What was found
DURING A ROUTINE C CHECK RT WING OB L/E OUTER SECTION UPPER SKIN SURFACE CORRODED, STA. XW 761.000. REPAIR WAS ACCOMPLISHED. FASTENERS AND CORROSION WERE REMOVED ALONG WITH THE DAMAGED AREA IAW SRM 51-1-20D PG 21., 51-3-0 PG. 7, 51-1-21 PG 1. AN NDT INSPECTION WAS PERFORMED IAW NDT SPM PART 6-10-01-011. FABRICATED FILLER & DOUBLER IAW DWG. V22-R15 CLEANED, TREATED AND PRIMED AREA, INNER FACE OF FILLER & DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT ( PRC) TO FAYING SURFACES IAW DC8 SRM. 51-1-11 PG. 9 INSTALLED FILLER & DOUBLER AND NEW FASTENERS IAW DWG. V22-R15. SRM 51-1-21 PG.1, 51-2-20D PG. 9, 51-3-03 PG.1