Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF201812270402Unknown · warning messageDURING TAXI AND PERFORMING ONE ENGINE TAXI DEPATURE PROCEDURE WITH ENGINE AVAIL MESSAGE ON ECAM:ELEC GEN 2 FAULT.PERFORMED ECAM PROCEDURE UNSUCCESFULL // CORRECTIVE ACTION: DEC 4. THIS REPORT IS DEFERRED TO DMI WO 1822567 LOG PAGE RED BOOK 18495. N593EL-CNMCC-SDR ANCF2018FA0000385Proximity Sensor · faultySHOCK ABSORBER FAULT IN LANDING GEAR EXT PROX SN SR 25GATGT POS IN LFEXT PROX SN SR (24GA) TGT POS. IAW AMM 32-31-73-000-005A PROXIMITY SENSORS 24GA / 25GA WERE REPLACED.SDR ANCF2018FA0000372Shock Absorber · faultedPILOT REPORT UNABLE TO RAISE LANDING GEAR AFTER LIFTOFF, LT SHOCK ABSORBER FAULT ON ECAM.SDR ANCF2015021101Bleed Valve · faultyENGINE 1 COMPRESSOR ARE DISPLAY ON ECAM DESCENT, A STRONG NOISE ON ENG 1, STALL ON ECAM FOLLOWED BY ENG 1 STALL ON ECAM FOLLOWED BY ENG 1 COMPRESSOR VANE DURING THE REST. OF THE FLIGHT, WE HAD 2 COMPRESSOR STALL EVENTS. IAW AMM 75-31-50-000 400-A THE BLEED VSDR ANCF2014083101Valve · faultyGROUND RETURN TO GATE DUE TO INTERMITTENT ECAM MSG AIR BLEED 1 & AIR BLEED 2 FAULT WHEN APPLYING FLEX TO THRUST THE PACKS WERE OFF & THE TAKEOFF WAS DISCONTINUED AT 40 KNOTS REVERSE THRUST WAS NOT APPLIED & AUTO BRAKES SYS DID NOT ACTIVATE. IAW AMM 36-12-52-SDR ANCF2014080101Fan · malfunctionedAFTER APPROX 2 MINUTES INFLIGHT, A STRONG NOISE WAS FELT ON THE NOSE AREA, THEN A STRONG RUBBER SMELT WAS FELT IN THE COCKPIT & PAX CABIN. THE BLOWER & EXTRACT FAULT WAS PRESENTED ON THE OVERHEAD PANEL WITHOUT ECAM ALERT. THE RUBBER SMELT DISAPPEAR ABOUT 5 MSDR ANCF2014FA0000331Unknown · vibrationDURING CRUISE, AT FL 390 AND MACH 0.78, THE CABIN CREW INFORMED ABOUT A HIGH VIBRATION IN THE TAIL, TSM 53-35-00-810-801 WAS ACCOMPLISHED AND NO DAMAGES WERE FOUND.SDR 2014FA0000190Display · malfunctionedREJECTED TAKEOFF DUE TO NO FMA ANNUNCIATIONS ON PFD, NO FLEX AND NO A/P 1 AND 2, NO AUTOTHROTTLE. PERFORMED BITE TEST AT FAC NR 1 AND NR 2 IAW AMM 22-60-00-710-001A AND OPS TEST AT AUTO PILOT SYSTEM IAW AMM 22-90-00-710-001. GROUND TEST SATISFATORY.SDR ANCF2013012300147Warning System · activatedDURING CLIMB, DOOR RIGHT EMERGENCY EXIT AMBER CAUTION PRESENTED DURING CLIMB. IN ACCORDANCE WITH AMM 52-21-11-400-001-A THE COVER FLAP WAS INSTALLED PROPERLY.