What was found
DURING ROUTINE C-CHECK INSPECTION FOUND RT WING OB L/E INNER SECTION UPPER SKIN SURFACE CORRODED, STA XW 485.000. REPAIRS WERE ACCOMPLISHED IAW APPROVAL DOCUMENT DWG V22-R02, REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, 51-1-20D PAGE 21, 51-3-0 PAGE 1, REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGE 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-1 PAGE 11 TRIMMED OUT THE DAMAGED AREA IAW DWG V22-RO2, PERFORMED NOT INSPECTION IAW DC8 NOT SPM PART 6-10-01.001, CLEANED TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED A REPAIR DOUBLER AND A FILLER.