Landing (descent or approach)

The pilot and copilot reported in their written statements that the airplane was above glideslope on the final approach. They said the airplane touched down about 1,500 feet from the approach end of the 4,700 feet long runway. The pilot said he applied the brakes but could not stop the airplane on the runway. The airplane departed the end of the runway and continued forward over rough and uneven terrain. The main landing gear sheared off and penetrated both wings. The airplane came to a stop in a gully. Other witnesses located on the ground and in the air traffic control tower reported the airplane was 'high and fast' and touched down at about midfield or after.

The wreckage was located on the northeast side of halfway mountain heading approximately 270° at the 1,600 foot level. The accident site is located within two miles of the initial approach fix for the localizer/dme runway 16 approach at McGrath. The mea for the dme arc is listed as 3,600 feet above mean sea level. The sector obstruction clearance altitude is listed as 3,100 feet above mean sea level. Weather for the area, airmet sierra, indicated that mountain tops would be obscured and that ceilings would occasionally be 1,500 feet broken. There were reports of snow showers in the area of sufficient intensity that would not allow the search aircraft to fly through the snow showers. The pilot, sole on board, was killed.

The approach to Bucharest-Otopeni Airport was completed in poor weather conditions with a visibility reduced to 100 metres in fog. The aircraft landed slightly to the right of the runway 26L centerline, causing the right wing to struck a 60 cm high snow wall. The aircraft went out of control and eventually collided with an observation tower. All 10 occupants escaped uninjured while the aircraft was damaged beyond repair.

While descending to Warsaw-Okecie Airport, the crew encountered poor weather conditions with thunderstorm activity. On final approach, the copilot suggested the captain to abandon the landing procedure and to initiate a go-around maneuver. The captain dismissed the copilot's suggestion, disengaged the autopilot system and continued the approach when visual contact with the ground was established at an altitude of 400 feet. In a nose-down attitude and at an excessive speed of 155 knots (about 25-30 knots above the recommended speed), the aircraft struck the runway 33 surface nose gear first. The aircraft bounced then veered off runway to the left, rolled on soft ground for about 860 metres and lost its nose gear before coming to rest. All 96 occupants were evacuated, among them three passengers were slightly injured. The aircraft was damaged beyond repair.

The crew (one pilot and one instructor) was completing a local training flight at Suva Airport. On approach, the crew failed to lower the landing gear, causing the aircraft to land on its belly. It slid on the runway for few dozen metres before coming to rest. Both pilots escaped uninjured while the aircraft was damaged beyond repair.

The twin engine aircraft was ferried from Medellín to Bogotá after repairs were conducted at Medellín Airport following a gear problems last September 23. On approach to Bogotá-El Dorado Airport, the aircraft struck the slope of a mountain located 20 km north of the airport. All eight occupants were killed.

The crew departed Luxeuil-Saint Sauveur AFB on a training flight to Vélizy-Villacoublay AFB on behalf of the 'Système de Navigation d’Attaque' (SNA). On approach, both engines lost power and the crew elected to divert to Toussus-le-Noble Airport for an emergency landing. The captain eventually attempted to land on a sports field when the aircraft struck a concrete wall and crashed, bursting into flames. The wreckage was found in Élancourt, about 17 km west of Vélizy-Villacoublay AFB. The aircraft christened 'Étoile du Berger' was destroyed and all four crew members were killed.
Crew:
Cdt Jean-Luc Luciani,
Cpt Christian Huth,
Cpt Pierre Schmitt,
Lt Philippe Hirson.

The twin engine airplane departed Brasília at 0600LT on a flight to Guaratinguetá, carrying high ranking officers who should take part to a military parade. On approach to Guaratinguetá Airport, the crew encountered marginal weather conditions when the aircraft struck the slope of Mt Pico dos Marins located 33 km northeast of the airport. The aircraft was destroyed by impact forces and all 16 occupants were killed.

On final approach to Parma Airport, the aircraft struck the ground and crashed 400 metres short of runway. Both pilots were injured and the aircraft was damaged beyond repair. At the time of the accident, the visibility was below minimums and the aircraft descended below the MDA until ground impact.

The aircraft departed Nizhnevartovsk on a charter flight to Bugulma, carrying four crew members and 37 employees from an oil company. Weather conditions in Bugulma were poor with clouds down to 80 metres, icing conditions and a visibility of 800 metres. At an altitude of 1,100 metres on approach, the crew encountered icing conditions but did not consider it necessary to activate the deicing systems. Still descending to the altitude of 900 metres, the icing alarm sounded in the cockpit but the captain decided to continue the approach in such configuration. After the crew selected the flaps down to an angle of 30°, he was cleared to land when the aircraft became unstable and departed the approach path to the right. After the aircraft crossed the permissible deviation limit, the crew was instructed by ATC to initiate a go-around procedure. The captain increased engine power and initiated a go-around maneuver when the aircraft adopted a high angle of attack then stalled and pitched down to an angle of 75-80°. At a speed of 260 km/h, the aircraft struck the ground 802 metres short of runway and was destroyed upon impact. The wreckage was found 598 metres to the right of the extended runway centerline and all 41 occupants were killed.