NTSB CAROL · Event
Event CEN25LA327
Registry · N692AC
FAA Aircraft Registry record.
Make / Model
VAN'S AIRCRAFT RV-6A
Year of manufacture
2012 · 13 years old at event
Engine
LYCOMING O-320-D2J (160 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20121116
ADS-B equipped
Yes — Mode-S A93227
Registrant of record
MARSHALL CAROL A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On August 19, 2025, at 1640 central daylight time, a Vans RV-6A airplane, N692AC, was substantially damaged when it was involved in an accident near Centerview, Missouri. The commercial pilot sustained minor injuries and the passenger was uninjured. The airplane was operated under Title 14 Code of Federal Regulations as a Part 91 personal flight. The pilot stated there were no issues with the engine runup prior to the accident flight. He stated that this was his first flight in the make and model of accident airplane which was to familiarize himself with the airplane. After performing several maneuvers at 4,500 ft msl, he began to fly towards Skyhaven Airport (RCM), Warrensburg, Missouri. He said the engine sounded normal, but it was not producing power. He planned on continuing the flight to RCM where he now planned on performing a magneto check and to “recheck the engine.” About 3 miles from RCM, he performed the before landing checklist, changed the fuel tank selection, turned the fuel pump on, and confirmed the fuel mixture control was in the rich position. He reduced the throttle control about ¼ inches, heard a “slight pop,” and the engine lost power. He then changed the fuel tank selection, confirmed the fuel pump was on, and adjusted the engine throttle control, but was unable to regain engine power. He then changed fuel tank selection to the right fuel tank, added wing flaps, and performed a forced landing to a cornfield. He stated that the airplane, which was not equipped with a stall warning system, stalled above the corn during landing, and the airplane impacted the ground. The airplane sustained substantial damage to the fuselage. The airplane was retained for examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2025_CEN25LA327.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 ↗