As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE PILOT REPORTED AFTER HIS FLIGHT THAT THERE WAS EXCESSIVE PLAY IN THE HORIZONTAL STAB ATTACH AT THE FUSELAGE LT SIDE. CLOSE INSP UNCOVERED THE STRUCTURAL BRACKET PN: 0712042-1 TO BE CRACKED RIGHT THROUGH. THE PART WAS REPLACED WITH A FACTORY SUPPLIED PART AND ALL SYS FUNCTION CHECKED NORMAL.