Cirrus SR22T User Manual

Cirrus Design Section 3
SR22T Emergency Procedures
P/N 13772-005 3-45P/N 13772-005 3-45
The Cirrus Airframe Parachute System (CAPS) should be activated
immediately in the event of a spin. It should also be used in other life-
threatening emergencies where CAPS deployment is determined to
be safer than continued flight and landing.
Expected impact in a fully stabilized deployment is equivalent to a drop
from approximately 13 feet.
Several possible scenarios in which the activation of the CAPS would
be appropriate are discussed in Section 10: Safety Information of this
Handbook. These include:
•Mid-air collision
•Structural failure
•Loss of control
•Landing on an unprepared surface
•Pilot incapacitation
All pilots should carefully review the information on CAPS activation
and deployment in Section 10 before operating the airplane.
CAPS Deployment at High Altitudes
For any indicated airspeed, as altitudes increase the true air speed of
the deployment increases. Higher true air speeds increase the
parachute inflation loads. Therefore, it is important for the operator
takes all reasonable efforts to slow to the minimum possible airspeed
prior to deploying the CAPS.
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