Cirrus SR22 Pilot Operating Handbook page 157

Cirrus Design
SR22
Wind Components
Example:
• Runway Heading................................................................................................ 10°
• Wind Direction.................................................................................................... 60°
• Wind Velocity .............................................................................................15 Knots
The max demonstrated crosswind is 21 knots. Value not considered limiting.
40
0°
30
20
10
0
-10
170°
180°
-20
P/N 13772-004 P/N 13772-004
Original Issue
• Note •
10°
20°
20
10
150°
140°
160°
10
CROSSWIND COMPONENT ~ KNOTS
30°
40°
50°
30
130°
20
Section 5
Performance Data
50
40
60°
70°
80°
90°
100°
110°
120°
30
SR22_FM05_1014
40
5-13 5-13