Incident Overview

Date: Thursday 28 July 2005
Aircraft Type: Beechcraft 200 Super King Air
Owner/operator: Northern Thunderbird Air
Registration Number: C-FCGL
Location: near Shovelnose Creek, BC – ÿ Canada
Phase of Flight: En route
Status: Destroyed, written off
Casualties: Fatalities: 2 / Occupants: 2
Component Affected: Aircraft Engine and Control SystemsAircraft Engine and Control Systems
Investigating Agency: TSBTSB
Category: Accident
A Beechcraft 200 Super King Air, registration C-FCGL, experienced a catastrophic crash during a visual flight rules flight to Smithers Airport, BC, on July 30, 2005. The aircraft, carrying two crew members, crashed in a narrow canyon at an elevation of 3900 feet, resulting in fatal injuries. The crash site was located in a steeply rising terrain area. The aircraft’s flight path was determined to be a deliberate maneuver into a narrow canyon, despite limitations in climb rate and terrain clearance.A Beechcraft 200 Super King Air, registration C-FCGL, experienced a catastrophic crash during a visual flight rules flight to Smithers Airport, BC, on July 30, 2005. The aircraft, carrying two crew members, crashed in a narrow canyon at an elevation of 3900 feet, resulting in fatal injuries. The crash site was located in a steeply rising terrain area. The aircraft’s flight path was determined to be a deliberate maneuver into a narrow canyon, despite limitations in climb rate and terrain clearance.

Description

A Beechcraft 200 Super King Air, registration C-FCGL, operating as Northern Thunderbird Air flight 202, departed Vancouver International Airport, BC (YVR), at 08:24 for a visual flight rules flight to Smithers Airport, BC (YYD), with a crew of two on board. The aircraft did not arrive at its destination, and a search was commenced later that same day. The aircraft was found on 30 July 2005. The crash site was in a narrow canyon at an elevation of about 3900 feet above sea level, in an area of steeply rising terrain. Both occupants were fatally injured. A post-crash fire destroyed most of the aircraft. The emergency locator transmitter was destroyed in the fire and no signal was detected. FINDINGS AS TO CAUSES AND CONTRIBUTING FACTORS: 1. The aircraft was flown up a narrow canyon into rapidly rising terrain for reasons that could not be determined. The aircraft’s proximity to terrain and the narrowness of the canyon precluded a turn, and the aircraft’s climb rate was insufficient to clear the rising terrain. 2. The pilot decision-making training received by the crew members was ineffective because they were unprepared for the unique hazards and special operating techniques associated with flying low in mountainous terrain.

Primary Cause

Pilot decision-making training inadequacies, specifically related to navigating challenging mountainous terrain and low-altitude flying.Pilot decision-making training inadequacies, specifically related to navigating challenging mountainous terrain and low-altitude flying.

Share on:

Leave a Reply

Your email address will not be published. Required fields are marked *