Landing (descent or approach)

After landing at Malanje Airport, the crew encountered technical problems with the brakes. The aircraft came to rest on the runway, bursting into flames. All five crew members escaped uninjured while the aircraft was destroyed by fire.

The aircraft was returning to Kigali after an official flight from Dar es Salaam, carrying members of Rwanda and Burundi government, among them both Presidents, who took part to a congress in Tanzania and ratified the Arusha Agreements. On short final to Kigali-Grégoire Kayibanda Airport runway 28, at a height of about 100 metres, the aircraft was struck by a SAM16 surface-to-air missile and crashed in the garden of the Presidency Residence, about 500 metres from the Kanombe Camp. The wreckage was found 1,850 metres short of runway 28. The aircraft disintegrated on impact and all 12 occupants were killed.
Crew:
Jacky Héraud, pilot,
Jean-Pierre Minaberry, copilot,
Jean-Michel Perrine, flight engineer.
Passengers:
Juvénal Habyarimana, President of the Republic of Rwanda,
General Déogratias Nsabimana, Chief of Staff of the Rwanda Armed Forces,
Major Thaddée Bagaragaza, orderly officer for President Habyarimana,
Colonel Elie Sagatwa, personnel secretary of President Habyarimana,
Ambassador Juvénal Renzaho, political affairs counselor to the presidency,
Dr Emmanuel Akingeneye, personnel doctor or President Habyarimana,
Cyprien Ntaryamira, President of the Republic of Burundi,
Bernard Ciza, Minister of Communication olf Burundi,
Cyriaque Simbizi, Minister of Planning of Burundi.

While descending to Hiroshima Airport, the pilot encountered marginal weather with dark and limited visibility due to rain falls. On approach, the single engine aircraft struck the slope of Mt Noboru Lu (542 metres high) located about 15 from the airport. The wreckage was found at an altitude of 450 metres and the pilot, sole on board, was killed.

Seven minutes after takeoff from Seville-San Pablo Airport, while climbing, the crew reported technical problems and elected to return. Few minutes later, the situation worsened, the crew declared an emergency and started a rapid descent. The aircraft landed on runway 27 at an excessive speed. Upon touchdown, the right main gear collapsed. The aircraft rolled for about 2 km then veered off runway to the right and came to rest. All 10 occupants escaped uninjured while the aircraft was damaged beyond repair.

After take off from runway 24, the aircraft followed a VALKO departure as cleared by Air Traffic Control (ATC) . During climb, passing flight level 165 (FL165), the Master Warning was triggered by the right engine oil pressure Central Warning Panel (CWP) light. The Captain slowly retarded the right hand power lever to flight idle and called for the emergency checklist. After completion of the emergency checklist procedure, the right hand engine oil pressure CWP light was still on and the Captain decided to return to Amsterdam . The right hand engine remained in flight idle during the remainder of the flight. While returning to Amsterdam, the flight was radar vectored by ATC for an Instrument Landing System (ILS) approach on runway 06 . After passing approximately 200 feet height, the aircraft became displaced to the right of the runway and a go around was initiated. During the go around, control of the aircraft was lost and, at 12 :46 UTC, the aircraft hit the ground, in a slight nose low attitude with approximately 80° bank to the right, approximately 560 meters right from the runway 06 centerline, just outside the airport. Two passengers and the Captain died in the accident; eight passengers and the First Officer (FO) were seriously injured.

En route from Los Roques to Caracas, the crew encountered engine problems and declared an emergency. He was cleared to divert to Caracas-Maiquetía-Simón Bolívar Airport. Upon landing, the crew encountered strong cross winds and the twin engine aircraft went out of control and crashed in a drainage ditch located 45 metres from the runway. Both pilots were injured and the aircraft was destroyed.

While on a visual approach to Arthur's Town Airport by night, the twin engine aircraft went out of control and crashed short of runway, bursting into flames. Both occupants were seriously injured and the aircraft was destroyed.

The crew was completing a positioning flight from Veracruz. After touchdown, the crew encountered difficulties to stop the aircraft within the remaining distance (runway 13/31 is 1,300 metres long). It overran and eventually crashed past the runway end. The aircraft was destroyed and both pilots were killed.

On final approach to Vigo Airport runway 20, the crew encountered foggy conditions with a visibility limited to 1,500 metres. The aircraft descended below the glide and the left main gear struck an element of the approach light system located 100 metres short of runway threshold. The aircraft then landed 50 metres short of runway, causing both main landing gear to collapse. The aircraft slid on its belly for about 580 metres before coming to rest, bursting into flames. All 116 occupants were rescued, among them 21 were injured. The aircraft was destroyed.

The pilots flew to Lawrence, MA to refuel for the return flight back to the west coast. They stated the fuel truck malfunctioned and stopped after it had pumped about 221 gallons into the airplane. They were warned about possible fuel contamination, but they reported sump samples did not reveal abnormal amounts of water. The pilots observed erroneous fuel totalizer indications during the low alt flight to Burlington, VT, where they topped off with fuel. The flight crew stated while in cruise flight at FL410, the left engine low fuel pressure light illuminated. Sometime later, the left engine lost power, followed by a loss of power in the right engine. Numerous restart attempts on both engines and the apu were unsuccessful. The pilots maneuvered towards the nearest airport, but were unable to visually identify the runway in time to land on it. The airplane touched down in a field, striking an irrigation structure and trees. Water-contaminated fuel was found in the fuel tanks, fuel filters, and throughout the fuel system.