As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .125 INCH CRACK IN RT WING NR 7 SLAT LOWER SPANWISE CHORD ANGLE AT CUTOUT FOR I/B TRACK AND A .3125 INCH CRACK AT STOP PAD AREA SIX INCHES INBOARD. THE ANGLE WAS REMOVED. AN ANGLE AND REPAIR SPLICE WERE INSTALLED IAW SRM 51-40-3, 51-10-2, AND 57-30-2.