CIRRUS DESIGN SR22 - Page 190

7-22 Information Manual
Section 7 Cirrus Design
Airplane Description SR22
Figure 7-5
MAIN BUS 2
ESSENTIAL BUS
Avidyne PFD
SR22_FM07_1607B
PFD 1
10
PFD 2
10
PITOT
STATIC
Avidyne MFD
STEC System 55x
Autopilot
Data Aquisition Unit
OAT Sensor /
Magnetometer
#2 GNS-430
GPS
#1 GNS-430
GPS
A
P
O
N
Flight Director System
(Optional)
A
P
O
F
F
F
D
O
N
PFD System - Simplified Schematic
March 2010