7 fatalities

Test Flight Accident Involving Antonov AN-8RU (CCCP-55517)

Kiev-Gostomel, UkraineTakeoff (climb)

On September 16, 1964, an Antonov AN-8 (registration CCCP-55517) operated by Antonov Industries was involved in an aviation accident near Kiev-Gostomel, Ukraine during takeoff. 7 people were killed. Investigators recorded the probable cause as: The exact cause of the accident could not be determined with certainty. However, the crew encountered difficulties, was unable to and/or forgot to feather the propeller on the left engine. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 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

During a test flight of an Antonov AN-8RU at Kiev-Gostomel Airport, the left engine was shut down but the propeller could not be feathered, leading to loss of control and crash. All seven crew members died.

Incident Overview

On a local test flight at Kiev-Gostomel Airport, the crew—comprising pilots, technicians, and engineers—were conducting a mission to test the JATO propulsion system for the Antonov AN-8, which had been renamed the AN-8RU version for this program. Twenty seconds after takeoff, while climbing to a speed of 220 km/h, the JATO system was ignited. Six seconds later, once the speed reached 264 km/h, the left engine was voluntarily shut down. At this time, the crew was unable to feather the propeller, which went into auto-rotation.

Sequence of Events

The aircraft banked left to a 70–80° angle, then dove into the ground and crashed in a field located 1,850 meters past the runway end. The aircraft was totally destroyed. All seven crew members were killed.

Official Findings

The probable cause, as determined by the official investigation, states: The exact cause of the accident could not be determined with certainty. However, the crew encountered difficulties, was unable to and/or forgot to feather the propeller on the left engine. This caused asymmetric thrust and high drag, which made the aircraft uncontrollable and led to the crash.