1 fatality

Overweight and Out-of-Balance Cargo Aircraft Crashes After Liftoff, Passenger Dies (CCCP-09679)

Krasnodar, RussiaTakeoff (climb)

On May 5, 1989, a PZL-Mielec AN-2 (registration CCCP-09679) operated by Aeroflot - Russian International Airlines was involved in an aviation accident near Krasnodar, Russia during takeoff. One person was killed. Investigators recorded the probable cause as: The crew failed to prepare the flight according to procedures and boxes were not properly weighted. Due to a misevaluation of the box weight, the crew allowed a too high number of boxes to be stored in the cargo compartment. 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 2026-06-11Data APIEditorial standards

A single-engine cargo aircraft carrying bees crashed after liftoff due to overweight and aft center of gravity. The four occupants were injured, and a passenger died hours later.

Accident Details

A single-engine aircraft, engaged in a cargo flight from Krasnodar to Sterlitamak with intermediate stops in Volgograd and Uralsk, crashed shortly after liftoff. The aircraft carried two pilots, two passengers (beekeepers), and a load of boxes containing thousands of bees. Immediately after liftoff, at a height of approximately 1.5 meters, the aircraft's speed dropped and the tail stalled, striking the runway surface. The aircraft then flew or rolled out of control for several hundred meters before crashing 420 meters past the runway end.

Injuries and Damage

All four occupants sustained injuries. A passenger died from his injuries a few hours after the accident. The aircraft was damaged beyond repair.

Probable Cause

The official investigation determined that the crew failed to prepare the flight according to procedures and that the boxes were not properly weighed. Due to a misevaluation of the box weight, the crew allowed an excessive number of boxes to be stored in the cargo compartment. At the time of the accident, the total weight of the aircraft was 6,081 kilograms, which is 831 kilograms above the maximum allowable takeoff weight. Additionally, the center of gravity (CofG) was 40.8% over the aft limit. In such conditions, the aircraft could not be flown safely.