On August 23, 2019, about 1115 eastern daylight time, an experimental amateur-built Aventura II airplane, N9143M, was substantially damaged when it was involved in an accident near Minneola, Florida. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to the pilot's son, he and his father had assembled the airplane. He stated that they had installed an after-market supercharger on the engine several months before the accident, and the airplane had been flying well since then. He further stated that, about 2 days before the accident, his father said the airplane had been consuming fuel at a higher-than-normal rate (about 6 gallons per hour as opposed to the normal 4 gallons per hour). On the day before the accident, he and his father replaced the jets in the carburetor with smaller jets to attempt to improve the fuel consumption. After they replaced the jets, they started the engine, and it was running roughly (coughing and missing). The pilot’s son stated that the next morning, when he arrived at Florida Flying Gators Airport (3FD4), Minneola, Florida, his father told him he had fixed the airplane by adjusting the tabs on the carburetor float bracket and allowing more fuel to enter the carburetor bowl. They performed a run-up of the engine, and it ran normally. He stated that his father planned to fly to DeLand Municipal Airport-Sidney H Taylor Field (DED), DeLand, Florida, and that he would drive a truck and trailer there to meet him. He watched his father start his takeoff roll on runway 36. He stated that the takeoff looked normal but that the airplane was not climbing like it had in the past. When the airplane reached about 300 ft above ground level, the engine started to sputter and run roughly. He stated that it looked like his father tried to turn back to the runway and made a sharp left turn but that shortly after the left turn, the airplane descended straight down to the ground. The airplane came to rest about 200 yards from the end of runway 36. The wreckage was oriented on a 270° magnetic heading, and all major components were located with the main wreckage. Flight control continuity was verified from the cockpit to all primary flight control surfaces. Examination of the wreckage revealed that the airplane impacted the ground in an almost vertical nose-down attitude. The nose of the airplane was fractured in several pieces, and the instrument panel was destroyed; the instruments were found in the grass beside the main wreckage. The landing gear was extended. The wing was impact damaged, and the fabric was torn down the entire length of the wing. The aluminum tubing inside the wing structure was fractured off and had torn through the wing fabric material. The engine was fractured off the engine mounts and remained connected through the wiring and cables from the throttle and mixture controls. The engine was found inverted, and automotive gasoline was pouring out of the fractured fuel lines. The three-blade composite propeller remained attached to the engine, and one propeller blade was fractured mid-blade by impact forces. Both carburetors were fractured off the induction system and connected by only the throttle linkage. The tail section of the airplane did not contact the ground and was undamaged. Further examination of the engine found that the choke on the carburetors was safety wired in the open position. The right exhaust gas temperature probe was cut off at the exhaust pipe. A new temperature probe was drilled into the exhaust pipe and clamped to the pipe with two worm-style, stainless-steel clamps. The supercharger spun freely, and no binding was noted. The top spark plugs were removed and noted to be black and sooty from exhaust gases. Thumb compression was established on all cylinders. A lighted boroscope was used to examine the cylinders, valves, and pistons; no anomalies were noted. The pilot had reported 306 total flight hours to the Federal Aviation Administration (FAA) at the time of his most recent medical examination but had reported no chronic medical conditions and no use of medications. According to the autopsy performed by the State of Florida Medical Examiner, Districts 5 & 24, the pilot’s cause of death was multiple blunt force injuries. No significant natural disease was identified. Toxicology testing performed by NMS Labs identified 5.8 ng/mL of Delta-9-THC (tetrahydrocannabinol, the active compound in marijuana) and 15 ng/mL of its inactive metabolite, Delta-9-Carboxy-THC, in the pilot’s iliac blood. Toxicology testing performed by the FAA's Forensic Science Laboratory identified 7.4 ng/mL of Delta-9-THC in the pilot’s cavity blood, along with 16.4 ng/mL of Delta-9-Carboxy-THC and 0.9 ng/mL of 11-Hydroxy-Delta-9-THC (a psychoactive metabolite). In addition, 3 ng/ml of Delta-9-THC was identified in liver tissue, along with 107.8 ng/mL of Delta-9-Carboxy-THC. Testing for 11-Hydroxy-Delta-9-THC was inconclusive in liver tissue.