Cirrus SR20 - Page 265

Cirrus Design Section 7
SR20 Airplane and Systems Description
P/N 21399-004 7-81P/N 21399-004 7-81
Figure 7-18
Perspective Integrated Avionics System Schematic
IRIDIUM GLOBAL
SATELLITE
DATALINK
(optional)
TRANSPONDER
ENGINE
AIRFRAME UNIT
AIR DATA
COMPUTER 1
PITCH TRIM ADAPTER
(optional)
ROLL SERVO
(optional)
PITCH SERVO
(optional)
AHRS 1
XM RADIO
RECEIVER
(optional)
XM SATELLITE DATA
LINK RECEIVER
(optional)
FMS KEYBOARD
AUTOPILOT
MODE CONTROLLER
(optional)
MAG 1 MAG 2
INTEGRATED
AVIONICS UNIT 1
INTEGRATED
AVIONICS UNIT 2
SR20_FM07_2914B
PFD
AUDIO PANEL
MFD
AHRS 2
(optional)
AIR DATA
COMPUTER 2
(optional)
Revision A1