Cirrus DESIGN SR20 - Airspeed Calibration; Normal Static Source

5-10 P/N 13999-002 Info Manual
Section 5 Cirrus Design
Performance Data SR20
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
• Weight .................................. 3000 LB
Calibrated Airspeed ............. 86 Knots
KIAS
KCAS
Flaps
0%
Flaps
50%
Flaps
100%
50 49
60 60 60
70 72 71 71
80 81 81 81
90 91 91 91
100 101 101 101
110 111 111
120 120 120
130 130
140 140
150 150
160 160
170 170
180 180
190 190
200 200
September 2011