Incident Overview

Date: Friday 25 May 1979
Aircraft Type: Vickers 806 Viscount
Owner/operator: British Airways
Registration Number: G-AOYS
Location: Cardiff-Wales Airport (CWL) – ÿ United Kingdom
Phase of Flight: Landing
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 55
Component Affected: Landing gear linkage (specifically, the bolt connecting the left wing to the landing gear).Landing gear linkage (specifically, the bolt connecting the left wing to the landing gear).
Category: Accident
An aircraft experienced a landing gear failure during a flight from Cardiff to Paris. The left gear failed to extend during approach to Bristol, prompting an emergency procedure involving fuel burn and a modified approach. After unsuccessful attempts to lower the gear, the aircraft landed on grass, requiring crane operation to retract the gear and subsequent towing to a hangar for investigation. A critical component ? a bolt from the landing gear linkage ? was found broken off in the wheel bay, indicating fatigue failure.An aircraft experienced a landing gear failure during a flight from Cardiff to Paris. The left gear failed to extend during approach to Bristol, prompting an emergency procedure involving fuel burn and a modified approach. After unsuccessful attempts to lower the gear, the aircraft landed on grass, requiring crane operation to retract the gear and subsequent towing to a hangar for investigation. A critical component ? a bolt from the landing gear linkage ? was found broken off in the wheel bay, indicating fatigue failure.

Description

The aircraft was on a flight from Cardiff/Wales to Paris with an intermediate landing at Bristol . When the landing gear was selected during the approach to Bristol, the left gear failed to extend. The aircraft returned to Cardiff where full engineering facilities were available and, after a flypast, the tower confirmed the left gear was retracted. As repeated attempts to lower the gear were unsuccessful, extra fuel was burnt off before commencing an approach to runway 31 with the left gear retracted. The aircraft made a smooth touchdown and continued along the runway before finally coming to rest on the grass turning 90ø to the left after leaving the runway approximately 1200 m from the threshold. Full emergency services were available, and quickly at the scene, and evacuation was successfully completed without injuries to occupants. There was no fire. Examination of the aircraft hydraulic system showed it to be serviceable, including the emergency system. The aircraft’s left wing was lifted by crane and the landing gear lowered by removing the uplock lug from the oleo leg. Ground locks were fitted and the aircraft towed to the hangar for further investigation. Inspection of the uplock mechanism showed that a bolt was missing from the operating linkage. The bolt is in part of the linkage which is common to both main and emergency hydraulic systems. The bolt was found in the wheel bay and it was seen that the threaded portion had broken off. Initial metallurgical opinion is that it had failed in fatigue.

Primary Cause

Fatigue failure of a landing gear linkage bolt.Fatigue failure of a landing gear linkage bolt.

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