What was found
RT WING TO FUSELAGE PANEL SUPPORT STRUCTURE ANGLE IS CRACKED AT FS 449.85. REPLACED RT WING TO FUSELAGE PANEL SUPPORT ANGLE IAW SRM 51-42-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT WING TO FUSELAGE PANEL SUPPORT STRUCTURE ANGLE IS CRACKED AT FS 449.85. REPLACED RT WING TO FUSELAGE PANEL SUPPORT ANGLE IAW SRM 51-42-06.