NTSB CAROL · Event
Event DEN07LA130
Aircraft involved
Probable cause & findings
The loss of engine power due to carburetor icing. Contributing factors were the lack of suitable terrain for a forced landing and the weather conditions conducive for carburetor icing.
Factual narrative
On July 27, 2007, at 0817 eastern daylight time, a Cessna 150L, N19052, owned and piloted by the accident pilot, was substantially damaged when it impacted terrain following a loss of engine power while departing from Cooperstown-Westville Airport, Cooperstown, New York. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under the provisions of Title 14 Code of Federal Regulations Part 91 without a flight plan. The student pilot sustained serious injuries. The local flight was originating at the time of the accident. According to the Pilot/Operator Aircraft Accident Report Form submitted by the student pilot, he had just departed runway 20 (2,337 feet by 125 feet, turf). At approximately 400 feet the "engine sputtered, and then smoothed out." The student pilot stated that the engine sputtered again and then "quit." He attempted to restart the engine but was not successful. The student pilot stated that he attempted a shallow turn to reach a clearing but missed it by "about 20 or 30 feet." He stated that he felt the loss of power was due to "icing, as it was very warm and humid." According to the Federal Aviation Administration inspector who traveled to the accident scene, the airplane impacted trees. Both wings were crushed aft and both wings spars were bent. The engine separated partially from the airframe and the firewall was wrinkled. Both fuel tanks were compromised; however, approximately 3 gallons of automotive fuel was recovered from the left and right fuel tanks. An examination of the airplane and its related systems revealed no anomalies. The engine was secured to a forklift and rigged with an "improvised fuel system" for a test run. The engine started and ran for several minutes at varying power settings. Several weather observation stations recorded the temperature and dewpoint as 24 degrees Celsius (C) and 19 degrees C, respectively. According to the carburetor icing chart, conditions were conducive for "serious icing at glide power." According to the pilot, at approximately 400 feet the "engine sputtered, and then smoothed out." The pilot stated that the engine sputtered again and then "quit." He attempted to restart the engine but was not successful. The airplane impacted trees, resulting in substantial damage. An examination of the airplane and the powerplant revealed no anomalies. Several weather observation stations recorded the temperature and dewpoint as 24 degrees Celsius (C) and 19 degrees C, respectively. According to the carburetor icing chart, conditions were conducive for "serious icing at glide power." Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_DEN07LA130.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 ↗