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 INBOARD FORWARD (WING SIDE) HINGE LOWER MOUNT INBOARD HOLE BORE CORROSION. HOLE BORE (HOLE 7) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. SHOULDER BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-130948A P2 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.