As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 6 LEADING EDGE SLAT (PN 114W4508-29) CRACKED AT INBOARD TRACK CUTOUT. ONE CRACK THREE INCHES LONG AND THE SECOND IS FIVE INCHES LONG. *S/D* INTERIM REPAIR ACCOMPLISHED AND REPETITIVE INSPECTIONS SCHEDULED AT TEN CYCLE INTERVALS. PERMANENT REPAIR ACCOMPLISHED AT C-CHECK PER SRM 57-41-01.