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• Increased fuel capacity,
• wing tip with integral, leading edge recognition lights.
• relocation of the fresh air inlets to the engine cowl and related
environmental system changes,
• improved trailing edge aerodynamics
• improved wing root fairings,
• relocation of the stall warning port.
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Section 9 Cirrus Design
Supplements SR22
Figure - 1
9.1 ft. (2.77 m)
0.5 ft. (0.15 m)
24.3 ft. (7.41 m)
RADIUS FOR NOSE GEAR 7.0 ft. (2.16 m)
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
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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
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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)
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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.
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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.
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Cirrus Design Section 9
SR22 Supplements
Center of Gravity Limits
Reference Datum ....................................100 inches forward of firewall
Forward ...................................................................... Refer to Figure 3
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