What was found
RIGHT INTERNAL VERTICAL STABILIZER ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 551-30-02 AND DWG 5912188, REV BD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT INTERNAL VERTICAL STABILIZER ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 551-30-02 AND DWG 5912188, REV BD.