As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE PILOT REPORTED THAT THE RUDDER TRIM WAS WEAK. INVESTIGATION LED TO FINDING THE ARM ATTACH POINT ON THE RUDDER CONTROL ARM ASSY (63457-003) HAD BROKEN OFF. THE RUDDER PEDAL ASSY WAS REMOVED FROM THE ACFT AND SUBSEQUENT INSPECTION FOUND THAT THE CENTER SUPPORT BRACKET (63451-000) WAS BROKEN AT THE FWD 2 ATTACH BOLTS, LEAVING ONLY THE AFT 2 BOLTS HOLDING THE SUPPORT IN PLACE. NEW PART WERE OBTAINED AND INSTALLED.