What was found
INSPECTION FOUND A 3 INCH CRACK IN LEFT HORIZONTAL STABILIZER PANEL SIDE UPPER CHORD. THE CHORD WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-33-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3 INCH CRACK IN LEFT HORIZONTAL STABILIZER PANEL SIDE UPPER CHORD. THE CHORD WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-33-01.