What was found
MAIN FUSELAGE; PRESSURE FLOOR/WING TIE BEAM FITTING IS DENTED AND CRACKED ALONG LOWER FLANGE; LBL 3.0 FS 460.00. DISCOVERED DURING C-CHECK INSPECTION. NEW TIE BEAM FIT, DRILLED AND INSTALLED IAW CRJ SRM 51-40-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN FUSELAGE; PRESSURE FLOOR/WING TIE BEAM FITTING IS DENTED AND CRACKED ALONG LOWER FLANGE; LBL 3.0 FS 460.00. DISCOVERED DURING C-CHECK INSPECTION. NEW TIE BEAM FIT, DRILLED AND INSTALLED IAW CRJ SRM 51-40-11.