Engine failure leads to fatal aircraft crash near Grand Canyon

Casualties unknown • Sedona, AZ, US

An aerial sightseeing flight to Grand Canyon National Park ended in a fatal crash after an internal engine component failure caused a total loss of power.

What happened

A pilot and 4 fare-paying passengers were enroute to the Grand Canyon National Park for aerial sightseeing when the aircraft experienced a total loss of engine power. The engine failure was caused by an internal failure of the left magneto. Following the loss of power, the aircraft collided with terrain. The impact resulted in the destruction of the aircraft by ground fire.

The investigation

Investigators examined the left magneto and determined it was not in compliance with AD 78-09-07 R3, which addressed impulse coupling failure. The investigation revealed that the air taxi company employed only two people: an owner/president/pilot and a director of maintenance/mechanic. The mechanic acknowledged failing to follow the correct guidelines specified in the applicable Airworthiness Directive.

Technical analysis showed that the impulse coupling jammed when the clearance between the flyweight and the stop pin reached zero. This mechanical failure caused the teeth on the engine's crankshaft gear and the dowel pin to shear off.

Probable cause

The total loss of engine power was caused by an internal failure of the left magneto, resulting from a failure to comply with Airworthiness Directive 78-09-07 R3 regarding impulse coupling maintenance.

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Frequently asked questions

What happened in the 1988-10-16 Piper PA-32-300 accident near Sedona, AZ?

An aerial sightseeing flight to Grand Canyon National Park ended in a fatal crash after an internal engine component failure caused a total loss of power.

What aircraft was involved and where did it happen?

The accident on 1988-10-16 involved a Piper PA-32-300, registration N4113R, operated by Northern Arizona Aircraft, at Sedona, AZ.

What was the probable cause of the accident?

The total loss of engine power was caused by an internal failure of the left magneto, resulting from a failure to comply with Airworthiness Directive 78-09-07 R3 regarding impulse coupling maintenance.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X27078. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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