NTSB CAROL · Event
Event DFW07CA127
Aircraft involved
Probable cause & findings
The loss of engine power while climbing due to the pilot's failure to refuel the airplane prior to fuel exhaustion. A factor associated with the accident was the soft terrain at the forced landing site.
Factual narrative
The 450-hour private pilot reported that shortly after takeoff, the engine of his single-engine airplane developed an abnormal engine fluctuation while climbing through an altitude of 1,300 feet MSL. As a precaution, the pilot elected to return to the departure airport; however, while turning back to the airport, the engine lost power and he prepared for a forced landing to an open field. Prior to the forced landing, the pilot noticed freshly dug ditches on both side of the field, so he repositioned to an adjacent field located to the right of his initial landing spot. The pilot added that the engine began to surge when the airplane was about 300 feet above the ground, which extended his glide. The airplane touched down on soft ground, the tires sunk in the soft ground and the airplane nosed-over. Examination of the airplane revealed the fuel bladders in both wings were not breached and there was no evidence of fuel stains around the vented fuel caps. Approximately 1-gallon of light blue colored fuel was drained from the right tank, and less than 1-gallon of light blue colored fuel was drained from the left tank. The fuel was found to be free of water and debris. The engine mounted fuel strainer bowl was found empty and the fuel screen was also absent of debris. The pilot reported that he did a pre-flight inspection of the airplane, but did not visually inspect the fuel tanks. Instead he relied on a fuel flow meter installed in the cockpit, which indicated a total of 43.6 gallons. The pilot reported that the gauge was usually accurate and he was unaware of what happened to the fuel he thought was onboard. Weather at the departure airport was reported as calm winds, visibility 8 statute miles, and clear skies. The private pilot reported that shortly after takeoff, the engine of his single-engine airplane developed an abnormal fluctuation while climbing through 1,300 feet MSL. As a precaution, the pilot elected to return to the departure airport; however, while turning to the airport, the engine lost power, and he prepared for a forced landing to an open field. Prior to the forced landing, he noticed freshly dug ditches on both side of the field, and he repositioned to an adjacent field to the right of his initial landing spot. The pilot added that the engine began to surge when the airplane was about 300 feet above the ground, which extended his glide. The airplane touched down on soft ground, the tires sunk in, and the airplane nosed-over. Examination of the airplane revealed the fuel bladders in both wings were not breached and there was no evidence of fuel stains around the vented fuel caps. Approximately 1-gallon of light blue fuel was drained from the right tank, and less than 1-gallon of light blue fuel was drained from the left tank. The fuel was free of water and debris. The engine mounted fuel strainer bowl was empty, and the fuel screen was clean. The pilot reported that he did a preflight inspection of the airplane, but did not visually inspect the fuel tanks. Instead he relied on a fuel flow meter installed in the cockpit, which indicated a total of 43.6 gallons. The pilot reported that the gauge was usually accurate, and he was unaware of what happened to the fuel he thought was onboard. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_DFW07CA127.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 exhaustion). 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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