As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED VISUAL INSPECTION, A CRACK WAS DISCOVERED THE RUDDER CONTROL ARM THAT CONNECTS THE RUDDER TRIM ACTUATOR MECHANISM TO THE RUDDER PEDAL CONTROL ASSEMBLY. THE CRACK EXTENDED FROM THE BOLT HOLE THAT ATTACHES THE CONTROL ARM ASSEMBLY TO THE RUDDER PEDAL ASSEMBLY BAR.