Brazil

During the takeoff roll at Campo de Marte AFB runway 12, the right engine lost power. The crew decided to abandon the takeoff procedure and initiated an emergency braking manoeuvre. Unable to stop within the remaining distance, the airplane overran, struck a perimeter fence, crossed a road and came to rest. All four occupants escaped uninjured while the aircraft was damaged beyond repair.

On final approach in limited visibility due to rain falls, the pilot failed to realize his altitude was insufficient when the airplane struck trees and crashed in a wooded area located less than 2 km from the runway threshold. The aircraft was destroyed and all six occupants were killed.

Three minutes after takeoff from Rio de Janeiro-Santos Dumont Airport, while climbing, the pilot reported technical problems and elected to return when control was lost. The twin engine airplane crashed in a field near the airport and was destroyed. All three occupants, one pilot and two engineers, were killed.

The twin engine airplane departed Rio de Janeiro-Santos Dumont Airport at 1231LT on a special flight to Campinas-Viracopos, carrying six passengers and a pilot. The goal of the mission was a survey flight on behalf of the 'Rondon Project (Projeto Rondon) of the Ministry of Defence. At 1251LT, the pilot cancelled his IFR flight plan and informed ATC he was continuing under VFR mode. This was the last radio contact. As the airplane failed to land at Viracopos Airport, SAR operations were initiated but eventually abandoned 19 days later as no trace of the aircraft nor the 7 occupants was found.

On approach to Florianópolis-Hercílio Luz Airport, the crew encountered poor weather conditions with thunderstorm activity and heavy rain falls. The approach was abandoned and the captain initiated a go-around. Few minutes later, while completing a second attempt to land, the crew failed to realize that the airplane was not properly aligned. At a higher speed than prescribed, the airplane struck the top of a hill and crashed in flames about 26 km from the airport. Three passengers were rescued while 55 other occupants were killed. At the time of the accident, the airplane was approaching the airport below the glideslope and off course. It appears that an inspector pilot was at control at the time of the accident.

After takeoff from Cuiabá-Marechal Rondon Airport, while climbing, the twin engine airplane struck a hill and crashed few km from the airport. All nine occupants were killed.

Crashed in unknown circumstances 5 km from Cascavel. Occupant fate unknown.

The twin engine airplane was completing a flight from São Paulo to Brasilia with an en route stop at Brotas, carrying two engineers and one pilot. While approaching Brotas, the pilot encountered poor weather conditions and lost control of the airplane that crashed on a hill. A passenger was injured while both other occupants were killed.

After landing at Campinas-Viracopos Airport, the twin engine airplane was unable to stop within the remaining distance. It overran and came to rest few dozen meters further. Both pilots escaped uninjured while the aircraft was damaged beyond repair.

Flight 527 was cleared for a No.16 departure by ground control and was instructed to make a right turn after takeoff, heading the Caxias VOR, climbing to and maintaining 2000 feet. The aircraft took off from runway 27 at 21:27. Approach control then asked the crew to increase their speed. The speed increased progressively to 304 knots, exceeding the 250 knots maximum speed inside the terminal control area below 10000 feet. While Flight 527 was flying towards mountainous terrain and increasing its speed (in the north sector of the radar scope), the controller was busy vectoring an excessive amount of traffic in the south sector. The assistant departure controller failed to monitor the traffic. When the controller turned his attention to LH527 again, he was surprised by the position of the aircraft and instructed 'LH, turn right heading 140, just now, over'. The controller repeated his instructions and instructed the crew to increase their rate of climb. At that time the GPWS sounded in the cockpit. The aircraft struck trees on the slope of a mountain in a nose-up, left wing down attitude and continued 800 m while breaking up.