Private

The twin engine airplane departed Gonzales-Louisiana Regional Airport at 1456LT on a short flight to Patterson. Following a left hand turn, the airplane descended to Patterson-Harry P. Williams Airport when it crashed 300 feet short of runway 06 threshold, bursting into flames. The airplane was destroyed and both occupants were killed. Patterson-Harry P. Williams Airport is located 64 km southwest of Gonzales-Louisiana Regional Airport.

Just after liftoff from runway 35 at Bom Futuro Airport, while in initial climb, the twin engine airplane rolled to the left, descended and impacted the surface of the apron with its left wing. Upon impact, the undercarriage were torn off then the airplane slid for few dozen metres before it crashed against a hangar under construction, bursting into flames. Both passengers were injured while the pilot and one person on the ground were killed.

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.

On 19th August 2023 at approximately 12:25 pm local (1625 UTC), a Cessna 402B aircraft which was last registered in The Bahamas until 17th July 2022 as C6-SPK (serial number 402B-1054), departed from the Fort Lauderdale International Airport (KFLL), Fort Lauderdale, FL, USA with one (1) person on board enroute to the North Eleuthera International Airport (MYEH), Eleuthera, Bahamas. The aircraft was expected to return to KFLL shortly after 2:00 pm later that afternoon, however, it never arrived at its intended destination. It was reported that at approximately 12:58 pm (1658 UTC), KFLL air traffic control observed the aircraft in a rapid descent from an altitude of approximately 8,400 feet mean sea level (MSL) to about 4,500 feet MSL, while at coordinates 25.84N 78.90W, approximately some 70 nautical miles south east of KFLL, or approximately 18 nautical miles north east of Bimini, Bahamas. The aircraft was not observed on radar after the rapid descent. Upon notification that the aircraft was overdue, search and rescue protocols were initiated with coordination between the United States Coast Guard (USCG), Royal Bahamas Defence Force (RBDF), Royal Bahamas Police Force (RBPF), with assistance from the Bahamas Air Sea Rescue Association (BASRA). During search and rescue, aerial and marine assets from the US Coast Guard and RBDF responded to areas in vicinity of the last known position of the aircraft, initially identified at coordinates 25.84N 78.90W. An updated position of the aircraft was later provided by the US Coast Guard and identified at coordinates 25°20'35.00"N 76°59'46.00"W, at a distance of approximately 17 nautical miles southwest from MYEH. Assets also searched the updated position with combined search efforts extending up to 21st August 2023. As of the time of release of this report, neither the pilot nor the aircraft has been located.

The pilot was enroute to the destination airport and overflying the Gulf of Mexico when about 15 nautical miles from the airport and at an altitude of 3,000 ft, the right engine suddenly lost power. The pilot described that about that time, the fuel totalizers indicated that 48 gallons of fuel were onboard, and his fuel quantity gauge indicated similarly. He then contacted air traffic control and declared an emergency. Shortly thereafter, the left engine also suddenly lost power. The pilot attempted to troubleshoot the issue and restart both engines but was unsuccessful. He subsequently ditched the airplane and was rescued from the water without injury. The airplane was not recovered and could not be examined after the accident, therefore the reason for the loss of engine power could not be determined.

The airplane departed Veracruz-General Heriberto Jara Corona Airport Runway 01 at 2047LT on a private flight to Toluca, carrying one passenger and two pilots. Three minutes later, while climbing at night, it entered an uncontrolled descent until it crashed into the sea off Ciudad de Veracruz. The airplane was destroyed upon impact and all three occupants were killed.

The flight, which was a private flight, was the third of the day. The pilot had landed on a field at Tumberg just north of Vårgårda and after a ground stop they planned to take off from the field. On board were one pilot and four passengers. The pilot decided to take off from the field in an easterly direction because there were obstacles in the form of buildings and lamp posts in the westerly direction. There were trees at the end of the field to the east, but the pilot assessed that these did not pose a problem and that the field was long enough for a take-off in an easterly direction. No precise calculations were made to determine the required take-off distance. The pilot initiated the take-off and set the engine controls to full take-off power. According to the pilot and the passenger in the right front seat, the indicated values for engine rpm and manifold pressure were normal. The acceleration of the aircraft was also perceived as normal. At lift-off, the aircraft rolled to the right and the pilot felt that the aircraft did not climb as expected. The pilot pulled hard on the control yoke and tried to climb over the trees at the end of the field. However, he failed to manoeuvre the aircraft away from the trees and as a result the aircraft collided with the trees. No one was injured in the collision but the aircraft sustained significant damage.

During an early morning night flight, the flight encountered deteriorating weather conditions with a low overcast ceiling and rapidly decreasing visibility at the destination due to fog. A few minutes before the flight’s arrival time at the destination airport, the weather had changed from being clear with 10 statute miles (sm) visibility to 300 ft overcast with 3/4 sm visibility. Additionally, in the next 20 minutes, the visibility further decreased to about 1/2 sm with fog. The airplane was cleared for the RNAV (GPS) Runway 18 instrument approach to the airport. The lowest visibility requirement on the approach was 7/8 of a mile. During the final approach, the pilot executed a missed approach and asked to try another instrument approach. During the second instrument approach, while on final approach, the pilot failed to fly a stabilized approach as the airplane’s descent rate and airspeed were excessive. Subsequently, the airplane descended below the decision altitude of the approach without appropriate visual references and impacted terrain about 810 ft short of the runway threshold. The circumstances of the accident flight were consistent with controlled flight into terrain (CFIT). The postaccident examination of the airplane and engines revealed no evidence of mechanical failures or malfunctions that would have precluded normal operation of the airplane. The pilot had very low levels of ethanol detected in postmortem vitreous fluid and cavity blood. Some or all of this small amount of ethanol may have been from sources other than alcohol consumption. Although it is uncertain whether the pilot had consumed alcohol overnight, the toxicology results indicate that it is unlikely that the pilot’s performance would be significantly affected by ethanol. The copilot’s ethanol levels were high in all tested postmortem specimens. Based on the toxicology results and the circumstances of the event, it is likely that the copilot had consumed alcohol. However, based on the extent of his injuries, the presence of indicators of microbial decomposition, and the relative differences in ethanol levels across specimens, it also is likely that some of the detected ethanol was from sources other than alcohol consumption. The copilot’s blood alcohol level at the time of the crash cannot be reliably determined from available evidence. Overall, alcohol-related impairment may have limited the copilot’s ability to make a positive contribution to flight safety (such as by helping to monitor the approach); however, whether the effects of alcohol use by the copilot contributed to the accident outcome could not be determined.