Garmin G2000 Pilots Guide - Page 48

SyStem overview FliGHt inStrumentS SyStem overview 1.4 SyStem operation The displays are connected via a single Ethernet bus for high-speed communication. As shown in Figure 1-1, each IAU is connected to a single display. This allows the units to share information, enabling true system integration. normal DiSplay operation In normal operations, PFD present graphical flight instrumentation (such as heading, airspeed, altitude, vertical speed) on the Primary Flight Display (PFD) in either Full Mode or Split Mode. In Full Mode, the PFD occupies the entire display portion of the GDU 1400W. In Split Mode, the PFD is condensed to accommodate a Display Pane on the inboard portion of the GDU 1400W. The MFD displays a navigation information, as well as flight plan, weather, traffic and terrain information in either two Half Mode Display Panes or one Full Mode Display Pane, depending on the selection made on the Touchscreen Controller. The left portion of the MFD is dedicated to the Engine Indication System (EIS; see the EIS Section). The Touchscreen Controller provides radio management, Display Pane control, data entry, as well as feature selection and display of system information. eiS aauuDDi&ioocpn&aScnenlS FliGHt manaGement HaZarD avoiDance aFcS aDDitional FeatureS appenDiceS inDeX Figure 1-26 G2000 Normal Operation 34 Garmin G2000 Pilot's Guide for the Cessna T240 190-01263-01 Rev. A