As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT LEADING.EDGE SLAT NR 1 CLOSURE PANEL HAS 3 INCHES PUNCTURE, CRACKED, APPROX 20 INCHES FROM INBOARD EDGE. PERFORMED TEMPORARY REPAIR PER ENGINEERING VARIATION AUTHORITY. SLAT TO BE PERMANENTLY REPAIRED WITHIN 300 HOURS. PUNCTURE CAUSED BY GROUND EQUIPMENT CONTACT.