As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 7 INCH LONGITUDINAL CRACK ALONG UPPER SURFACE OF LT WING LEADING EDGE BETWEEN SLAT NR 3 AND NR 4. THE AREA WAS REPAIRED IAW ECRA 5720-01665. A DIP WAS INITIATED TO INSPECT FOR DELAMINATION AND WEAR EACH 1000 HOURS AND ACCOMPLISH PERMANENT REPAIR WITHIN 18 MONTHS OR NEXT C-CHECK, WHICHEVER OCCURS FIRST.