As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS EPR CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342161 P1 STEP 2A AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342161 P1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.