As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 2 CRACK IN BOTH INBOARD AND OUTBOARD BRACKETS WHERE LT WING NR 2 LEADING EDGE FLAP ACTUATOR ATTACHES INSIDE LEADING EDGE. NEW BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. THE FLAP ACTUATOR WAS REMOVED AND REINSTALLED IAW MM 27-80.