As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RUDDER LT CONDUCTIVE FRAME DEBONDED. REMOVED DAMAGED CONDUCTIVE FRAME PER SRM 51-10-02 GENERAL ; AND FASTENERS PER SRM 51-40-02. ACCOMPLISHED PERMANENT REPAIR OF CONDUCTIVE FRAME ZONE 3. IAW SRM 55-40-01-1A-3 ALLOWABLE DAMAGE 3. RUDDER BALANCE ACCOMPLISHED ON TTG8Q01BCK5C. ACCOMPLISHED HFEC OF THE CUT LINE FOR THE CONDUCTIVE FRAME PER NDT PART 6; 51-00-00 PROCEDURE 23. NO DEFECTS FOUND;[04] RII INSPECTION C/W