What was found
RT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA 0.594", FINAL HOLE DIA 0.705", MAXIMUM ALLOWABLE DIA: 0.667". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325943, PART 1, STEP 1B WINGS-FLIGHT SURFACES EO1-5750-7-5002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.