What was found
LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, PIVOT HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDING LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 2.306", FINAL HOLE DIA: 2.3290", MAXIMUM ALLOWABLE DIA: 2.3135". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325892, PART 1, STEP 1A WINGS, FLIGHT SURFACES-EO1-5750-7-5002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.