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