What was found
DURING VERTICAL STABILIZER INSPECTION, FOUND RIGHT INTERNAL ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE AND FASTENERS IAW DWG 5912188 AND SRM 51-30.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING VERTICAL STABILIZER INSPECTION, FOUND RIGHT INTERNAL ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE AND FASTENERS IAW DWG 5912188 AND SRM 51-30.