NTSB CAROL · Event
Event CHI04CA115
Registry · N12JV
FAA Aircraft Registry record.
Make / Model
VILLENEUVE RV-3
Year of manufacture
1979 · 25 years old at event
Engine
LYCOMING 0-290 SERIES (140 hp)
Seats / Engines
1 seats · 1 engine
Last airworthiness date
19850924
ADS-B equipped
Yes — Mode-S A05235
Registrant of record
RAUN IAN O
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot failed to maintain airspeed and aircraft control during final approach, which resulted in a stall/mush flight condition. A factor to the accident was the crosswind and the trees.
Factual narrative
On May 8, 2004, at 1230 central daylight time, an amateur-built Villeneuve RV-3, N12JV, piloted by a private pilot, was substantially damaged during an in-flight collision with trees while on final approach to a private east/west airstrip (1,800 feet by 50 feet, dry turf) near Mayetta, Kansas. Visual meteorological conditions prevailed at the time of the accident. The personal flight was operating under the provisions of 14 CFR Part 91 without a flight plan. The pilot reported no injuries. The flight originated from the Phillip Billard Municipal Airport (TOP), Topeka, Kansas, at 1200 and was landing at the time of the accident. According to the pilot's written statement, he obtained weather information from the TOP automatic terminal information service (ATIS) and the winds were reported to be from the south at 15 knots, gusting to 20 knots. The pilot reported that the wind conditions were at his "upper personal limitations" and that he had previously landed in similar conditions. The pilot stated that after flying over the private airstrip he decided the winds favored a landing to the east. The pilot reported that when he was on final approach, approximately 100-200 feet above ground level (agl), the airplane "suddenly and abruptly rolled approximately 30 degrees right and then left while the nose maintained the same pitch attitude." The pilot stated he was able to level the wings, however, the "controls felt abnormally mushy." The pilot also reported that the "rate of descent also suddenly increased to a dangerous level." The pilot stated he added full engine power, but the aircraft kept descending. The pilot reported, "Given the mushy controls and rate of descent I was afraid to pull up too much and risk a stall. The aircraft was already at a nose high angle of attack... It already felt like it was on the edge of a stall. [The] aircraft continued to feel unstable with a dangerously high sink rate." The pilot reported the airplane was unable to "build up enough speed to break out of wind currents before contacting trees." Surface wind data was collected from a nearby weather observation facility. The collected wind data, along with the location of the facility was: Topeka, Kansas (TOP) (17 nm, 165 degrees magnetic) 1153: Wind 180 @ 9 knots, gusting 18 knots 1253: Wind 200 @ 11 knots The airplane impacted trees while on final approach. The pilot reported that when he was on final approach, approximately 100-200 feet above ground level, the airplane "suddenly and abruptly rolled approximately 30 degrees right and then left while the nose maintained the same pitch attitude." The pilot stated he was able to level the wings, however, the "controls felt abnormally mushy." The pilot also reported that the "rate of descent also suddenly increased to a dangerous level." The pilot stated he added full engine power, but the aircraft kept descending. The pilot reported, "Given the mushy controls and rate of descent I was afraid to pull up too much and risk a stall. The aircraft was already at a nose high angle of attack... It already felt like it was on the edge of a stall. [The] aircraft continued to feel unstable with a dangerously high sink rate." The pilot reported the airplane was unable to "build up enough speed to break out of wind currents before contacting trees." The pilot reported that the winds were from the south at 15 knots, gusting to 20 knots. The pilot stated the wind conditions were at his "upper personal limitations" and that he had previously landed in similar conditions. Surface wind data was collected from nearby weather observation facilities. The collected wind data indicated the winds at the time of the accident were from the south-southwest, between 9 and 18 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_CHI04CA115.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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