Cirrus DESIGN SR20 - Page 239

Cirrus Design Section 7
SR20 Airplane and Systems Description
P/N 11934-004 7-65
Figure 7-14
Perspective Integrated Avionics System Schematic
TRANSPONDER
ENGINE
AIRFRAME UNIT
AIR DATA
COMPUTER
PITCH TRIM ADAPTER
(optional)
ROLL SERVO
(optional)
PITCH SERVO
AHRS 1
XM RADIO
RECEIVER
(optional)
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_2914
PFD
AUDIO PANEL
MFD
AHRS 2
(optional)
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