As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING AN INSPECTION OF THE RUDDER SYSTEM ON A 4TH PHASE 800 HOUR INSPECTION THE BLIND RIVETS WHICH ATTACH THE CONTROL ARM QUADRANT P/N 101-524038-1, TO THE RUDDER TORQUE SHAFT P/N 101-524012-11, WERE FOUND TO BE LOOSE. THE COMPLETE ASSEMBLY WAS REMOVED FROM THE AIRCRAFT AND THE LOOSE RIVETS REMOVED AND REPLACED WITH SERVICEABLE UNITS IAW THE SRM. THE ASSEMBLY WAS REINSTALLED AND CHECKED SERVICEABLE.