Plain, Valley

While on final approach to San Angelo-Mathis Field, the single engine airplane entered a rapid descent with a rate of 5,058 feet per minute then crashed in an open field located about 12 km south of the airport. The airplane was totally destroyed and both occupants were killed.

The single engine airplane departed Pevek on a cargo flight to Polyarny, carrying two passengers, one pilot and a load of 150 kg of various goods. Approaching the destination, weather conditions deteriorated with heavy rain falls. In limited visibility, the airplane impacted the ground and crashed in the snow covered tundra few km from Polyarny. The wreckage was found few hours later and all three occupants were injured, the captain seriously. The airplane was a TR-301, a version of the AN-2 without the lower wings. Modification were performed by Tekhnoregion under MSN ТR301.21.004.

In the early afternoon, the twin engine airplane departed Toowoomba Airport on an aerial survey flight under callsign BDOG370 to Mount Isa with three people on board. The purpose of the flight was to conduct a survey mission of the area in case of bushfire. While cruising at an altitude of 28,000 feet, the airplane entered an uncontrolled descent. It reached a rate of descent of 9,600 feet per minute until it crashed in an uninhabited area located approximately 70 km southeast of Cloncurry. All three occupants were killed.

The single engine airplane departed Pucallpa-Captain David Abensur Rengifo Airport around 1000LT on a cargo flight to Breu with two pilots on board. On approach to Breu-Tipishsa Airport, the airplane crashed in unknown circumstances in a wooded area located about 4 km northwest of Breu. The captain was killed and the copilot was injured.

The pilot reported that before takeoff on the cross-country flight, the airplane contained 100 gallons of fuel, with 11 gallons in the header fuel tank, and the airplane’s automatic fuel transfer system was configured as per the checklist. No anomalies were noted during the engine start, takeoff, and initial climb. About 7 minutes into the flight and climbing through 12,000 ft mean sea level (msl), the engine sustained an abrupt loss of power that was confirmed by the loss of torque and engine compressor turbine rpm (Ng) speed. The pilot noted no cockpit warning or abnormal indications before the loss of engine power. The pilot declared an emergency and then executed a 180° turn back to the departure airport. The pilot attempted two engine restarts, and both were unsuccessful. Unable to make it back to the airport, the pilot executed an off airport forced landing. During the forced landing, the airplane sustained substantial damage to the fuselage and both wings. A postaccident examination of the airframe, fuel system components, and functional engine test revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. The fuel transfer pump switch was found in the manual position. The engine’s fuel was provided by the airframe header tank. Avionics data indicated that during the short flight, the header fuel tank quantity consistently decreased, and the airplane’s automatic fuel system did not continually resupply fuel to the header tank. Based on the available data, a functional engine test, and functional testing of the airplane’s fuel system, it is likely the pilot improperly configured the airplane’s fuel transfer system, which prevented the header fuel tank from automatically refilling during the flight and resulted in fuel starvation and total loss of engine power. Although the pilot reported that he had configured the airplane’s automatic fuel transfer system per the checklist, it is likely that the fuel transfer switch was in the manual or OFF position during the flight. In addition, the pilot did not properly monitor the header tank’s fuel quantity.

The pilot reported that he had completed a charter flight and departed to pick up new passengers at an airport about 200 nautical miles away. While on approach to the destination airport, the previous passengers notified the pilot that they were ready to be picked up, so the pilot did not land and turned the airplane back toward the departure airport. The pilot climbed to 10,000 ft and noticed the airplane’s fuel burn was high, so he climbed to 16,000 ft. The pilot reported that “everything was routine until about a 3-mile final” to the runway, when the controller asked the pilot to slow to a final approach speed. An airplane was still on the runway, so the controller told the pilot to go around. The pilot told controllers twice that he had minimum fuel available. The pilot continued on a visual approach for the same runway when the right engine lost power followed by the left engine. He feathered both propellers and made a forced landing to a wooded area. The airplane sustained substantial damage to the fuselage, both wings, and the empennage. The pilot reported that there were no preimpact mechanical malfunctions or failures that would have precluded normal operation. The pilot later stated that he was “trying to do too much with too little” fuel and the accident was a result of poor fuel management. Although the controller directed the pilot to go around, the pilot should have recognized the criticality of the minimum fuel situation and landed the airplane.

The single engine airplane crashed in unknown circumstances in Mbukula while performing a flight from Lubumbashi to Kananga. The crew was supposed to make a stop in Mbukula to deliver fuel cans and chairs to the village chief's home when the accident occurred.

The Legacy departed Moscow-Sheremetyevo Airport shortly before 1645LT on a flight to St Petersburg-Pulkovo, carrying seven passengers and three crew members. According to the radar, while cruising at FL280, it entered an uncontrolled descent and spiraled into the ground until it crashed in an open field located near the village of Kuzhenkino, bursting into flames. The airplane was destroyed and all 10 occupants were killed. The airplane was the property of the Wagner Group owned by Evgueni Viktorovitch Prigozhine who was on board with Dmitry Utkin, n°2 of the group. It is showable on videos that the airplane was emanating white/grey smoke while spiraling to the ground.

The twin engine airplane was en route from Caracas-Maiquetía-Simón Bolívar Airport to Medellín-José María Córdova Airport (Rionegro) with two people on board. In unknown circumstances, it went out of control and crashed in a pasture located near the village of Las Velas, bursting into flames. The aircraft was destroyed by impact forces and a post crash fire and both occupants were killed.

The crew departed Auburn-Lewiston Municipal Airport on a local training mission under callsign WIG634. After making a circuit over Sebago Lake located southwest of the airport, the crew continued to the northeast when control was lost. The airplane entered a descent with a rate of 7,300 feet per minute until it crashed in a wooded area located near Mt Oak Hill, about 25 km northeast of Auburn-Lewiston Municipal Airport. The airplane was destroyed and both occupants were killed.