What was found
INSPECTION FOUND A 6 INCH CRACK IN LT WING LOWER SURFACE ON I/B CORNER OF FUELING BAY DOOR CUTOUT. THE AREA WAS REINFORCED WITH A DOUBLER USING RIVETS IAW SRM 57-10-00, FIGURE 68 AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 6 INCH CRACK IN LT WING LOWER SURFACE ON I/B CORNER OF FUELING BAY DOOR CUTOUT. THE AREA WAS REINFORCED WITH A DOUBLER USING RIVETS IAW SRM 57-10-00, FIGURE 68 AND 51-31-01.