No fatalities

Unauthorised Flight Crash Involving Intoxicated Pilot and Structural Failure (CCCP-L1668)

Berezhnovka, RussiaLanding (descent or approach)

On November 23, 1942, a Yakovlev AIR-6 (registration CCCP-L1668) operated by Aeroflot - Russian International Airlines was involved in an aviation accident near Berezhnovka, Russia during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The crash resulted from structural failure due to overloading during a steep turn, exacerbated by a pre-existing crack in the left front strut bolt and the pilot's intoxication. 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)Source recordUpdated 2026-08-04Data APIEditorial standards

An aircraft crashed during final approach after a steep turn caused structural failure, killing both crew members. The flight was unauthorised, and the pilot was intoxicated.

What happened

On the day of the incident, the Squadron Leader was absent. A pilot and a flight engineer departed from Berezhnovka at 0830 local time without permission to fly to Kamychyn. In addition to the crew, four passengers were on board: the spouse of the President of Kamychyn and her three children.

After landing in Kamychyn, the crew accepted an invitation from the passengers to stay at their residence. During this period, they consumed one litre of vodka over a span of two hours. At 1400 local time, the aircraft departed for the return trip to Berezhnovka.

During the final approach phase, at an altitude estimated between 200 and 300 metres, the pilot executed successive turns. While completing a left turn with a bank angle of 50 to 60 degrees, the left wing detached from the airframe. The aircraft subsequently dove into the ground and crashed. Both crew members were killed in the accident.

Findings

The official investigation identified several contributing factors leading to the destruction of the aircraft in flight. The primary mechanical issue was the overloading of aircraft components during the steep turn and subsequent recovery manoeuvre. Additionally, a pre-existing crack was found in the cross-section of the fork bolt securing the left front strut, which had extended to up to 60% of the surface area. A critical human factor was that the flight was conducted by an intoxicated pilot.

Probable cause

The crash resulted from structural failure due to overloading during a steep turn, exacerbated by a pre-existing crack in the left front strut bolt and the pilot's intoxication.