As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .75 INCH CRACK IN RIB AND DOUBLER AT LT WING LEADING EDGE INTERNALLY BETWEEN NR 9 AND NR 10 SLAT TRACK CUTOUTS, STA XRS 324. THE CRACKED RIB AND CLIP ANGLE WERE REMOVED AND A NEW RIB AND CLIP ANGLE WERE INSTALLED IAW SRM 51-10-03, 51-30-02, AND 51-30-05.