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• Normal Approach, Flaps Up.....................................90-95 KIAS
• Normal Approach, Flaps 50% ..................................85-90 KIAS
• Normal Approach, Flaps 100%................................80-85 KIAS
• Short Field, Flaps 100% (VREF) ....................................77 KIAS
Go-Around, Flaps 50%:
• Full Power......................................................................80 KIAS
Maximum Recommended Turbulent Air Penetration:
• 3400 lb.........................................................................133 KIAS
• 2900 lb.........................................................................123 KIAS
Maximum Demonstrated Crosswind Velocity:
• Takeoff or Landing........................................................20 Knots
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Section 9 Cirrus Design
Supplements SR22
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Cirrus Design Section 9
SR22 Supplements
Section 5 - Performance
Airspeed Calibration
Normal Static Source
• Note •
• Indicated airspeed values assume zero instrument error.
Conditions: Example:
• Power for level flight or maximum
continuous, whichever is less.
Flaps............................................50%
Indicated Airspeed................90 Knots
Calibrated Airspeed..............91 Knots
KIAS
KCAS
Flaps
0%
Flaps
50%
Flaps
100%
60 57 56 57
70 68 68 70
80 79 80 80
90 89 91 89
100 100 101 99
110 111 111 111
120 121 121
130 132
140 142
150 152
160 163
170 173
180 183
190 193
200 204
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Section 9 Cirrus Design
Supplements SR22
Airspeed Calibration
Alternate Static Source
• Note •
• Indicated airspeed values assume zero instrument error.
Conditions: Example:
• Power for level flight or maximum
continuous, whichever is less.
Flaps ........................................... 50%
Indicated Airspeed ............... 90 Knots
• Heater, Defroster & Vents............. ON
Calibrated Airspeed ............. 83 Knots
KIAS
KCAS
Flaps
0%
Flaps
50%
Flaps
100%
60 61 58 54
70 68 66 63
80 77 74 72
90 85 83 82
100 94 92 92
110 103 102 101
120 112 112
130 121 122
140 131
150 141
160 150
170 160
180 170
190 179
200 189
210 198
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Cirrus Design Section 9
SR22 Supplements
Altitude Correction
Normal Static Source
• Note •
• Add correction to desired altitude to obtain indicated altitude to fly.
• Indicated airspeed values assume zero instrument error.
• KIAS = Knots Indicated Airspeed.
Conditions:
• Power for level flight or maximum continuous, whichever is less.
• 3400 LB
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 9 5 0 -11 -23 -36 -49 -59
5000 13 10 5 0 -13 -27 -42 -56 -69
10000 16 12 6 0 -15 -32 -49 -66 -80
15000 18 14 7 0 -17 -37 -58 -77 -94
50%
S.L 9 2 -4 -10 -16
5000 11 3 -5 -12 -18
10000 12 3 -6 -14 -22
100%
S.L 10 1 -1 2 6
5000 10 -1 1 6 6
10000 37 45 48 50 56
Revision 02: 08-26-09
22 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
Altitude Correction
Alternate Static Source
• Note •
• Add correction to desired altitude to obtain indicated altitude to fly.
• Indicated airspeed values assume zero instrument error.
• KIAS = Knots Indicated Airspeed.
Conditions:
• Power for level flight or maximum continuous, whichever is less.
• Heater, Defroster, & Vents ..................................................................................ON
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 28 43 57 82 104 126 148 172
5000 16 35 54 71 104 136 168 203 242
10000 20 43 66 87 128 169 211 258 311
15000 23 51 78 103 152 200 251 308 373
50%
S.L 43 65 87 108 148
5000 21 32 39 42 26
10000 36 54 70 82 88
100%
S.L 42 56 67 80 95
5000 37 45 48 50 56
10000 61 81 99 119 148
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