What was found
RIGHT WING TO FUSELAGE PANEL ATTACH ANGLE IS CRACKED AT FS 476.00. REPLACED ANGLE IAW CRJ 200 SRM 51-42-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING TO FUSELAGE PANEL ATTACH ANGLE IS CRACKED AT FS 476.00. REPLACED ANGLE IAW CRJ 200 SRM 51-42-06.