No fatalities

Test Flight Ends with Belly Landing in Severn Estuary (G-ALRX)

Littleton-upon-Severn, United KingdomLanding (descent or approach)

On February 4, 1954, a Bristol Britannia (registration G-ALRX) operated by Bristol Aeroplane Company was involved in an aviation accident near Littleton-upon-Severn, United Kingdom during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The explosion of engine number three was the consequence of the failure of the reduction gear. The fire was caused by shrapnel piercing the engine oil tank, igniting the oil. 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
Aircraft registered G-ALRX
Aircraft registered G-ALRX. Photo: MilborneOne / CC BY 2.5, via Wikimedia Commons

During a test flight from Bristol-Filton, engine three exploded due to reduction gear failure. Fire caused short circuit, leading to both left engines stopping. The captain performed a belly landing in the Severn estuary; all 13 occupants suffered minor injuries.

Flight

The crew, consisting of Bristol pilots and engineers and KLM pilots, was conducting a test flight from Bristol-Filton Airport. Seven minutes after takeoff, the temperature of engine number three rose. The engine was shut down and later restarted as the temperature cooled. While climbing to an altitude of 10,000 feet, the temperature rose again and the engine exploded. The fire could not be extinguished. As a precaution, engine number four was shut down, and the crew decided to return to Filton.

Landing

On approach, both left engines stopped but were quickly restarted. In these conditions, the captain decided to attempt a belly landing in the Severn estuary, off Littleton-upon-Severn. All 13 occupants escaped with minor injuries, while the aircraft was damaged beyond repair.

Probable Cause

The explosion of engine number three was the consequence of the failure of the reduction gear. A pinion at the front of the propeller shaft had been stripped of its teeth. The revolutionary Proteus turboprop engine had a free turbine design, so the reduction gear failure left the propeller turbine unloaded. In this state it rapidly oversped and eventually disintegrated in an explosion. The fire was caused by shrapnel piercing the engine oil tank, igniting the oil. The reduction gear was later redesigned and installed in subsequent aircraft; the straight teeth on the offending pinion were replaced with helical teeth. The shutdown of engines number one and two was due to a short circuit caused by the fire.