As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE NR 8 SLAT WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED. THE DELAMINATION IS A 3 INCH DIA CIRCLE, APPROX 4 FROM THE AFT EDGE OF THE TRAILING EDGE WEDGE. THE WEDGE IS MANUFACTURED WITH 0.016 5052-H38 FACE SHEETS WITH A METALLIC HONEYCOMB CORE PER BMS 4-6, TYPE 4.1-25.