NTSB CAROL · Event
Event ATL06CA015
Aircraft involved
Probable cause & findings
The loss of engine power due to carburetor icing, and the pilot's failure to use carburetor heat.
Factual narrative
According to the pilot, approximately 30 minutes into the instrument flight after reaching a cruise altitude of 7,000 feet in the clouds the engine surged, and began to lose power. The pilot switched fuel tanks, and turned on the electric fuel pump. No fuel pressure was noted on the fuel gauge, and the engine did not regain full power. The pilot reported that he did not apply carburetor heat during the loss of engine power. The pilot radioed air traffic control, and declared an emergency. During the emergency landing the airplane collided with trees. Post-accident examination of the airplane revealed the fuselage was buckled; both wing assemblies were separated from the fuselage. Post-accident examination of the airplane revealed no mechanical or flight control anomalies. Review of Advisory Circular 20-113 item 7.A-8 states: If induction system ice is suspected of causing a power loss, apply full heat or alternate air. Do not disturb the throttle until improvement is noted. Expect a further power loss momentarily and then a rise in power as the ice is melted. According to the pilot, approximately 30 minutes into the instrument flight after reaching a cruise altitude of 7,000 feet in the clouds the engine surged, and began to lose power. The pilot switched fuel tanks, and turned on the electric fuel pump. No fuel pressure was noted on the fuel gauge, and the engine did not regain full power. The pilot reported that he did not apply carburetor heat during the loss of engine power. The pilot radioed air traffic control, and declared an emergency. During the emergency landing the airplane collided with trees. Post-accident examination of the airplane revealed the fuselage was buckled; both wing assemblies were separated from the fuselage. Post-accident examination of the airplane revealed no mechanical or flight control anomalies. Review of Advisory Circular 20-113 item 7.A-8 states: "If induction system ice is suspected of causing a power loss, apply full heat or alternate air. Do not disturb the throttle until improvement is noted. Expect a further power loss momentarily and then a rise in power as the ice is melted." Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_ATL06CA015.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 ↗