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

Cirrus Design Section 3A
SR20 Abnormal Procedures
P/N 21399-004 3A-19P/N 21399-004 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, Taxiing, Steering, and Braking Practices
for additional information.
BRAKE TEMP
Revision A1