As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C5 CHECK - FORE RUDDER SKIN T/E HAS 3 AREAS OF DAMAGE BY THE UPPER HINGE POINT. PERFORMED CLEAN UP OF DAMAGED AREAS IAW SRM 51-14-00, REPAIR-03. MATERIAL LOSS LOWER AREA FOUND WITHIN LIMITS AND UPPER AREAS TO BE OUT OF LIMITS IAW SRM 51-14-00 REPAIR-03 PART 5-C-7-C. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-01-250-801. COMPLIED WITH TC RD 8/4-55-571 FOR PERMANENT REPAIR.