What was found
RIGHT WING, OTBD FLAP OTBD FWD HINGE BRACKET, WING SIDE, LOWER INBD STUD ATTACH BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.584", FINAL HOLE DIA: 0.612" AND MAXIMUM ALLOWABLE HOLE DIA: 0.584". NEW SHOULDER BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0325483 PT 1, STEP 1A, TITLE: WINGS FLIGHT SURFACES, EO 1-5750-7-5002. RIGHT WING OTBD FLAP, OTBD HINGE, WING SIDE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100. REFER TO NR 57503738 FOR WORK DETAILS.