What was found
RIGHT EXTERNAL FUSELAGE WING TO BODY PANEL SUPPORT SPLICE CRACKED AT BS 500D, BETWEEN STRINGER 18R TO 19R. R & R THE SUPPORT SPLICE IAW DWG AND SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT EXTERNAL FUSELAGE WING TO BODY PANEL SUPPORT SPLICE CRACKED AT BS 500D, BETWEEN STRINGER 18R TO 19R. R & R THE SUPPORT SPLICE IAW DWG AND SRM.