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. HINGE UPPER BARREL NUT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIAMETER 0.384", FINAL HOLE DIAMETER: 0.409", MAXIMUM ALLOWABLE HOLE DIAMETER: 0.391". OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0341019 P1 STEP 1C AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.