Combined Hydraulic Control Actuator

Technical Description
Combined hydraulic flight-control actuator. It receives mechanical pilot input, hydraulic pressure and electrical correction signals and provides powered actuation for longitudinal, lateral, directional and collective channels. The actuator works with redundant hydraulic supply and must be selected by full modification, overhaul status and aircraft configuration.

Verification Status
High – function and Mi-family use documented.

Source
https://aviamisto.com/catalog/helicopter-systems-for-mi-8-mi-17/control-and-hydraulic-systems-mi-8-mi-17/kau-115am-3/

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.