NTSB CAROL · Event
Event CEN12CA576
Registry · N215VS
FAA Aircraft Registry record.
Make / Model
CIRRUS DESIGN SR20
Year of manufacture
2003 · 9 years old at event
Engine
CONT MOTOR IO-360-ES (210 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20030528
ADS-B equipped
Yes — Mode-S A1CE01
Registrant of record
BELLUE BARRY LEE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot did not maintain control of the airplane while landing in gusty wind conditions.
Factual narrative
The pilot was conducting touch-and-go landings on runway 35. While on final approach for his third touch-and-go, the pilot felt a buffet and anticipated gusting wind conditions during the touchdown. Approximately 200 feet above the ground the stall warning horn sounded briefly and the airplane "dropped straight down." The airplane impacted the runway hard and bounced several times. The pilot added power in attempt to go around; however, the airplane did not respond and impacted the runway again in a nose low attitude. During the accident sequence the nose landing gear separated, the propeller was damaged, and the firewall wrinkled. The Federal Aviation Administration inspector who responded stated that there were no mechanical anomalies with the airplane. The pilot was conducting touch-and-go landings on runway 35. While on final approach for his third touch-and-go landing, the pilot felt a buffet and anticipated gusting wind conditions during the touchdown. About 200 feet above the ground, the stall warning horn sounded briefly and the airplane "dropped straight down." The airplane impacted the runway hard and bounced several times. The pilot added power in an attempt to go around; however, the airplane did not respond and impacted the runway again in a nose-low attitude. During the accident sequence the nose landing gear separated, the propeller was damaged, and the firewall wrinkled. Postaccident examination revealed no mechanical malfunctions or anomalies that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Windshear-Effect on operation
Verbatim from NTSB's published report. Source file
NTSB_2012_CEN12CA576.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 ↗