Aeroflot - Russian International Airlines

The crew was engaged in a training flight out from Novosibirsk-Severny Airport. En route, while in cruising altitude, the crew simulated a failure of the left engine and gave maximum right rudder, leading to an aerodynamic overbalancing and resulting to a side-slip (it was impossible to return the rudder to the neutral position in this situation). The aircraft went out of control, entered a dive and crashed in a snow-covered swampy bush land located near the village of Penyok, some 91 km of the Novosibirsk-Tolmachevo Airport. All six crew members were killed.

On approach to Zhdanov Airport, while descending between the outer marker and the inner marker, the pilot-in-command decided to continue under VFR mode while the SP-50 ILS system was not yet activated. While approaching the inner marker, the three engine airplane entered an area of fog when visual contact was lost. At an insufficient height, the airplane struck a 9-meter high concrete pole with its right wing that was partially torn off. The aircraft caught fire, rolled to the right at an angle of 90° then crashed 420 meters further. The wreckage was found 610 meters short of runway threshold and 140 meters to the right of its extended centerline. Three crew members and five passengers were killed while 20 other occupants were injured. The aircraft was destroyed.

A group of seven PZL-Mielec AN-2 must be transferred from Urgench, Uzbekistan, to Myashkovo, with intermediate stops in Uralsk and Penza, carrying mechanics and crew members. En route from Uralsk to Penza, while cruising at an altitude of 500 meters, both aircraft registered CCCP-28938 and CCCP-32112 entered a cloudy area with light rain. They collided then entered a dive and crashed in flames 350 meters further, 25 meters from each other. Both aircraft were totally destroyed and all 10 occupants were killed.

A group of seven PZL-Mielec AN-2 must be transferred from Urgench, Uzbekistan, to Myashkovo, with intermediate stops in Uralsk and Penza, carrying mechanics and crew members. En route from Uralsk to Penza, while cruising at an altitude of 500 meters, both aircraft registered CCCP-28938 and CCCP-32112 entered a cloudy area with light rain. They collided then entered a dive and crashed in flames 350 meters further, 25 meters from each other. Both aircraft were totally destroyed and all 10 occupants were killed.

The single engine airplane departed Ust-Kulom Airport at 1228LT bound for Syktyvkar with seven passengers and a crew of two on board, accompanied by a second Aeroflot AN-2 (CCCP-98382) that left at the same time. En route, weather conditions worsened and both crew lost visual contact with each other. Approaching Syktyvkar, the crew was informed about the deterioration of the weather with a limited visibility of 1,500 - 2,500 meters in snow. Few radios communications issues occurred and while descending at a height of 150 meters and making a right turn, the pilot saw the second AN-2 and made a sharp turn to avoid collision when control was lost. The airplane crashed on the icy Vychegda River, about 13 km from the Syktyvkar main Station. While the aircraft was destroyed, all nine occupants were injured. About four days later, one of the passengers died from his injuries.

After several spraying missions on behalf of the sovkhoz of Kizil-Kum, the crew made an unauthorized landing in a field and stop for few minutes to smoke cigarettes with locals. After takeoff, the airplane continued at low height, between 5 and 7 meters, then climbed to about 70 meters when it reached a super critical angle of attack. It stalled and crashed by an angle of 70°. The aircraft was destroyed and both pilots were killed.

In the morning, the crew completed two flights in the area. Due to engine problems, a technician was asked to make some engine test run. While the aircraft was parked on the ground, a technician proceeded to an engine test but forgot to install chocks on wheels. After the engine was started, power was added. The pilot who was standing by the door fell out of the plane that started to roll. After takeoff, the airplane climbed to a height of 12 meters, made a sharp turn to the left, stalled and crashed upside down. The technician, sole on board, was killed. It was determined that when the airplane started to roll quite roughly, the technician fell down from the pilot seat. Then, after liftoff, the cargo shifted to the rear of the cabin, causing the aircraft to stall.

On final approach to Mineralnye Vody Airport by night, the crew encountered poor weather conditions. At a speed of 290 km/h, flaps were deployed at an angle of 30°, causing the airspeed to drop to 260 km/h. At a distance of 1,500 metres from the runway threshold, the captain decided to initiate a go-around as he was unable to establish a visual contact with the runway. During initial climb, at an altitude of about 90 metres, the airplane entered a right turn then rolled to the right at an angle of 15-30° and adopted a critical angle of attack of 15-18°. The tail stall and the airplane crashed in flames 2 km south of the airport. A crew member and 76 passengers were killed while 21 other occupants were injured. The aircraft was destroyed.

While cruising in marginal weather conditions with limited visibility due to fog and snow showers, the crew encountered technical problems with the engine. The attempted an emergency landing but lost control of the airplane that crashed in a snow covered field located in the region of Jizzakh. All three occupants were rescued while the aircraft was damaged beyond repair.

On final approach to Almaty Airport runway 23, while at an altitude of 400 metres, the left engine caught fire. An explosion occurred and the airplane descended at a speed of 150-190 km/h and crashed in flames in a snow covered field located 3,280 metres short of runway threshold. The aircraft was destroyed and all 90 occupants were killed.