As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 10 CRACK IN LT WING FIXED LEADING EDGE PANEL AFT OF NR 4 LEADING EDGE SLAT AND A 6.75 INCH CRACK WAS FOUND AFT OF NR 3 LEADING EDGE SLAT. THE AREAS WERE REPAIRED IAW ECRA 5720-01666. A DIP WAS ISSUED IAW ECRA 5720-01666.