WPR20CA171
2020-06-04 · Murphy, Idaho, United States · Minor · 1 aircraft · Status: Completed
Aircraft involved
Probable cause & findings
The pilot's failure to maintain clearance from a power line while maneuvering during an aerial application flight.
Factual narrative
The pilot reported that during the aerial application flight, while maneuvering at low altitude, he came upon some trees and increased altitude to climbed above the treetops. He did not see that there were power lines behind the trees and did not have enough time to avoid colliding with two of the lines. The pilot was unable to maintain control of the helicopter descended in a slow spin to ground impact. The helicopter sustained substantial damage to the fuselage and tail boom. The pilot reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Environmental issues-Physical environment-Object/animal/substance-Wire-Effect on operation
- — Personnel issues-Psychological-Attention/monitoring-Monitoring environment-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2020_WPR20CA171.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.
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Related research
Matched on aircraft type. All research papers
- NASA NTRS 2019 · Abstract Convective Weather Avoidance with Uncertain Weather Forecasts
Convective weather events have a disruptive impact on air traffic both in terminal area and in en-route airspaces. In order to make sure that the national air transportation system is safe and efficie…
- NASA NTRS 2019 · Conference Paper Constitutive modelling of single crystal and directionally solidified superalloys
The trend towards improved engine efficiency and durability places increasing demands on materials that operate in the hot section of the gas turbine engine.
- Embry-Riddle Scholarly Commons 2016 · Conference paper Late Afternoon Concurrent Sessions: GSIS Symposium: UAS Collaboration & Research Opportunities: Presentation: Adaptation of Forward Military Airspace Management Systems for Civilian UAS Emergency Services Operations
Potential use of unmanned aircraft system (UAS) to save lives, improve safety, and protect property has generated preliminary research in three major areas of the fire service, including aviation, str…
- NASA NTRS 2013 · Conference Paper Thermodynamic and fluid mechanic analysis of rapid pressurization in a dead-end tube
Three models have been applied to very rapid compression of oxygen in a dead-ended tube. Pressures as high as 41 MPa (6000 psi) leading to peak temperatures of 1400 K are predicted.