Alternate Static Source: Standby Altimeter - Cirrus SR22 Pilot Operating Handbook

S 5: P
ECTION ERFORMANCE
S C
TANDARD HARTS

Alternate Static Source: Standby Altimeter

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
5-16
D
ATA
KIAS: Knots Indicated Airspeed.
Alt
60 70
16
18
21
25
2
2
3
-2 3
-2 3
-3 4
• N •
OTE
fly.
CORRECTION TO BE ADDED (ft)
Alternate Static Source - KIAS
80 90 100 120 140 160 180 200
17 19 22
20 22 25
23 26 29
27 30 34
5 9 11
6 10 13
7 12 16
7 11 15
8 12 18
9 15 20
C
IRRUS
29 40 56
33 46 65
39 54 75 104 140
46 63 89 122 164
17 25 42
20 30 49
23 34 57
27
32
37
P/N 13772-006
D
ESIGN
SR22
77 103
89 120
Reissue A