Incident Overview

Date: Saturday 23 December 2000
Aircraft Type: Beechcraft 200 Super King Air
Owner/operator: Videovision Broadcast Ltd.
Registration Number: VP-BBK
Location: 1,8 km NE of Blackbushe Airport (BBS) – ÿ United Kingdom
Phase of Flight: Take off
Status: Destroyed, written off
Casualties: Fatalities: 5 / Occupants: 5
Component Affected: PropellersPropellers
Investigating Agency: AAIBAAIB
Category: Accident
An aircraft carrying four passengers and a pilot departed Blackbushe runway 08 in dense fog with visibility below 500 meters. The aircraft banked sharply to the left before disappearing. It crashed into a factory complex, resulting in a major fire. All on board were fatally injured. Analysis of the cockpit voice recorder revealed a reduction in one of the propellers’ RPM, suggesting a potential for thrust asymmetry, which contributed to loss of control.An aircraft carrying four passengers and a pilot departed Blackbushe runway 08 in dense fog with visibility below 500 meters. The aircraft banked sharply to the left before disappearing. It crashed into a factory complex, resulting in a major fire. All on board were fatally injured. Analysis of the cockpit voice recorder revealed a reduction in one of the propellers’ RPM, suggesting a potential for thrust asymmetry, which contributed to loss of control.

Description

The aircraft, with the pilot and four passengers on board, departed Blackbushe from runway 08 in fog with a visibility of less than 500 metres. As the aircraft reached the upwind end of the runway it was seen to bank to the left before disappearing from view. It crashed 13 seconds later into a factory complex where a major fire ensued. All on board were fatally injured. A substantial amount of the aircraft structure was consumed by fire. Engineering examination of that which remained showed that there was no malfunction found within the engines, propellers or controls that would have affected the flight. Analysis of the cockpit voice recorder however showed a reduction in one of the propellers rpm as the aircraft rotated that would have led to thrust asymmetry. Through a combination of lack of visual reference, confusion as to the cause of the power reduction and possible disorientation the pilot lost control of the aircraft and although he may have realised the situation seconds before impact with the ground there was insufficient height available to effect a safe recovery.

Primary Cause

Reduced propeller RPM due to rotation during flight, potentially leading to thrust asymmetry and loss of control.Reduced propeller RPM due to rotation during flight, potentially leading to thrust asymmetry and loss of control.

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