What was found
COCKPIT FLOOR, AFT END OF THE CONNECTOR FWD FUSELAGE I SUPPORT BETWEEN FRAMES 11 AND 12 HAS A CRACKED ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-23-04, 51-23-05, 51-23-06, 51-40-08.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
COCKPIT FLOOR, AFT END OF THE CONNECTOR FWD FUSELAGE I SUPPORT BETWEEN FRAMES 11 AND 12 HAS A CRACKED ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-23-04, 51-23-05, 51-23-06, 51-40-08.