Landing Gear System; Brake Failure During Taxi; Brake Temp Caution - Cirrus SR22 Pilot Operating Handbook

C D
IRRUS ESIGN
SR22

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 cannot be maintained:
a. Ignition Switch..................................................................................OFF
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 Caution

Left/Right Brake Over-Temperature
1. Stop aircraft and allow the brakes to cool.
Do not set parking brake unless required for safety.
Brake temperature is between 270 °F and 293 °F for more than 5
seconds. Refer to Section 10,
P/N 13772-006
Reissue A
Procedure Complete
• N
OTE
BRAKE TEMP
• WARNING •
Procedure Complete
• N
OTE
Taxiing, Steering, and Braking Prac-
tices for additional information.
S 3A: A
ECTION BNORMAL
L
ANDING
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P
ROCEDURES
G S
EAR YSTEM
3A-21