9 fatalities

1990-10-11: Antonov AN-8 (CCCP-69320) — MAP - Ministerstvo Aviatsionnoi Promyshlennosti - Minaviaprom — Novosibirsk-Yeltsovka, Russia

Novosibirsk-Yeltsovka, RussiaLanding (descent or approach)

On October 11, 1990, an Antonov AN-8 (registration CCCP-69320) operated by MAP - Ministerstvo Aviatsionnoi Promyshlennosti - Minaviaprom was involved in an aviation accident near Novosibirsk-Yeltsovka, Russia during landing or approach. 9 people were killed. Investigators recorded the probable cause as: The dual engine failure was the consequence of an error on part of one of the crew members who inadvertently switched off the electrical systems supplying both engines while trying to deactivate the anti-icing systems. 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 1781212535Data APIEditorial standards

On final approach to Novosibirsk-Yeltsovka Airport, both engines stopped simultaneously, leading to impact with power lines and a railway embankment, resulting in nine fatalities and injuries to the captain.

Incident Overview

During the final approach to Novosibirsk-Yeltsovka Airport, at an altitude of 140 meters and a speed of 260 km/h, approximately 3 kilometers from the runway threshold, both engines ceased operation simultaneously. The aircraft subsequently lost altitude, struck overhead power lines, and collided with the embankment of a railway line. The crash occurred 2,010 meters short of the runway, near a wooded area, where the aircraft burst into flames. The captain sustained injuries, while nine other occupants were killed.

Investigation Findings

The official investigation determined that the dual engine failure resulted from an error by a crew member who inadvertently switched off the electrical systems supplying both engines while attempting to deactivate the anti-icing systems. The crew's response was deemed inappropriate, as they delayed in identifying the failure and failed to feather both propellers. The aircraft was not equipped with an automatic feathering system, and the combination of the late crew reaction with both propellers non-feathered increased aerodynamic drag, causing the aircraft to lose height and crash.

Probable cause

The dual engine failure was the consequence of an error on part of one of the crew members who inadvertently switched off the electrical systems supplying both engines while trying to deactivate the anti-icing systems. The crew reaction was inappropriate since they took time to identify the failure and failed to feather both propellers. The combination of a late crew reaction with both propellers non feathered (the aircraft was not equipped with an automatic feathering system) increased drag and caused the aircraft to lose height and to crash.