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9. Avionics Power Switch ...............................................................ON
10. Activate required systems one at a time. Pause several seconds
between activating each system to isolate malfunctioning system.
Continue flight to earliest possible landing with malfunctioning
system off. Activate only the minimum amount of equipment
necessary to complete a safe landing.
11. Temperature Selector............................................................COLD
12. Vent Selector......................... FEET/PANEL/DEFROST POSITION
13. Airflow Selector ...............................SET AIRFLOW TO MAXIMUM
14. Panel Eyeball Outlets............................................................OPEN
March 2010
3-12 Information Manual
Section 3 Cirrus Design
Emergency Procedures SR22
Wing Fire In Flight
1. Pitot Heat Switch......................................................................OFF
2. Navigation Light Switch............................................................OFF
3. Landing Light ...........................................................................OFF
4. Strobe Light Switch ..................................................................OFF
5. If possible, side slip to keep flames away from fuel tank and cabin.
• Note •
Putting the airplane into a dive may blow out the fire. Do not
exceed VNE during the dive.
6. Land as soon as possible.
Engine Fire During Start
A fire during engine start may be caused by fuel igniting in the fuel
induction system. If this occurs, attempt to draw the fire back into the
engine by continuing to crank the engine.
1. Mixture ............................................................................. CUTOFF
2. Fuel Pump................................................................................OFF
3. Fuel Selector............................................................................OFF
4. Power Lever ..................................................................FORWARD
5. Starter ................................................................................ CRANK
6. If flames persist, perform Emergency Engine Shutdown on
Ground and Emergency Ground Egress checklists.
March 2010
Cirrus Design Section 3
SR22 Emergency Procedures
Information Manual 3-13
Smoke and Fume Elimination
If smoke and/or fumes are detected in the cabin, check the engine
parameters for any sign of malfunction. If a fuel leak has occurred,
actuation of electrical components may cause a fire. If there is a strong
smell of fuel in the cockpit, divert to the nearest suitable landing field.
Perform a Forced Landing and shut down the fuel supply to the engine
once a safe landing is assured.
1. Temperature Selector............................................................COLD
2. Vent Selector......................... FEET/PANEL/DEFROST POSITION
3. Airflow Selector ...............................SET AIRFLOW TO MAXIMUM
If source of smoke and fume is firewall forward:
a. Airflow Selector .................................................................OFF
4. Panel Eyeball Outlets............................................................OPEN
5. Prepare to land as soon as possible.
If airflow is not sufficient to clear smoke or fumes from cabin:
6. Cabin Doors.......................................................PARTIALLY OPEN
Airspeed may need to be reduced to partially open door in flight.
March 2010
3-14 Information Manual
Section 3 Cirrus Design
Emergency Procedures SR22
Emergency Descent
Emergency Descent
1. Power Lever ............................................................................IDLE
2. Mixture ................................................................... AS REQUIRED
• Caution •
If significant turbulence is expected do not descend at
indicated airspeeds greater than VNO (177 KIAS)
3. Airspeed.................................................................VNE (200 KIAS)
Maximum Glide
Best Glide Speed
88 KIAS at 3400 lb
Maximum Glide Ratio ~ 9.6: 1
Conditions Example:
Power OFF Altitude 10,000 ft. AGL
Propeller Windmilling Airspeed Best Glide
Flaps 0% (UP) Glide Distance 15.8 NM
Wind Zero
14000
12000
10000
8000
6000
2000
4000
0
0 2 4 6 8 10 12 14 16 18 20
GROUND DISTANCE - NAUTICAL MILES
HEIGHT ABOVE GROUND - FEET
March 2010
Cirrus Design Section 3
SR22 Emergency Procedures
Information Manual 3-15
Forced Landings
If all attempts to restart the engine fail and a forced landing is
imminent, select a suitable field and prepare for the landing. If flight
　
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