Casualties unknown

Helicopter Accident During Elk Survey in New Mexico (N124DA)

Reserve, NM, US

On December 18, 1997, a Bell 206B-III (registration N124DA) operated by Aero West was involved in an aviation accident near Reserve, NM. Investigators recorded the probable cause as: The pilot's inadvertent loss of tail rotor effectiveness. A factor was the high density altitude weather condition. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 2 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

A helicopter contracted for elk evaluation experienced a loss of control during a low-speed turn, resulting in a ground impact. Pilot and passenger gave differing accounts of altitude and speed.

Accident Description

A helicopter under contract by the New Mexico Game and Fish Department was conducting an elk herd evaluation flight when it experienced a loss of control and impacted the ground. The flight was intended to split a herd of elk for counting purposes. The helicopter was traveling at low speed when the pilot initiated a right turn, after which the aircraft rotated to the ground within seconds.

Pilot and Passenger Accounts

The right front seat passenger reported that the helicopter was flying northbound at an altitude of approximately 180 to 200 feet above ground level (AGL) and at a speed of less than 10 knots. He stated that the pilot initiated a turn, and within 3 to 5 seconds, the helicopter rotated to the ground.

The pilot provided a different account, stating that he believed they were traveling north at about 100 feet AGL and approximately 30 knots when he initiated the right turn. He noted that once the turn started, he could not stop it despite applying full left pedal. The pilot reported hearing nothing unusual nor feeling anything abnormal before the accident.

Meteorological Conditions

The pilot estimated the wind was from the west at 5 to 10 knots. The density altitude was calculated to be 9,043 feet, indicating high-altitude conditions.

Reference Materials

According to Federal Aviation Administration Advisory Circular (AC) 90-95, unanticipated right yaw can occur in helicopters at low airspeeds, high power regimes, and during left crosswinds, tailwinds, or right turning maneuvers. The advisory circular provides general guidance on this aerodynamic phenomenon.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X09320. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.