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 LOWER LEADING EDGE SUPPORT ANGLE INSIDE LT WING LEADING EDGE AFT OF NR 3 LEADING EDGE FLAP AREA, FSS 120. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2.