As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND RUDDER TAB DENTED ON RT SIDE. THE RUDDER TAB WAS REMOVED IAW MM 27-20-02. THE RUDDER TAB WAS REPAIRED IAW SRM 51-30-3. THE RUDDER AB WAS REINSTALLED IAW MM 27-20-02. A WEIGHT AND BALANCE WAS PERFORMED IAW SRM 55-40-01.