What was found
RT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD BORE SURFACE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.387", MATERIAL REMOVED: 0.008", REMAINING THICKNESS: 0.379", MINIMUM ALLOWABLE THICKNESS: 0.408". REPAIR SHIM FABRICATED AND INSTALLED IAW EA 1-5750-T0309816 A PART 2, STEP 1. TITLE: WINGS, FLIGHT SURFACES, EO 1-5750-7-5002, RT WING-OTBD FLAP, OTBD HINGE ASSY, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504779 FOR WORK DETAILS.