Cirrus DESIGN SR22T User Manual

P/N 13772-143 5 of 6
Cirrus Design Section 9
SR22 / SR22T Supplements
Aircraft Serials with Perspective PFD/MFD Avionics
ALT 1 Failure (Alt 1 Light Steady)
Steady illumination indicates failure of alternator 1. Attempt to restore
alternator. If alternator cannot be restored, Alternator 2, and Bat 2 will
provide sufficient electrical power to supply all requirements for
emergency operation of equipment indefinitely as is required by 14
CFR 135.163(f).
1. ALT 1 Master Switch ................................................................OFF
2. Alternator 1 Circuit Breaker .................................Check and Reset
3. ALT 1 Master Switch ..................................................................ON
If alternator does not reset
4. ALT 1 Master Switch ................................................................OFF
5. Notify ATC of Alternator Failure
6. Autopilot ...........................................................................ENGAGE
Use of autopilot will reduce work load. Expect a slight pitch
change when autopilot is disengaged.
7. Air Conditioning and Fan ........................................................ OFF
8. Convenience Outlet ......................................Disconnect appliance
Revision 02: 01-06-10

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