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 O/B FWD HINGE (WING SIDE) BARREL NUT HOLE CORROSION. HINGE BARREL NUT HOLE (NR 10 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.678", FINAL HOLE DIA: 0.707", MAXIMUM ALLOWABLE DIA: 0.667. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-127792 A P2 STEP 1D AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.