NTSB CAROL · Event
Event ATL03LA149
Aircraft involved
Probable cause & findings
Loss of engine power due to undetermined reasons.
Factual narrative
On September 27, 2003, at 1100 eastern daylight time, a Cessna 150A, N5581E, registered to and operated by a commercial pilot, collided with the ground while making an emergency landing on Core Banks Island, near Beaufort North Carolina. The personal flight was operated under the provisions of Title 14 CFR Part 91. Visual meteorological conditions prevailed at the time of the accident and no flight plan was filed. The airplane sustained substantial damage. The commercial pilot and passenger received minor injuries. The flight departed from a private grass strip in Harlowe, North Carolina, on September 27, 2003 at 1020. According to the pilot, while enroute to the Core Banks Island, he descended to an altitude of 500 feet to survey a "duck-blind" site. The pilot then reduced flaps, applied carburetor heat, and reduced the power. The engine began to run rough, and full throttle was applied. The carburetor heat control lever was in the "off" position, and the engine quit. Efforts by the pilot to restart the engine were unsuccessful, and an emergency landing area was chosen. During the emergency landing the airplane collided with the ground and came to rest inverted. No mechanical or flight control anomalies were reported by pilot prior to the accident. Examination of the airplane revealed that the left wing's leading edge was damaged from the tip-cap inboard approximately 24 inches. The nose strut assembly was bent aft at the attachment points. The firewall and fuselage aft of the baggage compartment were buckled. Examinations of the engine, revealed movement of all the intake and exhaust valves in all combustion cylinders, no anomalies with the ignition system were noted. A review of the icing probability chart revealed conditions were favorable for induction system icing. The Raleigh-Durham International Airport reported a temperature of 75 degrees Fahrenheit with a dew point of 68 degrees Fahrenheit. According to the pilot, while en route to the Core Banks Island, he descended to an altitude of 500 feet to survey the site. The pilot reduced flaps, applied carburetor heat, and reduced the power. The engine began to run rough, and full throttle was applied. The carburetor heat control was turned off and the engine quit. During the emergency landing the airplane collided with the ground and came to rest inverted. Examinations of the engine, revealed movement of all the intake and exhaust valves in all combustion cylinders, no anomalies with the ignition system were noted. No mechanical or flight control anomalies were reported by pilot prior to the accident. The Raleigh-Durham International Airport reported a temperature of 75 degrees Fahrenheit with a dew point of 68 degrees Fahrenheit. A review of the icing probability chart revealed conditions were favorable for induction system icing. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_ATL03LA149.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 ↗