What was found
MAIN FUSELAGE FITTING CRACKED AT FS 460.00 RBL 9.0 OUTBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11 AND RII 53 401.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN FUSELAGE FITTING CRACKED AT FS 460.00 RBL 9.0 OUTBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11 AND RII 53 401.