NTSB investigations · 1
Matched to this aircraft by N493TA and the event date: up to this one’s cancellation.
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR SOKF20211108003None · noneDURING TAKE OFF FROM SAL TO LAX THE AIRCRAFT REJECTED THE TAKE OF DUE TO UNRELIABLE SPEED CAPTAIN SIDE FOLLOWING TSM 34-13-00-810-998-B WAS PERFORMED CLEANING OF CAPTAIN, F/O AND STANDBY PITOT PROBE IN ACCORDANCE WIH AMM 34-10-00-170-004-A REV 58 PERFORMED FUNSDR SOKF2020030600000Pump · damagedDDURING FLIGHT FROM SAL TO SFO THE AIRCRAFT DIVERTED TO MEX DUE TO PILOT REPORT BLUE PUMP OVERHEAT AND BLUE HYDRAULIC SYSTEM WAS LOST AND ECAM WARNING MESSAGE CAME ON, THEN WHEN THE FAULT LIGHT WENT OFF THE BLUE HYD SYSTEM WAS RECOVERED, IN ACCORDANCE WITH TSSDR SOKF2018100210006Fmc · damagedDURING TO FROM LIM TO JUL THE, TO WAS REJECTED DUE ECAM WARNING A/T OFF. REMOVED AND REPLACED FMGC IAW AMM 22-83-34-000-001-A AND AMM 22-83-34-400-001-A OP TEST AFS IAW AMM 22-96-00-710-001 TEST SATISFACTORY. THE AIRCRAFT RETURN TO NORMAL OPERATION.SDR SOKF20180927005Autothrottle Sys · malfunctionedDURING TO FROM LIM TO CUZ THE TO WAS REJECTED DUE TO A/THR INOP AND DURING T/O PWR CLB DO NOT SHOW INDICATION THRUST MODE AND FLEX TOGA. AUTO FLIGHT AUTO THRUST OFF DURING TAKE OFF ROLL. AT LIM STATION LAND CAT 3 CAPABILITY TEST PERFORMED IAW AMM 22-97-00-710-SDR SOKF20170818008Filter · contaminatedDURING MAJOR CHECK, PERFORMED TASK CARD 731000-11-1, FOUND FUEL FILTER CONTAMINATED. FUEL FILTER ELEMENT WERE EVALUATED IAW AMM 73-12-42-210-061-A PARAGRAPH A ITEM (2)REV.40 01. LT AND RT ENGINE FUEL FILTERS ELEMENT WERE REPLACED. LT FUEL COOLED OIL COOLER SDR SOKF20160902006Servo Control · faultyDURING CLIMB, THE ACFT RETURN TO DEPARTURE DUE TO ECAM WARNING FLIGHT CONTROL ELAC 2 PITCH FAULT, AT STATION, PERFORMED TSM 27-93-00-810-867-A. R & R ELEVATOR SERVO CONTROL LT SIDE, 34 CE1 IAW AMM 27-34-51-000-001-A AND 27-34-51-400-001-A. ADJUSTMENT TEST OFSDR SOKF20140812006Computer · faultyDURING CLIMB THE ACFT RETURNED DUE ELAC 2 FAULT. IAW TSM 27-93-00-810-967-A PERFORMED R & R OF ELAC 2 IAW AMM 27-93-34-000-001 & AMM 27-93-34-400-001. PERFORMED OPERATIONAL TEST IAW AMM 27-93-00-710-001 & LAND CAT III CAPABILITY TEST IAW AMM TASK 22-97-00-71SDR SOKF20140730005Servo Control · damagedVIBRATION AFTER TAKEOFF & CLIMB IAW TSM 05-50-00-810-802-A. PERFORMED CHECK OF THE LOAD REPORT PARAMETER AFTER HARD & OVERWEIGHT LANDING IAW AMM 31-37-00-200-001-A & NO OVERWEIGHT LANDING CONDITION WAS FOUND. CHECKED OK IAW TSM 05-50-00-810-801-A & TSM 27-2SDR MU1Z2011020200004Strut · bentFLAP INTERCONNECTING STRUT ON BOTH LT AND RT SIDES PROXIMITY SENSORS BENT.SDR MU1Z2011020200005Skin · dentedFUSELAGE SKIN - DENT LOCATED IN RT SIDE BETWEEN FR 2 AND FR 3 AND STR Z508.