Cirrus DESIGN SR22T User Manual

Cirrus Design Section 2
SR22T Limitations
P/N 13772-003 2-11
Maneuver Limits
Aerobatic maneuvers are prohibited.
Spins are prohibited.
This airplane is certified in the normal category and is not designed for
aerobatic operations. Only those operations incidental to normal flight
are approved. These operations include normal stalls, chandelles, lazy
eights, and turns in which the angle of bank is limited to 60°.
• Note •
Because the aircraft has not been certified for spin recovery,
the Cirrus Airframe Parachute System (CAPS) must be
deployed if the airplane departs controlled flight. Refer to
Section 3 – Emergency Procedures, Spins.
Flight Load Factor Limits
Flaps UP (0%), 3400 lb. .....................................................+3.8g, -1.9g
Flaps 50% .............................................................................+1.9g, -0g
Flaps 100%, 3400 lb..............................................................+1.9g, -0g
Minimum Flight Crew
The minimum flight crew is one pilot.
Original Issue

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