Khartoum

The aircraft was cleared for takeoff and began its departure roll with flaps retracted, according to flight data recorder. The aircraft rotated at 280 kph (151 knots) and became airborne at 288 kph (155 knots) at an angle of attack of about 8-9 degrees. Tyre marks on the runway showed, that the aircraft had gone past the end of the runway, the main tyres had impacted runway end lights and the tyre tracks continued past the paved surface of the stopway. Climbing through 15 feet the pilot flying commanded the gear up and increased the pitch angle, the angle of attack increased to more than 10 degrees while the gear doors opened for gear retraction increasing the drag of the aircraft, which began to slow, the speed reduced to 305 kph (164 knots), stall speed for the takeoff weight, and the left wing began to stall, the angle of attack increased to 17 degrees, the aircraft at a height of 5-7 meters/15-23 feet. The pilot flying tried to counteract the roll to the left by fully applying left aileron which also deployed the right wing spoilers, right rudder input was provided. The pilot flying instructed the flight engineer to NOT retract flaps indicative neither pilot was aware the flaps were up. Following that instruction the flight engineer selected the flaps down, the aircraft speed was 300 kph (162 knots) and the aircraft in an unrecoverable stall with no height left. The left hand wing struck a high voltage mast about 1200 meters past the runway end at a height of 5.4 meters (18 feet) shearing off the left wing tip, contacted the flag post at the entrance of the Green Square, the left wing contacted the stem of a tree at a height of about 40 cm (1.3 feet) separating the ailerons and causing fuel spilling from the left wing, the aircraft broke through the eastern brick wall of Green Square, collided with two more electric poles causing engine #4 to separate 1504 meters from the end of the runway and impacted ground at 30 degrees nose down, 30 degrees left bank. Debris was distributed over a length of more than 500 meters, the aircraft burst into flames. All 4 crew perished in the crash, 4 people on the ground received serious, 3 more received minor injuries.

The aircraft departed Khartoum at 0555LT on a cargo flight to Juba with 8 crew members on board. While cruising at FL170 in bad weather conditions, the engines n° 1 failed. One minute later, the engine n°3 failed as well, followed 40 seconds later by the failure of the engine n°4. The aircraft initiated a descent with a rate of 3,450 feet per minute and reach the altitude of 800 feet three minutes and 40 seconds after the failure of the engine n°1. At an altitude of 600 feet, the crew stabilized the aircraft and elected to restart the three engines but without success. Too low, the aircraft struck trees, lost its left stabilizer and crashed in a prairie 264 metres past the initial impact, bursting into flames. A crew member was rescued while 7 other occupants were killed.

The Airbus 310 serial number 548 owned by Sudan Airways Was entered in Sudan Civil Register on 15/09/2007 , designated registration marks ST-ATN in accordance to registration certificate No. 0493 dated 15/09/2007 and issued with Certificate of airworthiness No AWP/COA/0203/2007 dated 19/09/2007. On the morning of 10th June at 8:30 hrs (local time 05:30 UTC) after arriving from Cairo with a deactivated no 1 engine reverse as being a carry forward defect and being labeled according to MEL, the captain accepted the aircraft to carry out its scheduled flight to Amman via Damascus. The trip en-route to Amman was uneventful. Same day in the afternoon, the Airbus A310, ST-ATN, was en-route flying from Damascus (Syria) to Khartoum (Sudan) with 203 passengers and 11 crew members on board. The Airbus approached Khartoum in the afternoon and due to bad weather conditions, the captain decided to divert to Port Sudan. The aircraft landed Port Sudan Airport normally and was refuelled with 20 tons of Jet A1. As mentioned by the Captain that he was in contact with Khartoum enquiring about the weather. After staying on ground at Port Sudan for about 1:15 hour, and being informed that the weather was getting better, the Captain decided to return back to Khartoum. A310, ST-ATN, took off to Khartoum where the captain initiated a night approach for the runway 36 as pilot flying. He got the clearance to land after the controller provided him with wind information (320° / 7 Kt) and runway condition (wet). The left engine thrust reverser was unserviceable and inhibited as per Minimum Equipment List (MEL) procedures. The aircraft landed smoothly about 17:26 UTC. R/W 36 landing and within 900 meters range from the threshold of R/W 36 as stated by the flying pilot. The captain reported that he experienced some difficulties in maintaining the aircraft on the centre line just after setting both thrust levers in the reverse position. Then he did not succeed in slowing down the aircraft nor could stop it before the end of the runway. The aircraft longitudinally overran the runway and came to a stop 215 meters after the runway end. Then it caught fire on its right side. The right hand slides could not be deployed, the crew and the passengers evacuated the aircraft from the left front slide, twenty nine passengers and one cabin crew were fatally injured.

The four engine aircraft departed Khartoum-Haj Yusuf Airport at 0759LT on a cargo flight to Juba, carrying four crew members and a load of 11 tons of various goods. After takeoff, while climbing, the crew reported the failure of the engine n°3 and was cleared to return for an emergency landing. After touchdown, the aircraft went out of control, veered off runway and came to rest in the military area of the airport, bursting into flames. All four crew members were injured while two people on the ground were killed. The aircraft was destroyed by a post crash fire.

Owned by United Arabian Airlines, the four engine aircraft departed Khartoum on a cargo flight to Geneina on behalf of AZZA Air Transport. After touchdown, the aircraft was unable to stop within the remaining distance, overran and came to rest in a sandy area. There were no injuries but the aircraft was damaged beyond repair after the undercarriage were torn off and the left wing tip was sheared off. Witnesses interviewed by the Panel stated that the majority of the passengers were military personnel. In addition to the passengers there were two D-22 type 122 mm artillery howitzers and 40 to 50 wooden boxes painted olive drab, suspected to contain arms and ammunition. The cargo was offloaded during the days following the crash under the supervision of the Sudanese Armed Forces (SAF) who continued to guard the aircraft throughout the following week. In an official report published at the end of April 2007, UNO criticized the Sudanese authorities for not respecting the various points of resolution 1591 which stipulates that Sudan is not authorized to deliver military equipment to the Darfur region.

During the takeoff roll at Khartoum-Haj Yusuf Airport, the left engine caught fire and exploded. The captain rejected takeoff and initiated an emergency braking procedure. Unable to stop within the remaining distance, the aircraft overran and came to rest few dozen metres past the runway end, bursting into flames. Three passengers were killed while all other occupants were rescued. The following day, four survivors including a stewardess, died from their injuries.

On 23 March 2005 at 0533 hours an Ilyushin IL-76 cargo jet with the Republic of Moldova registration letters ER-IBR landed at Mwanza on a flight from Benghazi, Libya. It was carrying a crew of 8 including 2 ground engineers. All the 8 crew members were later involved in the accident. While at Mwanza, some 50,000 kg of fish was uplifted. At 1930 hours the commander filed a flight plan for Khartoum. The endurance was 0450 hours. The cargo manifest showed that ER-IBR was operating Air Trans Inc. Flight RIN 982 from Mwanza to Osijek, Croatia, with refueling stops at Khartoum and Benghazi. At 2000 hours the aircraft was given information relevant for take off as well as the departure clearance. ER-IBR subsequently advised that he was starting the take-off roll. This was the last communication received from the aircraft. The aircraft was observed to execute a normal take-off roll from runway 30. This runway ends 120m short of Lake Victoria. After observing that the aircraft was airborne, the controller who was handling the flight reported that he turned to complete the flight progress strip. Having done so, he lost visual contact with the aircraft that was supposed to be in a climb profile over the lake. Efforts to raise the aircraft on the radio failed. In about two minutes from the time that the aircraft was airborne, he saw a fire tender speeding along runway 30. It was then that he realized that the flight may have crashed. The Mwanza Airport Rescue and Fire Fighting Services were not equipped for operations in the lake. They were therefore unable to reach the aircraft, which was more than 1 km away from the shore. It was the fishermen at the lake shore near Mwanza airport who saw the aircraft going down in the lake. They proceeded to the crash site in fishing boats and brought back some documents (flight manuals and wiring diagrams) which they found floating near the wreckage.

The four engine aircraft departed Sharjah Airport on a cargo flight to Nyala with an intermediate stop in Khartoum, carrying 46 tons of humanitarian aid for refugees in Darfur. On board were sisx Russian crew members and one Sudanese translator. While approaching Khartoum-Haj Yusuf Airport, the crew reported fuel issues and elected to make an emergency landing when the aircraft crashed in a desert area located 800 metres from the Ad Babkr District, about 15 km East of Khartoum. The aircraft disintegrated on impact and all seven occupants were killed.

Shortly after takeoff, while in initial climb, the aircraft collided with a flock of birds. Engines n°3 & 4 failed and the crew elected to make an emergency landing in an open field. The aircraft crash landed in a field and came to rest, bursting into flames. All five occupants were injured along with a young boy in the nearby field.

The aircraft was completing a cargo flight from Khartoum to Wau, carrying seven passengers, six crew members and a load consisting of foods and bank notes. On final approach to Wau Airport, the aircraft went out of control and crashed in an open field located 6 km short of runway, bursting into flames. All 13 occupants were killed, among them soldiers and members of the National Bank of Sudan.