What was found
LEFT WING INBD FLAP OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.2834", FINAL HOLE DIA: 1.315" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5750-162343D PT 4 STEPS 1A & 1C TITLE: WINGS, FLIGHT SURFACES, LT WING, INBD FLAP, OTBD HINGE BRACKET ASSY-CORROSION REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO 57503744 FOR WORK DETAILS.