What was found
INSPECTION FOUND A 1.25 INCH CRACK IN LT WINGTIP SUPPORT ANGLE AT INBOARD END OF CLOSURE RIB. A DOUBLER WAS INSTALLED IAW SRM 51-30-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.25 INCH CRACK IN LT WINGTIP SUPPORT ANGLE AT INBOARD END OF CLOSURE RIB. A DOUBLER WAS INSTALLED IAW SRM 51-30-02.