Casualties unknown

2000-05-20: Bell 206L LongRanger (Helicopter) C-GJOL — Helicopter Transport Services (Canada) Inc. — Resolute, Nunavut 35 nm SW, CA

Resolute, Nunavut 35 nm SW, CA

On May 20, 2000, a Bell 206L LongRanger (Helicopter) C-GJOL operated by Helicopter Transport Services (Canada) Inc. was involved in an aviation accident near Resolute, Nunavut 35 nm SW, CA. Investigators recorded the probable cause as: The pilot lost control of the helicopter because whiteout conditions eliminated all visual references to the horizon and surface, and the pilot lacked the instrument rating required to navigate the terrain without visual cues. This summary draws on records from the Transportation Safety Board of Canada (TSB); 2 related events involving the same aircraft type or operator are linked below.

Sourcesthe Transportation Safety Board of Canada (TSB)Primary reportUpdated 1785068748Data APIEditorial standards

A Bell 206L LongRanger helicopter crashed on sea ice near Lowther Island, Nunavut, after the pilot encountered whiteout conditions, resulting in two deaths.

What happened

A charter flight transporting scientific researchers was traveling from the sea ice near Lowther Island, Nunavut, toward Resolute. The crew, consisting of the pilot and two passengers, was conducting research on polar bear behavior. During the flight, which was being conducted under day visual flight rules, the pilot attempted to turn the Bell 206L LongRanged toward the destination at approximately 400 feet altitude.

During this maneuver, the pilot encountered whiteout conditions, which obscured all visual references to the terrain. In an attempt to regain visual contact with Lowther Island, the pilot initiated a left turn. During this turn, the pilot lost control of the aircraft, leading to a descent and collision with the ice surface. The impact caused the helicopter to disintegrate. Although the occupants were restrained, the force of the crash ejected them from the fuselage. The two passengers sustained two fatal injuries, while the pilot survived with serious injuries.

The investigation

Investigators examined the wreckage and found that the helicopter's drive and rotor systems were functioning normally at the time of impact, with no evidence of mechanical failure or airframe malfunction. The aircraft's weight and center of gravity were within approved limits, and maintenance records indicated the helicopter was properly certified.

The investigation also looked into the survival equipment and emergency systems. The emergency locator transmitter (ELT) activated automatically, but its effectiveness was limited because the antenna cable separated from the unit during the crash. Furthermore, the aircraft's survival kit was found to be extremely difficult to access due to multiple layers of heavy plastic and complex metal fasteners, which would have posed a significant challenge to an injured survivor in freezing temperatures.

Findings

  • Whiteout conditions caused the pilot to lose visual reference to the surface, leading to a loss of aircraft control.
  • The disintegration of the fuselage caused the seat belts and shoulder harnesses to fail.
  • The design of the survival kit made it nearly impossible for an injured person to open the equipment in cold weather.
  • The separation of the ELT antenna cable during the impact hindered the transmission of the emergency signal.

Probable cause

The pilot lost control of the helicopter because whiteout conditions eliminated all visual references to the horizon and surface, and the pilot lacked the instrument rating required to navigate the terrain without visual cues.