What was found
DURING A ROUTINE C CHECK INSPECTION FOUND RT INNER WING AFT TOP PANEL PLATING CRACK DAMAGED AT STA XRS 74.869, S-5. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED SECTION. PERFORMED NDT INSPECTION AND FABRICATED EXTERNAL DOUBLER + FILLER PLUG. CLEANED, TREATED AND PRIMED AREA + FILLER PLUG + REPAIR DOUBLER SIDE. APPLIED SEALANT TO FAYING SURFACES AND INSTALLED REPAIR PARTS IAW SEMAN DWG ED-3832 AND FAA FORM 8110-3 NR 05020, DC8 SRM 51-1-11, 51-1-15, 51-1-20D, 51-1-22, 51-1-26, 51-3-1, 51-3-2.