Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF2019030201Warning System · false activationMAR 2. REJECTED TAKE OFF RWY 26 PEI DUE TO AMBAR CAUTION BELOW 100 KTS ON THE ECAM DISPLAY. CORRECTIVE ACTIONS: WE CERTIFY THAT THE FIRST THING THAT WAS DONE WAS TO REMOVE THE POST FLIGHT REPORT. WAS PRINT THE POST FLIGHT REPORT, IT DIS NOT SHOW FAULTS THE ECSDR ANCF2019011102Unknown · malfunctionedDURING T.O. ON FO DISPLAY AND FO AS PF AIR DATA INFORMATION WAS LOST ECAM SHOWED YAW DAMPER NR 2 RUD TRIM 2 FAULT. REJECTED T.O. WAS PERFORMED. CORRECTIVE ACTION: IN ACCORDANCE WITH TSM 34-13-00-810-851-A INTERNAL FAILURE OF THE ADR 2 WAS PERFORMED AND AMM 34-SDR ANCF2017091201Idg · low quantityREJECTED TAKE OFF, BELOW 100 KNTS. NR 1 IDG LOW OIL PRESSURE ON ECAM. IAW AMM 05-51-16-200-001A THE MLG BRAKES NR 3 AND 4 WERE INSPECTED, NO DAMAGE FOUND . CHECKED THE LT IDG SERVICING 4/4 QTY ADDED AMM 12-13-24-612-041, AND MINIMUN IDLE CHECK WAS PERFORMEDSDR ANCF2013041200155Oven · smokeNR 2 OVEN IN REAR GALLEY HAS A BURNING SMOKE. NR 2 OVEN REAR GALLEY WAS REMOVED AND REPLACED IAW AMM 25-35-19-PB 401.SDR ANCF2012110900136Wheel · failedDURING WALK AROUND, TIRE NR 4 WAS FOUND WITHOUT CANVAS AND PANEL NR 673AB ON RT WING WAS FOUND CRACKED. C/A IAW AMM 32-41-11-000-006A AND 32-41-11-400-006-A THE MAIN WHEEL 3 AND 4 WERE R & R. TIRE PRESS 189 PSI IAW AMM TASK 05-51-15-200-001-A. THE INSPECTIOSDR ANCF2012102600135Valve · damagedAFTER T/O THE VENT OUT DIDN´T CLOSE WITH OVERRIDE P/B. IN ACCORDANCE WITH AMM 21-26-00-710-001 OPERATIONAL TEST OF THE AEVC SYSTEM VIA MCDU WAS ACCOMPLISHED. TEST SATISFACTORY AND SKIN AIR-INLET VALVE FIN 15HQ, AVIONICS FILTER AIR WERE REPLACED. IN ACCORDANSDR ANCF2012102500134Unknown · smokeDURING CRUISE HAD PACK 1 OVERHEAT ON ECAM. PROCEDURES WERE MADE ACCORDING TO ECAM BUT WHEN WE PUT ON THE PACK 1 THERE WAS SMOKE IN THE COCKPIT. IN ACCORDANCE WITH AMM TASK 21-61-00-710-001A OPERATIONAL TEST OF THE PACK 1/2 TEMPERATURE CONTROL WAS PERFORMED SSDR ANCF2012080300127Valve · damagedAFTER TAKEOFF PROCEDURE TO PEI - VENT SKIN VALVE ECAM APPEARS AND THE CAB ALT STAYS AT 5000FT AND DOES NOT PRESSURIZE. -- IN ACCORDANCE WITH TASK 21-31-00-710- 002-A OPERATIONAL TEST OF THE PRESSURIZATION CONTROL MONITORING WAS ACCOMPLISHED IN BOTH PCP. IT WSDR ANCF2012050400122Unknown · smokeON GROUND WITHOUT PASSENGERS ON BOARD, AFTER OPENING PAX DOOR 1L AND COMING INTO THE AIRCRAFT A STRONG ELECTRICAL SMOKE. DOOR WAS LEFT ON FORWARD GALLEY CLOSE C/B PANEL. IN ACCORDANCE WITH 05-21-20 AND 05-22-10 THE FORWARD CABIN UTILITY AREA OVERHEAD COMPARTMSDR ANCF2011123000101Warning System · activatedDURING FLY WHEEL N/W STEERING FAULT.