As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT TOP OF DESCENT NR 1 ENGINE WOULD NOT RESPOND TO THRUST LEVER INPUT ABOVE IDLE POSITION, SHUTDOWN USING IN-FLIGHT ENGINE FAILURE AND SHUTDOWN. COULD NOT DUPLICATE ON THE GROUND, ALL TROUBLESHOOTING SHOWED NO DEFECTS IAW 71-00-42. DID A PRECAUTIONARY, REMOVED AND REPLACED FUEL CONTROL PER MM 73-21-01, OPS NORMAL PER MM 71-00-00. C/W WINDMILL INSP, NO DEFECTS NOTED.