What was found
DURING INITIAL INSPECTION, OF THE NR 5 LEADING EDGE SLAT, THE LOWER AFT ANGLE AT THE O/B END WAS FOUND TO HAVE A CRACK. THE CRACK WAS REPAIRED PER MM 57-54-0 FIG 805A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INITIAL INSPECTION, OF THE NR 5 LEADING EDGE SLAT, THE LOWER AFT ANGLE AT THE O/B END WAS FOUND TO HAVE A CRACK. THE CRACK WAS REPAIRED PER MM 57-54-0 FIG 805A.