As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RUDDER FRONT SPAR HINGE BRACKET FOR UPPER PUSH-PULL ROD IS CRACKED APPROX. 2.5". CRACK WAS DISCOVERED DURING THE L8 INSPECTION. SUSPECT THAT THE DAMAGE OCCURRED FROM THE WIND PUSHING THE RUDDER TO THE RT, AGAINST THE RT STOP, REPEATEDLY WITH THE GUST LOCK OFF.