10 fatalities

Post-takeoff crash near Stalino Airport due to dual engine failure (CCCP-L1381)

Donetsk, UkraineTakeoff (climb)

On January 19, 1949, an Ilyushin II-12 (registration CCCP-L1381) operated by Aeroflot - Russian International Airlines was involved in an aviation accident near Donetsk, Ukraine during takeoff. 10 people were killed. Investigators recorded the probable cause as: A structural defect in the screw regulator caused the right engine to overspeed, while an unverified issue led to left engine power loss, compounded by an inadequate crew response to the dual failure. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 4 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Source recordUpdated 2026-08-05Data APIEditorial standards

An aircraft crashed into a residential building shortly after departing Stalino Airport following simultaneous engine failures, resulting in ten fatalities and one serious injury.

What happened

The incident occurred immediately after departure from Stalino Airport. While the aircraft was climbing to an altitude of approximately 90 meters, it experienced a critical mechanical failure involving both powerplants. The right-hand engine oversped, while the left-hand engine lost all thrust. This dual-engine dysfunction caused the airframe to stall. Unable to maintain controlled flight, the aircraft struck an electric pole before impacting a house situated in close proximity to the airport perimeter. The collision resulted in a post-crash fire that destroyed the airframe. Ten people died in the accident: eight occupants on board and two residents of the building. One crew member sustained serious injuries.

Findings

Investigations identified a structural shortcoming in the screw regulator as the root cause of the right engine overspeed event. The left engine was too heavily damaged by fire to allow for a definitive determination of its failure mode. Additionally, the inquiry concluded that the crew's response to the simultaneous loss of power on both engines was not appropriate, serving as a significant contributing factor to the outcome.

Probable cause

A structural defect in the screw regulator caused the right engine to overspeed, while an unverified issue led to left engine power loss, compounded by an inadequate crew response to the dual failure.