What was found
MAIN CABIN FLOORBEAM HAS CORROSION STA 365 RBL 14 TO RBL 26. REPAIRED FLOORBEAM AT BS 365 BETWEEN RBL 33.5, LBL 11 IAW 53-00-51 REPAIR 10; CORROSION DAMAGE REMOVED MAT LOSS, ORIG MAT THICKNESS 0.125" PER DWG 140N5190.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN FLOORBEAM HAS CORROSION STA 365 RBL 14 TO RBL 26. REPAIRED FLOORBEAM AT BS 365 BETWEEN RBL 33.5, LBL 11 IAW 53-00-51 REPAIR 10; CORROSION DAMAGE REMOVED MAT LOSS, ORIG MAT THICKNESS 0.125" PER DWG 140N5190.