Plain, Valley

The crew departed Zaporozhie Airport on a local test flight according to local authorities, carrying three crew members. While flying at low height, the airplane collided with power line and crashed in an open field located in Mykhailivka, some 11 km northwest of the airport. A crew member was killed and two others were injured. The aircraft was destroyed.

The pilot, sole on board, departed Los Mochis International Airport on a flight to the Club Aéreo Nuevo Santa Rosa located east-northeast of the city. After landing on a road, the airplane suffered an apparent undercarriage failure, veered to the right and came to rest in a grassy area, bursting into flames. The pilot evacuated safely while the aircraft suffered serious damages due to fire.

Crashed in unknown circumstances in bushes near Cobán, Guatemala, while engaged in an illegal flight. The aircraft was damaged beyond repair and no one was found on the scene. The registration seems to be false.

The aircraft crashed in unknown circumstances in a snow covered field located in Ostrogozhsk. Russian Authorities reported that all occupants were killed.

The aircraft crashed in an open field located in Zhukivtsi, about 30 km south of Kiev-Borispol Airport. It is believed there were 14 people on board and that five of them were killed. Maybe the aircraft was shot down by Russian Forces that entered Ukraine territory few hours earlier.

En route, the pilot encountered engine problems and elected to make an emergency landing on a motorway. Upon landing, the aircraft impacted the road bank, lost its left wing and came to rest. All six occupants evacuated with minor injuries and the aircraft was damaged beyond repair.

Shortly after takeoff from Koryaki, en route to Tymlat, the crew lost control of the airplane that crashed in a wooded and snow covered area located one km from Koryaki, bursting into flames. The aircraft was totally destroyed by a post crash fire and both pilots were killed.

The aircraft departed Goma on a cargo flight to Shabunda, carrying two conveyors and three crew members. On approach to Shabunda Airport, the crew encountered poor weather conditions when the arcraft crashed 15 km from the airport. All five occupants were killed.

The single engine airplane departed Houston-George Bush-Intercontinental Airport at 0910LT on a cargo service to Victoria. Twelve minutes later, while climbing to an altitude of 4,200 feet, the aircraft collided with a paraglider. Out of control, it entered a dive and crashed three minutes later in a field. The aircraft was totally destroyed and the pilot, sole on board was killed, as well as the paraglider.

The company pilot and two employees had departed on an aerial imagery survey flight of forest vegetation. The airplane began to level off at an altitude of about 16,100 ft mean sea level (msl) and accelerated to a maximum recorded groundspeed of 209 knots. Less than 2 minutes later, the groundspeed decreased to about 93 knots, and the airplane descended about 500 ft while on a steady heading. The airplane subsequently entered a rapid descent and a right turn, and “mayday, mayday, mayday” and “we’re in a spin” transmissions were broadcast to air traffic control (ATC). A witness, who was located near the accident site, noticed the airplane nose down at high rate of speed and then saw the airplane spinning rapidly about its longitudinal axis. The airplane wreckage was located in remote wetlands and wooded terrain. Postaccident examination revealed that the airplane impacted the ground in a nose-low vertical attitude and at high speed. All major components of the airplane were located at the accident site. Examination of the airframe, engines, and propellers revealed no preimpact mechanical malfunctions or failures that would have precluded normal operation. According to the aircraft performance study for this accident, when the airplane pitched down, the normal load factor decreased rapidly from about 1.6 to less than 1 G. A rapid decrease in normal load factor is consistent with a stall when the wing exceeds its critical angle of attack. At that point, the air flow becomes separated at the wing, and the wing can no longer generate the necessary lift. If the airplane is in uncoordinated flight at the stall, a spin can result. Thus, the pilot likely did not maintain adequate airspeed, causing the airplane to exceed its critical angle of attack and enter a stall and spin. An important but unknown factor before and during the initial stall was the behavior of the pilot regarding his flight control inputs, including his possible attempt to recover. The airplane’s Pilot Operating Handbook states that spins are not authorized and does not include a procedure for inadvertent spin recovery.