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 ASSY I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE LOWER MOUNT O/B BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08, EXISTING HOLE DIA 0.705", FINAL HOLE DIA 0.722" MAXIMUM ALLOWABLE HOLE DIA 0.709". SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T03421926 P1 STEP 1B AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0341926 P1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.