2001-06-25: Hughes 269A — Paso Robles, CA

Casualties unknown • Paso Robles, CA, US

Probable cause

the pilot's failure to maintain rotor rpm during a practice autorotational landing, which resulted in a hard landing.

— NTSB Determination

Accident narrative

The single engine helicopter impacted the ground hard during an autorotational landing following a simulated loss of engine power. The flight instructor was simulating the loss of engine power to his student and noticed the rotor rpm was low when the helicopter was approximately 400 feet above the ground. The instructor ensured the collective was lowered all the way and placed the cyclic forward, but was unable to recover the rotor rpm. He flared the helicopter, but it landed hard resulting in the main rotor blades severing the tail boom.

Frequently asked questions

What happened in the 2001-06-25 Hughes 269A accident near Paso Robles, CA?

The single engine helicopter impacted the ground hard during an autorotational landing following a simulated loss of engine power. The flight instructor was simulating the loss of engine power to his student and noticed the rotor rpm was low when the helicopter was approximately 400 feet above the ground. The…

What aircraft was involved and where did it happen?

The accident on 2001-06-25 involved a Hughes 269A, registration N8724F, at Paso Robles, CA.

What was the probable cause of the accident?

the pilot's failure to maintain rotor rpm during a practice autorotational landing, which resulted in a hard landing.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010703X01301. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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