Technical Description
Tail rotor assembly used by the anti-torque and directional-control system. It converts blade-pitch commands into lateral thrust to counter main-rotor torque and control yaw. Public references identify this P/N as a complete tail rotor assembly rather than only an isolated hub, so procurement scope should be confirmed against the aircraft IPC.
Verification Status
High for the assembly P/N; verify supply scope and series.
Source
https://aviamisto.com/catalog/helicopter-systems-for-mi-8-mi-17/powerplant-rotor-transmission-for-mi-8-mi-17/246-3904-000-ser-01/
Identification Note
The photograph is provided for reference. Procurement identification must be based on data plate markings, P/N, S/N, approved configuration and airworthiness documentation, not visual appearance alone.






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