3 fatalities

Stall Sequence During Flight Demonstration Leads to Crash (N1HV)

Rayville, United States of AmericaFlight

On November 1, 2002, a Rockwell Aero Commander 500 (registration N1HV) operated by Robin Williams was involved in an aviation accident near Rayville, United States of America in flight. 3 people were killed. Investigators recorded the probable cause as: The pilot-in-command's failure to maintain adequate airspeed resulting in an inadvertent stall/spin. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

During a demonstration flight, a twin-engine airplane performed stall maneuvers at 1,000 feet. After a second stall, the right wing dropped and the airplane spun, crashing. Radar indicated airspeed below stall speeds. No mechanical issues found.

Incident Summary

A twin-engine airplane was conducting power-off stall maneuvers at an altitude of approximately 1,000 feet above ground level during a flight intended to demonstrate the aircraft to a prospective buyer. A witness observed the first stall maneuver and recovery, describing it as "good." During the second stall, the nose rose higher than the first, followed by the right wing dropping and a steep nose-down attitude. The airplane rotated approximately one and a half revolutions before disappearing behind trees. Prior to ground impact, the witness reported hearing the engines rev up.

Radar and Performance Analysis

A radar and aircraft performance study revealed that the accident airplane had departed the airport and subsequently executed a series of heading, speed, and altitude changes, ultimately crashing 14.6 nautical miles east of the departure airport. During several time periods, calculations of calibrated airspeed indicated a trend toward and below the published stall speeds of 63 knots with flaps extended and 71 knots with flaps retracted.

Examination Findings

An examination of the airplane and engines found no structural or mechanical anomalies.

Probable Cause

The probable cause, as determined by the official investigation, was the pilot-in-command's failure to maintain adequate airspeed resulting in an inadvertent stall/spin.