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

S 5: P
ECTION ERFORMANCE
S C
TANDARD HARTS

Normal Static Source: Standby Altimeter

Conditions:
• Power for level flight or maximum continuous, whichever is less.
• 3600 LB
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
5-14
D
ATA
KIAS: Knots Indicated Airspeed.
Alt
60 70
12
14
16
19
21
24
28
22 6
25 7
29 8
• N •
OTE
fly.
CORRECTION TO BE ADDED (ft)
Normal Static Source - KIAS
80 90 100 120 140 160 180 200
9 5 0
10 6 0
12 7 0
14 8 0
0 -14 -21 -30 -46 -66
0 -16 -25 -35 -54 -77
0 -18 -29 -41 -63 -90
-1 -9 -19 -30
-1 -10 -22 -34
-2 -12 -25 -40
C
IRRUS
-11 -24 -38 -50 -61
-13 -28 -44 -58 -71
-16 -33 -51 -68 -82
-18 -39 -60 -80 -97
P/N 13772-006
D
ESIGN
SR22
Reissue A