As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1.5 INCH CRACK IN RADIUS OF ANGLE AT OUTBOARD UPSTOP BLOCK ON NR 8 LEADING EDGE SLAT. A 1.5 INCH CRACK WAS ALSO FOUND IN RADIUS OF ANGLE AT INBOARD UPSTOP BLOCK ON NR 8 LEADING EDGE SLAT. THE CRACKED AREAS WERE CUT OUT, REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-10-4.