WPR10CA337
2010-07-03 · Neola, Utah, United States · Minor · 1 aircraft · Status: Completed
Airport 74V
Current FAA registration · N3143V
- Make / Model
- CESSNA 150M
- Year of manufacture
- 1974 · 36 years old at event
- Engine
- CONT MOTOR 0-200 SERIES (100 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19741209
- ADS-B equipped
- Yes — Mode-S A35882
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A partial loss of engine power for undetermined reasons and the pilot's failure to maintain clearance from a power line.
Factual narrative
The pilot reported that while practicing ground reference maneuvers the airplane's engine had what he described as a temporary partial loss of power. The pilot was flying back to the airport when the nose landing gear struck a power line. The pilot continued the flight back to the airport. When he attempted to land, the nose landing gear collapsed aft, substantially damaging the firewall. While review of the carburetor icing probability chart revealed that the weather conditions during the flight--a temperature of 26 degrees Celsius and a dew point of 6 degrees Celsius--were conducive to light icing during glide and cruise power, the investigation was unable to determine a cause for the reported power loss. The pilot reported that while practicing ground reference maneuvers the airplane's engine had what he described as a temporary partial loss of power. The pilot was flying back to the airport when the nose landing gear struck a power line. The pilot continued the flight back to the airport. When he attempted to land, the nose landing gear collapsed aft, substantially damaging the firewall. While review of the carburetor icing probability chart revealed that the weather conditions during the flight--a temperature of 26 degrees Celsius and a dew point of 6 degrees Celsius--were conducive to light icing during glide and cruise power, the investigation was unable to determine a cause for the reported power loss. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Psychological-Attention/monitoring-Monitoring environment-Pilot - C
- C Environmental issues-Physical environment-Object/animal/substance-Wire-Response/compensation - C
- C Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
Verbatim from NTSB's published report. Source file
NTSB_2010_WPR10CA337.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
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Related research
Matched on aircraft type or causal vocabulary (icing). All research papers
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- 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…
- 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…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER) A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
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- 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…