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DIFFUSER
DISTRIBUTION
MANIFOLD
EVAPORATOR
ASSEMBLY
COMPRESSOR
RECIRCULATION
CHECK VALVE
VENTS
TEMPERATURE
AIRFLOW
CONDENSER
ASSEMBLY
NOTE: Illustration depicts maximum
cabin cooling airflows and
selector settings.
PANEL AIRFLOW
FLOOR AIRFLOW WINDSHIELD
DIFFUSER
AIR GASPER
SR22_FM09_2593
MIXING
CHAMBER
SERVO MOTOR
Air Conditioning System Schematic - Serials G3 and Subs
Revision 01: 03-27-07
P/N 13772-127 5 of 14
Cirrus Design Section 9
SR22 Supplements
Section 2 - Limitations
There is no change to the basic POH Limitations Section when the Air
Conditioning System is installed.
Section 3 - Emergency Procedures
Engine Failure In Flight
1. Air-conditioner..........................................................................OFF
Engine Airstart
1. Air-conditioner..........................................................................OFF
Engine Partial Power Loss
1. Air-conditioner..........................................................................OFF
Low Oil Pressure
1. Air-conditioner..........................................................................OFF
Smoke and Fume Elimination (See Figure - 2)
1. Air-conditioner..........................................................................OFF
2. Temperature Selector............................................................COLD
3. Vent Selector......................... FEET/PANEL/DEFROST POSITION
4. Airflow Selector ........................SET FAN SPEED TO 3 POSITION
If source of smoke and fume is firewall foward:
a. Airflow Selector .................................................................OFF
5. Panel Eyeball Outlets............................................................OPEN
6. Prepare to land as soon as possible.
If airflow is not sufficient to clear smoke or fumes from cabin:
7. Cabin Doors.......................................................PARTIALLY OPEN
Airspeed may need to be reduced to partially open door in flight.
Revision 01: 03-27-07
6 of 14 P/N 13772-127
Section 9 Cirrus Design
Supplements SR22
Cabin Fire In Flight
1. Air-conditioner..........................................................................OFF
Section 3A - Abnormal Procedures
Alternator Failure
1. Air-conditioner..........................................................................OFF
Engine Indicating System Failure
1. Air-conditioner..........................................................................OFF
LOW VOLTS Warning Light Illuminated
1. Air-conditioner..........................................................................OFF
Revision 01: 03-27-07
P/N 13772-127 7 of 14
Cirrus Design Section 9
SR22 Supplements
Section 4 - Normal Procedures
Preflight Walk-Around
1. System Vents .............................................................Unobstructed
2. System Drains............................................................Unobstructed
Ground Operation
• Note •
To facilitate faster cabin cooling, prior to engine start leave the
cabin doors open for a short time to allow hot air to escape
cabin.
For maximum cabin cooling, set Airflow Selector to fan speed
3, Vent Selector to feet/panel/defrost position, and
Temperature Selector to recirculation mode. Additionally,
ensure the instrument panel and armrest eyeball outlets are
open. (See Figure - 1)
1. Control Panel .................SELECT Desired Mode and Temperature
2. Voltage...........................................................................MONITOR
• Note •
Decrease electrical load if battery discharge is noted.
3. Annunciator Lights ............................................................. CHECK
a. Verify ALT 1 caution light out and positive amps indication.
4. Engine Parameters ............................................................ CHECK
Before Takeoff
1. Air-conditioner..........................................................................OFF
Revision 01: 03-27-07
8 of 14 P/N 13772-127
Section 9 Cirrus Design
Supplements SR22
Section 5 - Performance
When the air-conditioner is operating the following performance
changes will result:
1. Brake Horsepower is reduced by approximately 6 BHP.
2. Takeoff Distance: Add 100 feet to ground roll and 150 feet to
distance over 50 foot obstacle.
3. Maximum rate of climb performance is reduced by approximately
50 feet per minute. For maximum climb performance the airconditioner
should be off.
4. Cruise performance is reduced by 2 knots. If maximum
　
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