Landing Gear System; Brake Failure During Taxi; Left/Right Brake Over-Temperature - Cirrus SR20 Pilot Operating Handbook

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