What was found
INSPECTION FOUND A .3125 INCH CRACK IN RT INBOARD AFT FLAP LOWER LEADING EDGE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .3125 INCH CRACK IN RT INBOARD AFT FLAP LOWER LEADING EDGE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-02.