As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) WHILE INSPECTING VERTICAL STABILIZER LEADING EDGE IMPACT ON SKIN, A CRACK WAS IDENTIFIED ON THE LEFT HAND HORIZONTAL STABILIZER ATTACH BRACKET. NDT BY EDDY CURRENT METHOD CONFIRMED A .0625 INCH CRACK EMANATING FROM A WELD TERMINATION OF A DOUBLER ON BRACKET. NEW BRACKETS INSTALLED ON BOTH LEFT AND RIGHT SIDES AS NEW BRACKETS MADE FROM THICKER, NON-WELDED MATERIAL.