What was found
INSPECTION FOUND A .75 INCH CRACK AT STIFFENER ON INBOARD SIDE OF LT WING LEADING EDGE RIB, WBL 92.0. A DOUBLER WAS INSTALLED IAW SRM 51-40-4 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .75 INCH CRACK AT STIFFENER ON INBOARD SIDE OF LT WING LEADING EDGE RIB, WBL 92.0. A DOUBLER WAS INSTALLED IAW SRM 51-40-4 AND 51-30-2.