Incident Overview

Date: Friday 16 August 1996
Aircraft Type: Hawker Siddeley HS-748-235 Srs. 2A
Owner/operator: Emerald Airways
Registration Number: G-ATMI
Location: Liverpool Airport, Speke, Liverpool – ÿ United Kingdom
Phase of Flight: Take off
Status: Substantial
Casualties: Fatalities: 0 / Occupants: 2
Component Affected: Elevator gust lock systemElevator gust lock system
Investigating Agency: AAIBAAIB
Category: Accident
On 16 August 1996, during a take-off run on Runway 27 at Liverpool, an aircraft experienced an abort due to a malfunctioning elevator gust lock. The pilot steered the aircraft off course to avoid running into the River Mersey. The aircraft struck a building and swung hard to the left, resulting in a stop. The take-off was performed by the co-pilot. An inspection revealed multiple rigging faults in the gust lock system, including an omission of a pivot bush and an overtightened bolt, which contributed to the system?s inherent susceptibility to anomalies.On 16 August 1996, during a take-off run on Runway 27 at Liverpool, an aircraft experienced an abort due to a malfunctioning elevator gust lock. The pilot steered the aircraft off course to avoid running into the River Mersey. The aircraft struck a building and swung hard to the left, resulting in a stop. The take-off was performed by the co-pilot. An inspection revealed multiple rigging faults in the gust lock system, including an omission of a pivot bush and an overtightened bolt, which contributed to the system?s inherent susceptibility to anomalies.

Description

On 16-8-1996, during the take-off run on Runway 27 at Liverpool, the aircraft would not rotate and the crew elected to abort the take-off. However, the aircraft was not stopped before the end of the runway and, in order to avoid over running into the River Mersey, the pilot steered it off towards the right. The aircraft ran across the grass for some 200 metres before its right wing struck a small building. The aircraft then swung hard to the left and came to a stop. The take-off was being performed by the co-pilot. The accident happened at night (00:57 hours Local time). Runway 27 at Liverpool is 2,286 metres long and has an asphalt surface. Prior to departure, the crew had correctly disengaged the gust lock lever on the flight controls and had performed the ‘Full and Free’ control check satisfactorily. However, it would seem that the elevator gust lock had re-engaged itself as the ‘Full and Free’ check was completed. An inspection of the gust lock system discovered multiple rigging faults including the omission of a pivot bush and the overtightening of a bolt which tended to move the lock towards engagement when the control column was moved forwards. It was noted that the maintenance standard on the aircraft and that the specified procedures for maintaining and checking the flight controls gust lock were both ‘inadequate’. This was not detected by the CAA. Service experience had led to emphasis having been placed on the need to achieve effective locking performance for the gust lock system. The unlocking performance of the elevator gust lock was found to be ‘marginal’ even after substantial rectification work to correctly rig the system had been carried out. The AAIB found that the system was inherently susceptible to anomalies and external influences

Source of Information

https://assets.publishing.service.gov.uk/media/5422f79de5274a1314000639/1-99_G_ATMI.pdf, https://siteapps.caa.co.uk/g-info/rk=ATMI, http://www.danairremembered.com/hs-748.phphttps://assets.publishing.service.gov.uk/media/5422f79de5274a1314000639/1-99_G_ATMI.pdf, https://siteapps.caa.co.uk/g-info/rk=ATMI, http://www.danairremembered.com/hs-748.php

Primary Cause

Faulty elevator gust lock system resulting in inadequate locking performance and susceptibility to anomalies.Faulty elevator gust lock system resulting in inadequate locking performance and susceptibility to anomalies.

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