2-4 P/N 13772-003
Section 2 Cirrus Design
Limitations SR22T
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 up to 17,500
feet MSL
200 204 Never Exceed Speed is the speed that may
not be exceeded at any time.
V
NE at 25,000 feet
MSL
170 173 V
NE
is reduced linearly from 17,500 feet to
25,000 feet.
V
NO up to 17,500
feet MSL
177 180 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
151 153 V
NO
is reduced linearly from 17,500 feet to
25,000 feet.
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 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
To Next Page
Loading...
Need help?
General
