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This chapter discusses the hydraulic power systems on the Bell 212 helicopter. It has two independent hydraulic systems that power the dual servoactuators for the main rotor cyclic and collective controls. One system also powers the single anti-torque servoactuator. The hydraulic systems provide assistance to the pilot in moving the flight controls and dampening dynamic feedback forces. Components of the hydraulic systems include reservoirs, pumps, filters, relief valves, accumulators, and servoactuators. M

Author

Bechir Foudhaili

Language

EN