As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A ROUTING 100HR/ANNUAL INSPECTION, CRACKS WERE FOUND IN SUPPORTING .025 WEB OF HORIZONTAL STABILATOR HORN ASSY AND ALSO A CRACK RADIATING FROM LIGHTNING HOLE OF .063 FORWARD COVER PLATE (PN 391-020-305-2) THAT IS PART OF THE BOLTED ASSEMBLIES SECURING THE 2 STABILATOR HALFS TOGETHER.