No fatalities

1 Jun 2010: HUGHES 269A — Cannon Falls, MN

Cannon Falls, MN, United States

On 1 Jun 2010, a HUGHES 269A was involved in an aviation accident near Cannon Falls, MN. No fatalities were reported. Investigators recorded the probable cause as: The pilot's failure to maintain rotor speed during the autorotation, which resulted in an excessive sink rate and a hard landing. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A pilot experienced a vibration shortly after takeoff, initiated an autorotation, but rotor speed decayed, resulting in a hard landing with tail boom separation and right landing skid collapse.

Incident Summary

A helicopter pilot reported experiencing a disturbing vibration shortly after liftoff. In response, the pilot initiated an autorotation to an open agricultural field. During the descent, the pilot executed a 180-degree turn to avoid a line of trees.

Pilot Actions and Outcome

The pilot noted that the rotor speed became too low, and he was unable to reduce the sink rate. This led to a hard landing. The pilot stated that additional practice in autorotation descents and landings might have prevented the accident.

Aircraft Damage

During the accident sequence, the main rotor contacted and separated the tail boom. Additionally, the right landing skid collapsed.

Contributing factors

Prop/rotor parameters — Not attained/maintainedDescent rate — Not attained/maintainedPilot