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from 118.00 to 136.990 MHz,
in 25 kHz (760-channel) or 8.33 kHz
(3040-channel) spacing.
• Very-high frequency omnidirectional
range/ILS localizer (VOR/LOC) receiver
tuning 108.00 to 117.95 MHz, at 50 kHz
increments.
• ILS glide slope receiver tuning 328.6 to
335.4 MHz, as matched with the ILS frequency
tuned in the VOR/LOC receiver.
• FD processor, which interfaces with the
GFC 700 automatic flight control system
(AFCS)
• Digital aural warnings
XPDR1 MODE S
TRANSPONDER w/DIVERSITY
(GTX33D)
XPDR2 MODE S
TRANSPONDER
(GTX33)
WEATHER
RADAR
(GWX 68)
HIGH-SPEED DATA BUS
ARINC 429
DATA INTERFACE CABLE (RS-485)
DATA INTERFACE CABLE (RS-232)
REVERSIONARY CONTROL
#1 AIR DATA
COMPUTER
(GDC 74B)
• OAT
• AIRSPEED
• ALTITUDE
• VERTICAL
SPEED
#1 ATTITUDE
/HEADING
REFERENCE
SYSTEM
(GRS 77)
• ATTITUDE
• RATE OF TURN
• SLIP/SKID
• HEADING
DISCRETE
ENGINE/AIRFRAME
SYSTEMS SENSORS
• L/R FADEC
• L FUEL
• PRESSURIZATION
• CESSNA DIAGNOSTICS
• ELT
• L/R FADEC
• R FUEL
DISCRETE
ENGINE/AIRFRAME
SYSTEMS SENSORS
ANALOG &
DISCRETE
ENGINE/
AIRFRAME
SYSTEMS
SENSORS
ANALOG &
DISCRETE
ENGINE/
AIRFRAME
SYSTEMS
SENSORS
PITCH SERVO (GSA 81)
PITCH TRIM SERVO (GSA 81)
YAW SERVO (GSA 80)
ROLL SERVO (GSA 80)
#2 AIR DATA
COMPUTER
(GDC 74B)
• OAT
• AIRSPEED
• ALTITUDE
• VERTICAL
SPEED
#2 ATTITUDE
/HEADING
REFERENCE
SYSTEM
(GRS 77)
• ATTITUDE
• RATE OF TURN
• SLIP/SKID
• HEADING
#2 MAGNETOMETER
(GMU 44)
MAGNETIC HEADING
#1 MAGNETOMETER
(GMU 44)
MAGNETIC HEADING
#1 ENGINE
/AIRFAME
ADAPTER
(GEA 71)
#2 ENGINE
/AIRFAME
ADAPTER
(GEA 71)
HIGH-SPEED DATA BUS
XM WEATHER
DATALINK
(GDL 69A)
#2 INTEGRATED
AVIONICS UNIT
(GIA 63W)
• G1000 PROCESSORS
• VHF COM
• VHF NAV/LOC
• GLIDESLOPE
• GPS
• FLIGHT DIRECTOR
#1 INTEGRATED
AVIONICS UNIT
(GIA 63W)
• G1000 PROCESSORS
• VHF COM
• VHF NAV/LOC
• GLIDESLOPE
• GPS
• FLIGHT DIRECTOR
LEFT EXTERNAL LEGEND
ARINC 429 LRUs
RIGHT EXTERNAL
ARINC 429 LRUs
BACKUP GPS
BACKUP GPS
510OM-00 16-5
CITATION MUSTANG OPERATING MANUAL
Figure 16-2. G1000 Integrated Avionics Architecture
ITEM FUNCTION DESCRIPTION
GIA 63W Interface Adapter Main modules of the G1000 system. Coordinates information input from all sources to
the cockpit displays. Also receives discrete data and ARINC 429 from various engine
systems, and processes for presentation to other G1000 components. Each GIA
includes a WAAS-enabled GPS receiver, VOR/ILS localizer receiver, ILS glide-slope
receiver, FD system, and a VHF communications transceiver.
GDU Primary Flight Left and right color LCD displays. Each PFD displays flight instruments and flight
1040A Display (PFD) guidance and basic avionics indications. MFD information may also appear on the
Unit PFDs and vice versa. TAWS is a built-in feature.
GDU Multifunction Center-panel color LCD display. The MFD displays a multifeature map. Also display
1500 Display (MFD) EICAS.
GMC Automatic Flight Located in top center panel. Part of GFC700 system.
710 Control System (AFCS)
Controller
GSA 80 High Torque Yaw and roll servos for AFCS. Part of GFC700.
Servo
GSA 81 Low Torque Pitch and pitch trim servos for AFCS. Part of GFC700.
Servo
GCU MFD/FMS MFD and flight management system controller on lower cockpit pedestal.
475 Controller
GRS 77 Attitude and Provides aircraft attitude and heading guidance to G1000 displays and AFCS.
Heading Reference
System (AHRS)
GMU 44 Magnetometer Measures local magnetic field information.
GDC Air Data Processes inputs from pitot-static system, temperature sensors to determine airspeed,
74B Computer (ADC) altitude, and vertical speed.
GEA 71 Engine/Airframe Receives and processes signals from various engine and airframe sensors.
Unit (GEA)
GMA Audio Amp and Audio panel for controlling audio sources; integrated marker beacon receiver.
1347D Marker Beacon
KN63 Distance Provides DME distance information to G1000 displays.
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CITATION MUSTANG OPERATING MANUAL 2(12)
