What was found
INSPECTION FOUND A .25 INCH CRACK AT O/B CORNER OF RT WHEEL WELL FORWARD FAIRING AFT ATTACH STRIP. AN ANGLE WAS INSTALLED IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK AT O/B CORNER OF RT WHEEL WELL FORWARD FAIRING AFT ATTACH STRIP. AN ANGLE WAS INSTALLED IAW SRM 51-40-02.