What was found
(CAN) DURING DESCENT, THE ENGINE WOULD NOT RESPOND TO THROTTLE INPUTS FOR POWER REDUCTION. THE ENGINE WAS SHUT DOWN ON FINAL APPROACH. THE FUEL CONTROL UNIT WAS SUBSEQUENTLY REPLACED. (TC# 20060704014)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING DESCENT, THE ENGINE WOULD NOT RESPOND TO THROTTLE INPUTS FOR POWER REDUCTION. THE ENGINE WAS SHUT DOWN ON FINAL APPROACH. THE FUEL CONTROL UNIT WAS SUBSEQUENTLY REPLACED. (TC# 20060704014)