What was found
INSPECTION FOUND A .3125 INCH CRACK IN NR 3 SLAT LOWER TRAILING EDGE EXTERIOR SKIN AT RIVET BELOW ACTUATOR PISTON. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .3125 INCH CRACK IN NR 3 SLAT LOWER TRAILING EDGE EXTERIOR SKIN AT RIVET BELOW ACTUATOR PISTON. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3.