As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING PHASE 1 ACFT INSPECTION, DISCOVERED THE RUDDER TO BELL CRANK RT ATTACH BOLT MISSING. FURTHER INVESTIGATION REVEALED THE BOLT HAD FAILED. AN INSPECTION OF THE RUDDER TORQUE TUBE WAS CONDUCT & IT WAS NOTED THAT THE ATTACH HOLES OF THE BELL CRANK & RUDDER WERE ELONGATED. PARTS MENTIONED WILL BE REPLACED WITH NEW & AS A PRECAUTION REPLACING THE UPPER & CTR RUDDER HINGE & HARDWARE. NO FURTHER ACTION REQUIRED.