What was found
DURING C-CHECK INSPECTION, MAIN FUSELAGE FLOORBEAM AT LBL 9.0 HAS A CRACKED INBOARD ATTACH ANGLE AT FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION, MAIN FUSELAGE FLOORBEAM AT LBL 9.0 HAS A CRACKED INBOARD ATTACH ANGLE AT FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM.