Cirrus SR22T User Manual

4 of 6 P/N 13772-109
Section 9 Cirrus Design
Supplements SR22 / SR22T
Descent
After airplane descends through altitude requiring oxygen:
1. Oxygen Shutoff Valve...............................................................OFF
2. Pilot and passengers .............................. Stow Masks or Cannulas
Section 5 - Performance
No change from basic Handbook.
Section 6 - Weight & Balance
The weight, arm, and moment for fully charged systems (1800 – 2200
psi) is provided in the following table:
Section 7 - System Description
Refer to approved system manufacturer’s data for a description of the
equipment, cleaning instructions, and specific operational instructions.
Mounting Instructions
The oxygen bottle must be properly mounted in the right front
passenger seat using the cylinder harness supplied with the system.
When properly mounted and secured, the pilot will be able to view the
oxygen pressure gage and operate the shutoff valve. See Figure 1 for
mounting instructions.
Model Weight - lb Arm Moment/1000
XCP-682 (682 Liter) 14.00 143.5 2.01
XCP-415 (415 Liter) 10.25 143.5 1.47
XCP-180 (180 Liter) 4.50 143.5 0.65
Revision 02: 01-06-10

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