Cirrus Design
Section 5
SR22T
Performance Data
P/N 13772-005
5-9
P/N 13772-005
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
20000
29
32
36
41
54
75
105
144
194
25000
35
38
43
48
64
89
124
171
231
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
Original Issue
