What was found
RIGHT WING INBD FLAP OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.250", FINAL HOLE DIA: 1.285" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-162344B, PT 4, STEPS 1A & 1C TITLE: WINGS, FLIGHT SURFACES, RT WING, INBD FLAP, OTBD HINGE BRACKET ASSY, CORROSION REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO NR 57503746 FOR WORK DETAILS.