No fatalities

1995-01-25: Yakovlev Yak-40 (RA-87464) — Volga Airlines - Aviakompania Volga — Rostov-on-Don, Russia

Rostov-on-Don, RussiaLanding (descent or approach)

On January 25, 1995, a Yakovlev Yak-40 (registration RA-87464) operated by Volga Airlines - Aviakompania Volga was involved in an aviation accident near Rostov-on-Don, Russia during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Following a wrong manipulation, the flight engineer activated the thrust reversers on engine n°1 and n°3 but not on the engine n°2 that was providing full power. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781208325Data APIEditorial standards

A three-engine aircraft overran the runway at Rostov-on-Don Airport, lost its landing gear, struck a concrete wall, and came to rest 870 meters past the runway end. All 10 occupants escaped without injury, but the aircraft was destroyed.

Incident Overview

A three-engine aircraft overran the runway after landing at Rostov-on-Don Airport. The aircraft failed to stop within the available distance, exited the runway, lost its undercarriage, struck a concrete wall, and came to rest 870 meters beyond the runway end. All 10 occupants evacuated without injury, though the aircraft sustained damage beyond repair.

Sequence of Events

The aircraft had just landed when it encountered difficulties decelerating. It continued past the runway threshold, crossing the overrun area until it hit a concrete structure. The impact sheared off the landing gear and caused extensive structural damage. Emergency services responded, but all occupants were already out of the aircraft.

Official Findings

The investigation determined that the flight engineer, following a wrong manipulation, activated the thrust reversers on engine number 1 and engine number 3, but did not activate the thrust reverser on engine number 2. At the same time, engine number 2 was providing full power. This asymmetric configuration reduced the overall braking effectiveness, and the crew was unable to stop the aircraft within the landing distance available.

Probable cause

Following a wrong manipulation, the flight engineer activated the thrust reversers on engine n°1 and n°3 but not on the engine n°2 that was providing full power. Such configuration reduced the braking action and the crew was unable to stop the aircraft within the landing distance available.