Cirrus Design
Section 5
SR22T
Performance Data
P/N 13772-005
5-7
P/N 13772-005
5-7
Altitude Correction
Normal 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.
• 3600 LB
Flaps
Density
Alt
CORRECTION TO BE ADDED - FEET
Normal Static Source - KIAS
60
70
80
90
100
120
140
160
180
200
0%
S.L
12
9
5
0
-11
-24
-38
-50
-61
5000
14
10
6
0
-13
-28
-44
-58
-71
10000
16
12
7
0
-16
-33
-51
-68
-82
15000
19
14
8
0
-18
-39
-60
-80
-97
20000
23
17
9
0
-21
-46
-71
-95
-114
25000
27
20
11
0
-26
-55
-85
-112
-136
50%
S.L
21
0
-14
-21
-30
-46
-66
5000
24
0
-16
-25
-35
-54
-77
10000
28
0
-18
-29
-41
-63
-90
100%
S.L
22
6
-1
-9
-19
-30
5000
25
7
-1
-10
-22
-34
10000
29
8
-2
-12
-25
-40
Original Issue
