Aspen Avionics Evolution EFD1000 PFD - Flight Plan; Basemap Data Source and Reversion

CHAPTER 4, REFERENCE GUIDE
EFD1000 PFD Pilot’s Guide
Page 4-40 A-01-184-00 REV B
EFD1000 PFD Pilot’s Guide
EFD1000 PFD Pilot’s Guide
4.3.12.2. Flight Plan
When a ight plan is provided by a congured GPS, the basemap shows ight plan
waypoints and legs. The active leg and waypoint and associated identier are displayed
in magenta. Other waypoints and legs are white. Straight and curved ight plan details
are rotated within the basemap display to maintain their correct compass orientations
at all times.
4.3.12.3. Basemap Data Source and Reversion
When congured with compatible GPS equipment, aircraft position, ight plan, and
basemap data are provided by the selected GPS navigation source (either GPS1 or
GPS2).
If the aircraft GPS position data is no longer available or becomes invalid:
The associated ight plan and basemap data are retained and displayed. •
The ight plan and waypoints become inactive and are displayed in white.•
The aircraft position is provided by:•
Another congured GPS source if providing valid position data. In 1.
this case, a GPS# REVERSION annunciation is shown above the CDI
navigation source select legend (Figure 4-88) (“#” indicates the
congured GPS source that is now providing the aircraft’s position, either
1 or 2).
The RSM GPS, if enabled, and position data are available. In this case, a 2.
RSM GPS REVERSION EMER USE ONLY annunciation is shown above the
CDI navigation source select legend (Figure 4-89).
When a GPS source’s position data are invalid or no longer available, an amber
annunciation, GPS1, GPS2, or RSM GPS, is shown to the left of the lower display to
indicate which has failed (Figure 4-90).
NOTE
The RSM GPS ENABLED / DISABLED
settings are retained following a
power cycle of the unit, defaulting to
“ENABLE” if not previously set.
The RSM GPS usage settings are
retained following a power cycle of
the unit, defaulting to “EMER ONLY” if
not previously set.
Figure 4-88 GPS1 Failure, Reversionary Navigation
Figure 4-89 GPS1 Failure, Reversionary Navigation
Figure 4-90 Invalid or Failed
GPS Annunciations