As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE INSPECTION, DISCOVERED THE RUDDER CONTROL SYS LEFT CAM SHAFT QUADRANT ASSEMBLY HAD A CRACK ON THE BELLCRANK ORIGINATING FROM THE BELLCRANK TAPER PIN HOLE USED TO ATTACH IT TO THE TORQUE TUBE. R & R WITH A SERVICEABLE PART.