As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION, THE CENTER OMEGA BEAM AROUND THE ANCHOR NUT WAS FOUND CORRODED BETWEEN FRAME 24 AND FRAME 25. THE CENTER OMEGA BEAM AROUND ANCHOR NUT BETWEEN FRAME 24 AND FRAME 25 WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012075.