What was found
MAIN CABIN FLOORBEAM ANGLE AT FRAME 80 IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN FLOORBEAM ANGLE AT FRAME 80 IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-21.