Casualties unknown

Hard Landing During Practice Autorotation Bends Tail Boom (N972AE)

Mesa, AZ, US

On November 15, 2000, an Eurocopter AS 350B-3 (registration N972AE) operated by Petroleum Helicopters, Inc. was involved in an aviation accident near Mesa, AZ. Investigators recorded the probable cause as: The dual student's misjudged landing flare and level off, which resulted in a heel first touchdown and subsequent hard landing during a practice autorotation. Also causal was the instructor pilot's inadequate supervision of the student. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

During a practice autorotation to touchdown, a student helicopter pilot made a hard landing that bent the tail boom at the fuselage attachment. The instructor reported an abrupt entry by the student and insufficient collective pitch to arrest the descent rate.

Incident Overview

A practice autorotation to touchdown resulted in a hard landing that bent the tail boom of the helicopter at the fuselage attachment juncture. The flight was a training session with an instructor and a student.

Sequence of Events

The instructor first demonstrated a practice autorotation to touchdown, then turned control of the helicopter over to the student to perform the next autorotation to landing. According to the instructor, the student's entry into the autorotation was abrupt, leading first to high rotor rpm and subsequently to low rotor rpm. However, before initiating the landing flare, the rotor rpm had returned to proper values.

During the flare, the student's initial pitch application was slightly too high but considered satisfactory. As the aircraft approached the landing point, additional collective pitch was applied, but the input was insufficient to check the sink rate. The heels of the skids made ground contact, causing the helicopter to rock forward onto the toe of the skids and then back down onto the full skids.

Findings

After the landing, the pilot heard a metallic sound. An external inspection revealed that the tail boom was bent downward at its attachment point to the fuselage.

No injuries or other damage were reported.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X22306. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.