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Cirrus DESIGN SR20 - Airspeed Calibration - Normal Static Source

Cirrus DESIGN SR20
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5-4 P/N 11934-004
Section 5 Cirrus Design
Performance Data SR20
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 1

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