10 fatalities

1992-03-22: Antonov AN-30 (CCCP-30002) — Myachkovo Avia — Nizhneyansk, Russia

Nizhneyansk, RussiaFlight

On March 22, 1992, an Antonov AN-30 (registration CCCP-30002) operated by Myachkovo Avia was involved in an aviation accident near Nizhneyansk, Russia in flight. 10 people were killed. Investigators recorded the probable cause as: The crew disengaged and re-engaged the automatic pilot system several times for unknown reasons, causing tail and elevator movements. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781211155Data APIEditorial standards

A cargo aircraft on a flight from Anadyr to Baku crashed into an icy river after violent oscillations and partial disintegration at 2,000 meters, killing all 10 occupants. The probable cause involved repeated autopilot disengagements and inappropriate crew reaction.

Accident Summary

A cargo aircraft operating a flight from Anadyr Airport in Russia to Baku, Azerbaijan, crashed into an icy river following a loss of control at cruising altitude. All five passengers and five crew members on board were killed.

Flight Details

The flight departed Anadyr with intermediate stops planned in Chokurdakh and Tiksi before continuing to Baku. The aircraft was carrying five passengers and five crew members at the time of the accident.

Accident Sequence

While cruising at night, the aircraft experienced violent oscillations, pitching up and down repeatedly. It then entered an uncontrolled descent. At an altitude of approximately 2,000 meters, the aircraft partially disintegrated due to aerodynamic forces. It subsequently struck an icy river at a speed of 670 km/h, resulting in the destruction of the aircraft and the deaths of all occupants.

Investigation Findings

The official investigation determined the probable cause of the accident. The crew disengaged and re-engaged the automatic pilot system several times for reasons that could not be determined. These actions caused movements of the tail and elevators. The crew's response to these movements was inappropriate. Consequently, the aircraft developed violent oscillations on both the roll and pitch axes and entered an uncontrolled descent. The partial disintegration was the result of aerodynamic forces that exceeded the aircraft's certification limits.