As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT FUSELAGE WING TO BODY STRUCTURE STA 500D CURVED ANGLE AT WING LEADING EDGE IS CRACKED / REMOVED CRACKED ANGLE STA 500D RHCURVED ANGLE AT WING TO BODY STRUCTURE AND INSTALLED NEW ANGLE PART #116A3118U10 ATG# EU1255 ALL IAW SRM REMOVED AND REPLACED MARKED WORKING FASTENER IAW SRM 51-40-02-0G-0 STEP 4B/ AND DWG #116A3010 REV C. AND DWG# 11643118 REV-A.