7.7 INSTRUMENTS AND AVIONICS
7.7.1 GENERAL INFORMATION
The diagram in section 7.5 represents the instrument panel-mounted avionics. A
description of specific equipment functionalities and operation is provided in the
table below.
Note:
• Power to the PFD and EMS is provided directly by the main bus.
• Power to GTN 650, Audio Panel and Remote Transponder need activation
by Avionics 1 switch.
• Backup KI300 and optional GNC255 need activation by Avionics 2 switch.
Both switches (Avionics 1 and Avionics 2) are located on the instrument panel
(Refer to paragraph 7.5).