Cirrus SR22T User Manual

7-84 P/N 13772-005
Section 7 Cirrus Design
Systems Description SR22T
Figure 7-19
Equipment Locations
LEGEND
1. AHRS 1
2. Integrated
Avionics Unit 1
3. AHRS 2
4. Avionics Cooling Fan
5. Integrated
Avionics Unit 2
6. Engine Airframe Unit
7. Air Data Computer 2 (opt)
8. Air Data Computer 1
9. GFC 705 Mode
Controller
10. ADF (Opt)
11. CAPS Activation Handle
(Cabin Ceiling)
12. Hour Meters
13. Egress Hammer
14. Telephone and
Audio Jacks
15. Cabin Speaker
16. Roll Servo
17. Pitch Trim Adapter (opt)
18. Pitch Servo
19. XM Radio
Transceiver (Opt)
20. Transponder
21. Satellite Data Link
Receiver (Opt)
22. ELT
23. Yaw Servo (opt)
24. Battery 2
25. Iridium Global Satellite
Datalink (Opt)
26. Tiedown Loops
27. CAPS Parachute
28. WX Information
Receiver (Opt)
29. Microphone
30. TAS Receiver (Opt)
31. DME (Opt)
32. Fire Extinguisher
23
16
18
17
6
5
4
31
SR22_FM07_3576
9
4
14
8
11
12
13
15
19
20
21
32
28
27
24
22
3
2
1
4
26
30
29
26
10
25
7
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