As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND L/H UPPER RUDDER SKIN DENTED FOUR INCHES FROM LEADING EDGE AND APPROXIMATELY TWENTY INCHES DOWN FROM RUDDER ACTUATOR PANEL. THE CRACKED AREA WAS CUT OUT IAW SRM 55-20-3, FIGURE 1. A DOUBLER WAS INSTALLED IAW SRM 55-20-3, FIGURE 1 AND 51-10-2.