CHAPTER 5
REFERENCE GUIDE
EFD1000/500 MAX MFD Pilot’s Guide
Page 5-78
091-00006-002 ()
EFD1000/500 MAX MFD Pilot’s Guide
Page 5-79
091-00006-002 ()
5.10 SecondaryAttitude Instrument
(EFD1000 MFD only)
The Secondary Attitude Instrument VIEW provides a secondary display of aircraft
attitude, altitude, and airspeed. The VIEW consists of a basic attitude indicator overlaid
with numerical airspeed and altitude data displayed in the upper left WINDOW of the
thumbnail LAYOUT (PAGE 3/3) (
Figure 5-107
).
Airspeed and Altitude
The Indicated Airspeed (IAS) is displayed in a rolling drum format using the same units
of measure (i.e., Knots or Miles per Hours) as the PFD. The IAS displays with a resolution
of 1 unit and a range of 20 to 999 units and is dashed if the IAS is below 20.
The IAS is rendered in red if the current IAS is greater than Vne or is less than Vso and the
red low speed band is enabled. The red low speed band enables when the IAS exceeds
(Vs + 10) units for more than 30 seconds. The red low speed band remains in its enabled
or disabled state for IAS values between 20 units and (Vs + 10) units.
The altitude indicator is displayed in a rolling drum format displaying all height values
in feet. The altitude is displayed with a resolution of 20 units and a range of -1,600 to
51,000 units.
NOTE
Aircraft with an EFD500 MAX MFD configured with
an EFD1000 MAX PFD will not receive heading
information if the PFD fails.
NOTE
Refer to the EFD1000 MAX PFD Pilot’s Guide for detailed
information about the Attitude Indicator and HSI.
Figure 5-107
Secondary Attitude Instrument
