Casualties unknown

Helicopter Tail Boom Separated During Autorotation Training (N9049J)

Ozark, AL, US

On May 11, 1989, a Hughes 269A (registration N9049J) operated by Alabama Avi. & Tech. College was involved in an aviation accident near Ozark, AL. Investigators recorded the probable cause as: THE PILOT'S EXCESSIVE USE OF THE CYCLIC CONTROL AND THE MISJUDGED FLARE DURING A PRACTICE TOUCHDOWN AUTOROTATION. 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 2026-06-10Data APIEditorial standards

During a helicopter instructional flight, an attempted straight-in touchdown autorotation led to tail boom contact with the rotor, resulting in separation and a left rotation.

Incident Overview

During a helicopter instructional flight, the pilot attempted a straight-in touchdown autorotation. According to the pilot, witnesses observed the tail boom come up into the tip path plane of the main rotor.

Sequence of Events

The pilot explained that the event typically occurs when the helicopter touches down on the heel of the skids while the main rotor is still pitched aft due to cyclic input during the landing flare. As the helicopter rocks forward after a hard landing on the skid heel, the displaced main rotor severs the tail boom. Following the tail boom separation, the helicopter rotated approximately 120 degrees to the left.

The accident involved a training flight with no further details provided regarding the aircraft type, registration, operator, location, or occupant injuries.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X28241. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.