Eclipse 500 System Manual page 52

Section 2. Avio Avionics Suite
Ice Protection
Landing Gear
Flight Controls
Oxygen
Autoflight
Autopilot
⎯
Autothrottle (Future Functionality)
⎯
All aircraft subsystems have Aircraft Computer System interfaces that are outlined in
the various systems chapters. For most of the aircraft systems direct pilot control is
provided through MFD synoptic pages. Exceptions to this are Oxygen (controlled on
the left switch panel), Landing Gear (controlled through the center switch panel), and
Autoflight (controlled through the autopilot control panel).
While most aircraft systems functions are shared between the ACS units, there are
some that are routed through a specific on-side ACS. Flap and landing gear
actuators are controlled by the onside ACS (i.e. left ACS controls left flap actuators).
Trim also functions in this manner; the left ACS controls the left pitch trim actuator as
well as the roll trim actuator, while the right ACS controls the right pitch trim actuator,
as well as the yaw trim.
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Copyright © — Eclipse Aviation Corporation
Eclipse 5OO Systems Manual
Version 2.0 April 2007