What was found
INSPECTION FOUND A 1 INCH CRACK IN CLIP AT VERTICAL STABILIZER LOWER LT AFT CORNER JUST FORWARD OF RUDDER LEADING EDGE. THE CLIP WAS REMOVED AND A NEW CLIP WAS INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-4, AND 51-10-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN CLIP AT VERTICAL STABILIZER LOWER LT AFT CORNER JUST FORWARD OF RUDDER LEADING EDGE. THE CLIP WAS REMOVED AND A NEW CLIP WAS INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-4, AND 51-10-3.