As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. FWD HINGE PIVOT HOLE BORE (NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 2.3159", FINAL HOLE DIA 2.321", MAXIMUM ALLOWABLE HOLE DIA 2.3135". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341052 PART 1 STEP 2A AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.