What was found
LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE), OUTBOARD ACTUATOR HOLE BORE WAS CORRODED. THE CORROSION WAS REWORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113, PART 1, STEP 1D, AND STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.