NTSB CAROL · Event
Event WPR20LA123
Aircraft involved
Probable cause & findings
The total loss of engine power after takeoff due to water contamination of the fuel.
Factual narrative
On April 18, 2020, about 1041 Pacific daylight time, a Cessna T206 airplane, N756TH, was destroyed when it was involved in an accident near Auburn, California. The pilot was fatally injured, and the pilot-rated passenger was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The passenger reported that the pilot planned to fly them in another airplane he owned; however, he noted discrepancies during the preflight (oil residue in the engine compartment) and opted to fly the accident airplane instead, which he also owned. The passenger reported that the pilot performed the preflight inspection on the airplane. Although he did not observe the pilot perform the inspection, he observed the pilot perform preflight inspections previously and he believed the pilot “performed thorough checks.” The passenger stated that shortly after takeoff, at an altitude of about 200 to 300 ft above the ground, the engine lost power. The passenger took over the flight controls and performed an emergency landing to a field near the departure airport. During the landing, the airplane impacted terrain and a post-crash fire ensued. Radar data indicated that the airplane departed runway 25 and turned to the left while climbing to about 155 ft above sea level (agl). The airplane then turned 90° to the right and started to descend until radar data was lost about 1,500 ft northwest of the departure end of the runway 25. The entire flight lasted less than one minute. A postaccident examination of the airplane revealed no catastrophic pre-impact mechanical anomalies; however, when the fuel manifold valve was disassembled, corrosion type debris was noted on the internal screen and liquid was observed within the fuel manifold valve cavity. Water finding paste was used to test the liquid and it was positive for water. A friend of the pilot’s flew the accident airplane on March 13, 2020 and March 26, 2020. During the preflight inspection of both flights, he noted substantial amounts of water in the fuel tanks and fuel system. He stated the fuel tank caps were older and known to leak and allow water into the fuel tanks. The pilot’s friend also stated that the pilot had ordered new fuel tank caps, but they were backordered at the time of the accident. He told the pilot not to fly the airplane until the new fuel tank caps were installed. An autopsy was performed on the pilot by the Office of the Sherriff-Coroner, Placer County, Auburn, California. The cause of death was multiple blunt force and thermal injures. The forensic pathologist reported that the pilot had marked abdominal aorta atherosclerosis and 75 to 90 percent calcific stenosis of portions of his left anterior descending coronary, left circumflex, and left main coronary arteries. Toxicology testing was performed on the pilot by the FAA Forensic Sciences Laboratory. The testing detected hydroxychloroquine in the pilot’s heart blood and urine. Hydroxychloroquine is indicated for use in rheumatoid arthritis, lupus, and malaria treatment. Patients are advised that serious cardiac side effects could occur including a fast or irregular heartbeat, lightheadedness, dizziness, or syncope. The non-impairing medication tamsulosin was also detected in the pilot’s heart blood and urine. The pilot reported taking hydroxychloroquine for a new medical diagnosis of inflammatory arthritis, on his most recent FAA third-class medical certificate, issued February 28, 2020. Shortly after takeoff, at an altitude of about 200 to 300 ft above the ground, the airplane’s engine lost power. The pilot-rated passenger took over the flight controls and performed an emergency landing to a field near the departure airport. During the landing, the airplane impacted terrain and a post-crash fire ensued. A postaccident examination of the airplane revealed water in the fuel manifold valve cavity and corrosion type debris on the internal screen. Witness statements revealed several people associated with the pilot knew water had been accumulating in the fuel tanks due to leaky fuel tank caps, one of which was another pilot who flew the airplane twice in the weeks before the accident. The accident pilot reported that he performed a preflight inspection; however, it is unknown whether he checked the fuel tanks for contamination as the pilot-rated passenger did not observe him during the preflight. Autopsy and toxicology reports revealed the pilot had severe stenosis of his aorta and three coronary arteries and that he was taking hydroxychloroquine, a medication to treat rheumatoid arthritis. Both the cardiovascular disease and medication use placed him at an increased risk for a sudden cardiac event. However, there was no evidence to suggest that occurred and based on the circumstances of this accident, the pilot’s cardiovascular condition and the effects from his use of hydroxychloroquine were not factors in the accident. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid condition
Verbatim from NTSB's published report. Source file
NTSB_2020_WPR20LA123.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
Browse the full corpus — academia portal ↗