What was found
AT C-CHECK, LEFT WING INSPECTION REVEALED CRACK AT WING RIB STA 629, ATTACH FLANGE AT S-2 LOWER SIDE. STOP DRILLED CRACK, ACCOMPLISHED HFEC OF STOP HOLE, ENLARGED STOP HOLE ADDITIONAL .062 PER S/B 57-0127. INSTALLED ANGLE REPAIR PER SRM 57-10-5 AND S/B 57-0127, 10 BY 3.