Damper · leakingAIR TURNBACK, CREW CALLED GEAR AND GEAR WOULD NOT RETRACT. *S/D* REMOVED AND REPLACED LT BOGIE PITCH DAMPER PER MM 32-11-15. LEAK CK C/W, NO LEAKS NOTED.SDR 98FDEA00264Control Unit · malfunctioned98-0100, AT FL290 CREW RECEIVED AN ECAM WARNING OF MAIN DECK SMOKE WARNING. CREW DONNED 02 MASK AND FOLLOWED AFM PROCEDURES. NEVER DID SMELL SMOKE. DECLARED PRECAUTIONARY AND RETURNED TO AIRPORT. T/S SYSTEM PER TSM, ALL DETECTORS TESTED GOOD. BITE TEST OFSDR 98FDEA00024Retract Mech · malfunctionedFLAPS STUCK AT APPROX 5 DEG ON RETRACTION. FLAPS SYS 1 AND 2 FAULT ILLUMINATED. FLAPS WOULD NOT EXTEND BEYOND 5 DEG ON LANDING. SLATS OPERATED NORMALLY. SFPI FLAP FAULT DID NOT ILLUMINATE. AIRCRAFT RETURNED TO LAS AND LANDED WITH NO INCIDENCE. FOUND RIGH