What was found
INSPECTION FOUND RT SIDE OF RUDDER TRIM TAB DENTED. THE TRIM TAB WAS REMOVED AND REPLACED IAW MM 27-20-02, PARAGRAPH 3A, B, C. A WEIGHT AND BALANCE WAS PERFORMED ON THE TAB IAW SRM 55-40-1 AND THE CHECK WAS WITHIN LIMITS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND RT SIDE OF RUDDER TRIM TAB DENTED. THE TRIM TAB WAS REMOVED AND REPLACED IAW MM 27-20-02, PARAGRAPH 3A, B, C. A WEIGHT AND BALANCE WAS PERFORMED ON THE TAB IAW SRM 55-40-1 AND THE CHECK WAS WITHIN LIMITS.