Propeller overspeed and engine failure during final approach

Casualties unknown • Denver, CO, US

An aircraft experienced an instantaneous propeller overspeed and left engine failure following turbulence encountered during the final approach phase of flight.

What happened

While on final approach, the captain was operating the aircraft with his right hand resting on the power controls. The aircraft encountered turbulence of enough intensity to cause the captain's feet to come off the rudder pedals. During this event, the pilot felt a click in his hand, followed by an instantaneous propeller overspeed.

The crew eventually secured the engine by closing the fuel shutoff valve. The aircraft subsequently completed an uneventful landing without the use of flaps.

The investigation

Post-incident examination revealed that both the air and ground circuit breakers were in the open position. The left engine was found to be functionally destroyed.

Data from the digital flight data recorder provided the following technical details:

  • Maximum propeller RPM reached 150.49% for the left engine and 120.4% for the right engine.
  • Vertical acceleration values ranged from .647 to 1.26 G's.
  • Longitudinal acceleration values ranged from .037 to .096 G's.
  • The right engine torque peaked at 37%, while the left engine torque remained at 0%.
  • Right engine fuel flow was between 16% and 19% lower than the left engine fuel flow.
  • Propeller imbalance values for the left engine were approximately 50% higher than those recorded for the right engine.

Frequently asked questions

What happened in the 1992-07-21 Embraer EMB-120 RT accident near Denver, CO?

An aircraft experienced an instantaneous propeller overspeed and left engine failure following turbulence encountered during the final approach phase of flight.

What aircraft was involved and where did it happen?

The accident on 1992-07-21 involved a Embraer EMB-120 RT, registration N221YV, operated by Mesa Airlines, Inc., at Denver, CO.

What was the probable cause of the accident?

OPEN AIR GROUND CIRCUIT BREAKERS THAT ALLOWED THE PROPELLERS TO OVERSPEED. A FACTOR WAS: CLEAR AIR TURBULENCE.

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.

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