NTSB CAROL · Event
Event NYC01LA060
Aircraft involved
Probable cause & findings
A loss of engine power for undetermined reasons.
Factual narrative
On December 24, 2000, about 1130 Eastern Standard Time, a Cessna 182P, N58833, was substantially damaged during a forced landing after takeoff from the Freeway Airport (W00), Mitchellville, Maryland. The certificated commercial pilot and a passenger sustained minor injuries. Visual meteorological conditions prevailed and no flight plan had been filed for the personal flight destined for the Easton Airport, Easton, Maryland. The flight was conducted under 14 CFR Part 91. During a telephone interview, the pilot stated that he performed a pre-flight inspection of the airplane, which included sumping the airplane's wings and "belly" fuel drains. After an engine run-up, which included a carburetor heat check, the airplane departed Runway 18. The pilot described the takeoff roll and lift-off as normal; however, when the airplane was about 250 to 300 feet above the runway, he experienced a significant loss of engine power, "like the throttle was pulled back to the idle position." He applied carburetor heat, and verified that the throttle, propeller, and mixture settings were in the full forward positions. The pilot performed a forced landing into trees, about 3/4 mile south of the airport. The pilot further described the power loss as, "very smooth, with no sputtering." He did not recall the engine RPM. Examination of the wreckage by a Federal Aviation Administration (FAA) inspector and representative from Teledyne Continental Motors did not reveal any mechanical malfunctions. The top rows of spark plugs were removed. Their electrodes were intact and sooted. The engine crankshaft was then rotated by turning the propeller and thumb compression was noted on all cylinders. Additionally, spark was obtained from all top spark plug leads. Examination of the carburetor did not reveal any malfunctions. Additionally, the fuel observed in the carburetor inlet line and carburetor bowl was light blue and absent of contamination. It was noted that the carbureted air box was unobstructed. The pilot reported 800 hours of total flight experience, of which, about 600 hours was in the make and model of the accident airplane. The temperature and dewpoint reported about the time of the accident, at an airport about 17 miles north-northeast of W00 was: 34 degrees F, and 12 degrees F, respectively. Examination of an FAA carburetor icing probability chart revealed that the reported temperature and dewpoint was outside of the probable icing range. Additionally, the pilot stated that the engine was equipped with a carburetor ice detector, which did not indicate a carburetor icing condition. The pilot stated that he performed a pre-flight inspection of the airplane and an engine run-up, which included a carburetor heat check. He then began his takeoff roll. The pilot described the takeoff roll and lift-off as normal; however, when the airplane was about 250 to 300 feet above the runway, he experienced a significant loss of engine power. The pilot performed a forced landing into trees, about 3/4 miles south of the airport. Examination of the wreckage did not reveal any mechanical malfunctions. Additionally, the fuel observed in the carburetor bowl was light blue in color and absent of contamination. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_NYC01LA060.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 (icing). 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 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗