GAA15CA212
2015-08-02 · Reidsville, North Carolina, United States · Minor · 1 aircraft · Status: Completed
Airport SIF
Aircraft involved
Probable cause & findings
The student pilot landed with variable wind conditions, which resulted in an in-flight loss of control and subsequent impact with terrain.
Factual narrative
The student pilot reported that the weight-shift control aircraft crossed the runway threshold at 20 feet above the ground, the aircraft drifted to the right. The student pilot "raised the right wing tip, to correct up"; a "large gust" of wind lifted the right wing upward and turned the aircraft sideways. The aircraft impacted the ground, left main landing gear first. His foot "got stuck" in the foot actuated throttle, full throttle position, the aircraft impacted terrain on the edge of the adjacent taxi way. The pilot reported there were no pre-impact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The weight-shift-control aircraft sustained substantial damage to the wing.
METEOROLOGICAL INFORMATION
A review of recorded data from the automated weather observation station located on the airport that the accident occurred, elevation 693 feet, revealed that, at 1515, conditions were wind at 120 at 3 knots, visibility of 10 statute miles, sky clear. Runway Used: 31 Landing conditions at the time of the accident: about 3 knot tailwind and about .5 knot right crosswind. The student pilot reported that the weight-shift control aircraft crossed the runway threshold at 20 feet above the ground, the aircraft drifted to the right. The student pilot "raised the right wing tip, to correct up"; a "large gust" of wind lifted the right wing upward and turned the aircraft sideways. The aircraft impacted the ground, left main landing gear first. His foot "got stuck" in the foot actuated throttle, full throttle position, the aircraft impacted terrain on the edge of the adjacent taxi way. The pilot reported there were no pre-impact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The weight-shift-control aircraft sustained substantial damage to the wing. 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-Crosswind correction-Not attained/maintained - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Tailwind-Contributed to outcome
Verbatim from NTSB's published report. Source file
NTSB_2015_GAA15CA212.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 (loss of control). All research papers
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- Semantic Scholar 2024 · Article (International Conference on Networking and Services) Risk Assessment of Loss of Control In-Flight Trajectories for Urban Air Mobility Safety
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- Semantic Scholar 2021 · Article (Aviation) ANALYSIS OF GENERAL AVIATION FIXED-WING AIRCRAFT ACCIDENTS INVOLVING INFLIGHT LOSS OF CONTROL USING A STATE-BASED APPROACH
Inflight loss of control (LOC-I) is a significant cause of General Aviation (GA) fixed-wing aircraft accidents. The United States National Transportation Safety Board’s database provides a rich source…
- NASA NTRS 2021 · Presentation Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
Abstract—We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.