What was found
LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUT HOLE SURFACE CORROSION. CORROSION REWORKED IAW CMM 57-44-08. EXISTING THICKNESS UPPER 0.376", LOWER 0.376", MATERIAL REMOVED UPPER 0.007", LOWER: 0.007", REMAINING THICKNESS UPPER 0.369", LOWER 0.369". REPAIR SHIM FABRICATED & INSTALLED IAW CMM 57-44-08. REPAIR EVALUATED & FOUND BARREL NUT MATING SURFACE REMAINING THICKNESS OF UPPER 0.369" & LOWER 0369", WITHIN LIMIT BASED THE DIFFERENCE BETWEEN DWG LIMIT & CMM MAX. REWORKED LIMITS FOR BARREL NUT HOLE, MIN THICKNESS 0.3685". REPAIR CLASSIFIED AS MINOR IAW GMM 6- 2-100.