Casualties unknown

L-13 Blanik Glider Crash at Panevėžys Aerodrome (LY-GKM)

LT

On May 6, 2006, a L-13 Blanik (registration LY-GKM) was involved in an aviation accident near LT. Investigators recorded the probable cause as: Piloting errors during approach to landing, specifically descending too early when passing an obstacle and losing airspeed while turning to avoid power lines, resulting in a stall. This summary draws on records from the Transport Accident and Incident Investigation Service of Lithuania (TAITS).

Sourcesthe Transport Accident and Incident Investigation Service of Lithuania (TAITS)Primary reportUpdated 2026-06-09Data APIEditorial standards

On May 6, 2006, an L-13 Blanik glider (LY-GKM) crashed near Panevėžys after the pilot became ill and handed control to a passenger. The passenger attempted to avoid power lines but entered a stall, resulting in one serious injury.

Incident Overview

On May 6, 2006, at approximately 17:15 local time, an L-13 "Blanik" glider with registration LY-GKM crashed into a field near the Panevėžys Aeroclub aerodrome. The aircraft was operated by the Panevėžys Aeroclub and manufactured by LET in the Czech Republic. The incident resulted in one serious injury to the pilot and no injuries to the passenger.

Flight Details and Sequence of Events

The flight began at 15:20 with a licensed pilot and a passenger aboard. Both individuals had not flown since 2005, making this their first flight of the year. During the flight, which took place over the aerodrome under good weather conditions, the pilot experienced nausea and decided to land. He transferred control to the passenger, who possessed significant flying experience but lacked a valid glider license at the time.

While on final approach with air brakes deployed, the passenger realized they were insufficiently high to clear power lines crossing the landing path. Attempting to avoid the obstacle by turning 180 degrees toward an adjacent field, the glider lost speed and entered a stall. The aircraft struck the ground first with the right wing, then the left wing, and finally the front cabin section.

Aircraft Condition and Injuries

The glider sustained severe structural damage, including broken wings at the sixth rib from the tip, a deformed fuselage, and a shattered canopy. The pilot suffered a back injury, while the passenger remained uninjured. Both occupants were wearing seatbelts, which likely mitigated the severity of their injuries.

Investigation Findings

The investigation determined that the crash was caused by piloting errors during the approach to landing. Specifically, the aircraft descended too early when passing an obstacle and lost critical airspeed while attempting a turn to avoid power lines, leading to a stall. The report noted that both crew members had been away from flying for a long period, which may have contributed to the lack of attention required for safe maneuvering.

Probable cause

Piloting errors during approach to landing, specifically descending too early when passing an obstacle and losing airspeed while turning to avoid power lines, resulting in a stall.