7 fatalities

Seven Killed and One Injured in Accident on Approach to Helsinki-Vantaa Runway 22 (N26RT)

Helsinki-Vantaa, FinlandLanding (descent or approach)

On February 24, 1989, a Swearingen SA226T Merlin III (registration N26RT) operated by Predator was involved in an aviation accident near Helsinki-Vantaa, Finland during landing or approach. 7 people were killed. Investigators recorded the probable cause as: It is believed that the pilot probably encountered difficulties in controlling the altitude and an excessive speed during the final approach procedure. As a result, he retarded engine power by pulling both speed levers backwards. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards
Aircraft registered N26RT
Aircraft registered N26RT. Photo: Aeroprints.com / CC BY-SA 3.0, via Wikimedia Commons

A twin-engine aircraft on a night charter flight from Southend to Helsinki struck ground short of runway 22 at Helsinki-Vantaa, injuring one passenger and killing seven others. The accident occurred after the pilot reduced speed on final approach.

Accident Summary

A twin-engine aircraft operating a night charter flight from Southend to Helsinki was on final approach to Helsinki-Vantaa Airport runway 22. The aircraft carried seven passengers and one pilot. During the approach, the pilot elected to reduce speed, causing the aircraft to lose altitude. It descended below the minimum descent altitude (MDA), struck the ground, and came to rest inverted in a snow-covered field approximately one kilometer short of the runway threshold. One passenger was seriously injured, while the other seven occupants were killed.

Investigation Findings

Official investigation determined that the pilot likely encountered difficulties controlling altitude and managing excessive speed during the final approach. In response, the pilot retarded engine power by pulling both speed levers backwards. Examination revealed that the flight idle gate, which normally prevents the speed levers from being positioned to idle before landing, was worn. This allowed the pilot to inadvertently move both levers to the idle position while still on approach, causing a loss of speed and altitude that led to the descent below the MDA and subsequent ground impact.

Contributing factors included the pilot's insufficient experience on this type of aircraft, inadequate training for such operations, and the demanding instrument flight conditions present at the time of the accident.

Probable cause

It is believed that the pilot probably encountered difficulties in controlling the altitude and an excessive speed during the final approach procedure. As a result, he retarded engine power by pulling both speed levers backwards. Investigations revealed that the flight idle gate allowing the speed levers to be stopped before being positioned at idle was worn, which allowed the pilot to position both levers to idle position while still on approach. This caused the aircraft to lose speed and altitude and to descend below the minimum descent altitude (MDA) until it struck the ground. The following contributing factors were reported: - The pilot did not have sufficient experience on this type of aircraft, - The pilot's training on such operation was insufficient, - The accident occurred in demanding instrument flight conditions.