Takeoff (climb)

Crashed shortly after liftoff from Johannesburg-Rand Airport. All five passengers were killed and the pilot was injured.

On August 2, 2022, about 1030 eastern daylight time, a Smith Aerostar 600, N9784Q, was destroyed when it was involved in an accident near South Haven Area Regional Airport (LWA), South Haven, Michigan. The air transport pilot and commercial pilot were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to a friend of the pilot, he spoke to the commercial pilot/owner on the morning of the accident. He said the commercial pilot purchased the airplane about five years ago and had been working on it since then. This was the first flight since he purchased the airplane and he planned on staying in the traffic pattern to conduct a few touch-and-go landings. He went on to say the air transport pilot had flown in to fly with the pilot. When the friend arrived at the airport, he noticed the airplane was not in the traffic pattern. After a few hours, he became concerned and assumed that the airplane landed at another airport. Later that evening, the wife of the commercial pilot called the friend and said she had not heard from her spouse. They contacted the local authorities, and reported the airplane was missing. The airplane was found the following morning. The airplane came to rest oriented on a magnetic heading of 010° in a heavily wooded area about one mile north of LWA. All major components of the airplane were still connected to the airframe and located at the accident site. The cockpit and instrument panel were destroyed by impact forces. The fuselage displayed impact and crush damage. The wings remained attached to the fuselage and displayed impact damage. An examination of the wings revealed the ailerons and flaps were still attached and displayed impact damage. Flight control push-pull tube continuity was observed from the primary flight control surfaces to the cockpit section. The empennage was separated from the fuselage and the left and right elevators remained attached to their respective horizontal stabilizer. The rudder remained attached to the vertical stabilizer and displayed impact damage. Initial examination of the engines revealed impact damage and they will be further examined once recovered. The propellers remained attached to both engine crankshaft flanges. The left propeller blades displayed aft bending. The right propeller blades displayed chordwise scoring and aft bending. The wreckage was recovered and retained for further examination.

The pilot reported that, he was departing in the float-equipped airplane in strong gusty wind conditions. After accelerating on the water for about 3 seconds, the airplane suddenly became airborne and crabbed into the wind about 60° to 90° from the intended takeoff path and started to climb as it continued to track away from the intended flight path. As the climb continued, the airplane stalled and impacted the water in a nose low attitude which resulted in substantial damage to the wings and fuselage. The pilot reported that there were no preaccident mechanical malfunctions or anomalies that would have precluded normal operation.

Shortly after takeoff from Santiago de Querétaro Airport, while climbing, the twin engine airplane went out of control and crashed inverted in a maize field located near the airport. The aircraft was destroyed and both occupants were killed.

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.

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.

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.