As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 SLAT DELAMINATED OB END OF LOWER SURFACE OF T/E WEDGE OF AREA 3.3 INCHES CHORDWISE X 1.6 INCHES SPANWISE. THE ABOVE NOTED DELAM CONDITION WAS DUE TO WEAR FROM NORMAL LOADS EXPERIENCED DURING A FLIGHT OVER A PERIOD OF TIME. THE TRAILING EDGE WEDGE OF THE SLAT WAS REPAIRED USING AN ADHESIVE INJECTION METHOD.