Cirrus DESIGN SR22 User Manual

2-4 P/N 13772-002
Section 2 Cirrus Design
Limitations SR22
Airspeed Limitations
The indicated airspeeds in the following table are based on Section 5,
Airspeed Calibration - Normal Static Source Table. 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
177 180 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 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 highest
speed permissible with wing flaps extended.
V
PD
133 135 Maximum Demonstrated Parachute Deploy-
ment Speed is the maximum speed at which
parachute deployment has been demon-
strated.
Reissue A

Cirrus DESIGN SR22 Specifications

General

Brand	Cirrus
Model	DESIGN SR22
Category	Aircrafts
Language	English