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What is Citation Sovereign Flight Control Overview about?

The flight control system uses manual controls with some hydraulic and electric assistance. Lateral control is provided by ailerons and roll spoilers. Pitch control uses an electrically actuated horizontal stabilizer and mechanically operated elevators. Yaw control is via a rudder with pneumatic rudder bias assistance during single-engine operation. Trim is available for all three axes. Nosewheel steering is via rudder pedals or a handwheel.

Author

Ajie Dendy

Language

EN