What was found
DURING A ROUTINE C CHECK INSPECTION FOUND LT WING OB L/E INNER SECTION UPPER SKIN SURFACE CORRODED, STA.XW. 485.000. REPAIR WAS ACCOMPLISHED. REMOVED DAMAGED AREA IAW DWGV22-R01 INCLUDING FASTENERS AND CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-1-21 PG.1, 51-1-20D PG. 21 AND SRM 51-1-8 PG. 17-18. NDT INSPECTION WAS PERFORMED IAW NDT SPM PART 6-10-01.001 AREA WAS CLEANED, TREATED AND PRIMED. FABRICATED A REPAIR DOUBLER AND FILLER . CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND THE FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW DCI SRM 51-1-11 PG 9. INSTALLED THE REPAIR DOUBLER AND FILLER USING THE NEW FASTENERS IAW DWG. V22-R01 AND DC8 SRM 51-1-21 PG 1 AND 51-1-20D P