No fatalities

2008-11-27: BAe Jetstream 31 (C-FNAY) — Northwestern Air Lease — Fort Smith, Canada

Fort Smith, CanadaLanding (descent or approach)

On November 27, 2008, a BAe Jetstream 31 (registration C-FNAY) operated by Northwestern Air Lease was involved in an aviation accident near Fort Smith, Canada during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Findings as to Causes and Contributing Factors: 1. Though icing conditions were encountered, the airframe de-icing boots were not cycled nor was the Vref speed increased to offset the effects of aircraft icing. 2. 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 1781197046Data APIEditorial standards

A Northwestern Air BAe Jetstream 31 (PLR734) encountered icing conditions, stalled, and landed hard, collapsing the left main gear. No injuries were reported among the five occupants.

Accident Overview

On an instrument flight rules (IFR) flight from Hay River to Fort Smith, Northwest Territories, a Northwestern Air British Aerospace Jetstream 31 (flight number PLR734) experienced a hard landing on Runway 29 at Fort Smith. The aircraft sustained damage but remained on the runway; all five occupants evacuated without injury.

Flight History

The flight conducted an IFR approach to Runway 11 but executed a missed approach. The crew then flew a full procedure approach for Runway 29. At approximately 0.2 nautical miles from the threshold, the crew sighted the approach strobe lights and continued for a landing.

Event Sequence

Prior to touchdown, the aircraft entered an aerodynamic stall. It landed hard on the runway at 1515 mountain standard time. The left main landing gear collapsed upon impact. There was no post-impact fire.

Injuries and Damage

The two flight crew members and three passengers were uninjured. They evacuated the aircraft through the left main cabin door. Damage was limited to the collapsed left main landing gear.

Probable Cause

The investigation identified the following causes and contributing factors: 1. Icing conditions were encountered; the airframe de-icing boots were not cycled, and the Vref speed was not increased to offset icing effects. 2. An abrupt change in aircraft configuration (reduction in power to flight idle and addition of 35° flap) caused the speed to decrease rapidly. 3. The aircraft entered an aerodynamic stall due to decreased performance caused by icing, with insufficient altitude to recover before impact.

A finding as to risk noted that the company had not incorporated the British Aerospace Notice to Aircrew into its standard operating procedures at the time, requiring crews to make configuration changes late in the approach, increasing the risk of an unstabilised approach.