Casualties unknown

2020-08-04: Rans S6-116 Coyote II (G-BUWK) — Bradley’s Lawn airstrip, Cross in Hand, Heathfield, East Sussex , GB

Bradley’s Lawn airstrip, Cross in Hand, Heathfield, East Sussex , GB

On August 4, 2020, a Rans S6-116 Coyote II (registration G-BUWK) was involved in an aviation accident near Bradley’s Lawn airstrip, Cross in Hand, Heathfield, East Sussex , GB. Investigators recorded the probable cause as: The loss of control of the aircraft was most likely caused by the pilot suffering a sudden cardiac event that led to incapacitation shortly after takeoff. This summary draws on records from the UK Air Accidents Investigation Branch (AAIB).

Sourcesthe UK Air Accidents Investigation Branch (AAIB)Primary reportUpdated 1785053200Data APIEditorial standards
Aircraft registered G-BUWK
Aircraft registered G-BUWK. Photo: Aeroprints.com / CC BY-SA 3.0, via Wikimedia Commons

A highly experienced pilot lost control of his Rans S6-116 Coyote II shortly after takeoff from an East Sussex airstrip, resulting in a fatal crash and aircraft destruction.

What happened

On 4 August 2020, a Rans S6-116 Coyote II, registration G-BUWK, departed from Bradley’s Lawn airstrip in East Sussex for a planned flight to Popham Airfield. The pilot, an experienced aviator with over 6,000 flying hours, had intended to meet a partner in the air. Witnesses at the airfield reported that the initial takeoff appeared normal, with the aircraft climbing steadily. However, shortly after the aircraft passed behind a line of trees, witnesses observed a sudden loss of control characterized by a spinning motion and a steep, spiral descent. The aircraft struck the ground in a near-vertical attitude, leading to a massive post-impact fire that completely destroyed the airframe. The pilot sustained fatal injuries.

The investigation

The AAIB examined the wreckage and recovered several electronic flight instruments, including tablets and a Dynon Avion ics D1 system, though fire damage prevented data recovery. ADS-B Out broadcasts from the aircraft provided a flight track, showing a normal climb rate of approximately 1,000 ft/min followed by a descent. An examination of the Rotax 912-UL engine and the aircraft's airframe revealed no evidence of pre-existing mechanical failure or structural defects. While one witness reported hearing a rough-running engine, the recorded flight data and engine strip examination did not support an engine malfunction. The investigation also noted that the aircraft's fuel tanks were likely near capacity at the time of the accident.

Findings

  • The aircraft experienced a sudden loss of control in flight shortly after departure.
  • Post-mortem examination of the pilot revealed moderate coronary artery atheroma and a history of hypertension.
  • The pathologist concluded that the pilot likely suffered a cardiac event resulting in incapacitation shortly after takeoff.
  • Evidence from the post-mortem, including the absence of soot in the airways, indicated the pilot was likely deceased before the post-impact fire began.

Probable cause

The loss of control of the aircraft was most likely caused by the pilot suffering a sudden cardiac event that led to incapacitation shortly after takeoff.