Casualties unknown

Fatal Yak-52 Formation Training Accident at Langford, Essex (RA-3585K)

Langford, near Maldon, Essex, GB

On April 28, 2011, a YAK-52 (registration RA-3585K) was involved in an aviation accident near Langford, near Maldon, Essex, GB. Investigators recorded the probable cause as: The aircraft entered an inverted spin at approximately 1,800 ft agl, probably because of unintentional pro-spin positioning of the flying controls. This summary draws on records from the UK Air Accidents Investigation Branch (AAIB).

Sourcesthe UK Air Accidents Investigation Branch (AAIB)Primary reportUpdated 2026-09-13Data APIEditorial standards

A Yak-52 (RA-3585K) crashed into a lake near Langford, Essex, on 28 April 2011 during a formation training exercise. Both occupants were killed after the aircraft entered an inverted spin and dived into the water.

Accident Overview and Aircraft Details On 28 April 2011 at 1150 UTC, a Yak-52 aircraft, registration RA-3585K, was destroyed when it impacted the surface of a lake at Langford, near Maldon, Essex. The aircraft was a 1990 model equipped with a single Ivchenko M14P piston engine. It was operating as a training flight with two crew members on board, both of whom were fatally injured. The commander held a Private Pilot’s Licence and was 43 years old, with a total flying experience of 673 hours, including 66 hours on the Yak-52 type. ## Flight History and Formation Exercise The accident occurred on the third day of a three-day formation flying school held at North Weald Aerodrome. The flight involved multiple aircraft practicing maneuvers in vic, echelon, and line astern formations, culminating in a demonstration of a formation loop and a tailchase. The minimum briefed height for the tailchase was 1,000 feet above ground level (agl). During the exercise, RA-3585K was positioned second in a tailchase of three aircraft. The lead aircraft was being flown by an experienced student pilot under the guidance of an instructor. ## Sequence of Events Video footage from a helmet camera on a student in the third aircraft captured the final moments of the flight. As the lead aircraft executed a series of wingovers and an aileron roll, RA-3585K followed. At an altitude of approximately 1,800 ft agl, RA-3585K reached a low speed and a high angle of attack. The aircraft then rolled and yawed into an inverted spin to the left. The spin continued for three turns before the aircraft recovered into an erect dive at a low height. Eyewitnesses reported the aircraft impacting the lake and sinking. Emergency services, including rescue divers, located the wreckage, and both occupants were confirmed to have been fatally injured. ## Investigation Findings The AAIB investigation identified several factors relevant to the accident, including the operation of the aircraft, the type of flight instruments fitted, and the manner in which the activity was conducted. The synopsis suggests the aircraft entered the inverted spin probably because of unintentional pro-spin positioning of the flying controls. Meteorological data indicated visibility of approximately 15 km, winds of 25 to 30 kt, and a cloud base between 1,500 ft and 1,800 ft agl. The school’s standard operating procedures required the leader to maintain visual meteorological conditions (VMC) at all times and adhere to minimum height and cloud clearance limits. The investigation noted that the school did not have a formal risk management or safety system.

Probable cause

The aircraft entered an inverted spin at approximately 1,800 ft agl, probably because of unintentional pro-spin positioning of the flying controls.