As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE NR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND WITH THE UPPER SKIN DELAMINATED ALONG THTE I/B EDGE 3 FWD OF THE TRAILING EDGE OF THE PANEL. THE DAMAGED AREA MEASURES APPROX 5 (FWD/AFT) X 12. THE DAMAGE WAS REPAIRED WITH AN SRM COMPOSITE REPAIR PER ER/A 364968-14AD.