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
Summary of Contents for SR20
Page 10: ...1 2 P N 11934 003 Section 1 Cirrus Design General SR20 Intentionally Left Blank Revision A3 ...
Page 22: ...2 2 P N 11934 003 Section 2 Cirrus Design Limitations SR20 Placards 2 21 Revision A6 ...
Page 308: ...9 2 P N 11934 003 Section 9 Cirrus Design Supplements SR20 Intentionally Left Blank Reissue A ...