PRIMUS
r
1000 Integrated Avionics System
A28--1146--112--00
Electronic Flight Instrument System (EFIS)
4-86
MFD System Displays
The data acquisition units (DAU) collect all the information required for
the system displays. This information is displayed in the lower third of
the MFD and it is selected using the MFD bezel menu SYS button.
NOTE:
The last selected system display is shown on the MFD unless
the TCAS or checklist display is selected.
The system display area can show the following type of system
information:
D
Takeoff (T/O)
-- The takeoff digital display shows engine takeoff
reference temperatures, anti--ice system status, and engine oil quantity
levels. In addition, a synoptic of aircraft door status is displayed.
D
Environmental Control/Anti--Ice System (ECS A/I)
-- The ECS A/I
display is a synoptic display of cabin and cockpit temperatures, oxygen
pressure, and engine bleed air temperatures (for anti--ice purposes).
D
FUEL
-- The FUEL display is a synoptic display of aircraft fuel
quantity, fuel used, fuel temperature, and fuel tank pump status.
D
Hydraulic (HYD)
-- The HYD display is a synoptic display of
hydraulic fluid quantity and pressure, pump status, and brake
temperatures.
D
Electrical (ELEC
) -- The ELEC display is a synoptic display of the
electrical bus connections, generators, APU, GPU, and battery
status.
TAKEOFF (T/O)
The takeoff display shown in figure 4--50, displays the following
information.