Casualties unknown

1991-03-16: Hughes 269A (N62269) — Potter, Richard J., Jr. — Addison, TX

Addison, TX, US

On March 16, 1991, a Hughes 269A (registration N62269) operated by Potter, Richard J., Jr. was involved in an aviation accident near Addison, TX. Investigators recorded the probable cause as: THE PILOT'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL DURING LANDING. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A pilot reported a strong gust of wind during a hover landing caused the helicopter to spin right. Despite applying full left pedal, the spin continued. After clearing obstacles with collective, the pilot reduced collective, stopping the spin but the aircraft descended, struck a tree and the ground, and rolled over.

Incident Overview

A helicopter pilot described an encounter with a strong gust of wind while attempting to land from a hover. According to the pilot, the gust caused the aircraft to begin spinning to the right. Despite applying full left pedal input, the pilot was unable to arrest the rotation. The spinning motion directed the helicopter toward a hangar and a fence. To avoid these obstacles, the pilot applied collective control, which allowed the aircraft to clear them.

Sequence of Events

After clearing the obstacles, the pilot managed to stop the spin by reducing collective. However, as the helicopter began to descend, it struck a tree and then the ground. The impact caused the aircraft to roll over. The pilot's account did not specify the helicopter type, registration, location, date, or any injuries.

Pilot Statement

The pilot stated that the loss of control occurred during a hover, just before setting the aircraft down. The strong gust was unexpected and led to a rapid, uncommanded right spin. Full left pedal was insufficient to stop the rotation. The decision to increase collective was made to ensure the aircraft cleared the hangar and fence. Once the spin was stopped by reducing collective, the subsequent descent resulted in collision with a tree and terrain.

Notes

No further details, such as meteorological conditions or helicopter specifications, were provided in the source. The investigation may determine contributing factors, but none were stated in the pilot's report.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X16604. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.