Cirrus DESIGN SR22 Pilot Operating Handbook page 147

Cirrus Design
SR22
Altitude Correction
Alternate Static Source: Standby Altimeter
Conditions:
• Power for level flight or maximum continuous, whichever is less.
• Heater, Defroster, & Vents.................................................................................. ON
Add correction to desired altitude to obtain indicated altitude to fly.
Indicated airspeed values assume zero instrument error.
KIAS: Knots Indicated Airspeed.
Flaps Density
Alt
S.L
5000
0%
10000
15000
S.L
50% 5000
10000
S.L
100% 5000
10000
P/N 13772-002 P/N 13772-002
Reissue A
• Note •
CORRECTION TO BE ADDED - FEET
Alternate Static Source - KIAS
60 70 80
10 25
11 29
13 34
16 39
25 40
29 46
34 54
28 42 53
33 49 62
38 57 72
90 100 120
40 56 87
47 65 100
55 76 117
64 89 138
55 69 91
64 81 106
75 94 123
62 71
72 83
84 96
Section 5
Performance Data
140 160 180
114 141 169
133 163 196
155 191 229
182 224 268
200
205
238
277
325
5-9 5-9