What was found
DURING FLIGHT AFTER 10000FT RH AILERON WITH RUDDER TRIM MAKE THE PLANE TO FLIGHT WITH APROX 10DEG BANK ANGLE. FOLLOWING TSM 27-20-00-810-804-A REV 56 THE RUDDER TRIM ACTUATOR (10CC) WAS REMOVED AND REPLACED IAW AMM 27-22-51-000-001-A REV 56 AND AMM 27-22-51-400-001-A REV 56. PENDING TEST. IN ACCORDING WITH TSM 27-20-00-810-804-A THE FAC 1CC1 WAS REMOVED AND REPLACED IAW AMM 22-66-34-000-002-A AND AMM 22-66-34-400-002-A AND PERFORMED OPERATIONAL TEST OF THE AUTOMATIC FLIGHT SYSTEM IAW AMM TASK 22-96-00-710-001. PERFORMED THE LAND CAT 3 CAPABILITY TEST IAW AMM TASK 22-97-00-710-001. ALL TEST OK.