Cirrus SR22 Pilot Operating Handbook page 441

Cirrus Design
SR22
Altitude Correction
Normal Static Source: Standby Altimeter
Conditions:
• Power for level flight or maximum continuous, whichever is less.
• 3400 LB
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
13772-130
Revision 03: 05-09-11
• Note •
CORRECTION TO BE ADDED - FEET
Normal Static Source - KIAS
60 70 80
12 9
14 11
17 12
20 15
11 3
13 3
15 4
15 1 -1
17 1 -1
20 1 -1
90 100 120
5 0 -11
6 0 -13
7 0 -15
8 0 -18
-5 -11 -14
-6 -13 -17
-7 -15 -20
4 6
5 7
6 8
Section 9
Supplements
140 160 180
-24 -37 -50
-28 -43 -57
-33 -50 -67
-38 -59 -79
17 of 48
200
-60
-69
-81
-95