No fatalities

2004-07-04: De Havilland DHC-6 Twin Otter (C-FMOL) — North-Wright Airways — Mile 222 (Canol Road), Canada

Mile 222 (Canol Road), CanadaTakeoff (climb)

On July 4, 2004, a De Havilland DHC-6 Twin Otter (registration C-FMOL) operated by North-Wright Airways was involved in an aviation accident near Mile 222 (Canol Road), Canada during takeoff. No fatalities were reported. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781200278Data APIEditorial standards
Aircraft registered C-FMOL
Aircraft registered C-FMOL. Photo: Aeroprints.com / CC BY-SA 3.0, via Wikimedia Commons

A DHC-6 Twin Otter (C-FMOL) encountered a strong crosswind after takeoff from a 1,500 ft gravel strip at Mile 222 of the Canol Road, leading to a veer-off and collision with willows and a shallow creek. The aircraft sustained substantial damage; crew uninjured.

Accident Details

On an unspecified date, a North-Wright Airways Ltd. de Havilland DHC-6 Twin Otter, registration C-FMOL, was departing from a gravel strip approximately 1,500 feet long at Mile 222 of the Canol Road, near the Tsichu River, Canada. The takeoff was initiated to the north and into wind.

Immediately after becoming airborne, the aircraft encountered a strong right cross-wind and settled back onto the strip. The left wheel contacted willows that had overgrown the edge of the strip. The aircraft veered left into the willows at about 60 knots and began to decelerate. Prior to flying speed being regained, the aircraft rolled off the end of the strip and came to rest in a shallow creek.

Damage and Injuries

The right wing partially separated from the fuselage at impact. The forward fuselage, nose gear, and right main gear sustained substantial damage. The pilot and first officer were uninjured.

Flight Purpose and Loading

The purpose of the trip was to move hunting gear and outfitter supplies back to an airstrip at Mile 170 of the Canol Road (Godlin Lake). The aircraft was at or near gross weight at the time of the occurrence.