Altitude Correction Normal Static Source: Standby Altimeter - Cirrus SR22 Pilot's Operating Handbook And Flight Manual

Cirrus Design
SR22
Altitude Correction
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 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
P/N 13772-004 P/N 13772-004
Original Issue
• Note •
CORRECTION TO BE ADDED - FEET
Normal Static Source - KIAS
60 70 80
12 9
14 10
16 12
19 14
21 0
24 0
28 0
22 6 -1
25 7 -1
29 8 -2
90 100 120
5 0 -11
6 0 -13
7 0 -16
8 0 -18
-14 -21 -30
-16 -25 -35
-18 -29 -41
-9 -19 -30
-10 -22 -34
-12 -25 -40
Section 5
Performance Data
140 160 180
-24 -38 -50
-28 -44 -58
-33 -51 -68
-39 -60 -80
-46 -66
-54 -77
-63 -90
200
-61
-71
-82
-97
5-7 5-7