2 fatalities

Aircraft Accident During Approach to Krenkel Airstrip (CCCP-04188)

Krenkel (Heiss Island), RussiaLanding (descent or approach)

On February 12, 1981, an Ilyushin II-14 (registration CCCP-04188) operated by Aeroflot - Russian International Airlines was involved in an aviation accident near Krenkel (Heiss Island), Russia during landing or approach. 2 people were killed. Investigators recorded the probable cause as: The approach configuration was wrong and that the pilot-in-command failed to react to the copilot calls. At the time of the accident, the total weight of the aircraft was 700 kilos above max gross weight. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-12Data APIEditorial standards

During dusk approach, the crew lost visual contact with runway lighting twice and continued, touching down in deep snow 32 m left of runway. Nose gear collapsed, fuel tanks broke loose, killing two passengers and injuring 11 others. The aircraft was destroyed.

Flight and Circumstances

The aircraft was completing a flight from Myachkovo to the Krenkel Airstrip on Heiss Island in the Franz-Joseph Land archipelago, Arkhangelsk oblast. The flight included intermediate stops at Vorkuta and Dikson. On board were six crew members and seven passengers described as scientists, along with various equipment for a scientific team based at Krenkel.

Approach and Accident

During the approach in dusk conditions, the crew twice lost visual contact with the runway lighting. Despite this, the pilot-in-command decided to continue the approach rather than initiate a go-around. The airplane touched down in deep snow approximately one meter deep, about 32 meters to the left of the runway. On impact, the nose gear collapsed, damaging the lower part of the nose. The long-range fuel tanks in the cabin broke away from their mountings and struck two passengers, killing them. The remaining 11 occupants sustained injuries. The aircraft was damaged beyond repair.

Probable Cause

The official investigation determined that the approach configuration was incorrect and that the pilot-in-command failed to react to calls from the copilot. At the time of the accident, the total weight of the aircraft was 700 kilograms above the maximum gross weight. At takeoff, the total weight exceeded the maximum takeoff weight by 1,650 kilograms.