5-10
P/N 11934-003
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
Reissue A
Summary of Contents for SR20
Page 10: ...1 2 P N 11934 003 Section 1 Cirrus Design General SR20 Intentionally Left Blank Revision A3 ...
Page 22: ...2 2 P N 11934 003 Section 2 Cirrus Design Limitations SR20 Placards 2 21 Revision A6 ...
Page 308: ...9 2 P N 11934 003 Section 9 Cirrus Design Supplements SR20 Intentionally Left Blank Reissue A ...