4 fatalities

Test Flight Crash in Cowbridge, Wales: Structural Failure Due to Excessive Rudder Movement (G-AHJJ)

Cowbridge, United KingdomFlight

On March 21, 1950, a Bristol 170 Freighter (registration G-AHJJ) operated by Bristol Aeroplane Company was involved in an aviation accident near Cowbridge, United Kingdom in flight. 4 people were killed. Investigators recorded the probable cause as: The accident was caused by a structural failure of the fuselage stern frame to which the fin was attached and must be attributed to the application on the fin and rudder of a load greater than the design ultimate load. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 7 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-12Data APIEditorial standards

During a certification test flight, an aircraft crashed near Cowbridge, Wales, 34 minutes after departure. All four occupants were killed. Official findings attribute the accident to a structural failure caused by overloading from excessive rudder movement at high speed.

Accident Overview

A test flight ended in tragedy when the aircraft, a recently converted MK.2 to 21 version, crashed in a field near Cowbridge, south of Wales. The flight departed from Bristol-Filton Airport approximately 34 minutes before the accident. The airplane went out of control and dove into the ground, resulting in the deaths of all four occupants: three engineers from Bristol and one pilot.

Investigation Findings

The official investigation determined that the accident was caused by a structural failure of the fuselage stern frame, to which the fin was attached. This failure was attributed to the application of a load greater than the design ultimate load on the fin and rudder. Calculations indicated that the overloading resulted from excessive rudder movement at a speed exceeding 120 knots.

Aircraft Details

The source notes that the aircraft was an MK.2 version that had recently been converted to a 21 version. This flight was the second test flight for the certification program. No other details about the aircraft type, registration, or manufacturer were provided in the source.

Probable cause

The accident was caused by a structural failure of the fuselage stern frame to which the fin was attached and must be attributed to the application on the fin and rudder of a load greater than the design ultimate load. Calculations suggested that the cause of this overloading was excessive rudder movement at a speed greater than 120 knots.