What was found
DURING THE INITIAL INSPECTION, THE NR 5 LEADING EDGE SLAT, THE AFT HOLE ON THE OUTER SKIN WHERE THE FENCE IS MOUNTED WAS FOUND TO HAVE A .5 INCH LONG CRACK BESIDE IT. THE SKIN WAS REPAIRED PER MM 57-54-0 FIG 813.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING THE INITIAL INSPECTION, THE NR 5 LEADING EDGE SLAT, THE AFT HOLE ON THE OUTER SKIN WHERE THE FENCE IS MOUNTED WAS FOUND TO HAVE A .5 INCH LONG CRACK BESIDE IT. THE SKIN WAS REPAIRED PER MM 57-54-0 FIG 813.