Garmin G950 Pilot's Manual page 16

SYSTEM OVERVIEW
GDU 1040
Primary Flight Display
No. 1 GIA 63W
Integrated Avionics Unit
System Inegration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS
Glideslope
4
GMA 1347
Audio Panel
Reversionary
Control
G GDC 74A
C Computer
Ve Vertical Speed
Rate of Turn
GPS Output
Magnetometer
Transponder
Figure 1-1 Basic G950 Block Diagram
Garmin G950 Pilot's Guide for the Tecnam P2006T
Reversionary
Control
A
Air Data
r
OAT
Airspeed
Altitude
ed
GRS 77
AHRS
Attitude
GPS Output
Slip/Skid
GMU 44
Heading
GTX 33
GDU 1040
Multi-Function Display
No. 2 GIA 63W
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS
Glideslope
190-01146-00 Rev. A