1 fatality

1999-06-25: De Havilland DHC-3 Otter (C-FIFP) — Blue Water Aviation - Manitoba Air Charter Services — Long Haul Lake, Canada

Long Haul Lake, CanadaTakeoff (climb)

On June 25, 1999, a De Havilland DHC-3 Otter (registration C-FIFP) operated by Blue Water Aviation - Manitoba Air Charter Services was involved in an aviation accident near Long Haul Lake, Canada during takeoff. One person was killed. Investigators recorded the probable cause as: The most likely accident scenario during the second take-off is that water contamination migrated from the centre fuel tank to the engine, resulting in a loss of engine power. 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 1781204289Data APIEditorial standards

A Blue Water Aviation Services seaplane lost engine power shortly after takeoff from Long Haul Lake, Manitoba. The aircraft struck trees and ground, resulting in fatal injuries to the engineer and serious injuries to the pilot. Investigation found water contamination in fuel system.

Accident Details

On an unspecified date, a Blue Water Aviation Services seaplane departed from Long Haul Lake, Manitoba, with a pilot and an aviation maintenance engineer on board. At 1320 central daylight savings time, shortly after take-off, the aircraft's engine abruptly lost power. The pilot attempted to restart the engine but was unsuccessful. The aircraft subsequently descended into a stand of trees and struck the ground. The engineer suffered fatal injuries, and the pilot was seriously injured. The aircraft was destroyed by impact forces.

Investigation Findings

The official investigation determined the probable cause of the accident. According to the findings, the most likely scenario during the second take-off was that water contamination migrated from the centre fuel tank to the engine, resulting in a loss of engine power. The engine stopped at a point from which there was insufficient time for the engine to restart or for a safe landing to be made. Indications of water contamination were found in the fuel system after the occurrence; however, the source(s) of the water contamination could not be identified.

Examination of the aircraft and testing of the engine and components did not identify any pre-occurrence structural, mechanical, or electrical defects or malfunctions that would have contributed to this occurrence. A post-crash fire in the carburettor most likely resulted from uncontaminated fuel brought forward by the windmilling engine and the pilot's efforts to clear contamination from the fuel system.

Additional Safety Observations

The investigation noted that the pilot's use of his shoulder harness likely prevented more serious injuries during the impact sequence. In contrast, the engineer's injuries likely would have been less severe had he been using both his seat belt and shoulder harness. The pilot was certified and qualified for the flight. The aircraft's weight and centre of gravity were within approved limits. Records indicated that the aircraft had been certified and maintained in accordance with existing regulations. Furthermore, the aircraft's engine power loss during the first attempted take-off was likely due to water contamination in the fuel.