Honeywell PRIMUS 1000 Pilot's Manual page 62

Integrated avionics system for the citation encore
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R
PRIMUS
1000 Integrated Avionics System
— CHECKLIST PAGE – Pushing ENT on a checklist page
acknowledges that the selected item is complete (green) and
moves the active selection to the next incomplete (blue) item. If
ENT is pushed with the active selection at the last item on a
checklist, its effect depends upon whether or not the checklist is
completed.
-
If the checklist has been completed, the system returns to the
index page containing the next checklist to be completed,
with the cursor on that checklist.
-
If the checklist has not been completed (one or more items
skipped), the system displays the page containing the first
incomplete item, with the cursor on that item.
D
Joystick – The joystick selects additional paging and cursor control.
Each movement results in the action described below.
— UP – Pushing the joystick up moves the active selection to the
previous item.
— DOWN – Pushing the joystick down moves the active selection
to the next item. This is identical to the SKP button.
— LEFT – Pushing the joystick to the left goes back to the previous
page.
— RIGHT – Pushing the joystick to the right displays the next page.
This is identical to the PAG button.
MODE SELECTOR ROTARY SWITCH
The MODE selector is a three–position rotary switch that selects the
following symbol generator modes of operation:
D
NORM – Selects normal symbol generator operation.
D
SG1 – Selects No. 1 symbol generator to drive all displays.
D
SG2 – Selects No. 2 symbol generator to drive all displays.
DIM (DIMMING) CONTROL
The DIM knob controls the MFD brightness level. It is concentric with
the mode selector switch.
Electronic Flight Instrument System (EFIS)
3-24
A28–1146–134
REV 1 Jan/03

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