What was found
DURING ROUTINE C CHECK INSPECTION, RT OTBD FLAP FWD UPPER PLATING WORN, STA XF 226.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05258 DATE 06-24-05, SEMAN DWG ED 4005 DATE 06-20-05, EO SEMAN 2005913 DATE 06-24-05. REMOVED FASTENERS IAW DC-8 SRM 51-3-0 PAGE 1, C-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED PLATING IAW SEMAN DWG ED 4005, PERFORMED NDT INSPECTION. IAW DC-8 NDT SPM PART 06-10-01-001. NO CRACK, NO CORROSION FOUND. FABRICATED NEW PLATING SEGMENT + INTERNAL SPLICE + EXTERNAL DOUBLERS IAW SEMAN DWG ED 4005, DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 S