What was found
RIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.708", FINAL DIA: 0.722". MAXIMUM ALLOWABLE DIA: 0.709". SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-T0325475, PART 1, STEP 1B. TITLE: WINGS, FLIGHT SURFACES-EO1-5750-7-5002. RT WING, OTBD FLAP, INBD HINGE, WING SIDE CORROSION REPAIR. REFER TO WRI: 57507889 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.