What was found
LEFT WING OUTBOARD FLAP, INBOARD FORWARD HINGE, WING SIDE LOWER MOUNT INBOARD HOLE SURFACE CORRODED. HOLE SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113, PART 1, STEP 1C, AND STEP 1. A REPAIR SHIM WAS FABRICATED, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.