As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE HINGE ARM BR1 AND ATTACH FORK FITTING OF THE VERTICAL STABILIZER WAS FOUND WITH A CRACK AT HOLES #5 AND #7 DURING INSPECTIONS. MAINTENANCE ATTEMPTED TO REMOVE THE CRACK DAMAGE BY OVERSIZING. THE CRACK STILL REMAINS AT EACH HOLE WITH A DIAMETER OF 0.279".