Salta

The twin engine aircraft departed Asunción on a charter flight to Salta with intermediate stops in Resistencia and Joaquín Víctor González, carrying 10 passengers and two pilots. On approach to Salta-Martín Miguel de Güemes Airport, both engines failed. The crew attempted an emergency landing but the aircraft struck trees and crashed in an open field located 3 km short of runway. All 12 occupants evacuated safely while the aircraft was damaged beyond repair.

The aircraft was completing a cargo flight from Córdoba to Salta with an intermediate stop in San Miguel de Tucumán, carrying two passengers and two pilots. The crew departed San Miguel de Tucumán-Teniente Benjamin Matienzo Airport at 2145LT and was cleared to climb to FL180. At 2201LT, the crew reported over PONPI VOR located 55 nm from Salta. Two minutes later, the crew was cleared to descent on top of the clouds in VMC conditions. While cruising at an altitude of 6,970 feet, the aircraft struck the slope of Mt Chivilme located 36,4 km southwest of Salta Airport. The aircraft was destroyed by impact forces and all four occupants were killed.

While approaching Salta Airport, the single engine aircraft crashed in unknown circumstances near Vaqueros, about 20 km north of the airport. All four occupants were killed.

On approach to Salta-Martin Miguel de Güemes Airport, the crew encountered stormy weather. In limited visibility, they failed to realize their altitude was insufficient when the aircraft struck the slope of a mountain and crashed few km from the airport. All seven occupants were killed. At the time of the accident, the visibility dropped below minimums.

The crew was completing a flight from Santiago del Estero to Salta-El Aybal Airport. After touchdown, the airplane went out of control, veered off runway and came to rest. There were no injuries among the four crew members but the aircraft was considered as damaged beyond repair. It is reported that sudden gust of crosswinds affected flight control after touchdown.

Crashed in unknown circumstances at Salta. No injuries.

While cruising at an altitude of 18,000 feet, the twin engine aircraft struck the slope of Mt Ingamayo. The wreckage was found few hours later in rocky terrain and both crew members were killed. It is believed the accident was the consequence of a controlled flight into terrain.

The aircraft was on a delivery flight from Mexico City to Asunción, Paraguay, with intermediate stops at Antofagasta, Chile and Salta, Argentina. At 1245LT the aircraft took off from Antofagasta for Salta. It was to be a VFR flight via Chosque, Chile and San Antonio de los Cobres, Salta Province. The aircraft was seen at 1400 hours flying in a straight line at very low altitude in the direction of San Antonio de los Cobres 40 km east of Olapacato. One witness, believing that the aircraft intended to land, followed it in a jeep only to find its burned wreckage some 20 km away. It had crashed into the side of a hill rising north of Rio Tocomar, approximately 70 metres above the river bed. The height above sea level at this point is approximately 4,500 metres. One eye witness stated that the aircraft crashed in rectilinear horizontal flight into the northern slope of the hill and that the pilot had not taken any avoiding action. The pilot, the sole occupant, was killed, and the aircraft was destroyed by the crash and the fire which followed.

The aircraft left Santa Cruz de la Sierra (Bolivia) on a scheduled airline flight and landed without incident at Salta 2 hours and 30 minutes later. It took off from Salta airport for Córdoba at approximately 1645LT. At take-off the aircraft was carrying a total load of 3,512 kg. The route forecast as far as Marcos Juarez was as follows: partly cloudy, visibility 15 km, stratocumulus cloud 7/8 at 800 meters, altocumulus 3/8 at 3'000 meters, upper wind 20' 13/15 knots. The aircraft contacted Córdoba Airport control tower at 1856LT and was cleared to enter the airport zone. At 1925LT it passed over the radio beacon and the control tower provided the following weather information: horizontal visibility 6 km, average height of cloud 250 meters, pressure for altimeter correction 30 inches, surface wind SE, 10 to 11 knots. The approach to the airport was begun under IFR conditions, at an indicated speed of mph and at an altitude of 5, 100 feet above the radio range (the requirement is 4,400 feet). aircraft flew a course to the north for 1 minute 50 seconds, with 15° flaps and then, continuing the descent, it turned to the right on a 45° course, flying in this direction for 1 minute more. The altitude just before the turn was 3, 100 feet. It then turned to the left on a course of 225°. When the aircraft direction finder indicated 40° to the left, the compass was set at 180° and the direction finder maintained at O°. At that moment, according to the evidence, the instruments indicated an altitude of 2, 980 feet. The aircraft flew at this altitude for 30 seconds, and the engine speed was reduced for landing. It continued to descend for another minute 20 seconds until the altimeter indicated 2, 200 feet. At that instant, according to the statements made by the pilot-in-command and the copilot, the aircraft came into contact with the ground. The aircraft was finishing the final straight-in approach to the airport and was aligned exactly with runway 17. All 41 occupants were evacuated safely, only both pilots were slightly injured. The aircraft was destroyed.

En route, the crew encountered unknown technical problems and the captain elected to make an emergency landing when the aircraft hit a tree and crashed on a hilly terrain. Three crew members and three passengers were killed while three other occupants were injured.