Cirrus DESIGN SR20 - Landing Gear System; Brake Failure During Taxi; Left;Right Brake Over-Temperature

Cirrus Design Section 3A
SR20 Abnormal Procedures
P/N 11934-004 3A-13
Landing Gear System
Brake Failure During Taxi
Ground steering is accomplished by differential braking. However,
increasing power may allow some rudder control due to increased
groundspeed and airflow over the rudder.
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
Left/Right Brake Over-Temperature
BRAKE TEMP Caution
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.
1. Stop aircraft and allow the brakes to cool.
BRAKE TEMP
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