What was found
RIGHT WING TO FUSELAGE PANEL ATTACHING STRUCTURE AT FS 470.00 IS CRACKED. REPLACED SUPPORT ANGLE AT FS 470.00, RT SIDE WING TO FUSELAGE PANEL IAW 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 ATTACHING STRUCTURE AT FS 470.00 IS CRACKED. REPLACED SUPPORT ANGLE AT FS 470.00, RT SIDE WING TO FUSELAGE PANEL IAW SRM 51-42-06.