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switches, and other devices detect conditions
in the aircraft and its systems. This information
is provided as analog signals or discrete
digital signals to the G1000 system. These
signals are received at the left and right Garmin
integrated avionics unit (GIAs), and at the left
and right Garmin engine/airframe interface
units (GEAs) (Figure 4-1). A detailed description
of G1000 system architecture is provided
in Chapter 16—“Avionics.”
With the battery switch selected to EMER,
only the left GIA and left GEA are powered;
CITATION MUSTANG OPERATING MANUAL
4-2 510OM-00
MULTIFUNCTION
DISPLAY
(INCLUDES EICAS)
NO. 1
INTEGRATED
AVIONICS
UNIT
(GIA63W)
NO. 1
ENGINE/
AIRFRAME
ADAPTER
(GEA71)
NO. 2
ENGINE/
AIRFRAME
ADAPTER
(GEA71)
DISCRETE
DIGITAL
INPUTS
PFD PFD
DISCRETE
DIGITAL
INPUTS
NO. 2
INTEGRATED
AVIONICS
UNIT
(GIA63W)
ANALOG
INPUTS
ANALOG
INPUTS
Figure 4-1. G1000 Block Diagram
CITATION MUSTANG OPERATING MANUAL
CAS messages requiring input from the right
GIA or right GEA are inhibited and do not appear,
regardless of aircraft or system condition.
CONTROLS AND
INDICATIONS
The Mustang master warning system includes:
• CAS messages
• Master indicators:
• MASTER WARNING lights
• MASTER CAUTION lights
• Aural warnings—Various audio warnings
are incorporated into aircraft systems
that warn of specific conditions
and malfunctions.
Control of the system is provided by:
• CAS scroll softkeys (up and/or down)
• Rotary TEST knob
CAS MESSAGES
The Mustang master warning system is primarily
a function of the G1000 avionics system.
The CAS displays warning, caution,
and advisory messages in response to data
from aircraft sensors and FADECs.
CAS Message Window
All CAS messages are displayed in the CAS
message window. The window is on either the
MFD, or on one or both of the PFDs:
• Normal display mode—CAS message
window is in the bottom left corner of the
EICAS display, which appears on the
left side of the MFD (Figure 4-2).
• Reversionary display mode—CAS message
window is on the right side of the
display (Figure 4-3, Sheet 1 of 2).
CAS Message Types
CAS messages are in one of three colors: red,
amber, or white.
Red (Warning) Messages
Red indicates a warning (hazardous situation
that requires immediate pilot corrective action).
When a red CAS message appears, it
flashes in reverse video in conjunction with the
MASTER WARNING lights. Pressing the
MASTER WARNING light acknowledges the
message, turns off the MASTER WARNING
lights, and changes the CAS message to a
steady ON state. Red CAS messages are displayed
until the situation is corrected. All red
CAS messages are grouped together at the top
of the CAS display window.
Amber (Caution) Messages
Amber indicates a caution (abnormal or special
situation that includes a possible need for future
pilot corrective action). When an amber
CAS message appears, it flashes in conjunction
with the illumination of the MASTER CAUTION
lights. Pressing the MASTER CAUTION
light acknowledges the message, turns off the
MASTER CAUTION lights, and changes the
CAS message to a steady ON state.
White (Advisory) Messages
White indicates an advisory. This may indicate
the following:
• Abnormal condition
• Change in status of an aircraft system
• Normal operation of a specific device
All white advisory messages are grouped together
at the bottom of the CAS message list.
When an advisory message appears, the checklist
may require an action. If required, find the
action in the FAA-approved Abnormal
Procedures Checklist.
510OM-00 4-3
Figure 4-2. Multifunction Display
CITATION MUSTANG OPERATING MANUAL
4-4 510OM-00
CITATION MUSTANG OPERATING MANUAL
510OM-00 4-5
Figure 4-3. Primary Flight Display (Sheet 1 of 2)
E
NAV1 113.80 109.10
116.80 113.80
ITWI
NAV2 ICT
126.700 COM1
121.900
118.200
125.150 COM2
140
130
120
110
100
90
1187
20
10
20
10
10 10 AP
R
2
2900
4
4
2
2
3400
3000
3300
3200
3000
2900
3100
BARO MIN 29.92IN
　
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