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16-3 Flight Phases and CDI Scaling ............................................................................ 16-19
16-4 Vertical Deviation Display ................................................................................... 16-19
16-5 Primary Flight Display Control Descriptions ...................................................... 16-23
16-6 MFD Softkeys ...................................................................................................... 16-30
16-7 MFD Controller Descriptions .............................................................................. 16-31
16-8 AFCS Controller Descriptions............................................................................. 16-39
16-9 Audio Panel Descriptions .................................................................................... 16-45
16-10 Precipitation Intensities........................................................................................ 16-50
16-11 Ground Target Return Intensity Levels ................................................................ 16-50
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INTRODUCTION
This chapter is an overview of the avionics systems and does not contain complete details
of every part of each system. Detailed operational information on the G1000 integrated
flight deck system is available in the Garmin Cockpit Reference Guide, P/N
190-00600-00 as revised for the Cessna Citation Mustang. It is incumbent upon the pilot
to adhere to the procedural policies stated within Garmin and Cessna FAA-approved documents,
which include warnings, cautions, and notes. Refer to Chapter 1—“Aircraft
General” for a list of Mustang publications.
GENERAL
The Cessna Citation Mustang utilizes a
highly integrated electronics/instrumentation
package (Figure 16-1). The Garmin
G1000 integrated flight deck avionics suite
is the main element of the system. In addition
to normal flight operations with the
G1000, standby and manual systems provide
backup capabilities for essential flight operations
and system control.
CHAPTER 16
AVIONICS
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COPILOT PRIMARY
FLIGHT DISPLAY
PILOT PRIMARY
FLIGHT DISPLAY
AUDIO
PANEL
AUDIO
PANEL
MULTIFUNCTION
DISPLAY
STANDBY
AIRSPEED
INDICATOR
STANDBY
ATTITUDE
INDICATOR
MAGNETIC
COMPASS
STANDBY
ALTIMETER
MFD/FMS
CONTROLLER
AUTOMATIC FLIGHT
CONTROL SYSTEM
MODE CONTROLLER
Figure 16-1. G1000 Integrated Flight Deck
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G1000 INTEGRATED FLIGHT
DECK OVERVIEW
The G1000 provides the pilot with communication,
navigation, flight guidance, flight instrumentation,
and monitoring of most aircraft
systems. Functions are performed by various
individual units. Three large displays and
four control panels give the crew access to all
functions.
Two primary flight displays (PFDs) provide
flight instrument indications.
The larger multifunction display (MFD) provides
a moving map display, incorporating information
from navigation instruments,
terrain/obstruction databases, weather information,
and traffic alerts. The MFD also provides
engine and airframe systems monitoring.
Supporting G1000 units provide data to these
three displays, including air data, attitude and
heading data, communications, navigation,
transponders, weather radar, satellite-broadcast
weather information, traffic information, and
sensors for the engines and airframe systems.
The G1000 analyzes aircraft systems status and
report crew alerts to the displays for various
emergency, abnormal and advisory situations.
The G1000 also provides automatic flight control,
flight direction and an integrated flight
management system. Finally, the processors
automatically detect, report, and adjust for
abnormal conditions in the G1000.
NOTE
While most monitoring of engine
and airframe systems is through the
displays, control of these systems is
mostly performed through conventional
electrical and mechanical
cockpit controls, or through cockpit
controls that command the independently
powered full authority digital
engine controls (FADECs).
STANDBY FLIGHT
INSTRUMENTS OVERVIEW
The G1000 is supplemented by three 2”-display,
stand-alone backup flight instruments
on the top-center area of the instrument panel.
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