As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
COCKPIT FLOOR, AFT END OF THE CONNECTOR FWD FUSELAGE I SUPPORT BETWEEN FRAMES 11 AND 12 HAS A CRACKED ANGLE. (C-CHECK RO 6/18/2021) / REMOVED AND REPLACED CKPT FLOOR ANGLE BETWEEN FR 11-12 REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR DETAILS.