1 fatality

2024-06-29: LAK-17B FES (RA-0799A) — Частное лицо — РФ, Пензенская обл., Бессоновский район, а удалении около 2 км. южнее н.п. Сосновка

РФ, Пензенская обл., Бессоновский район, а удалении около 2 км. южнее н.п. Сосновка

On June 29, 2024, a LAK-17B FES (registration RA-0799A) operated by Частное лицо was involved in an aviation accident near РФ, Пензенская обл., Бессоновский район, а удалении около 2 км. южнее н.п. Сосновка. One person was killed. Investigators recorded the probable cause as: Причиной авиационного происшествия с планером LAK-17В FES RA- 0799А явилось разрушение в полете конструкции лонжерона левой консоли крыла в результате превышения максимально допустимой перегрузки по прочности. This summary draws on records from the Interstate Aviation Committee (MAK); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Interstate Aviation Committee (MAK)Primary reportUpdated 1779639674Data APIEditorial standards

On 29 June 2024, the owner of glider LAK-17B FES (RA-0799A) conducted a second flight after a first flight by an acquaintance. The glider was towed by a Vilga-35A and released at about 1000 m. Details of the incident are limited.

Background

The owner of a LAK-17B FES glider, registration RA-0799A, planned flights on 29 June 2024 from the Penza (Sosnovka) airfield. The owner had a contract with the Penza Aviation Sports Club DOSAAF for tow services, dated 8 April 2024. The owner arrived at the airfield around 08:00 and passed a medical check.

Preflight and First Flight

Before the flights, the glider was assembled after purchase, with the outer wing parts attached. The first flight was conducted at 11:30, piloted by an acquaintance of the owner, lasting about two hours. No issues with the glider's performance or handling were reported after landing. An inspection followed, and the owner decided to fly solo.

Second Flight and Towing

The glider's takeoff weight was approximately 430 kg (structure 345.4 kg, pilot with parachute about 85 kg, no water ballast), below the maximum of 600 kg. The center of gravity was 285 mm, within the limits of 206–328 mm specified in the flight manual. At 14:10, the glider took off towed by a Vilga-35A aircraft. The tow pilot reported lifting off and climbing at 120 km/h due to the glider's characteristics. After reaching about 200 m on a straight line, the glider was released at an altitude of approximately 1000 m. No further details about the remainder of the flight or any incident are available from the provided source.