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PFD
GDU 1040
No. 1 GIA 63W
Integrated Avionics Unit
System Inegration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/WAAS
Glideslope
190-00692-00 Rev. B
High-Speed Data Bus (Ethernet)
Reversionary
Control
GPS Output
Engine/Airframe
Figure 1-1 Basic G1000 System
Garmin G1000 Pilot's Guide for Piper PA32
GMA 1347
Audio Panel
Reversionary
Control
GDC 74A
Air Data
Computer
OAT
Airspeed
Altitude
Vertical Speed
GRS 77
AHRS
Attitude
Rate of Turn
Slip/Skid
GMU 44
Magnetometer
Heading
GTX 33
Transponder
GEA 71
Unit
SYSTEM OVERVIEW
MFD
GDU 1040
No. 2 GIA 63W
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/WAAS
Glideslope
GPS Output
S-TEC System
Fifty-Five X
Autopilot
1-5
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