What was found
LEFT WING OUTBOARD FLAP (WING SIDE) INBOARD FWD HINGE PIVOT HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 2.311", FINAL HOLE DIA: 2.317", MAXIMUM ALLOWABLE HOLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0326464, PART 1, STEP 1B. TITLE: WINGS, FLIGHT SURFACE, EO 1-5750-7-5002, LT WING OTBD FLAP INBD HINGE ASSY, WING SIDE. CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI: 57504778 FOR WORK DETAILS.