What was found
DURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THE NR 11 RIB WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER M/M 57-54-0 FIG 804.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THE NR 11 RIB WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER M/M 57-54-0 FIG 804.