Cirrus SR22T User Manual

Cirrus Design Section 7
SR22T Systems Description
P/N 13772-005 7-71P/N 13772-005 7-71
Avionics
Perspective Integrated Avionics System
The Perspective Integrated Avionics System provides advanced
cockpit functionality and improved situational awareness through the
use of fully integrated flight, engine, communication, navigation and
monitoring equipment. The system consists of the following
components:
•GDU Primary Flight Display (PFD)
•GDU Multifunction Display (MFD)
•GCU 478 Flight Management System Keyboard
• GRS 77 Attitude and Heading Reference System
•GDC 74A Air Data Computer
•GIA 63W Integrated Avionics Units
•GEA 71 Engine Airframe Unit
•GTX 32 Mode A, C Transponder
• GMA 350 Audio Panel with Marker Beacon Receiver
•GFC 700 3-Axis Autopilot and GMC 705 Controller
•GTX 33 Mode S Transponder (Optional)
•GSR 56 Iridium Global Satellite Datalink (Optional)
•GDL 69/69A XM Satellite Weather/Radio Receiver (Optional)
-GRT 10 XM Radio Remote Transceiver (Optional)
-GRC 10 XM Radio Remote Control (Optional)
• Traffic Advisory System (Optional)
•Weather Information System (Optional)
•Bendix/King KR 87 Automatic Direction Finder (Optional)
•Bendix/King KN 63 Distance Measuring Equipment (Optional)
•Synthetic Vision System (Optional)
• Max Viz Enhanced Vision System (Optional)
Refer to the Perspective Integrated Avionics System Pilot’s Guide for a
detailed description of the system and it’s operating modes.
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