Cirrus SR22T User Manual

6 of 52 P/N 13772-151
Section 9 Cirrus Design
Supplements SR22T
Systems and Equipment Limits
Lift Transducer Heat System
Limit ground operations of Lift Transducer Heat (PITOT HEAT) to 45
seconds.
Autopilot System
Autopilot operation is prohibited when operating in icing conditions
which are outside of the CFR defined conditions as stated in the
preceding Environmental Conditions paragraph.
Flap System
Unless required for Emergency operations (i.e. Forced Landing), Flaps
are limited to a maximum deflection of 50% when the aircraft has
encountered icing conditions and/or has accumulated ice on the
airframe
When holding in icing conditions the flaps must be UP (0%).
Pilot Qualification and Training
• Note •
The Pilot Qualification and Training Limitation does not apply
to airplanes registered in the European Union.
The pilot-in-command must successfully complete the Cirrus Icing
Awareness Course or a Cirrus Design approved equivalent training
course, within the preceding 24 months prior to Flight Into Forecast or
Known Icing Conditions.
Contact Cirrus Design at (218) 529-7292 for additional information.
Original Issue: 02-01-13

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