GAA15CA004
2015-03-09 · Hurricane, Utah, United States · None · 1 aircraft · Status: Completed
Airport 1L8
Current FAA registration · N949WB
- Make / Model
- CIRRUS DESIGN SR22
- Year of manufacture
- 2003 · 12 years old at event
- Engine
- CONT MOTOR IO-550 SERIES (300 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20030109
- ADS-B equipped
- Yes — Mode-S AD308D
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control during the landing roll.
Factual narrative
The pilot reported that he entered a right traffic pattern for runway 19; on his first approach he noted that he was going to overshoot the runway and executed a go-around procedure. On his second attempt after he touched down on the runway, he reported a "radical" right quartering tail wind that pushed the airplane to the left of the runway. The airplane's left main tire departed the asphalt surface, the pilot then attempted a go-around by advancing the throttle to full and decreasing the flaps to 50 percent. The pilot stated that he was not gaining lift and the stall warning horn was audible. Subsequently the airplane impacted a ditch and bounced about 10 feet which resulted in substantial damage to the spar carry-through on the bottom of the fuselage. The pilot reported there were no pre-impact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The pilot reported that he entered a right traffic pattern for runway 19; on his first approach he noted that he was going to overshoot the runway and executed a go-around procedure. On his second attempt after he touched down on the runway, he reported a "radical" right quartering tail wind that pushed the airplane to the left of the runway. The airplane's left main tire departed the asphalt surface, the pilot then attempted a go-around by advancing the throttle to full and decreasing the flaps to 50 percent. The pilot stated that he was not gaining lift and the stall warning horn was audible. Subsequently the airplane impacted a ditch and bounced about 10 feet which resulted in substantial damage to the spar carry-through on the bottom of the fuselage. The pilot reported there were no pre-impact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Tailwind-Effect on operation
Verbatim from NTSB's published report. Source file
NTSB_2015_GAA15CA004.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.
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- NTSB CAROL Agency ↗
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Related research
Matched on aircraft type or causal vocabulary (stall, go-around). All research papers
- 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 …
- NASA NTRS 2025 · Conference Paper A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- 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.
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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…