Incident Overview

Date: Thursday 16 May 1929
Aircraft Type: Vickers 170 Vanguard
Owner/operator: Vickers-Armstrongs Ltd
Registration Number: G-EBCP
Location: Shepperton – ÿ United Kingdom
Phase of Flight: En route
Status: Destroyed, written off
Casualties: Fatalities: 2 / Occupants: 2
Component Affected: Tail unitTail unit
Category: Accident
On May 16, 1929, a Vickers 170 Vanguard twin-engined biplane crashed and burned at Shepperton, near the River Thames. The aircraft, piloted by Flight Lieutenant Edward Rodolph Clement Scholefield and his Mechanic S.W. Sherratt, lost control and nose-dived into the ground during a test flight. The tail unit was identified as a faulty unit due to excessive rudder force, leading to the crash.On May 16, 1929, a Vickers 170 Vanguard twin-engined biplane crashed and burned at Shepperton, near the River Thames. The aircraft, piloted by Flight Lieutenant Edward Rodolph Clement Scholefield and his Mechanic S.W. Sherratt, lost control and nose-dived into the ground during a test flight. The tail unit was identified as a faulty unit due to excessive rudder force, leading to the crash.

Description

The Vickers 170 Vanguard was a 22-passenger twin-engined biplane. When it was handed over to Imperial Airways in 1925 it was described as the World’s largest passenger aeroplane. The aircraft was withdrawn from its airline duties in October 1928 for modifications, probably to the tail. The airplane had been fitted with a new tail unit from a Vickers Virginia Mk X in an effort to eliminate control problems. On 16 May 1929 the aircraft crashed and burned at Shepperton on the shores of the River Thames. Vickers Test Pilot Flight Lieutenant Edward Rodolph Clement “Tiny” Scholefield DCM, AFC, and his Mechanic S.W. Sherratt were killed. They were test flying the Vanguard airliner from Brooklands Aerodrome when control was lost and the aircraft nose-dived from 2000 feet into the ground. The tail unit apparently failed as a result of excessive rudder force.

Primary Cause

Excessive rudder force on the tail unit caused a loss of control during a test flight.Excessive rudder force on the tail unit caused a loss of control during a test flight.

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