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Last updated: 17 September 2021
Status:Definitief
Datum:vrijdag 25 mei 1979
Type:Silhouette image of generic VISC model; specific model in this crash may look slightly different
Vickers 806 Viscount
Luchtvaartmaatschappij:British Airways
Registratie: G-AOYS
Constructienummer: 367
Bouwjaar: 1958-05-24 (21 years )
Motoren: 4 Rolls-Royce Dart 520
Bemanning:slachtoffers: 0 / inzittenden: 4
Passagiers:slachtoffers: 0 / inzittenden: 51
Totaal:slachtoffers: 0 / inzittenden: 55
Schade: Groot
Gevolgen: Repaired
Plaats:Cardiff-Wales Airport (CWL) (   Verenigd Koninkrijk)
Fase: Landing (LDG)
Soort vlucht:Binnenlandse lijnvlucht
Vliegveld van vertrek:Cardiff-Wales Airport (CWL/EGFF), Verenigd Koninkrijk
Vliegveld van aankomst:Bristol Airport (BRS/EGGD), Verenigd Koninkrijk
Beschrijving:
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to Cardiff where full engineering facilities were available and, after a flypast, the tower confirmed the left gear was retracted.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 90° 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.

Bronnen:
» AIB Bulletin 8/79


Foto's

photo of Vickers-806-Viscount-G-AOYS
accident date: 25-05-1979
type: Vickers 806 Viscount
registration: G-AOYS
 

Video, social media

Kaart
Deze kaart geeft het vliegveld van vetrek weer en de geplande bestemming van de vlucht. De lijn tussen de vliegvelden geeft niet de exacte vliegroute weer.
De afstand tussen Cardiff-Wales Airport en Bristol Airport bedraagt 43 km (27 miles).

This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.
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