As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT HAND WING OUTBOARD FLAP OUTBOARD FORWARD (WING SIDE) HINGE LOWER MOUNT OUTBOARD HOLE BORE CORROSION. HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0343410 P1 STEP 2B AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0343410 P1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.