NTSB CAROL · Event
Event NYC05LA010
Aircraft involved
Probable cause & findings
The pilot's failure to maintain aircraft control during takeoff, which resulted in a collision with terrain. A factor was a crosswind.
Factual narrative
On October 26, 2004, about 1355 eastern daylight time, a Fairchild 24R-40, N28539, was substantially damaged during takeoff from a private airstrip in Custar, Ohio. The non-certificated pilot was seriously injured, and subsequently passed away 42 days later. Visual meteorological conditions prevailed, and no flight plan was filed for the local personal flight conducted under 14 CFR Part 91. According to a Federal Aviation Administration (FAA) inspector, the pilot was involved in a forced landing with the same airplane during September 2002. That investigation revealed that the pilot was flying without a medical certificate, which had been denied approximately 10 years prior. In addition, the pilot had performed an unauthorized alteration to the airplane by installing a Chevrolet V-8 engine. Subsequently, his private pilot certificate, airframe and powerplant certificate, and inspector airworthiness certificate were revoked. The pilot's stepson stated that the pilot had intended to sell the airplane. The pilot reinstalled the original engine, and was attempting to bring the airplane up to specifications. On the day of the accident, the stepson heard the engine running, and assumed the pilot was testing it. The stepson then observed the tailwheel airplane traveling on runway 18, an approximate 1,100-foot long, 25-foot wide, turf runway. The stepson could not see the airplane as it passed behind a barn, and then saw it resting on its right side, off the right side of the runway. The reported wind at an airport approximately 20 miles north of the accident site, at 1352, was from 100 degrees at 8 knots. Examination of the wreckage by an FAA inspector did not reveal any pre-impact mechanical malfunctions. The pilot had his airman and mechanic certificates revoked by the FAA about 2 years prior to the accident. He intended to sell the airplane, and was in the process of reinstalling the original engine, and bringing the airplane up to specifications. On the day of the accident, the pilot started the engine and attempted to depart on runway 18, an approximate 1,100-foot long, 25-foot wide, turf runway. A witness could not see the airplane as it passed behind a barn, but then saw it resting on its right side, off the right side of the runway. The reported wind about the time of the accident, was from 100 degrees at 8 knots. Examination of the wreckage did not reveal any pre-impact mechanical malfunctions. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_NYC05LA010.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…
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