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RADIUS FOR OUTSIDE GEAR
RADIUS FOR INSIDE GEAR
RADIUS FOR WING TIP
TURNING RADII ARE CALCULATED USING ONE BRAKE AND
PARTIAL POWER. ACTUAL TURNING RADIUS MAY VARY AS
MUCH AS THREE FEET.
GROUND TURNING CLEARANCE
SR22_FM01_2412
Turning Radius
Original: 03-27-07
13772-130 5 of 58
Cirrus Design Section 9
SR22 Supplements
78 inches 3-BLADE
198 cm
38.3 ft
11.67 m
9.1 ft
2.8 m
9 inches (minimum)
23 cm (minimum)
26.0 ft
7.92 m
SR22_FM01_2414
8.9 ft
2.71 m
NOTE:
• Wing span includes
position and strobe lights.
• Prop ground clearance at
3400 lb - 9" inches (23 cm).
• Wing Area = 144.9 sq. ft.
Figure - 2
Airplane Three View
Original: 03-27-07
6 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
The Airplane
Fuel
Total Capacity .............................................94.5 U.S. Gallons (358.0 L)
Total Usable ................................................92.0 U.S. Gallons (348.0 L)
Original: 03-27-07
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Cirrus Design Section 9
SR22 Supplements
Section 2 - Limitations
Airspeed Limitations
The indicated airspeeds in the following table are based upon Section
5 Airspeed Calibrations using the normal static source. When using
the alternate static source, allow for the airspeed calibration variations
between the normal and alternate static sources.
Speed KIAS KCAS Remarks
VNE 200 204 Never Exceed Speed is the speed limit
that may not be exceeded at any time.
VNO 177 180 Maximum Structural Cruising Speed is
the speed that should not be exceeded
except in smooth air, and then only with
caution.
VO
3400 Lb 133 135
Operating Maneuvering Speed is the
maximum speed at which full control
travel may be used. Below this speed the
airplane stalls before limit loads are
reached. Above this speed, full control
movements can damage the airplane.
VFE
50% Flaps
100% Flaps
119
104
120
104
Maximum Flap Extended Speed is the
highest speed permissible with wing
flaps extended.
VPD 133 135 Maximum Demonstrated Parachute
Deployment Speed is the maximum
speed at which parachute deployment
has been demonstrated.
Original: 03-27-07
8 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
Airspeed Indicator Markings
The airspeed indicator markings are based upon Section 5 Airspeed
Calibrations using the normal static source. When using the alternate
static source, allow for the airspeed calibration variations between the
normal and alternate static sources.
Power Plant Limitations
Propeller
MT Propeller
Propeller Type........................................ Constant Speed, Three Blade
Model Number ............................................................ MTV-9-D/198-52
Diameter ........................................................................................78.0"
Weight Limits
Maximum Takeoff Weight ........................................3400 lb (1542 Kg)*
*no change
Marking
Value
(KIAS)
Remarks
White
Arc
62 - 104 Full Flap Operating Range. Lower limit is the most
adverse stall speed in the landing configuration.
Upper limit is the maximum speed permissible with
flaps extended.
Green
Arc
73 - 177 Normal Operating Range. Lower limit is the
maximum weight stall at most forward C.G. with
flaps retracted. Upper limit is the maximum structural
cruising speed.
Yellow
Arc
177 - 200 Caution Range. Operations must be conducted with
caution and only in smooth air.
Red Line 200 Never exceed speed. Maximum speed for all
operations.
Original: 03-27-07
13772-130 9 of 58
Cirrus Design Section 9
SR22 Supplements
Center of Gravity Limits
Reference Datum ....................................100 inches forward of firewall
Forward ...................................................................... Refer to Figure 3
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
　
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