Ilyushin II-18

The crew was completing a local training flight at Frunze-Manas Airport. On final approach, both right engines n°3 & 4 were shut down to simulate a double engine failure. While at 3,500 metres from the runway threshold at a speed of 300 km/h, the crew deployed the flaps at 30° when the airplane entered an area of limited visibility (less than 1,500 metres). The captain decided to initiate a go-around and triggered both right engine. For unknown reasons, the engine n°3 failed to restart. Due to an insufficient speed, the airplane banked right to an angle of 55-60° then lost height and crashed in flames short of runway threshold. The aircraft was totally destroyed and all six crew members were killed.

On approach to Krasnoyarsk-Severny Airport, the crew encountered poor weather conditions with low visibility. On final, the four engine aircraft was too low and hit the ground 250 meters short of runway threshold. On impact, the nose gear and left main gear were torn off. The aircraft crashed, slid for several meters and came to rest with its left wing partially detached. All occupants were rescued while the aircraft was considered as damaged beyond repair.

The approach to Budapest-Ferihegy Airport runway 31L was initiated in poor weather conditions with limited visibility due to fog. On short final, the pilot-in-command elected to make a go-around when the airplane struck the ground and crashed 1,360 meters short of runway 31L threshold and 120 meters to the left of its centerline. The airplane crashed and burned and all nine crew members who were completing a ferry flight from Berlin-Schönefeld Airport were killed. At the time of the accident, the horizontal visibility was reported to be 300 meters with a 1,500 meters RVR for runway 31L. The vertical visibility was 30 meters.

The aircraft completed several rotations from Cairo to Jeddah and back on a pilgrim charter program on behalf of Egyptair. The four engine airplane departed Jeddah-King Abdulaziz Airport at 1905LT on a ferry flight to Cairo, carrying nine crew members, six technical crew from TAROM and three stewardesses from Egyptair. 10 minutes after takeoff, while climbing by night and good weather conditions, the airplane went out of control and crashed into the Red Sea about 20 km northwest of Djeddah. The aircraft was lost and all nine occupants were killed.
Crew:
Ion Mihai Vasilescu, pilot,
Răzvan Ionescu, copilot,
Constantin Duschel, navigator,
Coman Stoia, flight engineer,
Justina Constantinescu, radio operator,
Ion Popescu, flight officer + 3 stewardesses.

The airplane was engaged in a monthly schedule flight from Bamako to Saudi Arabia. En route from Bamako to Kano, ATC informed the crew about the deterioration of the weather conditions and instructed the pilots to divert to Niamey. In marginal weather conditions, the crew apparently lost his orientation and probably following a navigational error, the airplane flew to the west when the crew realized he was flying over the region of Ouagadougou, about 400 km southwest of Niamey. Shortly later, as he was short of fuel, the crew was forced to attempt an emergency landing when the airplane crashed in an open field located in Linoghin, about 40 km east of Ouagadougou. Two crew members and 11 passengers were injured while 47 other occupants were killed.

During the takeoff roll, at a speed of 230 km/h, the engine n°4 failed. The captain decided to abandon the takeoff procedure and started an emergency braking maneuver. Unable to stop within the remaining distance, the airplane overran at a speed of 100 km/h, went through a road and a ditch before coming to rest, broken in two. 20 passengers were injured, three of them seriously as they were not wearing their seat belt. Few hours later, one of them died.

On a flight from Kiev-Borispol to Ivano-Frankivsk, the crew (who never had been at Ivano-Frankivsk before) mistook in bad visibility an agricultural airstrip located 17 km from Ivano-Frankivsk International Airport and landed there. As the runway was only 500 meters long, the aircraft overran and came to rest into a ravine, broken in two. All 65 occupants escaped unhurt while the aircraft was written off.

Less than three minutes after takeoff from Leningrad-Pulkovo Airport, while in initial climb, the crew informed ATC about the failure of the engine n°4, declared an emergency and was cleared to return. About three minutes later, the engine n°4 caught fire and exploded. On final, the airplane went out of control, nosed down by an angle of 60° and crashed in a huge explosion in an open field located 2,480 meters short of runway. The aircraft disintegrated on impact and most of the debris were found 242 meters to the right of the extended centerline. None of the 109 occupants survived the crash.

While cruising by night at an altitude of 7,800 meters in good weather conditions, the pilot-in-command initiated a turn to the left when control was lost. The airplane entered a dive and spiraled to the ground. At an altitude of 5,000 meters, some elements of the upper wing surface and the stabilisers detached and the airplane disintegrated in the air before crashing in a steppe located about 84 km south of Semipalatinsk. Wings and stabilisers parts were found at a distance of some 3.5 km from the crash site. All 63 occupants have been killed.