Cirrus DESIGN SR22 - Page 147

Cirrus Design Section 5
SR22 Performance Data
P/N 13772-002 5-9P/N 13772-002 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
10 25 40 56 87 114 141 169 205
5000
11 29 47 65 100 133 163 196 238
10000
13 34 55 76 117 155 191 229 277
15000
16 39 64 89 138 182 224 268 325
50%
S.L
25 40 55 69 91
5000 29 46 64 81 106
10000 34 54 75 94 123
100%
S.L 28 42 53 62 71
5000 33 49 62 72 83
10000 38 57 72 84 96
Reissue A