Incident Overview

Date: Tuesday 20 July 1965
Aircraft Type: Vickers 701 Viscount
Owner/operator: Cambrian Airways
Registration Number: G-AMOL
Location: 0,5 km from Liverpool International Airport (LPL) – ÿ United Kingdom
Phase of Flight: Approach
Status: Destroyed, written off
Casualties: Fatalities: 2 / Occupants: 2
Component Affected: FuselageFuselage
Category: Accident
A Viscount G-AMOL aircraft departed Ronaldsway at 16:49 for Liverpool, flying at flight level 70. Approximately 550 meters from touchdown, the radar approach was completed, and the aircraft was seen to be just discernibly to the right of the centreline. Witnesses observed the aircraft banking and turning to the right. The fuselage was level, and it was banked almost vertically for part of the turn. Upon heading in the opposite direction to the runway, it rolled onto its back and crashed into a factory roof. The intense fire consumed the entire fuselage.A Viscount G-AMOL aircraft departed Ronaldsway at 16:49 for Liverpool, flying at flight level 70. Approximately 550 meters from touchdown, the radar approach was completed, and the aircraft was seen to be just discernibly to the right of the centreline. Witnesses observed the aircraft banking and turning to the right. The fuselage was level, and it was banked almost vertically for part of the turn. Upon heading in the opposite direction to the runway, it rolled onto its back and crashed into a factory roof. The intense fire consumed the entire fuselage.

Description

Viscount G-AMOL departed Ronaldsway at 16:49 for a flight to Liverpool. The flight was made at flight level 70 and at 17:08 hours the aircraft was identified by Liverpool radar over Wallasey and positioned for a PPI continuous descent radar approach to runway 26. Half a mile from touchdown the radar approach was completed and the aircraft was then seen (on radar) to be just discernibly to the right of the centreline. No radio messages were received from the aircraft after the start of the talk-down. At 550 metres from the threshold, it was estimated to be at a height between 30 and 60 metres and about 40 metres to the right of the centre line. At this point witnesses saw the aircraft bank and turn to the right. The fuselage was level and the aircraft was banked almost vertically for part of the turn. When heading in approximately the opposite direction to the runway it rolled on to its back and crashed into the roof of a factory about 365 metres to the right of the extended centre line of the runway and about 550 metres from the threshold. After penetrating the roof, the aircraft had struck a heavy steel girder which had caused it to tip “tail-over-nose”. It had then come to rest the right way up on the floor of the workshop with the tail resting on the steel roof trusses. An intense fire broke out which consumed almost the whole structure of the fuselage. PROBABLE CAUSE: “The aircraft went out of control during the final stage of an approach to land but the reason for this has not been determined.”

Primary Cause

Loss of control during final approach to land.Loss of control during final approach to land.

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