Cirrus SR22T User Manual

Cirrus Design Section 5
SR22T Performance Data
P/N 13772-005 5-13P/N 13772-005 5-13
Wind Components
• Note •
The max demonstrated crosswind is 21 knots. Value not considered limiting.
Example:
•Runway Heading................................................................................................10°
•Wind Direction....................................................................................................60°
•Wind Velocity..............................................................................................15 Knots
10°
Headwind
Tailwind
0°
A
N
G
L
E
B
E
T
W
E
E
N
W
I
N
D
D
I
R
E
C
T
I
O
N
A
N
D
F
L
I
G
H
T
P
A
T
H
20°
30°
40°
50°
60°
70°
80°
90°
100°
110°
120°
130°
140°
150°
160°
170°
180°
VELO
C
ITY
~
K
N
O
T
S
W
I
N
D
40
40302010
WIND COMPONENTS ~ KNOTS
CROSSWIND COMPONENT ~ KNOTS
-20
-10
0
10
20
40
30
SR22_FM05_1014
10
20
30
50
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