What was found
INSPECTION FOUND A 1 INCH CRACK ON RIB OF RT WING FIXED LEADING EDGE JUST IN FRONT OF L/E DEVICE NR 5. THE CRACKED AREA OF RIB WAS TRIMMED OUT. THE AREA WAS REINFORCED WITH A DOUBLER IAW SRM 57-00-01, FIGURE 4, 51-21-01, AND 51-33-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK ON RIB OF RT WING FIXED LEADING EDGE JUST IN FRONT OF L/E DEVICE NR 5. THE CRACKED AREA OF RIB WAS TRIMMED OUT. THE AREA WAS REINFORCED WITH A DOUBLER IAW SRM 57-00-01, FIGURE 4, 51-21-01, AND 51-33-01.