As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING OUTBOARD FLAP INBOARD FORWARD (WING SIDE) HINGE ACTUATOR INBOARD BORE HOLE CORROSION. HINGE ACTUATOR INBOARD HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-130944A P3 STEP 1B AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.