As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 SLAT DELAMINATED AT OB END LWR SURFACE OF T/E WEDGE. AREA IS 1.6 INCHES CHORDWISE X 1.3 INCHES SPANWISE AT 1.3 INCHES FROM OB END AND 1.6 INCHES 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.