As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON POWER REDUCTION FOR DESCENT, THE ENGINE DID NOT RESPOND TO THROTTLE LEVER INPUT. THE ENGINE WAS SHUTDOWN ON FINAL APPROACH AND A DEAD-STICK LANDING ACCOMPLISHED. SUBSEQUENT INSPECTION REVEALED THE FUEL CONTROL INTER-CONNECT ROD END TO BE STIFF AND LIMITED IN MOVEMENT DUE TO A SEIZED ROD-END BALL SWIVEL.