NTSB CAROL · Event
Event NYC99LA044
Aircraft involved
Probable cause & findings
The pilot's inadequate preflight examination of the airplane, which resulted in a power loss due to fuel contamination.
Factual narrative
On January 2, 1999, about 0930 Eastern Standard Time, a Beech C24R, N1857G, was substantially damaged during a forced landing in Farmingdale, New York. The certificated private pilot and passenger sustained minor injuries. Visual meteorological conditions prevailed for the flight that originated from Republic Airport (FRG), Farmingdale, New York. No flight plan was filed for the personal flight conducted under 14 CFR Part 91. According to the pilot's written statement, he had a complete memory loss of the entire day of the accident. He wrote "[The] engine quit due to ice and water in [the] fuel." The passenger reported that he observed the pilot perform a preflight examination of the airplane, which included removing the fuel caps and looking into the tanks. He did not observe the pilot drain fuel from either the fuel tanks or the main airplane sump drain. After engine start, the pilot taxied to the run-up area, and reported that the engine was running rough. He also reported that he was going to taxi back to the ramp and speak with the owner of the airplane about the engine condition. Upon reaching the ramp, the pilot and passenger remained in the airplane with the engine running, while they visually scanned the area for the owner. Unable to see the owner, the pilot stated the engine was running normal now, and initiated taxi to the run-up area again. Upon completion of a successful run-up, the pilot radioed the tower and requested permission to takeoff. The airplane departed on Runway 32. After departure, on a right downwind, the passenger noticed that the engine, "began to stall." The passenger further reported that the engine lost all power, but the pilot was able to restart it. The pilot advised the tower of the power loss. The engine lost power again, and the pilot was unable to restart the engine. The pilot established a glide for Runway 32. The aircraft impacted the ground in a cemetery, approximately 1,800 feet short of Runway 32. The right aileron and nose gear were separated from the airplane. Both wings were partially separated from the airplane. The pilot was interviewed by an inspector from the Federal Aviation Administration (FAA). The Inspector reported that the pilot had struck his head during the forced landing and had no recollection of the flight. The Inspector's examination of the airplane revealed the main fuel bowl of the fuel strainer was contaminated with water, dirt, rust, paint, and sand. In addition, rust was found on the inlet screen to the fuel injection unit and on the fittings to the fuel injection manifold. The Inspector stated that there were no reports of fuel contamination to the other airplanes based at Republic Airport. After departure, on a right downwind leg, the passenger noticed that the engine 'began to stall.' The engine lost all power and the pilot was unable to restart it. The pilot established a glide for Runway 32, but the aircraft impacted the ground in a cemetery, approximately 1,800 feet short of Runway 32. According to the pilot's written statement, '[the] engine quit due to ice and water in [the] fuel.' During the preflight, the passenger did not observe the pilot drain fuel from either of the fuel tanks or the main airplane sump drain. A Federal Aviation Administration inspector found that the main fuel bowl of the fuel strainer was contaminated with water, dirt, rust, paint, and sand. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_NYC99LA044.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, fuel contamination). 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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