What was found
LEFT WING TO FUSELAGE PANEL ATTACH ANGLE IS CRACKED AT FS 450.00. REPLACED ANGLE IAW CRJ200 SRM 51-42-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING TO FUSELAGE PANEL ATTACH ANGLE IS CRACKED AT FS 450.00. REPLACED ANGLE IAW CRJ200 SRM 51-42-06.