As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND A CRACK ON THE NR 2 LEADING EDGE SLAT COVE PANEL, CRACK IS LOCATED ON THE OUTBD COVE PANEL INBD SIDE IN THE MIDDLE AND THRU A FASTENER, CRACK MEASURES 1 AND 1-4TH OF AN INCH. FOUND NR 2 SLAT WITH A 1.5 INCH CRACK ON THE O/B COVE SKIN PANEL. REMOVED NR 2 LEADING EDGE SLAT. REPAIRED NR 2 LEADING EDGE SLAT. OPS CHECKED GOOD.