Ilyushin II-18

During the takeoff roll at Sochi-Adler, at a speed of 220 km/h at a distance of 1,100 meters from the runway end, the aircraft's speed fluctuated for about 2-3 seconds. The captain decided to abandon the takeoff procedure and initiated an emergency braking maneuver. The airplane's speed increased to 250 km/h until the reverse thrust activated. Unable to stop within the remaining distance, the aircraft overran, lost its undercarriage and eventually collided with trees. 15 occupants, among them five crew members, were injured. The aircraft was written off.

The airplane was dispatched from Berlin to Luanda to transfer a load of weapons and ammunitions to the ZAPU (Zimbabwe African People's Union) militants based in Lusaka, Rhodesia. The cargo arrived from East Germany by boat and was transferred to the airplane. During the takeoff roll on runway 23, at a speed of 268 km/h, the engine n°2 failed. The captain decided to abandon the takeoff procedure and initiated an emergency braking maneuver. Unable to stop within the remaining distance, the aircraft overran, collided with the localizer antenna and crashed in flames. The aircraft was totally destroyed and all 10 occupants were killed.
Crew:
Dieter Hartmann, pilot,
Jochen Wilsdorf, pilot,
Horst Umlauft, navigator,
Frank-Rolf John, flight engineer.

On final approach to Conakry-Gbessia Airport, the four engine airplane crashed in unknown circumstances in a marshfield located few km short of runway threshold. A crew member and a passenger survived while 15 other occupants were killed.

The approach to Bucharest-Otopeni Airport was completed in heavy rain falls. After landing, the crew vacated runway and was taxiing when the airplane collided with two trucks parked on the taxiway. The pilot stopped the airplane and all occupants were evacuated safely. There were no injuries but the aircraft was damaged beyond repair. It was reported that both truck drivers stopped their vehicles at an unauthorized position.

The crew was engaged in a local training flight at Bucharest-Otopeni Airport consisting of touch-and-go manoeuvres. Upon touchdown, the four engine airplane landed hard and bounced. It went out of control, veered off runway and came to rest. All five crew members escaped uninjured while the aircraft was damaged beyond repair.

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.

Suffered an accident at Shenyang Airport. There were no casualties. The mishap occurred during February 1977 (exact date unknown).

The approach and landing at Tashkent-Yuzhny Airport were completed in marginal weather conditions with strong crosswinds. After touchdown, the airplane went out of control, veered off runway and came to rest. All 8 crew and 89 passengers escaped unhurt while the aircraft was damaged beyond repair.

While descending to runway 22 at Bratislava-Ivanka-Milan Rastislav Štefánik Airport, the crew adopted a wrong approach configuration and descended with a rate of descent of 22 m/s instead of 10 m/s. This caused the airplane to be unstable while its speed varied from 435 to 225 km/h. Flaps were directly selected from zero to full down position, which caused the airplane's speed to decrease. Reverse thrust were activated on both engines n°2 and 3 below the altitude of 1,000 metres. At this time, the engine n°3 failed and in a certain confusion, the crew inadvertently feathered the propeller on engine n°4. During the last segment, about 50 metres above the runway threshold, the captain considered a missed approach and decided to initiate a go-around manoeuvre. The airplane climbed to an altitude of 40 metres and turn to the right when the engine n°4 was restarted. The airplane rolled to the right then stalled and crashed in the Zlaté piersky Lake located one km short of runway 13 threshold, northwest of the airport. Four passengers were rescued while 75 other occupants were killed. Few hours later, one of the survivor died from his injuries.

While cruising by night at an altitude of 7,800 metres, the electrical system failed, causing several instruments to fail, among them gyros. Control was lost and the airplane entered a dive and eventually crashed in a nose-down angle of 70° in an open field located 150 metres from the village of Verkhnyaya Khava, about 50 km northeast of Voronezh. Some debris of the airplane were found at a depth of 14 meters. It disintegrated on impact and all 111 occupants were killed.