Vancouver – Whitehorse

The DC-3 aircraft, with the captain, first officer, and an apprentice aircraft maintenance engineer on board, was to be ferried from Vancouver, British Columbia, to Whitehorse, Yukon. Just after take-off from runway 08, as the first officer was setting the engine power, the right propeller began to over-speed. The captain told the first officer to shut down and feather the right engine. The first officer did as instructed, and advised the Vancouver tower controller of the engine problem and that they would return to the airport to land on runway 08. The captain turned the aircraft to the right, onto downwind for runway 08; however, because the aircraft's altitude and airspeed were decreasing, the first officer advised the tower controller that they would land on runway 30. The aircraft continued to lose height, narrowly avoiding buildings in its path, and crashed to the ground, one mile short of runway 30. The three occupants were seriously injured during the impact and the post-crash fire; the captain died of his injuries eight days after the accident.

Flight / Schedule

Vancouver – Whitehorse

Registration

C-GZOF

MSN

20833

Year of Manufacture

1944

Date

August 19, 1995 at 09:06 AM

Type

CRASH

Flight Type

Positioning

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Vancouver British Columbia

Region

North America • Canada

Coordinates

49.2609°, -123.1140°

Crash Cause

Technical failure

Narrative Report

On August 19, 1995 at 09:06 AM, Vancouver – Whitehorse experienced a crash involving Douglas C-47 Skytrain (DC-3), operated by Air North - Canada, with the event recorded near Vancouver British Columbia.

The flight was categorized as positioning and the reported phase was takeoff (climb) at a airport (less than 10 km from airport) crash site.

3 people were known to be on board, 1 fatalities were recorded, 2 survivors were identified or estimated. This corresponds to an estimated fatality rate of 33.3%.

Crew on board: 3, crew fatalities: 1, passengers on board: 0, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is technical failure. The DC-3 aircraft, with the captain, first officer, and an apprentice aircraft maintenance engineer on board, was to be ferried from Vancouver, British Columbia, to Whitehorse, Yukon. Just after take-off from runway 08, as the first officer was setting the engine power, the right propeller began to over-speed. The captain told the first officer to shut down and feather the right engine. The first officer did as instructed, and advised the Vancouver tower controller of the engine problem and that they would return to the airport to land on runway 08. The captain turned the aircraft to the right, onto downwind for runway 08; however, because the aircraft's altitude and airspeed were decreasing, the first officer advised the tower controller that they would land on runway 30. The aircraft continued to lose height, narrowly avoiding buildings in its path, and crashed to the ground, one mile short of runway 30. The three occupants were seriously injured during the impact and the post-crash fire; the captain died of his injuries eight days after the accident.

Aircraft reference details include registration C-GZOF, MSN 20833, year of manufacture 1944.

Geospatial coordinates for this crash are approximately 49.2609°, -123.1140°.

Fatalities

Total

1

Crew

1

Passengers

0

Other

0

Crash Summary

The DC-3 aircraft, with the captain, first officer, and an apprentice aircraft maintenance engineer on board, was to be ferried from Vancouver, British Columbia, to Whitehorse, Yukon. Just after take-off from runway 08, as the first officer was setting the engine power, the right propeller began to over-speed. The captain told the first officer to shut down and feather the right engine. The first officer did as instructed, and advised the Vancouver tower controller of the engine problem and that they would return to the airport to land on runway 08. The captain turned the aircraft to the right, onto downwind for runway 08; however, because the aircraft's altitude and airspeed were decreasing, the first officer advised the tower controller that they would land on runway 30. The aircraft continued to lose height, narrowly avoiding buildings in its path, and crashed to the ground, one mile short of runway 30. The three occupants were seriously injured during the impact and the post-crash fire; the captain died of his injuries eight days after the accident.

Cause: Technical failure

Occupants & Outcome

Crew On Board

3

Passengers On Board

0

Estimated Survivors

2

Fatality Rate

33.3%

Known people on board: 3

Operational Details

Schedule / Flight

Vancouver – Whitehorse

Flight Type

Positioning

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Region / Country

North America • Canada

Aircraft Details

Registration

C-GZOF

MSN

20833

Year of Manufacture

1944