Casualties unknown

2011-07-31: Bell 407 (Helicopter), C-GNVI — VIH Helicopters Ltd. — Stewart, British Columbia 14 nm N, CA

Stewart, British Columbia 14 nm N, CA

On July 31, 2011, a Bell 407 (Helicopter), C-GNVI operated by VIH Helicopters Ltd. was involved in an aviation accident near Stewart, British Columbia 14 nm N, CA. Investigators recorded the probable cause as: While working in close proximity to steep terrain, the helicopter's main-rotor blades made contact with terrain, causing a subsequent loss of control and collision with terrain. 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 VIH Helicopters Bell 407 (C-GNVI) crashed near Stewart, British Columbia, after main-rotor blades contacted terrain. No survivors. Investigation found no system failure.

History of the Flight

The helicopter departed Stewart Airport at approximately 0943 Pacific Daylight Time with a pilot and two passengers. It flew to a geological exploration site 14 nautical miles north of Stewart, adjacent to the Nelson Glacier. Flight tracking data ceased at 1004 PDT. No further voice communications were recorded.

Accident Sequence

After performing a left-skid toe-in landing on a mountain ledge at 5100 feet above sea level, one passenger exited via hover exit to retrieve a climbing rope. The helicopter lifted off, backed away, and then landed again to pick up that passenger. At 1001, the helicopter lifted off with both passengers and maneuvered slowly across the mountain face. The last GPS position at 1004 indicated a landing 760 feet above the rope pick-up location. The wreckage was discovered six hours later strewn down the steep mountainside. There were no survivors. No fire occurred.

Data Analysis

The investigation retrieved data from handheld cameras, a portable GPS, and the onboard GPS tracking system. The engine control unit (ECU) showed a gradual power reduction followed by a sudden drop in main-rotor rpm. A torque spike to 150% was consistent with a major rotor strike. The subsequent divergence of main-rotor speed (decrease) and power turbine speed (increase) indicated a severed driveshaft. No helicopter system failure was identified.

Findings

While working in close proximity to steep terrain, the helicopter's main-rotor blades made contact with terrain, causing a subsequent loss of control and collision with terrain. The emergency locator transmitter (ELT) antenna was damaged, preventing signal reception. The GPS tracking system did not send an automatic emergency notification. Ground personnel did not initiate the overdue-aircraft response plan in a timely manner, and the Joint Rescue Coordination Centre was not notified. Occupant restraints in the rear cabin were not fastened.

Probable cause

While working in close proximity to steep terrain, the helicopter's main-rotor blades made contact with terrain, causing a subsequent loss of control and collision with terrain.