What was found
LEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION BRACKET ASSEMBLY ARC0503-11. CORROSION AT HOLE 3 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE 0.522", FINAL HOLE 0.591", MAXIMUM ALLOWABLE HOLE 0.584". SHOULDER BUSHING FABRICATED BY MACHINING & INSTALLED AT LOWER MOUNT INBD, OTBD BORE IAW EA 1-5750-T0319681 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.