5-8
P/N 13772-005
Section 5
Cirrus Design
Performance Data
SR22T
Altitude Correction
Alternate Static Source: Primary Flight Display
• 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
4
8
14
21
40
64
94
127
164
5000
4
10
16
25
47
75
109
148
191
10000
5
11
19
29
55
87
127
172
222
15000
6
13
23
34
64
102
149
202
261
20000
7
15
27
40
76
121
176
239
308
25000
8
18
32
48
90
144
209
284
366
50%
S.L
-10
-4
4
11
29
50
80
5000
-12
-4
4
13
33
58
93
10000
-14
-5
5
15
39
68
108
100%
S.L
-2
-9
-2
6
15
39
5000
-2
-11
-2
7
17
45
10000
-3
-13
-3
8
20
53
Original Issue
