What was found
MAIN CABIN FLOORBEAM AT FRAME 30 IS CRACKED AT THE VERTICAL STIFFENER BETWEEN Y- 450 AND Y-953. REPAIRED FLOORBEAM IAW SRM 53-10-15; FIG 212.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN FLOORBEAM AT FRAME 30 IS CRACKED AT THE VERTICAL STIFFENER BETWEEN Y- 450 AND Y-953. REPAIRED FLOORBEAM IAW SRM 53-10-15; FIG 212.