Incident Overview

Date: Tuesday 20 January 1998
Aircraft Type: British Aerospace 3112 Jetstream 31
Owner/operator: Alberta Citylink
Registration Number: C-FBIE
Location: Lloydminster Airport, AB (YLL) – ÿ Canada
Phase of Flight: Landing
Status: Destroyed, written off
Casualties: Fatalities: 0 / Occupants: 15
Component Affected: Left Main Landing GearLeft Main Landing Gear
Investigating Agency: TSBTSB
Category: Accident
A scheduled flight from Calgary to Lloydminster experienced a significant landing incident due to a destabilized approach. The flight service station specialist reported a decrease in visibility, ice buildup, and wind conditions, prompting the crew to adjust the approach. The captain initiated a controlled landing, utilizing flaps and a descent to regain center line position. However, the aircraft’s descent rate was high, leading to a heavy landing. The left main landing gear collapsed, causing significant damage to the aircraft. The aircraft slid along the runway, impacting the surface with the left wing and resulting in a turn. Immediate evacuation followed, with occupants escaping through the right exit. The aircraft was subsequently sold to Dodson International Inc. for spares.A scheduled flight from Calgary to Lloydminster experienced a significant landing incident due to a destabilized approach. The flight service station specialist reported a decrease in visibility, ice buildup, and wind conditions, prompting the crew to adjust the approach. The captain initiated a controlled landing, utilizing flaps and a descent to regain center line position. However, the aircraft’s descent rate was high, leading to a heavy landing. The left main landing gear collapsed, causing significant damage to the aircraft. The aircraft slid along the runway, impacting the surface with the left wing and resulting in a turn. Immediate evacuation followed, with occupants escaping through the right exit. The aircraft was subsequently sold to Dodson International Inc. for spares.

Description

At 17:00 Alberta Citylink flight 933 took off from Calgary on a scheduled flight to Lloydminster. The crew planned a non-precision automatic direction finder (ADF) approach to runway 25 at Lloydminster with an overcast ceiling of 400 feet, visibility of 5 statute miles in blowing snow and mist, and the wind from 110 degrees true at 7 knots. When the aircraft was inbound, the flight service station (FSS) specialist reported that the visibility had decreased to 3 sm. The crew were aware of approximately to ¬ inch build-up of ice on the aircraft during descent and so planned for a flap 20 landing. The first officer was flying the approach from the right-hand seat while the captain was monitoring the instruments and looking outside the aircraft for visual contact with the runway environment. When the captain saw the runway from the minimum descent altitude (MDA), he took control for the landing. The aircraft was north of the extended centre line of runway 25. Flaps 35 was selected, the power was reduced to flight idle, a turn to regain the centre line was carried out, and a descent was commenced from MDA. The aircraft contacted the runway surface heavily, moving left to right. As a result, the left main landing gear collapsed. Both propellers struck the runway, and the left propeller separated from the engine. The aircraft slid along the runway on the belly pod for a distance of about 1 800 feet. The left wing contacted the snow on the edge of the runway, resulting in a turn of about 160 degrees. The evacuation took place immediately after the aircraft came to rest; all occupants escaped quickly through the right, over-wing exit. The aircraft was sold to Dodson International Inc. to be used for spares. CAUSES: “An unstabilized approach resulted in a heavy landing because the captain changed the configuration of the aircraft, and the high rate of descent that resulted was not arrested before contact was made with the runway surface. Contributing to the high rate of descent were the reduction of engine power to flight idle, airframe ice, and the time available for the final descent. Contributing to the damage on landing was the left to right movement of the aircraft.”

Primary Cause

Unstabilized approach, high descent rate, reduced engine power, airframe ice, and insufficient time to arrest descent.Unstabilized approach, high descent rate, reduced engine power, airframe ice, and insufficient time to arrest descent.

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