What was found
FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH ANGLE IS CRACKED, OUTBOARD SIDE FS280.00 RBL 9.0. REPLACED ATTACH ANGLE IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-42-13.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH ANGLE IS CRACKED, OUTBOARD SIDE FS280.00 RBL 9.0. REPLACED ATTACH ANGLE IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-42-13.