Casualties unknown

1994-07-12: Bell 206L-3 (N3178B) — Usda Forest Service — Mimbres, NM

Mimbres, NM, US

On July 12, 1994, a Bell 206L-3 (registration N3178B) operated by Usda Forest Service was involved in an aviation accident near Mimbres, NM. Investigators recorded the probable cause as: THE PILOT'S IMPROPER DECISION TO ATTEMPT TO HOVER OUT OF GROUND EFFECT UNDER ADVERSE CONDITIONS WHILE EXCEEDING THE MAXIMUM ALLOWABLE WEIGHT FOR THAT MANEUVER. FACTORS IN THE ACCIDENT WERE: HIGH DENSITY ALTITUDE AND THE TAILWIND. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 7 related events involving the same aircraft type or operator are linked below.

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

A USDA helicopter operating to transport firefighters experienced a loss of control and collided with trees after attempting to hover above a landing area on a 9,520-ft MSL ridge line.

Introduction

On an unspecified date, a helicopter operated by the United States Department of Agriculture (USDA) was transporting firefighters to a wildfire. The aircraft was conducting an approach to a pinnacle located on a ridge line at 9,520 feet above mean sea level (MSL). Two survivors provided statements regarding the sequence of events.

Approach and Accident Sequence

According to the survivors, the pilot executed a downwind approach to the intended landing area. During the final phase, the pilot attempted to bring the helicopter into a hover approximately 20 feet above the ground. Witnesses observed that the nose of the helicopter appeared higher than normal during this phase. Subsequently, the helicopter assumed a very high nose attitude and seemed to begin sliding backwards. This was followed by a loss of control, and the helicopter made contact with trees.

Conditions

At the time of the accident, the density altitude was calculated to be 13,200 feet. The aircraft weight was determined to be 3,750 pounds. Under the prevailing conditions—no wind, pressure altitude of 9,520 feet, and temperature of 32 degrees Celsius—the maximum gross weight for a hover in ground effect was computed to be 3,580 pounds, and for a hover out of ground effect, 3,515 pounds. The impact of these conditions on the accident sequence is not explicitly stated in the available information.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001206X01735. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.