Cirrus SR22T User Manual

4 of 30 P/N 13772-135
Section 9 Cirrus Design
Supplements SR22 / SR22T
Section 3 - Emergency Procedures
Autopilot Malfunction
Refer to Electric Trim/Autopilot Failure abnormal procedure in the
basic POH. Do not reengage the Autopilot until the malfunction has
been identified and corrected. The Autopilot may be disconnected by:
1. Pressing the A/P DISC on the control yoke.,
or
2. Pulling the AP SERVOS circuit breaker on MAIN BUS 1.
Altitude lost during a roll or pitch axis Autopilot malfunction and
recovery:
Flight Phase Bank Angle Altitude Loss
Climb 45° 300 ft
Cruise 45° 300 ft
Maneuvering 45° 300 ft
Descent 45° 300 ft
Approach 45° 70 ft
Revision 03: 12-14-10

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