Cirrus DESIGN SR22T User Manual

Cirrus Design Section 3A
SR22T Abnormal Procedures
P/N 13772-003 3A-19
Landing Gear System
Brake Failure During Taxi
1. Engine Power......................................................... AS REQUIRED
• To stop airplane - REDUCE
• If necessary for steering - INCREASE
2. Directional Control ............................... MAINTAIN WITH RUDDER
3. Brake Pedal(s) ......................................................................PUMP
If directional control can not be maintained:
4. Ignition Switch..........................................................................OFF
Amplification
Ground steering is accomplished by differential braking. However,
increasing power may allow some rudder control due to increased
groundspeed and airflow over the rudder.
Left/Right Brake Over-Temperature
BRAKE TEMP Caution
1. Stop aircraft and allow the brakes to cool.
Amplification
Brake temperature is between 270°F and 293°F for more than 5
seconds. Refer to Section 10 - Safety Information: Taxiing, Steering,
and Braking Practices for additional information.
BRAKE TEMP
Revision 1

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