No fatalities

2001-01-27: Antonov AN-70 (UR-NTK) — Antonov Design Bureau — Omsk-Intl, Russia

Omsk-Intl, RussiaTakeoff (climb)

On January 27, 2001, an Antonov AN-70 (registration UR-NTK) operated by Antonov Design Bureau was involved in an aviation accident near Omsk-Intl, Russia during takeoff. No fatalities were reported. Investigators recorded the probable cause as: The loss of power on engine n°3 was the result of the rupture of a hydraulic line located near the rotor. This failure caused a reduction of the blades' rotation on both propellers (counter-rotating system), creating severe vibrations. 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)Primary reportUpdated 1781202929Data APIEditorial standards
Aircraft registered UR-NTK
Aircraft registered UR-NTK. Photo: Marianivka at English Wikipedia / CC BY-SA 3.0, via Wikimedia Commons

During a certification test flight from Omsk to Yakutsk, an aircraft lost power on engine #3 during initial climb, followed by failure of engine #1. The crew executed an emergency belly landing in snow-covered terrain. All 33 occupants were rescued; four suffered injuries, two serious.

Incident Overview

A test flight departed Omsk Airport bound for Yakutsk, carrying 22 passengers and a crew of 11. The flight was part of a certification program to evaluate the aircraft in low-temperature conditions.

Sequence of Events

During the initial climb, at a height of 20 metres, engine number 3 lost power. The crew responded by increasing power on the remaining three engines and continued ascent. Less than 25 seconds later, at an altitude of approximately 60 metres, engine number 1 failed.

The captain initiated an emergency landing, touching down on snow-covered terrain 660 metres beyond the runway end. The aircraft performed a belly landing, resulting in severe damage to the fuselage—which nearly separated at the wing section—and to all engines.

Rescue and Injuries

All 33 individuals on board were evacuated. Four people sustained injuries, with two classified as serious.

Probable Cause

According to the official investigation, the loss of power on engine number 3 was caused by a ruptured hydraulic line near the rotor. This failure reduced blade rotation on both propellers (a counter-rotating system), inducing severe vibrations. The crew's subsequent power increase on the three remaining engines coincided with a technical malfunction in an electric sensor coupled to the turbine of engine number 1. This malfunction caused the automatic control unit to fail, leading to the shutdown of engine number 1.