Garmin G1000 Piper PA32 - Manual (Page 15)

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