As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING LEADING EDGE CAVITY, WEB CRACKED AT LES 588. DAMAGE TO WING FIXED LEADING EDGE NOSE BEAM WEB. AFFECTED SRM REPAIR PROCEDURE. VERIFIED CRACK CONTAINED BY STOP DRILLS PER HFEC NDT 51-00-19, PRT 6. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 57-41-13. A/C READY FOR SERVICE.