What was found
INSPECTION FOUND A 12.5 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD RIB UPPER STIFFENER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 12.5 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD RIB UPPER STIFFENER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-31-01.