NTSB CAROL · Event
Event WPR18TA157
Aircraft involved
Probable cause & findings
A total loss of engine power due to the development of carburetor icing.
Factual narrative
On May 18, 2018, about 0809 Pacific daylight time, a Cessna 182D airplane, N9163X, was substantially damaged when it was involved in an accident near Crescent Mills, California. The private pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that, as he approached the destination airport, he observed fog low in the valley where the airport was located and began to circle at a low engine power setting. While circling, the engine lost total power. The pilot established the airplane's best glide speed and proceeded toward a river for a forced landing. The airplane impacted rocks and came to rest nose down with the left wing in the water, resulting in substantial damage to the right wing. The atmospheric conditions present in the area of the accident site included a surface temperature of 22°C, dew point of 7.5°C, and a relative humidity of 63%; consistent with a potential for serious carburetor icing at glide power settings. The pilot reported that when he arrived in the vicinity of the destination airport, there was fog in the valley where the airport was located, and he began circling the airplane at a low engine power setting. The engine subsequently lost total power, and the pilot performed a forced landing to a river, resulting in substantial damage to the right wing. The atmospheric conditions present in the area at the time of the accident were conducive to the development of serious carburetor icing at glide power settings which likely resulted in the loss of engine power. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Environmental issues-Conditions/weather/phenomena-Temp/humidity/pressure-Conducive to carburetor icing-Effect on equipment
Verbatim from NTSB's published report. Source file
NTSB_2018_WPR18TA157.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 ↗