As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF RUDDER, TO REPAIR SKIN DAMAGE AT HINGE POINTS FOUND RUDDER SUPPORT STIFFENER ANGLE (PN 5412481-004) CRACKED UNDER RUDDER PRIMARY TRAVEL STOP AT FRAME STATION 48. RUDDER OVER TRAVELING WHEN GUST LOCK NOT INSTALLED AND WHEN PARKED OUTSIDE IN WINDY CONDITIONS. ENSURE FLIGHT CONTROL GUST LOCKS ARE INSTALLED WHEN PARKED OUTSIDE. (EA09200600885) (K)