What was found
INSPECTION FOUND A 1 CRACK IN LT WING LEADING EDGE CAVITY RIB ADJACENT TO OUTBOARD SLAT ACCESS PANEL, OUTBOARD SIDE. THE CRACKED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER IAW SRM 57-20-00, FIGURE 1, 51-21-01, AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 CRACK IN LT WING LEADING EDGE CAVITY RIB ADJACENT TO OUTBOARD SLAT ACCESS PANEL, OUTBOARD SIDE. THE CRACKED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER IAW SRM 57-20-00, FIGURE 1, 51-21-01, AND 51-31-01.