NTSB CAROL · Event
Event GAA19CA287
Aircraft involved
Probable cause & findings
The pilot's failure to maintain the proper airspeed and his exceedance of the airplane's critical angle of attack during takeoff, which resulted in an aerodynamic stall.
Factual narrative
The pilot receiving instruction reported that, during takeoff on the grass adjacent to a paved runway, after adding full power, he held the stick back during acceleration. He added that, the airplane did not accelerate "much above the red line (40 mph)". He felt a "bump", the airplane bounced, and veered to the right. The pilot added left rudder to correct, but the landing gear collapsed, and the propeller struck the ground. The flight instructor reported that, during the takeoff, the angle of attack was "higher than normal" and the airplane aerodynamically stalled 3 ft above the ground. The right wing dropped, the airplane yawed to the right, and he and the pilot receiving instruction attempted to recover with nose down, left rudder, and left aileron input. The airplane landed sideways, the landing gear collapsed, and the propeller struck the ground. The airplane sustained substantial damage to the right wing. The pilot and flight instructor reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The automated weather observation station, located about 4 miles southwest, reported that, about 5 minutes before the accident, the wind was from 290° at 5 knots. The pilot was departing runway 14. The pilot receiving instruction reported that, during takeoff from the grass adjacent to a paved runway, after adding full power, he held the stick back during acceleration. He added that the airplane did not accelerate "much above the red line (40 mph)" and that he felt a "bump." The airplane then bounced and veered right. The flight instructor reported that, during the takeoff, the angle of attack was "higher than normal" and that the airplane aerodynamically stalled 3 ft above ground level. The right wing dropped, the airplane yawed right, and he and the pilot attempted to recover with nose-down, left-rudder, and left-aileron inputs. The airplane landed sideways, the landing gear collapsed, and the propeller struck the ground. The airplane sustained substantial damage to the right wing. The pilot and instructor reported that there were no preaccident mechanical failures or malfunctions with the airplane 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
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Capability exceeded - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
Verbatim from NTSB's published report. Source file
NTSB_2019_GAA19CA287.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 ↗