What was found
LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE SURFACE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.328", MATERIAL REMOVED 0.013", REMAINING THICKNESS 0.315", MINIMUM ALLOWABLE THICKNESS 0.320". REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0319681 PART 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.