Cirrus Design Section 5
SR22 Performance Data
P/N 13772-004 5-9P/N 13772-004 5-9
Altitude Correction
Alternate Static Source: Standby Altimeter
• 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 Density
Alt
CORRECTION TO BE ADDED - FEET
Alternate Static Source - KIAS
60 70 80 90 100 120 140 160 180 200
0%
S.L
16 17 19 22 29 40 56 77 103
5000
18 20 22 25 33 46 65 89 120
10000
21 23 26 29 39 54 75 104 140
15000
25 27 30 34 46 63 89 122 164
50%
S.L
2 5 9 11 17 25 42
5000 2 6 10 13 20 30 49
10000 3 7 12 16 23 34 57
100%
S.L -2 3 7 11 15 27
5000 -2 3 8 12 18 32
10000 -3 4 9 15 20 37
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