ERA13CA090
2012-12-20 · Hot Springs, Virginia, United States · None · 1 aircraft · Status: Completed
Airport HSP
Aircraft involved
Probable cause & findings
The pilot’s failure to maintain airplane control while attempting to land in crosswind conditions.
Factual narrative
According to the pilot, the airplane experienced light turbulence during the final approach to runway 7 and the wind sock indicated a direct crosswind from the right. The airplane touched down on the runway, bounced, and the pilot added engine power. As the power increased, the attitude of the airplane increased, and the pilot attempted to level the airplane. Then, the stall warning horn sounded, the right wing of the airplane lifted, and the airplane turned about 45 degrees off the runway centerline. The airplane subsequently impacted the ground near a taxiway off the left side of the runway, and struck several trees prior to coming to rest, which resulted in substantial damage to both wings. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. The wind reported at the airport about the time of the accident was from 140 degrees at 8 knots gusting to 17 knots. According to the pilot, the airplane experienced light turbulence during the final approach to runway 7, and the wind sock indicated a direct crosswind from the right. The airplane touched down on the runway, bounced, and the pilot added engine power. As the power increased, the pitch of the airplane increased, and the pilot attempted to level the airplane. The stall warning horn sounded, the right wing of the airplane lifted, and the airplane turned about 45 degrees off the runway centerline. The airplane subsequently impacted the ground near a taxiway off the left side of the runway, and struck several trees before coming to rest, which resulted in substantial damage to both wings. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. The wind reported at the airport about the time of the accident was from 140 degrees at 8 knots gusting to 17 knots. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Crosswind-Contributed to outcome
Verbatim from NTSB's published report. Source file
NTSB_2012_ERA13CA090.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (stall, turbulence). All research papers
- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA) Comparative Study on the Prediction of Aerodynamic Characteristics of Mini - Unmanned Aerial Vehicle with Turbulence Models
When dealing with CFD simulations the turbulent nature is seen on most of the engineering flows and these flows need to be solved.
- arXiv 2020 · arXiv preprint Numerical Simulation of Iced Wing Using Separating Shear Layer Fixed Turbulence Models
Aerodynamic prediction of glaze ice accretion on airfoils and wing is studied using the Reynolds-averaged Navier-Stokes method.
- NASA NTRS 2019 · Conference Paper Prediction of stall and post-stall behavior of airfoils at low and high Reynolds numbers
An interactive boundary-layer method, together with the e(super n)-approach to the calculation of transition, has been used to predict the stall and post-stall behavior of airfoils at low and high Rey…
- arXiv 2026 · arXiv preprint Direct Numerical Simulations of Ice-Ocean Boundary Turbulence
Turbulent heat and freshwater transport at ice-ocean interfaces controls glacier and iceberg melt rates, yet the underlying physics remains poorly constrained.
- 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 2025 · arXiv preprint Explainable LiDAR 3D Point Cloud Segmentation and Clustering for Detecting Airplane-Generated Wind Turbulence
Wake vortices - strong, coherent air turbulences created by aircraft - pose a significant risk to aviation safety and therefore require accurate and reliable detection methods.