As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BOTH LT AND RT RUDDER CABLES NOT INSTALLLED CORRECTLY. PASSING OVER THE GUARD PINS INSTEAD OF THROUGH THE PULLEYS, RESULTING IN SEVERE CABLE CHAFING. THE LT GUARD PIN FAILED UNDER STRESS AND THUS REDUCING CABLE TENSION. THE RT GUARD PIN REMAINED INTACT, ABBRAIDING AND SEVERELY DAMAGING THE CABLE. (GUARD PIN ITEM NR182)