Airport (less than 10 km from airport)

The airplane was returning to its base in San Fernando following an ambulance flight from Comodoro Rivadavia to Río Grande. After takeoff from Río Grande-Gobernador Ramón Trejo Noel Airport runway 26, while in initial climb, the airplane rolled to the left, nosed down and crashed in a huge explosion about 350 metres south from the runway 08 threshold. The aircraft was totally destroyed and all four occupants were killed. A failure of the left engine after rotation is suspected.
Crew:
Claudio Canelo, pilot,
Héctor Vittore, copilot.
Passengers:
Diego Ciolfi, doctor,
Denise Torres Garcá, nurse.

The airplane departed Dyagilevo AFB (Ryazan) on a night flight apparently to Belgorod, carrying nine crew members. After takeoff, the engine n°4 caught fire. The crew elected to return for an emergency landing but the aircraft went out of control and crashed about one km from the airbase, bursting into flames. Four crew members were seriously injured and five others were killed. The aircraft was destroyed by impact forces and a post crash fire.

Following an uneventful flight from Santo Domingo-Las Américas Airport, the crew was cleared to land on runway 09 at Miami-Intl Airport. According to a video, it is believed that both main landing gear were not properly extended upon touchdown. The airplane rolled for few hundred metres then deviated to the left and departed the runway to the left. It collided with obstacles, lost its undercarriage and came to rest in a grassy area, bursting into flames. Fire was quickly extinguished. All 126 occupants evacuated safely, among them three passengers were taken to Jackson Hospital.

Shortly after takeoff from Deadmans Cay Airport Runway 09, while climbing, both engines lost power simultaneously. The airplane went out of control, impacted trees and crashed some 3 km northwest of the airfield. The airplane came to rest in bushes and was destroyed by impact forces. There was no fire. Among the seven people on board, a woman passenger was killed and six other occupants were injured.

On June 03, 2022, about 1347 Pacific daylight time, a Cessna C208B Supervan 900 airplane, N7581F, was substantially damaged when it was involved in an accident near Bob Maxwell Memorial Airfield, Oceanside, California. The left-seated pilot was fatally injured and right seated pilot was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 skydiving flight. On the day of the accident, the pilots were performing skydiving flights while the right-seated pilot was training the left-seated pilot on the operation. A flight would consist of the pilots taking a group of approximately 17 skydivers to an altitude of about 11,500 feet mean sea level (msl) to jump out and then they would land back at the airport. The flights started about 1015 and were an average of 17 minutes in duration with about 15 minutes on the ground between each flight; the airplane’s engine was operating the entire duration. The pilots completed six flights without incident and departed on the accident flight at 1331. The right-seated pilot stated that he could not recall many of the details leading up to the accident. He remembered that on the accident flight everything was normal with the departure and the unloading of the skydivers. The airplane was descending as expected with the power at idle. As the airplane turned onto final approach, about 3 miles from the approach end of runway 25, the right-seated pilot attempted to increase the power by slightly nudging the throttle forward. He noticed that the engine power did not increase as expected and moved the throttle lever further forward. The lever was still unresponsive, and he estimated the airplane was about 400 ft above ground level (agl). He aimed for an open dirt field and observed a berm in the immediate flight path. In an effort to avoid the berm, the pilot maneuvered the airplane into a right turn.Investigators reviewed Federal Aviation Administration (FAA) provided Automatic Dependent Surveillance-Broadcast (ADS-B) flight track data covering the area of the accident during the time surrounding the accident. After departing from runway 25, the airplane made a gradual climb to 11,575 ft msl as it circled to the right, back to the airport. The airspeed was reduced (presumably to unload the skydivers) and then the airplane made a steep, turning decent reaching 133 kts when transitioning to the downwind leg of the traffic pattern. The airplane was at an altitude of about 2,400 ft msl and 2.6 nautical miles (nm) from the approach end of runway 25 when it turned onto final approach. When the airplane was about 2 nm from the runway, it made a 360° right turn which was about 0.5 nm in diameter. At 1346:10, about 1,025 ft msl, the airplane rolled out of the 360° turn and continue west toward the runway. The airplane was roughly following Highway 76 making a gradual decent (see Figure 2 below). About 33 seconds later the airplane’s speed dropped to 92 kts as it passed through 500 ft msl. The last recorded hit was at 1347:10 and located about 975 feet east of the accident site. At that time, the data indicated that the airplane was at 100 msl (equivalent to 60 feet above ground level) at a speed of 68 kts. Witness stated that they observed the airplane flying at a very low altitude (see Figure 3). The airplane then pitched down in a nose-low attitude and bank to the right. The airplane impacted terrain and collided with the side of a berm.

The purpose of the flight was to transport three passengers and cargo. The pilot reported that, during takeoff, the airplane’s tail came up slightly lowered to the runway when he attempted to raise the tail by applying forward elevator. He stated that he thought this was unusual and attributed it to an aft-loaded airplane. He applied additional nose-down trim and departed without incident. While en route, the tail of the airplane seemed to move up and down, which the pilot attributed to turbulence. Upon arrival at his destination, the pilot entered a left downwind, reduced the power and extended the flaps to 10° abeam the end of the runway. He turned onto the base leg about ½ mile from the approach end of the runway and slowed the airplane to 80 mph. Turning final, he noticed the airplane seemed to pitch up, so he applied full nose-down pitch trim and extended the flaps an additional 10°. On short final he applied full flaps, and the airplane abruptly pitched up to about a 45° angle. He stated that he applied full nose-down elevator, verified the pitch trim, and reduced the power to idle. When the airplane was about 300 ft above ground level, the airplane stalled, the left wing dropped slightly, and the airplane entered about a 45° nose-down dive. After allowing the airplane to gain airspeed, the pilot applied full back elevator. The airplane impacted forested terrain near the approach end of runway 23 at an elevation of about 18 ft. A postaccident examination of the airframe and engine revealed no evidence of preaccident mechanical malfunctions or failures that would have precluded normal operation. Elevator and rudder control continuity was confirmed from the cockpit to the respective control surfaces. The airplane's estimated gross weight at the time of the accident was about 7,796 lbs and the airplane's estimated center of gravity was about 3.2 to 5.6 inches beyond the approved aft limit. Maximum gross weight for the airplane is 8,000 lbs.

The airplane departed Jundiaí on a cargo flight to Eldorado do Sul, carrying two pilots and a load of automotive parts. On final approach, the airplane crash landed in a rice paddy field and came to rest with its left wing detached. Both pilots were slightly injured.

The airplane was departing Chongqing-Jiangbei Airport on a regular schedule service to Nyingchi, Tibet, carrying 113 passengers and a crew of nine. During the takeoff run from runway 03, the captain encountered an unexpected situation and decided to abandon the takeoff procedure. He initiated an emergency braking manoeuvre when the airplane started to deviate to the left. It veered off runway, went through a grassy area, lost its undercarriage and both engines before coming to rest on a parallel taxiway, bursting into flames. 36 occupants were injured while all others evacuated safely. The aircraft was destroyed.

The single engine airplane departed Boituva Aerodrome on a local skydiving mission, carrying 14 skydivers and one pilot. After takeoff, the pilot apparently encountered electrical problems and elected to return for an emergency landing. Shortly later, the aircraft collided with high tension wires, stalled and crashed inverted in a field. Two passengers were killed while all other occupants were injured.

The pilot reported that, before the flight, the airplane was fueled with 140 gallons of Jet A fuel. Shortly after takeoff, both engines lost total power. Because the airplane had insufficient altitude to return to the airport, the pilot executed a forced landing to a field and the left wing sustained substantial damage. A postcrash fire ensued. The investigation determined that the airplane was inadvertently fueled with Jet A fuel rather than AVGAS, which was required for the airplane’s reciprocating engines. The line service worker who fueled the airplane reported that there were no decals at the airplane fuel ports; however, postaccident examination of the airplane found that a decal specifying AVGAS was present at the right-wing fuel port. The investigation could not determine whether the same or a similar decal was present at the left-wing fuel port because the left wing was partially consumed during the postimpact fire.