What was found
WHEN AUTOPILOT DISENGAGED DURING APPROACH PHASE OF FLIGHT, THE RUDDER CONTROLS JAMMED AND EXCESSIVE FORCE WAS REQUIRED TO MOVE RUDDER CONTROLS. REPLACED DEFECTIVE RUDDER SERVO.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHEN AUTOPILOT DISENGAGED DURING APPROACH PHASE OF FLIGHT, THE RUDDER CONTROLS JAMMED AND EXCESSIVE FORCE WAS REQUIRED TO MOVE RUDDER CONTROLS. REPLACED DEFECTIVE RUDDER SERVO.