As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 4 SLAT DELAMINATED AT OB END LOWER SURFACE OF T/E WEDGE. AREA 2.2 INCH CHORDWISE X 3.0 INCH SPANWISE LOCATED 1.5 INCH FROM OB END AND 3.0 INCH FROM T/E. 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.