What was found
LEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE SURFACE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.357", MATERIAL REMOVED 0.004", REMAINING THICKNESS 0.353", MINIMUM ALLOWABLE THICKNESS 0.408". REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0319681 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.