As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING SCHEDULED 500HR INSPECTION THE END OF THE RUDDER FITTING WHICH ATTACHES THE BOTTOM OF THE RUDDER TO THE FIN AND INCLUDES THE RUDDER STOPS WAS FOUND CRACKED ON THE LEFT FLANGE NEAR THE RUDDER PIVOT. NEW PART INSTALLED. (TC# 20190405011)