What was found
INSPECTION FOUND A 1.5 INCH CRACK IN NR 5 SLAT RIB WHERE ACTUATOR ATTACHES. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3, FIGURE 9.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN NR 5 SLAT RIB WHERE ACTUATOR ATTACHES. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3, FIGURE 9.