As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) WHILE COMPLETING A SCHEDULED INSPECTION, IT WAS NOTED BY AME THAT THE RUDDER TRIM HAD VERY LITTLE RESISTANCE AND THE TRIM WAS NOT MOVING PROPERLY. THE SWAGE END OF THE TRIM SHAFT THAT GOES FROM THE TRIM WHEEL TO THE RUDDER PEDALS WAS CRACKED AT THE RUDDER PEDAL END CAUSING THE SHAFT TO SLIP IN SWAGE INTERMITTENTLY.