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CIRRUS DESIGN SR22 - Airspeed Limitations

CIRRUS DESIGN SR22
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2-4 Information Manual
Section 2 Cirrus Design
Limitations SR22
Figure 2-1
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
V
NE
201 204 Never Exceed Speed is the speed limit
that may not be exceeded at any time.
V
NO
178 180 Maximum Structural Cruising Speed is
the speed that should not be exceeded
except in smooth air, and then only with
caution.
V
O
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.
V
FE
50% Flaps
100% Flaps
119
104
120
104
Maximum Flap Extended Speed is the
highest speed permissible with wing
flaps extended.
V
PD
133 135 Maximum Demonstrated Parachute
Deployment Speed is the maximum
speed at which parachute deployment
has been demonstrated.
Airspeed Limits
March 2010

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