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It includes an intercom system (ICS)
with public-address (PA) function.
Weather Radar
The GWX 68 weather avoidance radar provides
real-time radar information, including precipitation
and ground-mapping returns to the
G1000. Returns are displayed on the MFD. The
GWX 68 communicates though the high-speed
data bus by way of the GDL69A.
XM Weather Datalink
The GDL69A is a remote-mounted satellitebroadcast
receiver that receives XM weather for
display on the MFD (and/or PFD inset map).
The GDL 69A can receive XM weather and
XM radio services. It communicates to the
G1000 through the high-speed data bus.
AVIONICS POWER
SWITCHES
Three switches control power to the Citation
Mustang avionics and instruments:
• Battery switch
• Avionics power switch
• Standby instruments switch
BATTERY SWITCH
The battery toggle switch is in the DC
POWER section of the left lower instrument
panel and has three positions: BATT, OFF, and
EMER (Figure 16-3). The switch controls
DC power to the other switches, and directly
supplies power to components required for
EICAS operation.
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CITATION MUSTANG OPERATING MANUAL
Figure 16-3. Battery Switch
The EICAS display is needed by the pilot during
all aircraft operations, including start-up.
For this reason, some components are powered
when the battery switch is set to BATT
or EMER:
• BATT—Both PFDs, MFD, GIAs, GEAs
• EMER—PFD1, GIA1, GEA1
NOTE
Flight instruments, and all navigation,
communications, and flight
guidance functions are not enabled
by the battery switch alone. The
AVN PWR switch must also be
powered on (up).
AVIONICS POWER SWITCH
The avionics power switch is in the AVIONICS
section of the left lower instrument panel and
has two positions:AVN PWR and OFF (Figure
16-4). This switch energizes the avionics solidstate
relays (SSRs) closed. Each relay provides
DC power from a powered bus (left or right
electrical bus or emergency bus), through a corresponding
avionics bus, to power specific units.
All units receive from an avionics bus, except
those powered directly from the battery switch.
STANDBY FLIGHT
INSTRUMENTS SWITCH
The standby flight instruments switch is in the
AVIONICS section of the left lower instrument
panel and has three positions: STBY
INST, OFF, and BATT TEST (Figure 16-4).
When the switch is in the STBY INST position,
it provides DC power (from a backup battery)
to the standby flight instruments on the upper
center instrument panel:
• Airspeed indicator
• Attitude gyro
• Altimeter
A small amber light emitting diode (LED) on
the right side of the switch illuminates when
in the STBY INST position, indicating the
standby flight instruments are discharging
power from the dedicated standby lead-acid
battery pack. A fully charged battery supplies
power for approximately 30 minutes. The
amber light does not illuminate when aircraft
power is charging the battery and providing
power to the standby instruments.
In the BATT TEST position, the condition of the
backup battery is tested. Illumination of the
green light beside the switch indicates proper
battery charge. If the green light does not illuminate,
the backup battery is not properly
charged, and standby flight instruments may
not operate with the loss of normal DC power.
PRIMARY FLIGHT
DISPLAY
DESCRIPTION
The main control display units for the G1000
are the PFDs. The Citation Mustang has two
PFDs, one in front of the pilot and one in front
of the copilot (Figure 16-5).
The PFDs are 10.4-inch color LCDs, which
are designed for visibility in bright sunlight.
(Brightness is manually or automatically
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CITATION MUSTANG OPERATING MANUAL
Figure 16-4. Avionics Power Switch and
Standby Instruments Switch
DRAFT
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CITATION MUSTANG OPERATING MANUAL
NAV FREQUENCY
WINDOW
COM FREQUENCY
WINDOW
NAVIGATION
STATUS BAR
SLIP/SKID
INDICATOR
ATTITUDE
INDICATOR
SYSTEM
TIME BOX
TRANSPONDER
STATUS BAR
TURN RATE
INDICATOR
BAROMETRIC
SETTING BOX
VERTICAL SPEED
INDICATOR
ALTIMETER
SELECTED
ALTITUDE BOX
AIRSPEED
INDICATOR
HEADING
BOX
HORIZONTAL
SITUATION
INDICATOR
ISA DEVIATION
TEMPERATURE
BOX
RAM AIR
TEMPERATURE
BOX
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