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

C D
IRRUS ESIGN
SR22

Altitude Correction

Normal Static Source: Primary Flight Display

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
P/N 13772-006
Reissue A
KIAS: Knots Indicated Airspeed.
Alt
60 70
0
0
0
0
9
10 -10 -22 -25 -22 -25 -33
12 -12 -25 -29 -25 -30 -38
22 -6
25 -7
29 -9
• N •
OTE
fly.
CORRECTION TO BE ADDED (ft)
Normal Static Source - KIAS
80 90 100 120 140 160 180 200
0 0 0
0 0 0
0 0 0
0 0 0
-9 -19 -22 -19 -22 -28
-10 -14 -19 -18
-12 -16 -22 -21
-14 -18 -25 -25
S 5: P
ECTION ERFORMANCE
S
TANDARD
0 0 0
0 0 0
0 0 0
0 0 0
D
ATA
C
HARTS
0 0
0 0
0 0
0 0
5-13