Cirrus DESIGN SR22T User Manual

Cirrus Design Section 5
SR22T Performance Data
P/N 13772-003 5-13
Wind Components
• Note •
The max demonstrated crosswind is 20 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 DESIGN SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Model	SR22T
Seating Capacity	5
Engine	Continental TSIO-550-K
Horsepower	315 hp
Avionics	Cirrus Perspective+ by Garmin
Type	Single-engine piston aircraft
Maximum Speed	213 knots
Cruise Speed	183 knots
Service Ceiling	25, 000 feet
Maximum Takeoff Weight	3, 600 lbs
Wingspan	38 feet 4 inches
Length	26 ft
Height	8 feet 11 inches
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cabin Width	49 inches
Cabin Height	50 inches