What was found
PREVIOUS TO DEPART AS FLIGHT TA561. THE ACFT SHOWED THE FOLLOWING NO DISPATCH FAILURE MSGS. FLIGHT CONTROL RUDDER TRAVEL LIMIT 2 FAULT MSG ON ECAM. FOR THIS FAILURE IT WAS PERFORMED FAULT ANALYSIS IAW TSM 22-61-00-810-804-A BY RESETTING THE FAC 2 & TESTING THE AFS IAW AMM 22-96-00-710-001-A, OBTAINING NORMAL RESULTS. AUTO FLIGHT RUDDER TRIM SYS. FOR THIS FAILURE IT WAS PERFORMED FAULT ANALYSIS IAW TSM 22-62-00-810-817-A, THE TEST OF THE RUDDER TRIM WAS NOT SATISFACTORY, SO THEN, THE RUDDER TRIM ACTUATOR 10CC WAS REPLACED IAW AMM 27-22-51 PB 401, AFTER THAT THE TEST WAS SATISFACTORY. AFTER THOSE MX ACTIONS THE ACFT WAS RETURNED TO SERVICE.