NTSB CAROL · Event
Event NYC00LA121
Aircraft involved
Probable cause & findings
The pilot's inadequate preflight, and the water that remained in the fuel system after the preflight.
Factual narrative
On April 25, 2000, about 2020 Eastern Daylight Time, a Cessna 150D, N4182U, was substantially damaged when it collided with an electrical wire during a forced landing, just after takeoff from Red Stewart Airfield (40I), Waynesville, Ohio. The certificated private pilot was not injured. Visual meteorological conditions prevailed at the time of the accident. No flight plan had been filed for the flight, between Waynesville and Cincinnati West Airport (I67), Harrison, Ohio. The personal flight was conducted under 14 CFR Part 91. The pilot reported that the flight was the second one of the day. During the preflight for the first flight, he found water in the "right [fuel] tank and engine compartment sump; drained until completely clear." He started up the airplane, and completed his run-up checks. He then flew the airplane 39 statute miles without any problems, landed, and shut down the engine for approximately 20 minutes. He then restarted the engine, taxied to the runway, and made a full-throttle, soft-field takeoff. During the takeoff run, the engine sounded like it was producing full power, but the airplane appeared to take longer than normal to build up airspeed. Once airborne, about 75 to 100 feet, the engine sputtered, then quit. There wasn't enough time for a restart, and there were trees and houses ahead, so the pilot turned about 90 degrees to the left, towards a field between some power lines and a highway. Approaching the field, the airplane's landing gear hit the top power line, and the airplane stalled, then dropped from a height of about 25 feet. The nose landing gear collapsed, and the airplane flipped over. According to a Federal Aviation Administration (FAA) inspector, the airplane had about 15 gallons of fuel remaining onboard after the accident, but the engine could not be run due to carburetor damage. The inspector drained the carburetor bowl, and found about 4 ounces of liquid, all of which, was water. Also according to the inspector, the pilot stated he had previously had problems with water in the fuel system. During the pilot's preflight, he found water in the right fuel tank and sump, which he drained until they were completely free of the water. He then started up the airplane, went through all the ground checks, and flew the airplane about 39 statute miles without any problems. He landed the airplane, and shut down the engine for approximately 20 minutes. He then restarted the engine, taxied the airplane to the runway, and made a full-throttle, soft-field takeoff. During the takeoff run, the engine sounded like it was making full power, but the airplane appeared to take longer than normal to build up airspeed. Once airborne, about 75 to 100 feet, the engine sputtered, then quit. Approaching an open field, the airplane's landing gear hit an electrical power line. The airplane stalled, then dropped from a height of about 25 feet. The nose landing gear collapsed, and the airplane flipped over. During a post-accident inspection, about 4 ounces of liquid were found in the carburetor bowl, all of which, was water. The pilot stated that he had previously had problems with water in the fuel system. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_NYC00LA121.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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