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Indicated Airspeed................85 Knots
• Weight ...................................3000 LB
• Heater, Defroster & Vents .............ON Calibrated Airspeed..............84 Knots
KIAS
KCAS
Flaps
0%
Flaps
50%
Flaps
100%
50 45
60 59 56
70 70 69 67
80 80 79 78
90 90 89 88
100 100 99 98
110 110 109
120 120 118
130 130
140 140
150 150
160 161
170 171
180 182
190 192
200 203
Figure 5-2
March 2010
5-12 Information Manual
Section 5 Cirrus Design
Performance Data SR20
Figure 5-3
Altitude Correction
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 Desired Altitude..................12,000 FT
Altitude Correction .....................-7 FT
Altitude to Fly .....................11,993 FT
Flaps Press
Alt
CORRECTION TO BE ADDED - FEET
Normal Static Source - KIAS
60 70 80 90 100 120 140 160 180 200
0%
S.L -12 -11 -10 -9 -8 -5 -3 -3 -5 -10
5000 -14 -13 -12 -11 -9 -6 -4 -3 -5 -11
10000 -16 -15 -14 -12 -11 -7 -4 -4 -6 -13
15000 -19 -18 -16 -14 -12 -8 -5 -4 -7 -16
50%
S.L -2 -4 -5 -6 -5 +2
10000 -2 -4 -6 -7 -6 +2
15000 -2 -5 -7 -8 -7 +2
100%
S.L -1 -4 -6 -7 -5
10000 -1 -5 -7 -8 -6
15000 -1 -6 -9 -9 -6
March 2010
Information Manual 5-13
Cirrus Design Section 5
SR20 Performance Data
Altitude Correction
Alternate 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..............................................0%
Indicated Airspeed..............120 Knots
• Weight ...................................3000 LB Desired Altitude ................. 12,000 FT
• Heater, Defroster, & Vents.............ON Altitude Correction................... -11 FT
Altitude to Fly..................... 11,989 FT
Flaps Press
Alt
CORRECTION TO BE ADDED - FEET
Normal Static Source - KIAS
60 70 80 90 100 120 140 160 180 200
0%
S.L -9 -10 -10 -11 -10 -7 -1 11 27 51
5000 -10 -11 -12 -12 -12 -9 -1 12 32 59
10000 -12 -13 -14 -14 -14 -10 -1 14 37 69
15000 -14 -15 -16 -17 -16 -12 -1 17 44 80
50%
S.L -11 -15 -18 -21 -22 -19
10000 -13 -18 -21 -24 -26 -22
15000 -15 -20 -25 -28 -30 -26
100%
S.L -20 -20 -20 -20 -18
10000 -23 -24 -23 -23 -21
15000 -27 -27 -27 -26 -25
Figure 5-4
March 2010
5-14 Information Manual
Section 5 Cirrus Design
Performance Data SR20
Figure 5-5
Temperature Conversion
• Note •
• To convert from Celsius (°C) to Fahrenheit (°F), find, in the shaded columns, the
number representing the temperature value (°C) to be converted. The equivalent
Fahrenheit temperature is read to the right.
 EXAMPLE: 38° C = 100° F.
• To convert from Fahrenheit (°F) to Celsius (°C), find in the shaded columns area,
the number representing the temperature value (°F) to be converted. The equivalent
Celsius temperature is read to the left.
 EXAMPLE: 38° F = 3° C.
Temp to Convert
°C or °F
Temp to Convert
°C or °F
Temp to Convert
°C or °F
°C  °F °C  °F °C  °F
-50 -58 -72 -17 2 36 17 62 144
-49 -56 -69 -16 4 39 18 64 147
-48 -54 -65 -14 6 43 19 66 151
-47 -52 -62 -13 8 46 20 68 154
-46 -50 -58 -12 10 50 21 70 158
-44 -48 -54 -11 12 54 22 72 162
-43 -46 -51 -10 14 57 23 74 165
-42 -44 -47 -9 16 61 24 76 169
-41 -42 -44 -8 18 64 26 78 172
-40 -40 -40 -7 20 68 27 80 176
-39 -38 -36 -6 22 72 28 82 180
-38 -36 -33 -4 24 75 29 84 183
-37 -34 -29 -3 26 79 30 86 187
-36 -32 -26 -2 28 82 31 88 190
-34 -30 -22 -1 30 86 32 90 194
-33 -28 -18 0 32 90 33 92 198
-32 -26 -15 1 34 93 34 94 201
-31 -24 -11 2 36 97 36 96 205
-30 -22 -8 3 38 100 37 98 208
　
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