As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.223", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSHING FABRICATED & INSTALLED PER EA 1-5750-T0342012 P1 STEP 1B. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.