NTSB CAROL · Event
Event ERA25LA290
Registry · N67BG
FAA Aircraft Registry record.
Make / Model
SONEX AIRCRAFT SONEX
Year of manufacture
2015 · 10 years old at event
Engine
AEROVEE 2.1 (80 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20150910
ADS-B equipped
Yes — Mode-S A8D97F
Registrant of record
LEWINSKI GARY W
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On August 5, 2025, about 1131 eastern daylight time, a Lewinski Sonex, N67BG, was substantially damaged when it was involved in an accident near Tellico Plains, Tennessee. The private pilot was seriously injured. The airplane was operated as a Title 14?Code of Federal Regulations Part 91 personal flight. The pilot stated that in anticipation of an intended buyer coming to take possession of the airplane in several days, he washed it then performed several taxi tests. During one taxi run he noted a violent shake that stopped when he applied aft control input. He attributed the issue to be related to the nose wheel bearing. He then elected to fly once around the traffic pattern and after takeoff, with one notch of flaps extended, reported the airplane pulled suddenly to the left which he could not correct. Approaching trees ahead, he pulled aft on the control yoke and believed the airplane stalled. The airplane descended uncontrolled and came to rest in trees about 10 to 12 ft above ground level. A fire began in the engine compartment and with some difficulty he exited the cockpit and jumped to the ground. He reported no issues with the engine at any time during the flight. The pilot further stated that there was no failure or malfunction of the flight controls during his preflight check, or as part of a check before departure. Because he was wearing knee length cotton shorts, he sustained second-degree burns on the lower portion of one of his legs and first-degree burns on the lower portion of his other leg. The postcrash fire extensively damaged the cockpit area of the wreckage, which was recovered for further examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2025_ERA25LA290.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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