Cirrus SR22T User Manual

7-72 P/N 13772-005
Section 7 Cirrus Design
Systems Description SR22T
Figure 7-17
Perspective Integrated Avionics System Schematic
IRIDIUM GLOBAL
SATELLITE
DATALINK
(optional)
TRANSPONDER
ENGINE
AIRFRAME UNIT
AIR DATA
COMPUTER 1
AHRS 1
XM RADIO
RECEIVER
(optional)
XM SATELLITE DATA
LINK RECEIVER
(optional)
FMS KEYBOARD
AUTOPILOT
MODE CONTROLLER
MAG 1 MAG 2
INTEGRATED
AVIONICS UNIT 1
INTEGRATED
AVIONICS UNIT 2
PFD
AUDIO PANEL
MFD
AHRS 2
(optional)
AIR DATA
COMPUTER 2
(optional)
PITCH TRIM ADAPTER
YAW SERVO
(optional)
ROLL SERVO
PITCH SERVO
SR22_FM07_3574
Original Issue

Cirrus SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Engine	Continental TSIO-550-K
Horsepower	315 hp
Max Takeoff Weight	3, 600 lbs
Service Ceiling	25, 000 ft
Cabin Width	49 in
Cabin Height	50 in
Seating Capacity	4
Avionics	Cirrus Perspective+ by Garmin
Category	Single-engine piston aircraft
Propeller	Hartzell 3-blade composite
Wingspan	38 ft 4 in
Length	26 ft
Height	8 ft 11 in
Maximum Cruise Speed	213 KTAS
Fuel Capacity	92 gallons
Stall Speed	64 knots
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cruise Speed	183 knots