As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PILOTS LEFT "RUDDER BAR WELD ASSEMBLY (CESSNA IPC DESCRIPTION)" BROKE (CRACKED) ALLOWING THE VERTICAL RUDDER PEDAL POST TO SEPARATE FROM THE HORIZONTAL CROSS OVER TUBE. THE BREAK WAS LOCATED ON THE HORIZONTAL PORTION BELOW THE VERTICAL POST.