As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT O/B FLAP O/B FWD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) PIVOT HOLE BORE (4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 2.312", FINAL HOLE DIA 2.316", MAXIMUM ALLOWABLE HOLE DIA 2.3135". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341053 PART 1 STEP 2C AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.