What was found
INSPECTION FOUND A .25 INCH CRACK IN RIB OF NR 5 SLAT ACTUATOR ATTACH POINT INBOARD SIDE. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-40-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN RIB OF NR 5 SLAT ACTUATOR ATTACH POINT INBOARD SIDE. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-40-3.