As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) PILOT NOTED SLIGHT BINDING IN RUDDER PEDALS DURING RT RUDDER INPUT. FOUND THE RUDDER GAP STRIP WAS CATCHING THE RUDDER L/E AT TRIM TAB CUTOUT HOLE. RUDDER L/E WAS REWORKED SLIGHTLY TO CLEAR GAP STRIP. GAP STRIP WAS REWORKED TO REMOVE DENT. CLEARANCES OF RUDDER COMPONENTS WAS VERIFIED SERVICEABLE AFTER RE-WORK AND ACFT RETURNED TO SERVICE.