Cirrus DESIGN SR20 User Manual

2-4 P/N 11934-004
Section 2 Cirrus Design
Limitations SR20
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
200 204 Never Exceed Speed is the speed limit that
may not be exceeded at any time.
V
NO
163 166 Maximum Structural Cruising Speed is the
speed that should not be exceeded except in
smooth air, and then only with caution.
V
O
3050 Lb
130 131
Operating Maneuvering Speed is the maxi-
mum 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 high-
est 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 dem-
onstrated.
Original Issue

Cirrus DESIGN SR20 Specifications

General

Brand	Cirrus
Model	DESIGN SR20
Category	Aircrafts
Language	English