Specifications

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Cirrus Design Section 9
SR20 Supplements
Section 5 - Performance
Airspeed Calibration
Normal Static Source
• Note •
• Indicated airspeed values assume zero instrument error.
Conditions:
• Power for level flight or maximum continuous, whichever is less.
KIAS
KCAS
Flaps
0%
Flaps
50%
Flaps
100%
60 57 56 57
70 68 68 70
80 79 80 80
90 89 91 89
100 100 101 99
110 111 111
120 121 121
130 132
140 142
150 152
160 163
170 173
180 183
190 193
200 204
Revision 01: 08-26-09