43 fatalities

1967-12-30: Antonov AN-24 (CCCP-46215) — Aeroflot - Russian International Airlines — Liepaja, Latvia

Liepaja, LatviaLanding (descent or approach)

On December 30, 1967, an Antonov AN-24 (registration CCCP-46215) operated by Aeroflot - Russian International Airlines was involved in an aviation accident near Liepaja, Latvia during landing or approach. 43 people were killed. Investigators recorded the probable cause as: The loss of power following a left engine failure during an attempted go-around caused the aircraft to lose altitude and crash. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781239258Data APIEditorial standards

An aircraft crashed in an open field near Liepaja Airport following a left engine failure during a missed approach attempt.

What happened

During the final approach phase toward Liepaja Airport, the flight crew encountered difficulties locating the runway and approach lighting systems. At an altitude of approximately 300 meters and maintaining a speed of 300 km/h, the captain initiated a go-around procedure to re-establish visual contact with the landing strip.

As the pilot increased engine power to execute the maneuver, the left engine experienced a failure. This loss of power caused the aircraft type to bank toward the left at an angle of 40 degrees. The resulting increase in drag led to a significant loss of altitude. The aircraft impacted the snow-covered terrain approximately 1,800 meters beyond the outer marker.

Following the initial impact, the plane bounced and collided with a telegraph pole, which resulted in the destruction of three meters of the left wing. The wreckage continued to travel for an additional 1,410 meters before ultimately crashing in an open field and catching fire. The accident resulted in 43 fatalities and 8 survivors. The aircraft was completely destroyed during the sequence of events.

Findings

Investigations into the crash determined that the primary factor was the failure of the left engine. While the specific reason for this malfunction remained unconfirmed, it is suspected that a component within the turbine may have failed.

Probable cause

The loss of power following a left engine failure during an attempted go-around caused the aircraft to lose altitude and crash.