What was found
INSPECTION TYPE:N/A RIGHT WING LES 665 FRONT SPAR STIFFENER UPPER AREA FOUND CRACK. CRACK LENGTH .5 INCH APPROX. RIGHT WING LES 665 FRONT SPAR STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:N/A RIGHT WING LES 665 FRONT SPAR STIFFENER UPPER AREA FOUND CRACK. CRACK LENGTH .5 INCH APPROX. RIGHT WING LES 665 FRONT SPAR STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.