What was found
RUDDER FAIL - RUDDER SURFACE JAM FAULT / REPORTED BY PFCC UPPER RUDDER PCU (A606) TO REU ELECTRICAL FAULT / REPORTED BY PFCC. COMPLIED WITH RUDDER SURFACE JAM FAULT FIM TASK BD500-A-J55-40-00-01AAA-421A-A. DOWNLOADED REU'S NVM AND SENT TO BREEZE TO BE SENT TO AIRBUS. COMPLIED WITH RUDDER SKIN INSPECTION AND RUDDER PCU ACTUATOR FITTING INSPECTION. PERFORMED ACTUATION FLIGHT CONTROL SYSTEM TEST (PASSED) AND RUDDER ACTUATOR INTEGRITY TEST - BIT OPERATION (PASSED).