Cirrus SR22T User Manual

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.
V
O
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.
V
FE
50% Flaps
100% Flaps
150
110
152
111
Maximum Flap Extended Speed is the high-
est speed permissible with wing flaps
extended.
V
PD
140 142 Maximum Demonstrated Parachute
Deployment Speed is the maximum speed at
which parachute deployment has been dem-
onstrated.
Original Issue

Cirrus SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Engine	Continental TSIO-550-K
Horsepower	315 hp
Max Takeoff Weight	3, 600 lbs
Service Ceiling	25, 000 ft
Cabin Width	49 in
Cabin Height	50 in
Seating Capacity	4
Avionics	Cirrus Perspective+ by Garmin
Category	Single-engine piston aircraft
Propeller	Hartzell 3-blade composite
Wingspan	38 ft 4 in
Length	26 ft
Height	8 ft 11 in
Maximum Cruise Speed	213 KTAS
Fuel Capacity	92 gallons
Stall Speed	64 knots
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cruise Speed	183 knots