Altitude Correction - Cirrus SR22 Pilot Operating Handbook

Section 5
Performance Data

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 Press
Alt
S.L
5000
0%
10000
15000
S.L
50% 5000
10000
S.L
100% 5000
10000
5-6
• Note •
CORRECTION TO BE ADDED - FEET
Normal Static Source - KIAS
60 70 80
8 6
10 7
11 8
13 10
14 3
17 4
19 4
13 8 3
15 9 3
17 10 4
Figure 5-3
90 100 120
3 0 -9
4 0 -10
5 0 -12
5 0 -14
-6 -12 -6
-7 -14 -7
-9 -17 -8
0 -1
0 -1
0 -2
Cirrus Design
140 160 180
-19 -31 -44
-23 -36 -51
-26 -42 -59
-31 -50 -70
P/N 13772-001
Revision A10
SR22
200
-56
-65
-76
-90