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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
Left/Right Brake Over-Temperature
BRAKE TEMP Caution
Brake temperature is between 270°F and 293°F for more than 5
seconds. Refer to Section 10 - Safety Information: Taxiing, Steering,
and Braking Practices for additional information.
1. Stop aircraft and allow the brakes to cool.
BRAKE TEMP
March 2010
3A-14 Information Manual
Section 3A Cirrus Design
Abnormal Procedures SR22
Other Conditions
Aborted Takeoff
Use as much of the remaining runway as needed to safely bring the
airplane to a stop or to slow the airplane sufficiently to turn off runway.
1. Power Lever ............................................................................IDLE
2. Brakes .................................................................... AS REQUIRED
• Caution •
For maximum brake effectiveness, retract flaps, hold control
yoke full back, and bring the airplane to a stop by smooth,
even application of the brakes.
After a high-speed aborted takeoff, brake temperatures will be
elevated; subsequent aborted takeoffs or other high-energy
use of the brakes may cause brake overheat, failure and
possibly even fire. A 25-minute cooling time is recommended
following high-energy use of the brake system before
attempting to conduct operations that may require further
high-energy braking. Brake temperature indicator should be
inspected prior to flight following a high-energy brake event
(refer to Preflight Walk-Around Checklist for detail).
March 2010
Cirrus Design Section 3A
SR22 Abnormal Procedures
Information Manual 3A-15
Parking Brake Engaged Annunciation
PARK BRAKE Caution
Parking brake is set.
1. Parking Brake ................................................................ RELEASE
2. Monitor CAS for BRAKE TEMP Caution. Stop aircraft and allow
the brakes to cool if necessary.
Communications Failure
If, after following the checklist procedure, communication is not
restored, proceed with FAR/AIM lost communications procedures.
• Note •
In the event of an audio panel power failure the audio panel
connects COM 1 to the pilot’s headset and speakers. Setting
the audio panel ‘Off’ will also connect COM 1 to the pilot’s
headsets and speakers.
1. Switches, Controls ............................................................. CHECK
2. Frequency ........................................................................CHANGE
3. Circuit Breakers .......................................................................SET
4. Headset ...........................................................................CHANGE
5. Hand Held Microphone ................................................. CONNECT
PARK BRAKE
March 2010
3A-16 Information Manual
Section 3A Cirrus Design
Abnormal Procedures SR22
March 2010
Intentionally Left Blank
Information Manual 4-1
Cirrus Design Section 4
SR22 Normal Procedures
Section 4
Normal Procedures
Table of Contents
Introduction ........................................................................................ 3
Airspeeds for Normal Operation ........................................................ 3
Normal Procedures ............................................................................ 4
Preflight Inspection ......................................................................... 4
Preflight Walk-Around..................................................................... 4
Before Starting Engine.................................................................... 9
Starting Engine ............................................................................. 10
Before Taxiing............................................................................... 12
Taxiing .......................................................................................... 12
Before Takeoff .............................................................................. 13
Maximum Power Fuel Flow .......................................................... 15
Takeoff.......................................................................................... 16
Normal Takeoff ............................................................................. 16
　
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