Airport (less than 10 km from airport)

The crew was completing a local training flight at Khartoum-Haj Yusuf Airport. Following several touch-and-goes completed successfully on runway 18, the crew landed the airplane and elected to takeoff when the captain encountered difficulties to raise the flaps from 40° to 16,5°. In such conditions, he decided to reject the takeoff procedure and initiated an emergency braking manoeuvre. The aircraft skidded on runway, overran and lost its right main gear before coming to rest against the ILS antenna for runway 36. Both pilots escaped uninjured while the aircraft was damaged beyond repair.

The single engine airplane was engaged in a local skydiving flight at Namur-Temploux Airfield, carrying 10 skydivers and one pilot. Shortly after takeoff, while in initial climb, the aircraft stalled from the tail and crashed near the runway end. A passenger was killed while 10 other occupants were seriously injured. The aircraft was destroyed.

The crew was completing a local training flight at Jaipur-Sanganer Airport. After touchdown, the twin engine aircraft skidded on runway, veered off runway and came to rest. Both pilots escaped uninjured while the aircraft was damaged beyond repair.

Just after liftoff from Lovozero Airstrip, while climbing to a height of 15-20 metres, the engine lost power and white smoke escaped from the bottom of the engine. The aircraft lost height, struck an 8 metres tall tree located 191 metres past the runway end then crashed in a wooded area 58 metres further. All 12 occupants escaped uninjured while the aircraft was damaged beyond repair.

Shortly after takeoff from Breitscheid Airfield, while climbing to a height of about 10-15 metres, the single engine airplane stalled and crashed beside the runway. All nine occupants (eight skydivers and one pilot) were uninjured while the aircraft was damaged beyond repair.

The twin-tubofan airplane overran the runway during an aborted takeoff, impacting two fences before coming to rest. The pilot reported experiencing no anomalies with the airplane during the preflight inspection and taxi portion of the flight. During takeoff roll, at V1 (103 knots), the pilot began to pull aft on the control yoke. The pilot noticed the nose landing gear was not coming off of the runway and at 120 knots, with full aft control input, elected to abort the takeoff. He pulled the power to idle and applied maximum braking. Upon seeing the localizer antennas approaching the airplane at the departure end of the runway, the pilot veered the airplane to the right of centerline. The airplane departed the runway surface and impacted the fences. Post-accident examination of the runway revealed tire skid marks on the runway that led to the airplane's final resting place. The tire skid marks measured 1,765 feet in length. Examination of the wreckage revealed no pre-existing brake system anomalies that would have hindered the airplane's braking capability. Examination of the elevator trim system revealed it was 12 degrees out of trim in the nose down direction. The airplane underwent a Phase B and Phase 1 through 5 inspections approximately 5 months prior to the accident. The manufacturer's inspection manual indicates the elevator system should be examined every Phase 5 inspection. The aircraft's flight manual informs the pilot that the right elevator and trim tab should be inspected during the exterior inspection to ensure the elevator trim tab position matches its indicator.

The single engine aircraft was completing an aerial photography flight from Clermont-Ferrand, carrying one passenger and one pilot. On final approach to Moulins-Montbeugny Airport runway 08, at a speed of 85 knots, the pilot estimated that the nose-up attitude of the aircraft was excessive and increased engine power. The aircraft rolled to the left, causing the left wing tip to struck the runway surface. Out of control, the aircraft impacted the ground, lost its undercarriage and slid fo 95 metres before coming to rest, bursting into flames. Both occupants escaped uninjured and fire brigade arrived 15 minutes later. The aircraft was destroyed by fire.

The aircraft departed Cairo-Intl Airport at 1140LT on a regular schedule flight to Tunis-Carthage Airport with 56 passengers and six crew members on board. It entered the Tunis FIR at 1450LT, under control of the Tunis Regional CCR. After being transferred to the approach control at 1500LT, the crew was cleared for a VOR/DME approach to runway 11. On approach at 3,000 feet, the crew was informed he was number one for landing. The crew informed ATC that he departed 3,000 feet for 2,100 feet at 12 NM and wa later cleared to land. Wind was from 130 at 30 knots. At 1516LT, on final, the crew was transferred from the approach control to the tower and received a second clearance to land. In limited visibility, the aircraft struck a fence located on the top of a mountain and crashed in hilly terrain 6,6 km from the runway 11 threshold. Three crew members and 11 passengers were killed while 48 other people were injured. On board were 33 Egyptians including the six crew members, 16 Tunisians, three Algerians, three Jordans, two Chinese, two British, one Libyan, one Saudi and one Palestinian.

After a visual approach to the 3,975 foot long by 50-foot wide runway, the turbojet airplane touched down about 2,100 feet beyond the landing threshold, and overran the departure end of the runway. The 5,600 hour pilot in command (PIC) reported that the approach speed and descent rate were "normal," and the aircraft was on short final over the trees at the "desired speed." Once the trees were clear, the aircraft descended to the runway at idle power. During the descent the PIC noticed a 16-knot increase in speed above reference. The PIC elected to continue "because the aircraft was close to the runway" and the PIC thought he had "extra landing distance to work with beyond what was required." The PIC reported that the aircraft "floated beyond the desired touchdown point," and "at this point [the pilots were] committed to stopping the aircraft." Passing the last third of the runway, the aircraft turned to the right "without" input from the pilots, overran the departure end, and collided with trees. Once the aircraft left the runway, the PIC stowed the thrust reversers and attempted to shut down the engines. Due to the "violent ride," the PIC managed to shut down one engine. A post-impact fire consumed the aircraft after the crew assisted to evacuate the occupants. No mechanical or maintenance anomalies were discovered with the aircraft. According to the flight manual, based on 29.74 inches HG, 1,808 PA, 30 degrees Celsius, zero wind, and an aircraft landing weight of 14, 500 lbs, the calculated total stopping distance (air and ground distance) at reference speed (Vref), was estimated at 2,955 feet. According to the flight manual, the "total distance" is based on full flaps, speed brakes after touchdown, Vref at 50 feet over the runway threshold, idle thrust when crossing the threshold, and no thrust reverse.

The airplane impacted the terrain following a loss of control during a takeoff initial climb. A witness stated the airplane was noisier than what he is used to hearing. This witness reported the airplane was in a steep left bank in a level pitch attitude. The airplane then began to descent rapidly as it turned to a northerly heading. The witness reported the airplane then seemed to enter a right bank prior to impacting the ground. Another witness reported what sounded like an engine backfire. The pilot reported the airplane lost power. Torsional twisting was visible on the propeller blades following the accident. Following the accident, the undamaged emergency exit from the airplane was found next to the runway. The latching mechanism on the exit was not damaged and the pins were not found with the exit. It was reported that the airplane had sat on the ramp at the departure airport for at least 15 years without being flown. Although the registration for the airplane had not been changed, the pilot reportedly purchased it shortly before the accident. The pilot did not hold a multi-engine rating.