Aerospatiale AS-350B accident near Blanding, UT

On May 4, 2000, an Aerospatiale AS-350B (helicopter) was involved in an accident near Blanding, UT. 3 people died. Damage to the aircraft: destroyed.

Date
May 4, 2000
Place
Blanding, UT
Aircraft
Aerospatiale AS-350B · Helicopter
Injuries
3 fatal, 3 serious, 0 minor
Damage
Destroyed
Position
37.550°N, 109.480°W
NTSB ID
20001212X20971

Official records · DEN00FA084

NTSB summary

HISTORY OF FLIGHT On May 4, 2000, approximately 1555 mountain daylight time, an Aerospatiale AS-350B helicopter, Canadian registration CGPTT, was destroyed during impact with terrain while maneuvering near Blanding, Utah. The commercial pilot and two passengers were fatally injured, and the other three passengers were seriously injured. The helicopter was being operated by Peace Helicopters Ltd., Edmonton, Alberta, under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the local flight that originated from landing zone 1 (LZ1) 10 minutes earlier. No flight plan had been filed. The pilot arrived in Blanding, Utah, on May 1, 2000, to relieve the project pilot working for a geophysical seismic team. On May 2, 2000, he flew a familiarization flight with the previous project pilot, and was briefed on operational procedures and environmental concerns. The previous project pilot stated that "when you live with, and fly for a geophysical seismic crew for 3 or 4 weeks, they get used to you; a new guy has to prove himself." The operator stated that this was the first time that the pilot had been on assignment in the United States. On May 3, 2000, the pilot flew his first day as the project pilot. In the afternoon, the Safety Officer of the geophysical project said that the pilot told him that this was "his first time to fly in the desert, and the [desert's unpredictable] winds." He also said that the pilot seemed "very brash." On May 4, 2000, the helicopter mechanic said that the helicopter was fueled at the LZ1 staging area (landing zone 1; N37 degrees 22.77', W1

Probable cause

the pilot's loss of aircraft control due to abrupt flight maneuvering. Contributing factors were the high density altitude weather condition, the total loss of engine power due to the pilot manually introducing excessive fuel into the engine and over temping the turbine section, and the lack of suitable terrain for the ensuing autorotation.

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