System Description; Primary Flight Instruments - Garmin G3X TOUCH Single 7 Manual

7 SYSTEM DESCRIPTION

The G3X Touch EFIS is scalable with a variety of configurations supported. The functions described
in this section may not be available in all aircraft depending on installed equipment and interfaces. A
minimum installation with a single display may be a standalone MFD or a PFD which can be split
screened to provide both PFD and MFD functions. Optional functions include EIS, datalink traffic and
weather, AOA, autopilot interface, remote audio panel, GPS/NAV/COM interface, transponder
interface, and others.
7.1

Primary Flight Instruments

When a PFD is installed, attitude information is displayed over a virtual blue sky and synthetic ground
with a white horizon line. The Attitude Indicator displays the pitch (indicated by the Amber symbolic
aircraft on the pitch scale), roll, and slip/skid information.
The horizon line is part of the pitch scale. Pitch markings occur at 2.5˚ intervals through all pitch ranges.
The inverted white triangle indicates zero on the roll scale. Major tick marks at 30˚ and 60˚ and minor
tick marks at 10˚, 20˚, and 45˚ are shown to the left and right of the zero. Angle of bank is indicated by
the position of the pointer on the roll scale.
Slip/skid is indicated by the location of the ball.
Bezel Overview (GDU 460)
190-01754-01 Rev. 5 AFMS or Supplemental AFM for the Garmin G3X Touch EFIS
P a g e | 7-1