Africa

On approach to Cafunfo Airport, the encountered strong crosswinds. On short final, the aircraft was too low and struck the ground short of runway threshold. On impact, the undercarriage were torn off. The aircraft slid on its belly for few dozen metres then lost its empennage and left wing before coming to rest. All 15 occupants escaped uninjured.

Following an uneventful flight from Mogadishu, the crew started the descent to Djibouti City-Ambouli Airport. While the runway 09 was in use, the crew was cleared for an approach to runway 27. While completing a last turn to the left to join the glide, the aircraft went out of control and crashed in the sea. All four occupants were killed.

The aircraft was completing a charter flight from Khartoum to Heglig on behalf of an oil company, carrying 12 passengers and four crew members. On final approach in good weather conditions, the aircraft was too low and struck the ground short of runway 34 threshold. The aircraft bounced then landed hard, causing the undercarriage to be torn off. The aircraft slid on its belly, veered off runway and came to rest in bushes. Al 16 occupants evacuated safely while the aircraft was damaged beyond repair. Wind was gusting to 23 knots at the time of the accident.

Shortly after takeoff from Mbuji-Mayi Airport, while climbing, the engine n°1 caught fire. The flight engineer elected to extinguish the fire but without success. The aircraft lost height then rolled to the left to an angle of 85°. The crew extended the flaps to 45° to maintain a rate of descent of 700 feet per minute but due to an asymmetric flap condition, the rate of descent increased to 1,500 feet per minute. After the aircraft rolled to the left to an angle of 110°, at a speed of 98 knots, the captain attempted an emergency landing when the aircraft crash landed in a prairie. All 23 occupants were injured and the aircraft was destroyed.

While descending to Monrovia-Roberts Airport, the crew informed ATC about technical problems. The captain realized he could not reach the airport and attempted an emergency landing in an open field located about 11 km from the airfield. On impact, the aircraft lost its undercarriage and slid for few dozen metres before coming to rest. A crew member was killed while nine other occupants were rescued.

The aircraft was parked on the international departures apron at FALA, ready for a flight from FALA to Blantyre. The pilot assumed that the engineer had pressurised the hydraulic accumulator and therefore did not inspect it himself. When the passengers arrived, the pilot got in the aircraft and began the internal pre-start checks. The co-pilot removed the chocks after boarding the passengers, closed the door and then started to brief the passengers. At that moment the pilot noticed that the aircraft was rolling forward. Attempts to stop the aircraft were unsuccessful, the aircraft rolled forward, narrowly missed a hangar and a parked Bell Long-ranger helicopter next to the hangar, crossed the taxiway and finally stopped when entering a ditch between the taxiway and the runway. The pilot was the holder of a valid transport pilot’s licence and had the type endorsed in his licence. The operation of the hydraulic system was found to be satisfactory. The hand pump was used to pressurise the system after which the brakes could be applied successfully.

The aircraft was completing a cargo flight from Dakar to Athens with intermediate stops in Agadir and Algiers, carrying a load of fish and eight crew members. While cruising by night at an altitude of 9,900 feet in marginal weather conditions, the aircraft struck the slope of a mountain located 80 km northeast of Agadir. All eight occupants were killed.

While approaching runway 11/29 in heavy rain falls, the four engine aircraft crashed two km short of runway. Two crew members and three passengers were killed. The aircraft was completing a flight from Luanda to Luena on behalf of the Government of the State of Moxico.