CIRRUS DESIGN SR22 - Airspeed Calibration

5-10 Information Manual
Section 5 Cirrus Design
Performance Data SR22
Figure 5-1
Airspeed Calibration
Normal Static Source
• Note •
• Indicated airspeed values assume zero instrument error.
• KIAS = Knots Indicated Airspeed
• KCAS = Knots Calibrated Airspeed
Conditions: Example:
• Power for level flight or maximum
continuous, whichever is less.
Flaps ...........................................50%
Indicated Airspeed ...............85 Knots
Calibrated Airspeed .............85 Knots
KIAS
KCAS
Flaps
0%
Flaps
50%
Flaps
100%
60 58
70 68 69
80 79 80 80
90 90 91 90
100 100 101 100
110 110 111
120 121 121
130 131
140 142
150 152
160 162
170 172
180 183
190 193
200 203
March 2010