Russia

While flying in poor weather conditions, the single engine aircraft went out of control and crashed near Droskovo en route from Smolensk to Voronezh. All four occupants were killed.

While parked at Vnukovo Airport, the aircraft was hit by a Rossiya Ilyushin II-96 that was taxiing to its position. The II-96 just landed at Vnukovo Airport following an official flight from Amman, carrying a delegation of the Russian Government who took part to the funerals of the King Hussein of Jordan. While taxiing by night on a snow covered taxiway, the II-96 hit with its right wing the tail of the DC-9 that was parked 28 metres to the right of the taxiway. While the II-96 was slightly damaged, the DC-9 was damaged beyond repair. There were no injuries. The DC-9 was scheduled to leave Moscow in few hours on an official flight to Rome, carrying the Italian Prime Minister Massimo D'Alema who made an official visit in Moscow.

The aircraft was withdrawn from use 2 July 1998 following a hard landing in Moscow. The mishap occurred prior to June 1998, exact date unknown. There were no casualties.

Following a poor flight preparation, the crew chose the wrong runway according to the wind component and elected to takeoff with a tailwind, and moreover with the flaps retracted. The captain started the takeoff roll from an intersection instead using all the runway length, causing the takeoff distance to be 660 metres. After a course of about 190 metres, the aircraft deviated to the right, veered off runway and came into soft ground. The crew continued to roll on a distance of 95 metres when the tail gear (tail ski) was torn off while contacting a 40 cm high earth mound. The aircraft continued, overran and came to rest 30 metres past the runway end. All 11 occupants escaped uninjured while the aircraft was damaged beyond repair.

The aircraft was completing a cargo flight from Novosibirsk to MIrny with an intermediate stop in Krasnoyarsk, carrying six passengers, seven crew members and a load of 13,380 kilos of various goods consisting of food, tobacco, clothing and footwear. Weather conditions were marginal with snow falls and icing conditions. During the takeoff roll, after a course of 2,400 metres, the pilot-in-command started the rotation at a speed of 280 km/h. After liftoff, the aircraft started to roll left and right but the crew was able to continue to climb with a rate of about 4 metres per second. During initial climb, at a height of 150 metres and at a speed of 330 km/h, the crew raised the flaps. At this time, the aircraft started to lose height, entered an uncontrolled descent, collided with trees and crashed in a wooded area located 5 km from the airport. The aircraft was totally destroyed by impact forces and a post crash fire and all 13 occupants were killed.

The aircraft departed Sibay Airport with 13 passengers and a crew of three including one inspector. Despite marginal weather conditions, the crew initiated the flight under VFR mode. After takeoff, the crew failed to follow the departure route and deviated from the published one. About half an hour into the flight, weather conditions deteriorated with low clouds. After the aircraft entered clouds, the captain decided to return to Sibay but this decision was taken too late. At this time, the aircraft was off course by 45 km to the northeast of the initial route. While making a turn to the left, still in the clouds, the crew failed to realize his altitude was too low when, at an altitude of 980 metres, the aircraft collided with trees and crashed on the slope of Mt Masim (1,040 metres high). All 16 occupants were rescued, among them three passengers were injured.

Following an uneventful flight from Dikson, the aircraft landed at Norilsk-Alykel Airport at a speed of 200 km/h. After touchdown, the crew started the braking procedure when the captain inadvertently raised the landing gear. As the gear were locked down, they remained extended but after entering the taxiway, the crew increased power and the speed reached 135 km/h when an unloading of the landing gear and a decompression of the right hand main landing gear damper occurred. This caused the right main gear to collapse slowly. The airplane went out of control, veered to the right and came to rest out of the taxiway. All 20 occupants escaped uninjured while the aircraft was damaged beyond repair.

The single engine airplane departed Togliatti on a local skydiving mission, carrying 10 skydivers and two pilots. While flying over the region of Lunacharski, all skydivers jumped out but two of them fell in the Volga River and drowned. The crew elected to take part to the SAR operations and wanted to show the location to the rescuers but descended too low over water. The aircraft stuck the water surface and crashed. Both pilots were injured and the aircraft was destroyed.

Crashed in unknown circumstances in a river bed somewhere in Yakutia. Occupant's fate unknown.

After 33,5 seconds during the takeoff roll, after a distance of 975 metres and at a speed of 210 km/h, the engine n°4 failed and its propeller automatically feathered. For unknown reasons, the crew failed to identify this failure and the pilot-in-command started the rotation (elevator -26°) at an insufficient speed of 238 km/h instead of the recommended 250 km/h. After liftoff, the aircraft started to roll to the right, causing the right wing to struck the ground two seconds after rotation. The went out of control, lost its undercarriage, slid for about 300 metres and came to rest, bursting into flames. All nine occupants escaped with various injuries and the aircraft was destroyed by fire.