NTSB CAROL · Event
Event FTW96LA345
Aircraft involved
Probable cause & findings
loss of engine power due to fuel contamination. The lack of suitable terrain for a forced landing was a related factor.
Factual narrative
On August 7, 1996, at 1000 central daylight time, a Cessna 210-5, N8139Z, was substantially damaged during a forced landing near Muskogee, Oklahoma. The airplane was owned and operated by a private owner. The private pilot and his two passengers were not injured. Visual meteorological conditions prevailed for the personal flight conducted under Title 14 CFR Part 91. A weather briefing was obtained by the pilot prior to the flight and a flight plan was not filed. The flight originated from a private airstrip near Lonoke, Arkansas, at approximately 0800. According to the pilot, the engine started to run rough, and subsequently lost power while in cruise flight at 6,500 feet MSL. The pilot attempted to land at the Davis Airport, near Muskogee, Oklahoma; however, he was not able to reach the airport and landed in a field approximately one mile southeast of the airport. During the landing roll, the airplane impacted a fence and fence posts resulting in leading edge damage to one wing and structural damage to both wing struts. The engine was examined by the FAA inspector, the aircraft owner, and a representative from the engine manufacturer on August 28, 1996 at an FBO at Davis Field in Muskogee, Oklahoma. The contents of the fuel system were examined. The fuel in the tanks was "discolored" by an unknown substance and appeared yellow/straw in color. The fuel was also lacking the appearance and smell of 100LL fuel; however, no diesel or jet fuel was detected. New spark plugs were installed as the fuel tanks were drained and serviced with fresh 100LL fuel. The engine was started and operated normally through the normal operating range by the pilot/owner of the aircraft. The loss of engine power was attributed to the contaminated fuel found in the fuel tanks. According to the pilot, the engine started to run rough, and then lost power, while in cruise flight at 6,500 feet MSL. The pilot attempted to land at a nearby airport; however, he subsequently landed short of the airport in a field approximately one mile southeast of the airport. During the landing roll, the airplane impacted a fence and fence posts, which resulted in leading edge damage to one wing and structural damage to both wing struts. The engine was examined by an FAA inspector, the aircraft owner, and a representative from the engine manufacturer at an local FBO. The contents of the fuel system were examined, and evidence of fuel contamination was found. The fuel in the tanks was yellow/straw in color and lacked the appearance of 100LL fuel; however, no diesel or jet fuel was detected. New spark plugs were installed, and the airplane was defueled and serviced with fresh 100LL fuel. The engine was started, and it operated normally through the normal operating range. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_FTW96LA345.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, fuel contamination). 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…
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