As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) FORWARD MOUNT OUTBOARD LUG SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING THICKNESS: 0.380" MATERIAL REMOVED: 0.003" REMAINING THICKNESS: 0.377" MINIMUM ALLOWABLE THK: 0.380". REPAIR CARRIED OUT PER EA 1-5750-T0331715 PART 1 STEP 2B. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.