Cirrus DESIGN SR20 Information Manual

2-4 P/N 13999-002 Info Manual
Section 2 Cirrus Design
Limitations SR20
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
200 200 Never Exceed Speed is the speed limit
that may not be exceeded at any time.
V
NO
165 165 Maximum Structural Cruising Speed is
the speed that should not be exceeded
except in smooth air, and then only with
caution.
V
O
3000 Lb
2600 Lb
2300 Lb
131
122
114
131
123
115
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
120
100
120
101
Maximum Flap Extended Speed is the
highest speed permissible with wing
flaps extended.
V
PD
135 135 Maximum Demonstrated Parachute
Deployment Speed is the maximum
speed at which parachute deployment
has been demonstrated.
Airspeed Limits
September 2011

Cirrus DESIGN SR20 Specifications

General

Brand	Cirrus
Model	DESIGN SR20
Category	Aircrafts
Language	English