Engine failure and stall lead to accident during visual approach

Casualties unknown • Corona, CA, US

An engine failure during a visual approach for landing resulted in an aircraft stall and ground impact after the pilot failed to maintain sufficient airspeed.

What happened

While performing a visual approach for landing, the aircraft experienced an engine failure. In response to the loss of power, the pilot initiated an emergency landing. During the subsequent emergency descent, the pilot did not maintain an airspeed above the aircraft's stall speed. As a result, the aircraft entered a stall and impacted the ground in rough terrain. The pilot was not injured.

The investigation

Post-accident examination of the power plant revealed that the flyweights of the left magneto impulse coupling had struck the stop pins. This impact between the flyweight and the stop pin caused the magneto to seize and sheared the accessory drive gear alignment dowel. This mechanical failure led to the uncoupling of the accessory drive train, which ultimately caused the engine to fail.

Probable cause

The engine failure was caused by the left magneto impulse coupling flyweights striking the stop pins, which seized the magneto and sheared the accessory drive gear alignment dowel; the subsequent stall and ground impact occurred because the pilot failed to maintain airspeed above the stall speed during the emergency descent.

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Frequently asked questions

What happened in the 1991-07-17 Piper PA32-300 accident near Corona, CA?

An engine failure during a visual approach for landing resulted in an aircraft stall and ground impact after the pilot failed to maintain sufficient airspeed.

What aircraft was involved and where did it happen?

The accident on 1991-07-17 involved a Piper PA32-300, registration N5233S, operated by Darryl Rhodes & James Hanenber, at Corona, CA.

What was the probable cause of the accident?

The engine failure was caused by the left magneto impulse coupling flyweights striking the stop pins, which seized the magneto and sheared the accessory drive gear alignment dowel; the subsequent stall and ground impact occurred because the pilot failed to maintain airspeed above the stall speed during the emergency…

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X17604. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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