What was found
RT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET SIDE ATTACH SURFACE, FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 72 UPPER: EXISTING THICKNESS 0.451", MATERIAL REMOVED 0.005", REMAINING THICKNESS 0.446". LOWER: EXISTING THICKNESS 0.453", MATERIAL REMOVED 0.004", REMAINING THICKNESS 0.449". REPAIR ACCOMPLISHED IAW EA 1-5750-157179, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.