Pilot Debrief

RUSSELL W DYER VORTEX near Lakeport, CA — 2021-12-02

Final reportWPR22FA053
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Date
2021-12-02
Location
Lakeport, CA, USA
Airport
1O2
Aircraft
RUSSELL W DYER VORTEX
Registration
N425RD
Category
Helicopter
Highest injury
Fatal
Fatalities
1

Probable cause

The pilot’s loss of control for reasons that could not be determined and the delayed remedial action to recover from the power pushover event.

NTSB narrative

A witness reported seeing the gyroplane flying straight and level about two miles from the departure airport. The witness reported the gyroplane then tumbled tail over nose three times before he lost sight of it below the tree line. The gyroplane sustained substantial damage when it impacted the heavily vegetated terrain. The smell of fuel was present at the accident site and there was no evidence of a wire or bird strike. Additionally, there were no reports of downed power lines or power outages in the accident area. Examination of the gyroplane revealed no evidence of any preaccident mechanical malfunctions or failures that would have precluded normal operation. The gyroplane was equipped with a horizontal stabilizer that remained intact. The engine was likely producing power at the time of the accident, because two of its propeller blades contacted the main rotor blades during the accident sequence. The main rotor blades sustained minimal damage, consistent with the gyroplane entering a low-rotor-rpm state for undetermined reasons before ground impact. According to the Federal Aviation Administration (FAA), FAA-H-8083-21, Chapter 21, Gyroplane Emergencies, if rotor force is rapidly removed, some gyroplanes may pitch forward abruptly into a power pushover event and if not corrected can continue to tumble and become irreversible.

Analysis

Primary failure mode
Loss of control
First missed decision gate
Pilot could have maintained adequate airspeed during low altitude maneuver.

NTSB coding

Evidence available

  • 10 docket documents
View NTSB final reportView NTSB docket

Docket documents10

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