Cirrus SR22T, Pilot Operating Handbook

Page: 30 / 506

2-4 P/N 13772-005
Section 2 Cirrus Design
Limitations SR22T
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 up to 17,500
feet MSL
205 208
Never Exceed Speed
is the speed that may
not be exceeded at any time.
V
NE at 25,000 feet
MSL
175 178 V
NE
is reduced linearly from 17,500 feet to
25,000 feet.
V
NO up to 17,500
feet MSL
176 179 Maximum Structural Cruising Speed is the
speed that should not be exceeded except in
smooth air and then only with caution.
V
NO at 25,000
feet MSL
150 153 V
NO
is reduced linearly from 17,500 feet to
25,000 feet.
VO
3600 Lb
140 142
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.
VFE
50% Flaps
100% Flaps
150
110 152
111
Maximum Flap Extended Speed is the high-
est speed permissible with wing flaps
extended.
VPD 140 142 Maximum Demonstrated Parachute
Deployment Speed
is the maximum speed at
which parachute deployment has been dem-
onstrated.
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