Cirrus SR22T User Manual

Cirrus Design Section 2
SR22T Limitations
P/N 13772-005 2-23P/N 13772-005 2-23
2. The appropriate revision of the Max Viz Enhanced Vision System
Information Manual, (p/n 309100024) must be available to the pilot
during flight.
Air Conditioning System (Optional)
The use of Recirculation Mode during flight is prohibited.
Inflatable Restraint System
Use of a child safety seat with the inflatable restraint system is
prohibited.
Flap Limitations
Approved Takeoff Settings........................................... UP (0%) or 50%
Approved Landing Settings ..................................... 0%, 50%, or 100%
Do not use flaps above 17,500 feet MSL.
Paint
To ensure that the temperature of the composite structure does not
exceed 150°F (66°C), the outer surface of the airplane must be
painted in accordance with the paint colors and schemes as specified
in the Airplane Maintenance Manual. Refer to Airplane Maintenance
Manual (AMM), Chapter 51, for specific paint requirements.
Cirrus Airframe Parachute System (CAPS)
VPD Maximum Demonstrated Deployment Speed ................140 KIAS
• Note •
Refer to Section 10, Cirrus Airframe Parachute System
(CAPS) for additional CAPS guidance.
Other Limitations
Smoking
Smoking is prohibited in this airplane.
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