P/N 11934-003
5-17
Cirrus Design
Section 5
SR20
Performance Data
Wind Components
• Note •
• The maximum demonstrated crosswind is 21 knots. Value not considered limiting.
Conditions:
Example:
• Runway Heading ...........................10°
Wind/Flight Path Angle ................. 50°
• Wind Direction...............................60°
Crosswind Component .........12 Knots
• Wind Velocity........................ 15 Knots
Headwind Component ..........10 Knots
10°
H
ead
win
d
Ta
ilwi
nd
0°
A
N
G
LE
B
E
T
W
E
E
N
W
IN
D
D
IR
E
C
T
IO
N
A
N
D
F
LI
G
H
T
P
A
T
H
20°
30°
40°
50°
60°
70°
80°
90°
100°
110°
120°
130°
140°
150°
160°
170°
180°
VE
LO
C
IT
Y
~
K
N
O
T
S
W
IN
D
40
40
30
20
10
WIND COMPONENTS ~ KNOTS
CROSSWIND COMPONENT ~ KNOTS
-20
-10
0
10
20
40
30
SR20_FM05_1014
10
20
30
50
Figure 5-8
Reissue A
Содержание SR20
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