Normal Static Source - Cirrus SR22 Pilot Operating Handbook

Section 5
Performance Data
Airspeed Calibration - Normal Static Source
Conditions:
• Power for level flight or maximum continuous, whichever is less.
• Indicated airspeed values assume zero instrument error.
5-4
• Note •
KIAS
Flaps
0%
60
70
80
79
90
90
100
100
110
110
120
121
130
131
140
142
150
152
160
162
170
172
180
183
190
193
200
203
Figure 5-1
KCAS
Flaps Flaps
50% 100%
58
68 69
80 80
91 90
101 100
111
121
Cirrus Design
SR22
P/N 13772-001
Revision A10