What was found
LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE SURFACE CORROSION. CORROSION REWORKED IAW CMM 57-44-09. EXISTING THICKNESS UPPER 0.426", LOWER 0.448", MATERIAL REMOVED UPPER 0.006", LOWER 0.006", REMAINING THICKNESS UPPER 0.420", LOWER 0.442". REPAIR SHIM FABRICATED & INSTALLED IAW 1-5750-T0319681 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.