What was found
UPON INSPECTION OF THE NR 3 SLAT, THE SKIN WAS FOUND TO BE CRACKED AT THE ACTUATOR. A REPAIR WAS PERFORMED PER THE SRM 57-50-3, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON INSPECTION OF THE NR 3 SLAT, THE SKIN WAS FOUND TO BE CRACKED AT THE ACTUATOR. A REPAIR WAS PERFORMED PER THE SRM 57-50-3, FIGURE 1.