3A-18 P/N 13999-004 Info Manual
Section 3A Cirrus Design
Abnormal Procedures SR20
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
September 2011
Intentionally Left Blank
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