AP hydraulic unit – series actuators

The hydraulic unit (also called the auxiliary servo-control unit) is the power control of the AFCS: it transmits and amplifies the orders elaborated by the AFCS to the flight controls, and still allows manual piloting if the AFCS fails. Each series actuator comprises a servo-control actuator, a distributor valve and a servo-valve driven by the two APMs.

103 bar Output to flight rod –on to the control channel By-pass actuator spring –joins A and B without pressure Servo-control actuator,distributor valve, servo-valve Electrical connector –orders from APM 1 and APM 2 Common hydraulic block –103 bar from the LH system

Four series actuators, one per channel: pitch, roll, yaw and collective. Click an actuator to open the functioning principle.