As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .5 AND 1 INCH CRACK AT FASTENERS IN CURVED ANGLE INSIDE LEFT WING LEADING EDGE RIB OUTBOARD SIDE AT SLAT STA 0 (AFT OF NR 4 SLAT INBOARD MOST END). THE ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-2.