What was found
INSPECTION FOUND A 10 INCH CRACK IN OUTBOARD RIB AT NR 5 SLAT ACTUATOR ATTACH POINT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND 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 10 INCH CRACK IN OUTBOARD RIB AT NR 5 SLAT ACTUATOR ATTACH POINT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.