NTSB CAROL · Event
Event CEN13LA504
Aircraft involved
Probable cause & findings
The pilot's failure to properly set the engine power for takeoff, which resulted in the airplane subsequently settling into terrain.
Factual narrative
On August 22, 2013, at 0845 central daylight time, a Gulfstream AM G-164B airplane, N8402K, impacted terrain during takeoff near Walnut Ridge, Arkansas. The commercial pilot, who was the sole occupant, was not injured. The airplane sustained substantial damage to the fuselage and both wings. The airplane was registered to and operated illegally by the pilot under the provisions of 14 Code of Federal Regulations Part 137 as an aerial application flight. Visual meteorological conditions prevailed for the flight and a flight plan was not filed. The local flight was originating at the time of the accident. The pilot stated that during the takeoff, he did not have the engine power set properly for takeoff. While in ground effect, the airplane began to stall and settled into the terrain. The airplane came to rest upright. The pilot reported no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. According to the Federal Aviation Administration (FAA), the pilot did not possess a Part 137 operating certificate. Numerous requests to obtain a completed Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1) were unsuccessful. The pilot did not have the engine power set properly when he took off for an aerial application flight. While in ground effect, the airplane began to stall and settled into the terrain. The airplane came to rest upright. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. The pilot did not possess a Part 137 operating certificate. 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 Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Powerplant parameters-Incorrect use/operation - C
- C Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2013_CEN13LA504.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 ↗