Airspeed Calibration - Normal Static Source - Cirrus DESIGN 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 57
70 68
80 79
90 89
100 100
110 111
120 121
130 132
140 142
150 152
160 163
170 173
180 183
190 193
200 204
KCAS
Flaps Flaps
50% 100%
56 57
68 70
80 80
91 89
101 99
111 111
121
Cirrus Design
SR22
P/N 13772-002
Reissue A