Figure 24.Single Rotary Knob - Eclipse 500 System Manual

Section 2. Avio Avionics Suite
m. Single Rotary Knobs
Single rotary knobs on the PFD and MFD provide control of pilot and copilot
volume and squelch on the PFD and selection and acknowledgment of CAS
messages on the MFD.
2.5 Primary Sensors
Air data, attitude and navigation information are provided to the ACS by two
Integrated Sensor Suites (ISS). An ISS is comprised of three independent units
working together.
1. Three Air Data Computers (ADC)
2. Two Attitude Heading and Reference Systems (AHRS)
a. Two Magnetometers (MAGs)
3. Two Global Positioning Systems (GPS)
Information from all three of these systems is sent to the ACS for comparison and
failure monitoring, to FADECs for engine control and to the PFD and MFD for display.
2.6 Aircraft Subsystems
The Eclipse 500 aircraft Subsystems include:
Engines & Fire Protection
Fuel
Electrical
Electronic Circuit Breakers
⎯
Climate Control
Environmental
⎯
Pressurization
⎯
Version 2.0 April 2007
Figure 24. Single Rotary Knob
Copyright © — Eclipse Aviation Corporation
Eclipse 5OO Systems Manual
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