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3
AC
ON
COLD
HOT
OFF
S
P
S P
FOOT-WARMER
DIFFUSER
DISTRIBUTION
MANIFOLD
FRESH AIR
VALVE
EVAPORATOR
ASSEMBLY
HOT AIR
VALVE
COMPRESSOR
HEAT EXCHANGER
RECIRCULATION
CHECK VALVE
SR22_FM09_2081B
VENTS
TEMPERATURE
AIRFLOW
AIR
INLET
CONDENSER
ASSEMBLY
NOTE: Illustration depicts maximum
cabin cooling airflows and
selector settings.
PANEL AIRFLOW
FRESH AIR
INTAKE
FLOOR AIRFLOW
WINDSHIELD
DIFFUSER
AIR MIXING
CHAMBER
AIR GASPER
Figure - 1 (Sheet 1 of 2)
Air Conditioning System Schematic - Serials before G3 Wing
Revision 01: 03-27-07
4 of 14 P/N 13772-127
Section 9 Cirrus Design
Supplements SR22
Figure - 1 (Sheet 2 of 2)
AIR FLOW VALVE
RAM AIR RAM AIR
FRESH AIR
VALVE
HOT AIR
VALVE
HEAT
EXCHANGER
1 2
3
AC
ON
COLD
HOT
OFF
S
P
S P
FOOT-WARMER
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
　
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