Cirrus DESIGN SR22T - Page 273

Cirrus Design Section 7
SR22T Airplane and Systems Description
P/N 13772-003 7-71
Figure 7-17
Perspective Integrated Avionics System Schematic
TRANSPONDER
ENGINE
AIRFRAME UNIT
AIR DATA
COMPUTER
PITCH TRIM ADAPTER
YAW SERVO
(optional)
ROLL SERVO
(optional)
PITCH SERVO
(optional)
AHRS 1
AHRS 2
(optional)
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
SR22_FM07_2915A
PFD
AUDIO PANEL
MFD
AIR DATA
COMPUTER 2
(optional)
Revision 1