Incident Overview

Date: Sunday 19 May 1996
Aircraft Type: Britten-Norman BN-2A-26ÿIslander
Owner/operator: Loganair
Registration Number: G-BEDZ
Location: 1,5 km S of Lerwick/Tingwall Airport, Shetland Islands (LWK) – ÿ United Kingdom
Phase of Flight: Approach
Status: Destroyed, written off
Casualties: Fatalities: 1 / Occupants: 3
Component Affected: Aircraft control system (downwind leg and bank angle).Aircraft control system (downwind leg and bank angle).
Investigating Agency: AAIBAAIB
Category: Accident
An Islander aircraft experienced a near-miss incident during an ambulance flight to Inverness. The pilot executed a series of maneuvers, including an extended downwind leg and a steep bank angle, resulting in a collision with terrain. The aircraft descended to 550 feet and then lost altitude, resulting in a right wing low attitude and nose low attitude.An Islander aircraft experienced a near-miss incident during an ambulance flight to Inverness. The pilot executed a series of maneuvers, including an extended downwind leg and a steep bank angle, resulting in a collision with terrain. The aircraft descended to 550 feet and then lost altitude, resulting in a right wing low attitude and nose low attitude.

Description

The Islander had operated on an ambulance flight to Inverness and was ferried back to its base at Tingwall Airport. The pilot manoeuvred the airplane for an approach to runway 02. While turning to finals the aircraft was blown through the centerline, forcing the pilot to abandon the approach. He climbed to 550 feet and positioned the airplane for another approach. For this second attempt the pilot extended the downwind leg by approximately 800 metres before turning towards the airfield. A rapid turn to finals with a steep bank angle was performed during which the aircraft descended. In a right wing low attitude of some 70øand a nose low attitude of approximately 20ø the aircraft collided with grass covered gently rising terrain, 1,5 km South of the runway. Its groundspeed at this time was estimated at 125 kt. The investigation report did not contain a ‘probable cause’.

Primary Cause

Pilot error during maneuvering, specifically an extended downwind leg and steep bank angle, leading to a collision with terrain.Pilot error during maneuvering, specifically an extended downwind leg and steep bank angle, leading to a collision with terrain.

Share on:

Leave a Reply

Your email address will not be published.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