As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RUDDER TRIM INOP. DIVERTED TO ORD. C/B RESET, NO HELP. *S/D* THE INOP CONDITION OF THE RUDDER TRIM SYSTEM WAS DUE TO AN INTERMITTENT INTERNAL FAULT OF THE OF THE RUDDER TRIM ACTUATOR. THE SUBJECT ACTUATOR WAS REPLACED PER MM 27-21-11 AND ALL OPS CHECKS ARE NORMAL.