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

C D
IRRUS ESIGN
SR22

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
Indicated airspeed values assume zero instrument error.
Density
Flaps
0% S.L.
5000
10000
15000
50% S.L.
5000
10000
100% S.L.
5000
10000
P/N 13772-006
Reissue A
KIAS: Knots Indicated Airspeed.
Alt
60 70
4
4
5
6
-10
-12
-14
-2 -9
-2 -11
-3 -13
• N •
OTE
fly.
CORRECTION TO BE ADDED (ft)
Alternate Static Source - KIAS
80 90 100 120 140 160 180 200
8 14 21
10 16 25
11 19 29
13 23 34
-4 4 11
-4 4 13
-5 5 15
-2 6 15
-2 7 17
-3 8 20
S 5: P
ECTION ERFORMANCE
S
TANDARD
40 64 94 127 164
47 75 109 148 191
55 87 127 172 222
64 102 149 202 261
29 50 80
33 58 93
39 68 108
39
45
53
D
ATA
C
HARTS
5-15