NTSB CAROL · Event
Event ERA24LA197
Registry · N3880B
FAA Aircraft Registry record.
Make / Model
BEECH F35
Engine
CONT MOTOR E225 SERIES (225 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19570322
ADS-B equipped
Yes — Mode-S A47B5C
Registrant of record
STILES DAVID W
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s inadequate preflight planning and failure to abort the takeoff at the predetermined decision point.
Factual narrative
The pilot and his passenger were preparing for a cross-country flight. After a routine preflight inspection and engine start, the pilot taxied to runway 27, which was 2,644 ft-long and comprised of turf. The grass was “mid height” and wet from the morning dew. The pilot commonly used a “hump” in the runway as a go/no-go decision point, which was about midfield. During the takeoff roll, he scanned his tablet device for speed and noted 47 knots; 52 knots was stall speed, configured. As the takeoff roll continued, he tried to “pop” the airplane off the ground and into ground effect; this attempt was unsuccessful. He realized that the airplane would not become airborne and it departed the end of the runway, collided with a berm, and spun around to a stop. A postaccident fire ensued and the pilot and passenger egressed the airplane without injuries. Despite attempts to extinguish the fire, it progressed and eventually consumed the fuselage. An inspector with the Federal Aviation Administration reported that the airplane was destroyed. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. He also reported that performing the “no go” decision at the hump in the runway would have prevented the accident. 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).
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained
- — Personnel issues-Task performance-Planning/preparation-Performance calculations-Pilot
- — Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2024_ERA24LA197.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 ↗