Airspeed Limitations - Cirrus SR22 Pilot Operating Handbook

Section 2
Limitations

Airspeed Limitations

The indicated airspeeds in the following table are based on Section 5,
Airspeed Calibration - Normal Static Source
alternate static source, allow for the airspeed calibration variations
between the normal and alternate static sources.
Speed
V NE
V NO
V O
3600 Lb
V FE
50% Flaps
100% Flaps
V PD
2-4
KIAS KCAS
205 208
176 179
140 142
150 152
110 111
140 142
Table. When using the
Remarks
Never Exceed Speed is the speed limit that
may not be exceeded at any time.
Maximum Structural Cruising Speed is the
speed that should not be exceeded except in
smooth air, and then only with caution.
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.
Maximum Flap Extended Speed is the highest
speed permissible with wing flaps extended.
Maximum Demonstrated Parachute Deploy-
ment Speed is the maximum speed at which
parachute deployment has been demon-
strated.
Cirrus Design
SR22
P/N 13772-004
Original Issue