What was found
INSPECTION FOUND A 1.25 INCH CRACK AT INBOARD ROOT RIB OF RT WING SLAT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-02, FIGURE 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.25 INCH CRACK AT INBOARD ROOT RIB OF RT WING SLAT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-02, FIGURE 2.