What was found
INSPECTION FOUND A .625 INCH CRACK AND TWO SHEARED FASTENERS IN LEFT WINGTIP LOWER TRAILING EDGE SKIN. THE FASTENERS WERE REMOVED AND THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .625 INCH CRACK AND TWO SHEARED FASTENERS IN LEFT WINGTIP LOWER TRAILING EDGE SKIN. THE FASTENERS WERE REMOVED AND THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-02.