As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT HAND WING OUTBOARD FLAP OUTBOARD FORWARD (WING SIDE) HINGE LOWER MOUNT INBOARD HOLE 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-T0343430 P1 STEP 2A AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0343430 P1 STEP 2. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.