As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TYS, During a scheduled 1C inspection, corrosion was found on the support angle at main door entrance below the threshold strip. Maintenance removed and replaced the support angle. I/A/W-EMB-135/145-SRM-51-40-02. Repair procedure was satisfactory and aircraft will be released upon complection of inspection.