NTSB CAROL · Event
Event NYC04LA183
Aircraft involved
Probable cause & findings
The pilot's failure to maintain adequate airspeed and her premature rotation which resulted in an inadvertent stall/mush and subsequent impact with the ground.
Factual narrative
On August 3, 2004, at 1455 eastern daylight time, N7957U, a Cessna 172F, was substantially damaged when it impacted the runway, during takeoff from the Cooperstown-Westville Airport (K23), Cooperstown, New York. The certificated commercial pilot was seriously injured. Visual meteorological conditions prevailed and no flight plan was filed for the local personal flight conducted under 14 CFR Part 91. According to the pilot, she initiated the takeoff from runway 20 (a 2,600-foot long, 125-ft. wide turf runway), and during the takeoff roll, the airplane veered sharply to the left. She applied right rudder to realign the airplane on the centerline, and when "nothing changed," she "responded instinctively" and pulled back on the controls to lift the airplane off the runway. Because the airplane "lacked adequate airspeed," immediately after rotation, it descended, and impacted the ground. The pilot additionally stated that the correct action, to "pull the power back" and abort the takeoff, did not occur to her until it was too late. Examination of the airplane by the FAA inspector revealed substantial damage to the empennage of the airplane. No mechanical deficiencies were observed. The winds reported at an airport approximately 38 miles to the northwest, at 1456, were from 260 degrees at 3 knots. During the takeoff roll, the airplane veered sharply to the left. The pilot applied right rudder to realign the airplane on the centerline, and when the airplane did not respond, she "instinctively" pulled back on the controls to lift the airplane off the runway. Because the airplane "lacked adequate airspeed," immediately after rotation, it descended, and impacted the ground. The pilot stated that the correct action, "to pull the power back" and abort the takeoff, did not occur to her until it was too late. No mechanical deficiencies were observed with the airplane. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_NYC04LA183.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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