Cirrus SR22 - Takeoff Distance - 3600 LB

Cirrus Design Section 5
SR22 Performance Data
P/N 13772-004 5-13P/N 13772-004 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°
HeadwindTailwind
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°
V
E
LO
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