As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 10.5 INCH CRACK IN LT WING LEADING EDGE AT THE OUTBOARD END OF NR 1 LEADING EDGE SLAT. THE SURFACE WAS PREPARED IAW SRM 51-70-06. THE AREA WAS REPAIRED IAW ECRA 5720-01662. A DIP WAS ISSUED FOR FOLLOW-UP INSPECTION AND PERMANENT REPAIR PER ECRA 5720-01662.