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NTSB Safety Studies · Safety study
Bell 525 Relentless In-Flight Breakup
Attribution
This is the abstract and citation. Full text lives at NTSB Safety Studies — we link out rather than host. All credit to the authors and National Transportation Safety Board.
Abstract
Verbatim from NTSB Safety Studies. Not paraphrased, not summarized.
Investigation report and safety study on the 6 July 2016 in-flight breakup of a Bell 525 Relentless helicopter prototype during a developmental flight test near Italy, Texas. Examines vibration-induced pilot-output and biodynamic feedback that caused divergent control oscillations.
Author
- National Transportation Safety Board NTSB
Keywords
- rotorcraft
- flight test
- pilot-induced oscillation
Citation: National Transportation Safety Board (2019). Bell 525 Relentless In-Flight Breakup. National Transportation Safety Board. NTSB Safety Studies ID SS-19/01. https://www.ntsb.gov/investigations/AccidentReports/Pages/AAR1903.aspx ↗