Dynon Avionics EFIS-D60 Pilots Users Guide - Manual (Page 10)

Product Overview
2-2 EFIS-D60 Pilot’s User Guide
OUTPUTS
The EFIS-D60 has an output to drive an external customer-supplied audible device for AOA (if installed) and altitude
alerts.
A serial output is also provided for serial altitude encoder data. An optional Serial-to-Gray Code Converter is available
for connection to Mode C Gray Code transponders.
DISPLAY
The display is a 7-inch, 854 by 480 pixel, 800 nit LCD screen.
BUTTONS AND KNOBS
User interaction takes place via the six buttons along the bottom of the front panel of the unit.
ADAHRS Operation
The primary flight instruments on your EFIS display are generated using a group of calibrated sensors. All of them are
solid state – that is, there are no moving parts. These sensors include accelerometers, which measure forces in all three
directions; rotational rate sensors, which sense rotation about all three axes; pressure transducers for measuring air data;
and magnetometers on all three axes for measuring magnetic heading. These sensors form the core of Dynon’s Air Data
Attitude and Heading Reference System (ADAHRS).
The table below describes which inputs and sensors are used within the EFIS to generate the different displayed
instruments. It is not meant to enable in-flight troubleshooting, but is provided to convey how much of an integrated
system your EFIS is.