As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A MAINTENANCE VISIT, FOUND OVERSIZE HOLE TO LT FLAP LINK SUPPORT FITTING AT STA XF 339. REWORK TO 0.874/0.8762 B/P DAI HOLES. OPEN SUBJECT HOLES TO REMOVE MINIMUM MATERIAL, ENLARGE BOTH HOLES. FABRICATED AND INSTALLED 2 EACH BUSHINGS IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04269.