As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN)THE SUPPORT ASSEMBLY WAS FOUND CRACKED THROUGH 80 PERCENT OF THE STRUCTURE. THE SUPPORT ASSEMBLY WAS FOUND TO BE DISTORTED TO THE POINT WHERE THE RUDDER CONTROL WOULD BE INTERFERED WITH AND GROUND NOS E WHEEL STEERING WOULD BE DIFFICULT. THE SUBMITTER SUSPECTS THAT THE DAMAGE WAS CAUSED BY TOWING THE AIRCRAFT WITH THE FLIGHT CONTROLS LOCKED OR PERHAPS A SUDDEN STRONG WIND GUST FROM THE REAR OF THE AIRCRAFT WITHOUT THE GUST LOCKS IN PLACE.