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Aft ............................................................................... Refer to Figure 3
FORWARD LIMIT - The forward limit is FS 137.8 (9.8% MAC) at 2100 lb, with straight line taper
to FS 139.1 (12.5% MAC) at 2700 lb, to FS 142.3 (19.2% MAC at 3400 lb.
AFT LIMIT - The aft limit is FS 148.1 (31.5% MAC) at all weights from 2100 lb to 3400 lb.
2000
2200
2400
2600
2800
3000
3200
3400
3600
136 138 140 142 144 146 148 150
C.G. - Inches Aft of Datum
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
Revision 02: 08-26-09
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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.
Revision 02: 08-26-09
13772-130 11 of 58
Cirrus Design Section 9
SR22 Supplements
Placards
104 KIAS
100%
119 KIAS
50%
UP
N
O
I
T
C
I
R
F
M
I
X
T
U
R
E
OFF
LIFT BUTTON FOR OFF POSITION
OFF
TURN BOOST
PUMP ON
BEFORE SWITCHING
FUEL TANKS
RIGHT
46 U.S.
GALLONS
USABLE
LEFT
46 U.S.
GALLONS
USABLE
13614-001
FUEL
PUMP
PRIME
BOOST
P
O
W
E
R
IDLE CUTOFF
RICH
MAX
FLAPS
Engine control panel:
CONTROL HANDLES FULLY DOWN BEFORE FLIGHT
CREW SEATS MUST BE LOCKED IN POSITION AND
Airplanes Registered in Brazil
and Operating Under the Agência
Nacional de Aviação Civil Requirements:
Wing, adjacent to fuel filler caps:
SR22_FM09_2584B
Figure - 4
Placards
Revision 02: 08-26-09
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Section 9 Cirrus Design
Supplements SR22
Revision 02: 08-26-09
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.
Revision 02: 08-26-09
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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
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CIRRUS DESIGN SR22西锐22飞行员操作手册和飞机飞行手册(139)
