Cirrus SR22T User Manual

3A-20 P/N 13772-005
Section 3A Cirrus Design
Abnormal Procedures SR22T
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, Taxiing, Steering, and Braking Practices
for additional information.
BRAKE TEMP
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