Cirrus SR20 - Altitude Correction Normal Static Source: Primary Flight Display

5-6 P/N 21399-004
Section 5 Cirrus Design
Performance Data SR20
Altitude Correction
Normal Static Source: Primary Flight Display
• Note •
Add correction to desired altitude to obtain indicated altitude to fly.
Indicated airspeed values assume zero instrument error.
KIAS: Knots Indicated Airspeed.
Conditions:
• Power for level flight or maximum continuous, whichever is less.
• 3050 LB
Flaps Density
Alt
CORRECTION TO BE ADDED - FEET
Normal Static Source - KIAS
60 70 80 90 100 120 140 160 180 200
0%
S.L
0 00000000
5000 0 00000000
10000
0 00000000
15000
0 00000000
50%
S.L -1 -6 -10 -11 -3
5000 -2 -7 -12 -13 -4
10000 -2 -9 -14 -15 -4
100%
S.L 0 -11 -10 -1 6
5000 0 -13 -12 -1 7
10000 0 -15 -14 -1 8
Reissue A