What happened
During the initial climb phase of flight, the aircraft experienced a simultaneous loss of power across both engines. Specifically, the left engine suffered a failure while the right engine experienced a significant reduction in power. As a result of this dual-engine issue, the airspeed decreased to 70 km/h. At an altitude of approximately 50 meters, the aircraft entered a stall and descended into an open field situated roughly 3 kilometers from the runway threshold.
The impact resulted in the total destruction of the aircraft. There were five fatalities among the occupants of the plane.
Findings
Investigations determined that the primary factor leading to the accident was a failure within the fuel supply system. This malfunction caused both engines to lose power during the climb, which subsequently led to the aerodynamic stall and the subsequent crash.