2 fatalities

2010-07-24: De Havilland DHC-2 Beaver (C-FGYK) — Nordair Québec 2000 — La Grande-Rivière, Canada

La Grande-Rivière, CanadaTakeoff (climb)

On July 24, 2010, a De Havilland DHC-2 Beaver (registration C-FGYK) operated by Nordair Québec 2000 was involved in an aviation accident near La Grande-Rivière, Canada during takeoff. 2 people were killed. Investigators recorded the probable cause as: The aircraft was overloaded and its centre of gravity was beyond the aft limit, leading to a stall at low altitude. Baggage was not secured, causing the triple seat to pivot forward and separate from the floor during impact. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781195988Data APIEditorial standards

A de Havilland DHC-2 Mk. 1 amphibious floatplane (C-FGYK) operated by Nordair Québec 2000 Inc. crashed shortly after takeoff from La Grande-Rivière Airport, killing the pilot and front-seat passenger and seriously injuring three rear-seat passengers.

Accident Overview

On the day of the accident at approximately 1053 Eastern Daylight Time, a de Havilland DHC-2 Mk. 1 amphibious floatplane (registration C-FGYK, serial number 123) operated by Nordair Québec 2000 Inc. took off from runway 31 at La Grande-Rivière Airport, Quebec. The flight was conducted under visual flight rules to l’Eau Claire Lake, Quebec, about 190 nautical miles to the north.

Sequence of Events

The take-off run was longer than usual. The aircraft became airborne but was unable to gain altitude. At the runway end, at approximately 50 feet above ground level, the aircraft pitched up and banked left. It then nosed down and crashed in a small shallow lake.

Aircraft and Operations

The aircraft was a de Havilland DHC-2 Mk. 1 amphibious floatplane. The operator was Nordair Québec 2000 Inc. The aircraft broke up on impact, and the forward part of the cockpit was partly submerged. The emergency locator transmitter activated on impact.

Injuries and Damage

The pilot and 1 front-seat passenger were fatally injured. The 3 rear-seat passengers sustained serious injuries. The aircraft broke up on impact.

Probable Cause Findings

The official investigation identified the following causes and contributing factors: 1) The aircraft was overloaded and its centre of gravity was beyond the aft limit. The aircraft pitched up and stalled at an altitude that did not allow the pilot to execute the stall recovery manoeuvre. 2) The baggage was not secured. Shifting of the baggage caused the triple seat to pivot forward, propelling the 3 rear-seat passengers against the pilot and front-seat passenger during impact. 3) Although the design of the triple seat met aviation standards, it separated from the floor at the time of impact, principally due to the fact that the heavy cargo shifted. 4) The action taken by TC did not have the desired outcomes to ensure regulatory compliance; consequently, unsafe practices persisted. A finding as to risk stated that operating an aircraft outside the limits and conditions under which a permit is issued can increase the risk of an accident.