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
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