NTSB CAROL · Event
Event CEN10CA500
Aircraft involved
Probable cause & findings
A loss of engine power for undetermined reasons.
Factual narrative
The pilot reported that he was on a local flight and the engine gradually lost power. He performed the checklist for a loss of engine power and the airplane did not regain full power. The pilot stated that he picked a landing field, extended full flaps, and then the engine "quit." He pumped the throttle, the engine restarted, and he started to climb the airplane. The engine lost power again. The pilot picked another field and the airplane nosed over during the forced landing. The field contained corn. The airplane was recovered and the engine ran during a subsequent test run. The pilot reported that a cup of water was removed from the right fuel tank sump and a quarter cup from the front sump during the airplane preflight. The local airport's temperature and dew point were plotted on the carburetor icing chart listed in Special Airworthiness Information Bulletin CE-09-35. Their intersection fell in the “serious icing (glide power)” range. The pilot reported that he was on a local flight and the engine gradually lost power. He performed the checklist for a loss of engine power and the airplane did not regain full power. The pilot then chose an emergency landing field, extended full flaps, and the engine "quit." As the pilot pumped the throttle, the engine restarted and the airplane started to climb. The engine lost power again and the pilot chose another field. During the forced landing, the airplane nosed over. After the accident, the engine ran during a subsequent test run. The pilot reported that a cup of water was removed from the right fuel tank sump and a quarter cup from the front sump during the airplane preflight. The local airport's temperature and dew point were plotted on the carburetor icing chart listed in Special Airworthiness Information Bulletin CE-09-35, and their intersection fell in the “serious icing (glide power)” range. 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).
- C Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
Verbatim from NTSB's published report. Source file
NTSB_2010_CEN10CA500.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 ↗