As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND LOWER LEFT LEADING EDGE OF UPPER RUDDER CHAFED. THE ACCESS PANELS WERE REMOVED, THE AREA WAS CLEANED AND THE FASTENERS WERE REMOVED IAW SRM 51-30-2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-40-3, FIGURE 1. THE ACCESS PANELS WERE REINSTALLED IAW SRM 51-30-2.