1 fatality

2006-03-08: Piper PA-31-350 Navajo Chieftain (C-GNAY) — Orca Airways — Powell River, Canada

Powell River, CanadaLanding (descent or approach)

On March 8, 2006, a Piper PA-31-350 Navajo Chieftain (registration C-GNAY) operated by Orca Airways was involved in an aviation accident near Powell River, Canada during landing or approach. One person was killed. Investigators recorded the probable cause as: Findings as to Causes and Contributing Factors: 1. The downwind condition on approach contributed to the aircraft landing long and with a high ground speed. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781199027Data APIEditorial standards

A cargo repositioning flight from Vancouver to Powell River overran Runway 09 after a second approach, resulting in serious injuries to the pilot and fatal injuries to the first officer. The aircraft was destroyed.

Accident Summary

On the day of the accident, the aircraft departed from its home base at Vancouver, British Columbia, with two crew members on board. The flight was a repositioning to Powell River, approximately 30 minutes away, to begin a freight collection route. Upon arrival, the crew joined the circuit straight-in to a right downwind for a visual approach to Runway 09.

Sequence of Events

A weather system was passing through the area, causing actual local winds to shift from light southwesterly to gusty conditions ranging from 11 to 37 knots from the northwest. During the first approach, the aircraft was lower and faster than normal and was not aligned with the runway. The crew executed an overshoot and set up for a second approach to the same runway.

On the second approach, at approximately 1639 Pacific standard time, the aircraft touched down at least halfway down the wet runway and began to hydroplane. After touchdown, engine power was added in an unsuccessful attempt to abort the landing and carry out an overshoot. The aircraft overran the end of the runway and crashed into an unprepared area within the airport property.

The pilot-in-command suffered serious injuries, and the first officer was fatally injured. A local resident called 911 and reported the accident shortly after it occurred. The pilot-in-command was attended by paramedics and eventually removed from the wreckage with the assistance of local firefighters. The aircraft was destroyed, but there was no fire. The emergency locator transmitter (ELT) was automatically activated, but the signal was weak and was not detected by the search and rescue satellite.

Probable Cause

Findings as to Causes and Contributing Factors: 1. The downwind condition on approach contributed to the aircraft landing long and with a high ground speed. This, in combination with hydroplaning, prevented the crew from stopping the aircraft in the runway length remaining. 2. When the decision to abort the landing was made, there was insufficient distance remaining for the aircraft to accelerate to a sufficient airspeed to lift off. 3. The overrun area for Runway 09 complied with regulatory standards, but the obstacles and terrain contour beyond the overrun area contributed to the fatality, the severity of injuries, and damage to the aircraft.

Other Findings

Finding as to Risk:

  • Alert Service Bulletin A25-1124A (dated 01 June 2000), which recommended replacing the inertia reel aluminum shaft with a steel shaft, was not completed, thus resulting in the risk of failure increasing over time.

Other Findings: 1. The weather station at the Powell River Airport does not have any air–ground communication capability with which to pass the flight crew timely wind updates. 2. The decision to make a second approach was consistent with normal industry practice, in that the crew could continue with the intent to land while maintaining the option to break off the approach if they assessed that the conditions were becoming unsafe.