As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING ZONE #2 LEADING EDGE FASTENER; HOLE #8(NUMBERED FROM THE PYLON TO THE FUSELAGE) HAS A CRACK INDICATION IN THE SKIN ONLY. VERIFIED WITH NDT INSPECTION OF HOLE PER BOEING NDT MANUAL PART 6 51-00-00 PROC.23 AND PART6; 53-30-00 PROC.4. HOLE IS CURRENTLY REAMED TO .262. / REPAIRED PER EA#1-757-16556; AND EO #14084-57. SEE BOTH EA AND EO FOR ALL COMPLETED WORK AND SIGN-OFF.