Control Cable Corrosion Leads to Fatal Twin Otter Crash in British Columbia

Casualties unknown • de Havilland DHC-6-100 Twin Otter C-FDMR, CA

A de Havilland DHC-6-100 crashed into the water near Fish Egg Inlet after a control cable failure, resulting in three fatalities.

What happened

A charter flight departing from a logging camp at Fish Egg Inlet, British Columbia, ended in tragedy when a de Havilland DHC-6-100 lost control shortly after takeoff. The aircraft, operated by Pacific Coastal Airlines, was performing a 16-nautical-mile VFR flight to Pruth Bay with a crew of two and two passengers.

During the initial climb, as the aircraft reached approximately 100 feet above the surface and the flaps were being retracted, the aircraft experienced a violent nose-up pitch and entered a stall. The aircraft struck the water near the shoreline and sank immediately. While the captain sustained serious injuries and managed to swim to shore, the first officer and both passengers drowned within the submerged wreckage.

The investigation

The investigation focused on the mechanical failure of the elevator control system. Investigators determined that the down elevator control cable at station 376 had failed. Microscopic analysis of the broken cable revealed that several strands had significantly thinned due to long-term degradation.

Maintenance records were examined, noting that the aircraft had undergone a recent inspection. However, the engineer performing the inspection did not remove the baggage compartment floor panel, which is necessary to view the forward side of the pulley cluster at station 376. While the controls were cycled, the specific area of the cable prone to failure remained difficult to inspect. Additionally, investigators noted that the pilot had selected a 30-degree flap setting for takeoff, whereas the aircraft flight manual specifies 20 degrees for float-equipped operations.

Findings

  • The primary cause of the accident was the failure of the down elevator control cable due to corrosion.
  • The corrosion on the cable was not identified during the most recent maintenance inspection.
  • The aircraft was destroyed by the impact and subsequently submerged in salt water.
  • The crew and passengers were not wearing shoulder harnesses or available flotation devices at the time of the crash.

Probable cause

The down elevator control cable failed because of gradual deterioration caused by corrosion, which went undetected during the previous maintenance inspection, leading to a loss of aircraft control.

Frequently asked questions

What happened in the 1994-09-17 Pacific Coastal Airlines accident near de Havilland DHC-6-100 Twin Otter C-FDMR, CA?

A de Havilland DHC-6-100 crashed into the water near Fish Egg Inlet after a control cable failure, resulting in three fatalities.

What aircraft was involved and where did it happen?

The accident on 1994-09-17 involved a Pacific Coastal Airlines, operated by Flight control failure, at de Havilland DHC-6-100 Twin Otter C-FDMR, CA.

What was the probable cause of the accident?

The down elevator control cable failed because of gradual deterioration caused by corrosion, which went undetected during the previous maintenance inspection, leading to a loss of aircraft control.

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