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