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Last updated: 5 December 2021
Statuts:Enquête Officielle
Date:lundi 30 avril 1990
Type/Sous-type:Silhouette image of generic SHAC model; specific model in this crash may look slightly different
Avro Shackleton AEW.2
Compagnie:Royal Air Force - RAF
Immatriculation: WR965
Numéro de série:
Année de Fabrication: 1954
Moteurs: 4 Rolls-Royce Griffon 57
Equipage:victimes: 10 / à bord: 10
Passagers:victimes: 0 / à bord: 0
Total:victimes: 10 / à bord: 10
Dégats de l'appareil: Perte Totale
Conséquences: Written off (damaged beyond repair)
Lieu de l'accident:3,2 km (2 milles) S of Tarbert (   Royaume Uni)
Phase de vol: En vol (ENR)
Aéroport de départ:Lossiemouth RAF Station (LMO/EGQS), Royaume Uni
Aéroport de destination:Benbecula Airport (BEB/EGPL), Royaume Uni
On the morning of 30 April 1990, the crew of Shackleton AEW2 WR965 took off from RAF Lossiemouth to participate in a maritime exercise in the Benbecula area to the west of mainland Scotland. The exercise was to be in two parts with a time interval between. To make most economical use of the Shackleton's flying time it was intended to utilise the time interval to undertake some continuation training for which the crew had appropriate authorisation. Although the weather was forecast to be generally clear in the aircraft's operating area there were areas of low cloud and poor visibility over Scottish coastal areas.
The first part of the sortie was completed without incident and at 09:45 UTC the crew took the opportunity to participate with a Tornado F3 in mutual training which required the Shackleton's radar to be set to standby/off. After completing this training, the crew commenced their own continuation training which was to include a visual approach to Benbecula airfield.
The crew contacted Benbecula Air Traffic Control (ATC) at 10:25 UTC requesting permission for an approach, stating that they were about 20 miles west of the airfield; permission was given and Benbecula ATC passed their actual weather to the crew. Subsequent investigation determined, however, that the aircraft was actually 15 miles north of the position which it had reported at this time. At 10:30 two RAF personnel saw the Shackleton orbiting an island some 12 miles to the north of Benbecula airfield, and at 10:34 the Shackleton crew called Benbecula ATC stating that the weather was not sufficiently good for an approach and that they were turning right and climbing. At around 10:37 it struck the ground about 30 ft below the summit of an 823 ft hill on the Isle of Harris.
Reliable evidence indicates that at that time and in that vicinity the cloudbase was 200 ft above mean sea level, with cloud tops at 3000 ft. At impact, the aircraft was in controlled flight with all four engines developing cruise power.

Probable Cause:

CONCLUSION: "The Board of Inquiry concluded that the accident was caused because the aircraft was flown below a safe altitude in unsuitable weather conditions; the Board were unable to determine the reason for this."

» Broken Wings : Post-War Royal Air Force Accidents / James J. Halley
» The Avro Shackleton / as compiled by Chris Ashworth
» UK Ministry of Defence, Military Aircraft Accident Summary


photo of Avro-Shackleton-AEW-2-WR965
accident date: 30-04-1990
type: Avro Shackleton AEW.2
registration: WR965

Ce plan montre l'aéroport de départ ainsi que la supposée destination du vol. La ligne fixe reliant les deux aéroports n'est pas le plan de vol exact.
La distance entre Lossiemouth RAF Station et Benbecula Airport est de 239 km (150 miles).
Accident location: Approximate; accuracy within a few kilometers.

Les informations ci-dessus ne représentent pas l'opinion de la 'Flight Safety Foundation' ou de 'Aviation Safety Network' sur les causes de l'accident. Ces informations prélimimaires sont basées sur les faits tel qu'ils sont connus à ce jour.
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