As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE (WING SIDE) LOWER MOUNT O/B BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA: 0.709", FINAL HOLE DIA: 0.712", MAXIMUM ALLOWABLE DIA: 0.709. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-341992 P1 STEP 1C AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-341992 P1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.