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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
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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.
Measuring Equipment
(DME) System
GTX 33 Transponder Mode S transponder—Conventional Mode C transponder plus additional capability for
data communications with ground radar and traffic information systems.
GTX 33D Diversity Transponder Mode S transponder—Conventional Mode C transponder plus additional capability for
data communications with ground radar and traffic information systems and Mode S
diversity.
GWX 68 Weather Radar Provides airborne weather and ground map weather radar to MFD.
GDL 69A Datalink Satellite radio receiver that provides real-time weather information to the MFD
as well as digital audio entertainment. Communicates with the MFD via HSDB
connection. A subscription service required to enable.
RA350 2 Automatic Direction Provides ADF bearing to the G1000 displays (optional).
Finder (ADF) System
C406-N Emergency Locator When activated, the ELT sends out a distress signal of 121.5, 243.0, and 406.028 MHz.
Transmitter (ELT) The 406.028 MHz signal includes important information about the airplane including
System latitude and longitude, which is detected by the CosPas Sarsat Satellite System for
search and resue operations.
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Table 16-1. G1000 SYSTEM COMPONENTS
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NOTE
Marker beacon reception is in the
audio panel, which connects to the
GIAs.
DISPLAYS
Two PFDs and one MFD provide a central display
and crew interface for the G1000. Various
knobs and softkeys provide system control.
The PFDs are two identical, 10.4-inch color
liquid crystal displays (LCDs) in the instrument
panel (see Figure 16-1). Each PFD provides
flight instrument displays and basic
avionics indications (NAV/COM and transponder
settings, course deviation indicator (CDI)
and ILS indications.
The 15-inch MFD provides a moving-map display
and indications for most airframe and engine
systems. The moving map display indicates
current aircraft position relative to topography
and surface features, terrain obstructions, airspace
boundaries, airways, aviation facilities (including
airports and navaids), and weather. The
left side of the MFD provides indications for engine
　
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