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180 183
190 193
200 203
Reissue A
P/N 13772-001 5-11
Cirrus Design Section 5
SR22 Performance Data
Airspeed Calibration
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............................................50%
Indicated Airspeed................85 Knots
• Heater, Defroster & Vents .............ON
Calibrated Airspeed..............86 Knots
KIAS
KCAS
Flaps
0%
Flaps
50%
Flaps
100%
60 62
70 71 73
80 80 81 82
90 90 91 92
100 100 101 101
110 110 111
120 120 121
130 130
140 140
150 150
160 160
170 170
180 180
190 190
200 199
Figure 5-2
Reissue A
5-12 P/N 13772-001
Section 5 Cirrus Design
Performance Data SR22
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 ............................................. 0%
Indicated Airspeed ............. 120 Knots
Desired Altitude..................12,000 FT
Altitude Correction ...................-13 FT
Altitude to Fly .....................11,987 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 8 6 3 0 -9 -19 -31 -44 -56
5000 10 7 4 0 -10 -23 -36 -51 -65
10000 11 8 5 0 -12 -26 -42 -59 -76
15000 13 10 5 0 -14 -31 -50 -70 -90
50%
S.L 14 3 -6 -12 -6
5000 17 4 -7 -14 -7
10000 19 4 -9 -17 -8
100%
S.L 13 8 3 0 -1
5000 15 9 3 0 -1
10000 17 10 4 0 -2
Reissue A
P/N 13772-001 5-13
Cirrus Design Section 5
SR22 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
• Heater, Defroster, & Vents.............ON Desired Altitude ................. 12,000 FT
Altitude Correction..................... -4 FT
Altitude to Fly..................... 11,996 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 1 0 -1 -1 -3 -3 -1 4 13
5000 2 0 -1 -2 -3 -3 -1 5 15
10000 2 1 -1 -2 -4 -4 -1 6 18
15000 2 1 -1 -2 -4 -4 -1 7 21
50%
S.L -7 -6 -5 -5 -9
5000 -8 -7 -6 -6 -10
10000 -9 -8 -7 -7 -12
100%
S.L -14 -17 -18 -16 -10
5000 -16 -20 -21 -19 -12
10000 -18 -23 -25 -22 -14
Figure 5-4
Reissue A
5-14 P/N 13772-001
Section 5 Cirrus Design
Performance Data SR22
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
　
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