Altitude Correction - Cirrus SR22 Pilot Operating Handbook

Cirrus Design
SR22

Altitude Correction

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 fly.
Indicated airspeed values assume zero instrument error.
• KIAS: Knots Indicated Airspeed.
Flaps Press
Alt
S.L
5000
0%
10000
15000
S.L
50% 5000
10000
S.L
100% 5000
10000
P/N 13772-001
Revision A10
• Note •
CORRECTION TO BE ADDED - FEET
Normal Static Source - KIAS
60 70 80
1 0
2 0
2 1
2 1
-7 -6
-8 -7
-9 -8
-14 -17 -18
-16 -20 -21
-18 -23 -25
Figure 5-4
90 100 120
-1 -1 -3
-1 -2 -3
-1 -2 -4
-1 -2 -4
-5 -5 -9
-6 -6 -10
-7 -7 -12
-16 -10
-19 -12
-22 -14
Section 5
Performance Data
140 160 180
-3 -1 4
-3 -1 5
-4 -1 6
-4 -1 7
200
13
15
18
21
5-7