What was found
LEFT WING OTBD FLAP, FLAP SIDE, INBD AFT HINGE PIVOT INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT CMM 57-52-04. EXISTING HOLE: DIA 1.154", FINAL HOLE: DIA 1.217", MAXIMUM ALLOWABLE HOLE: DIA 1.150". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA1-5750-T0326466, PART 1, STEP 1A. TITLE: WINGS FLIGHT SURFACES, EO 1-5750-7-5002-LT WINGS-OTBD FLAP-INBD HINGE BRACKET ASSY CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REF TO WRI: 57504777 FOR WORK DETAILS.