NTSB CAROL · Event
Event DFW06LA104
Aircraft involved
Probable cause & findings
An in-flight electrical fire for undetermined reasons. A contributing factor was the lack of suitable terrain for the forced landing.
Factual narrative
On April 14, 2006, approximately 1500 central daylight time, a Cessna 210F single-engine airplane, N1966S, was destroyed by fire following an in-flight fire and subsequent emergency landing near Lubbock, Texas. The private pilot, sole occupant of the airplane, sustained minor injuries. The airplane was registered to and operated by the pilot. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The 429-nautical mile cross-country flight originated from the Town and Country Airpark (F82), near Lubbock, Texas, about 1455, and was en route to the Hawthorne Field Airport (45R), near Silsbee, Texas. According to the 200-hour pilot, approximately five to seven minutes after takeoff, he heard a "poof" sound come from behind the instrument panel, smelled an odor consistent with an electrical fire, and observed dark gray smoke and flames around his feet. The pilot further stated that he observed that none of the circuit breakers had "popped" and the amperage gauge was still indicating a " full charge." The pilot responded by turning off the electrical master switch, to which no change was noted. The pilot subsequently elected to perform an off-airfield emergency landing to plowed cotton field with the landing gear extended. Shortly after touchdown, the airplane nosed-over and came to rest in an inverted position. The pilot was able to egress the airplane unassisted. The airplane was engulfed in flames within a few minutes of coming to rest. The pilot attempted to fight the fire with the on-board portable fire extinguisher to no avail. The pilot further reported that three to four weeks prior to the accident flight, a loaner radio had been installed; however, the airplane had been flown approximately fifteen hours since its installation without problems. Representatives from the Federal Aviation Administration and Cessna Aircraft Company examined the wreckage of the airplane at the accident site. The cockpit area, extending forward to the firewall, and inboard section of both wings were destroyed by fire. No visible area of torching was present. Several components were further examined at Cessna Aircraft under FAA oversight; however, due to the extent of fire damage the origin of the fire could not be determined. The 200-hour private pilot elected to land in a plowed cotton field following an in-flight electrical fire. Shortly after touchdown the airplane nosed over and came to rest in an inverted position. The pilot was able to egress the airplane unassisted. The airplane was engulfed in flames within a few minutes after it came to rest. Due to the extent of fire damage, investigative team was unable to determine the origin of the in-flight fire. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_DFW06LA104.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…
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