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Weight - Pounds
12.5% M AC
FS 139.1
2700 lb
9.8% MAC
FS 137.8
2100 lb
19.2% M AC
FS 142.3
3400 lb
31.5% M AC
FS 148.1
3400 lb
31.5% MAC
FS 148.1
2100 lb
Figure - 3
C.G. Envelope
Original: 03-27-07
10 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
Fuel Limits
Approved Fuel ............... Aviation Grade 100 LL (Blue) or 100 (Green)
Total Fuel Capacity ...................................... 94.5 U.S. Gallon (358.0 L)
Total Fuel Each Tank ................................. 47.25 U.S. Gallon (179.0 L)
Total Usable Fuel (all flight conditions) ........ 92.0 U.S. Gallon (348.0 L)
Maximum Allowable Fuel Imbalance .............10.0 U.S. Gallon (¼ tank)
The fuel system BOOST pump must be on for takeoff, climb, landing,
and for switching fuel tanks.
Original: 03-27-07
13772-130 11 of 58
Cirrus Design Section 9
SR22 Supplements
Placards
Wing, adjacent to fuel filler caps:
SR22_FM09_2584
Figure - 4
Placards
Original: 03-27-07
12 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
Original: 03-27-07
Intentionally Left Blank
13772-130 13 of 58
Cirrus Design Section 9
SR22 Supplements
Section 3 - Emergency Procedures
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)
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 pattern 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 FAN SPEED TO FULL ON (3) POSITION
If source of smoke and fume is firewall foward:
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.
Original: 03-27-07
14 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
Engine Fire In Flight
If an engine fire occurs during flight, do not attempt to restart the
engine.
1. Mixture ............................................................................. CUTOFF
2. Fuel Pump................................................................................OFF
3. Fuel Selector............................................................................OFF
4. Airflow Selector ........................................................................OFF
5. Power Lever ...........................................................................IDLE
6. Ignition Switch ..........................................................................OFF
7. Cabin Doors ...................................................... PARTIALLY OPEN
Airspeed may need to be reduced to partially open door in flight.
8. Land as soon as possible.
Cabin Fire In Flight
If the cause of the fire is readily apparent and accessible, use the fire
extinguisher to extinguish flames and land as soon as possible.
Opening the vents or doors may feed the fire, but to avoid
incapacitating the crew from smoke inhalation, it may be necessary to
rid cabin of smoke or fire extinguishant. If the cause of fire is not
readily apparent, is electrical, or is not readily accessible, proceed as
follows:
• WARNING •
If the airplane is in IMC conditions, turn ALT 1, ALT 2, and BAT
1 switches OFF. Power from battery 2 will keep the Primary
Flight Display operational for approximately 30 minutes.
1. Bat-Alt Master Switches........................................ OFF, AS REQ’D
• Note •
With Bat-Alt Master Switches OFF, engine will continue to run.
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(140)
