Casualties unknown

Propeller Overspeed and Engine Failure During Final Approach (N221YV)

Denver, CO, US

On July 21, 1992, an Embraer EMB-120 RT (registration N221YV) operated by Mesa Airlines, Inc. was involved in an aviation accident near Denver, CO. Investigators recorded the probable cause as: OPEN AIR GROUND CIRCUIT BREAKERS THAT ALLOWED THE PROPELLERS TO OVERSPEED. A FACTOR WAS: CLEAR AIR TURBULENCE. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

A captain encountered turbulence on final approach, causing a propeller overspeed. The engine was shut down via fuel shutoff, and an uneventful no-flap landing followed. Investigation revealed open circuit breakers and a destroyed left engine.

Incident Summary

During a flight, the captain was piloting the aircraft with his right hand resting on the power controls. While turning onto final approach, the airplane encountered turbulence of sufficient intensity that the captain's feet came off the rudder pedals. He felt a 'click' in his hand and immediately noted a propeller overspeed. The crew secured the engine by closing the fuel shutoff valve, and subsequently performed an uneventful no-flap landing.

Post-Incident Examination

Post-incident examination disclosed that both air-ground circuit breakers were open. The left engine was found to be functionally destroyed. A readout of the digital flight data recorder provided detailed performance data.

Flight Data Recorder Analysis

The digital flight data recorder data indicated that the maximum left propeller rpm reached 150.49%, while the right propeller reached 120.4%. Vertical acceleration values ranged from 0.647 G to 1.26 G, and longitudinal acceleration values ranged from 0.037 G to 0.096 G. The right engine torque peaked at 37%, whereas the left engine torque remained at 0%. Right engine fuel flow was 16% to 19% lower than left engine fuel flow. Additionally, propeller imbalance values for the left engine were approximately 50% higher than those recorded for the right engine.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X15130. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.