As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING LANDING FLARE, PILOT'S CONTROL YOKE SEPARATED FROM THE CONTROL SHAFT. INSPECTION REVEALED THE SHAFT HAD SHEARED OFF AT THE HOLES FOR THE TAPER PIN HOLDING THE YOKE TO THE SHAFT. CONDITION IS THE SUBJECT OF AD 77-17-04. AIRCRAFT WAS IN COMPLIANCE WITH 443.8 HOURS ACCUMULATED SINCE LAST DYE PENETRANT INSPECTION OF THE SHAFT.