As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AIRCRAFT EXPERIENCED COMPLETE STABILATOR PRIMARY CONTROL FAILURE. CAUSE OF FAILURE WAS DETERMINED TO BE CORROSION OF LOWER STABILATOR CONTROL CABLE FORWARD CABLE END JUST T/E OF BARREL. ESTABLISH A TIME LIFE REPLACEMENT OF CONTROL CABLE. PROBLEM IS NOT DETECTABLE DURING PERIODIC INSP IAW MM. (K)