ERA22LA059
2021-11-14 · Burnsville, North Carolina, United States · Minor · 1 aircraft · Status: Completed
Airport 2NC0
Current FAA registration · N633CD
- Make / Model
- CIRRUS DESIGN SR22
- Year of manufacture
- 2002 · 19 years old at event
- Engine
- CONT MOTOR IO-550 SERIES (300 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20021101
- ADS-B equipped
- Yes — Mode-S A84917
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s failure to compensate for the high density altitude and the tailwind component while landing at a mountaintop airport, which resulted in an aerodynamic stall and a loss of aircraft control.
Factual narrative
The pilot was performing a visual approach to a mountaintop airport with an estimated density altitude of 9,860 ft, and a tailwind component. He stated he “carried some extra speed” during the approach to compensate for wind and turbulence that he described as “burpy.” As he started to flare, he got pushed hard to his left. He lowered the nose and increased engine power to abort the landing, but the airplane struck trees and a small building before coming to rest inside the wood line on the left side of the runway, which resulted in substantial damage to both wings and the fuselage. Airport surveillance video depicted the airplane on approach, and as its attitude flattened in the landing flare, its nose and left wing deflected downward, and the airplane departed the left side of the runway where it struck trees and a building. The pilot reported that there were no mechanical deficiencies with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Capability exceeded
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
- — Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot
- — Environmental issues-Conditions/weather/phenomena-Wind-Tailwind-Effect on equipment
- — Environmental issues-Conditions/weather/phenomena-(general)-(general)-Effect on equipment
Verbatim from NTSB's published report. Source file
NTSB_2021_ERA22LA059.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
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- Pilots of America Community ↗
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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.