What was found
INSPECTION FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER REAR SPAR LOWER ATTACH ANGLE ON LT SIDE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER REAR SPAR LOWER ATTACH ANGLE ON LT SIDE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-30-2.