Altitude Correction Alternate Static Source: Primary Flight Display - Cirrus SR22 Pilot Operating Handbook

Section 5
Performance Data
Altitude Correction
Alternate Static Source: Primary Flight Display
Conditions:
• Power for level flight or maximum continuous, whichever is less.
• Heater, Defroster, & Vents .................................................................................. ON
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
5-8
• Note •
CORRECTION TO BE ADDED - FEET
Alternate Static Source - KIAS
60 70 80
4 8
4 10
5 11
6 13
-10 -4
-12 -4
-14 -5
-2 -9 -2
-2 -11 -2
-3 -13 -3
90 100 120
14 21 40
16 25 47
19 29 55
23 34 64
4 11 29
4 13 33
5 15 39
6 15 39
7 17 45
8 20 53
Cirrus Design
140 160 180
64 94 127
75 109 148
87 127 172
102 149 202
50 80
58 93
68 108
P/N 13772-004
Original Issue
SR22
200
164
191
222
261