As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET AT LOWER INBOARD CORNER INSIDE LEADING EDGE AREA. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-1, AND 51-10-2.