C
IRRUS
D
ESIGN
S
ECTION
3A: A
BNORMAL
P
ROCEDURES
SR20
L
ANDING
G
EAR
S
YSTEM
P/N 11934-005
3A-21
Landing Gear System
Brake Failure During Taxi
BRAKE TEMP Caution
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 cannot be maintained:
a. Ignition Switch..................................................................................OFF
Procedure Complete
• N
OTE
•
Ground steering is accomplished by differential braking.
However, increasing power may allow some rudder control due to
increased ground speed and airflow over the rudder.
BRAKE TEMP
Left/Right Brake Over-Temperature
1. Stop aircraft and allow the brakes to cool.
Procedure Complete
• WARNING •
Do not set parking brake unless required for safety.
• N
OTE
•
Brake temperature is between 270 °F and 293 °F for more than 5
seconds. Refer to Section 10,
Taxiing, Steering, and Braking Prac-
for additional information.
Reissue A