10 fatalities

Test Flight Crashes Near Moscow After Engine Failure and Stall (002 red)

Moscow-Sheremetyevo, RussiaLanding (descent or approach)

On May 7, 1958, an Ilyushin II-18 (registration 002 red) operated by Soviet Air Force - Voyenno-vozdushnye sily CCCP was involved in an aviation accident near Moscow-Sheremetyevo, Russia during landing or approach. 10 people were killed. Investigators recorded the probable cause as: The aircraft was equipped with four Kuznetsov NK-4 engines that were not fitted with a propeller feathering system. 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 2026-06-12Data APIEditorial standards

A test flight with 10 crew crashed 4 km short of Moscow-Sheremetievo runway after engine failure prevented propeller feathering, causing loss of speed and stall. All 10 occupants were killed.

Accident

On a local test flight departing from Moscow-Sheremetievo Airport, the aircraft experienced a failure of engine number two a few minutes after takeoff. The propeller could not be feathered, resulting in increased drag. The aircraft subsequently lost altitude and speed. The crew decided to return to Sheremetievo Airport for an emergency landing, but during the final approach, the airplane stalled and crashed in flames approximately 4 kilometers short of the runway threshold. The aircraft was destroyed, and all ten occupants—five engineers and five test pilots—were killed.

Aircraft and Crew

The test flight was conducted on behalf of AKDON – Aviatsionnaya Krasnoznamyonnaya Diviziya Osobogo Naznacheniya, a division of the Soviet Army. The aircraft was equipped with four Kuznetsov NK-4 engines. No further details about the aircraft type, registration, or the crew were provided in the investigation report.

Probable Cause

The official investigation determined that the aircraft's four Kuznetsov NK-4 engines were not fitted with a propeller feathering system. When engine number two failed, the inability to feather the propeller caused high drag, leading to a loss of speed and eventual stall.