As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK VERTICAL STAB LEADING EDGE SUPPORT ANGLE, BS 1016. REMOVED SUPPORT ANGLE AND PLATE IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON AREA AND NO DAMAGE FOUND. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, AND DWG 176A3101 REV -.