Cirrus DESIGN SR22T User Manual

8 of 20 P/N 13772-115
Section 9 Cirrus Design
Supplements SR22 / SR22T
Section 5 - Performance
Cruise speed is lower by approximately three knots and range is
reduced by a maximum of 2%.
Experience with your airplane’s power settings may result in more
accurate performance numbers than those given above.
1. Reduce KTAS shown on the Cruise Performance tables and the
Range/Endurance Profile tables by 3 knots.
2. Reduce range shown on the Range/Endurance Profiles by 2%.
• Caution •
During certain flight conditions, such as at higher operating
altitudes and/or higher airspeeds, the stagnation point on the
leading edge of the wing (the point where the airflow splits) will
move up and aft enough to hinder the deicing fluid from
flowing adequately along the top surface of the wing. Airspeed
for optimum system performance is 95-139 KIAS. Do not
exceed 175 KTAS above 14000 ft.
Revision 09: 12-17-10

Cirrus DESIGN SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Model	SR22T
Seating Capacity	5
Engine	Continental TSIO-550-K
Horsepower	315 hp
Avionics	Cirrus Perspective+ by Garmin
Type	Single-engine piston aircraft
Maximum Speed	213 knots
Cruise Speed	183 knots
Service Ceiling	25, 000 feet
Maximum Takeoff Weight	3, 600 lbs
Wingspan	38 feet 4 inches
Length	26 ft
Height	8 feet 11 inches
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cabin Width	49 inches
Cabin Height	50 inches