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

Section 5
Performance Data
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 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
5-6
• Note •
CORRECTION TO BE ADDED - FEET
Normal Static Source - KIAS
60 70 80
0 0
0 0
0 0
0 0
9 -9
10 -10
12 -12
22 -6 -10
25 -7 -12
29 -9 -14
90 100 120
0 0 0
0 0 0
0 0 0
0 0 0
-19 -22 -19
-22 -25 -22
-25 -29 -25
-14 -19 -18
-16 -22 -21
-18 -25 -25
Cirrus Design
140 160 180
0 0 0
0 0 0
0 0 0
0 0 0
-22 -28
-25 -33
-30 -38
P/N 13772-004
Original Issue
SR22
200
0
0
0
0