What was found
INSPECTION FOUND A .375 INCH CRACK IN NR 3 SLAT LOWER ATTACH ANGLE FOR PANELS AT ACTUATOR ATTACH AREA. THE CRACK WAS ROUTED OUT. AN ANGLE DOUBLER WAS INSTALLED IAW SRM 51-40-4, FIGURE 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .375 INCH CRACK IN NR 3 SLAT LOWER ATTACH ANGLE FOR PANELS AT ACTUATOR ATTACH AREA. THE CRACK WAS ROUTED OUT. AN ANGLE DOUBLER WAS INSTALLED IAW SRM 51-40-4, FIGURE 3.