Specifications

11934-S37 23 of 56
Cirrus Design Section 9
SR20 Supplements
Altitude Correction
Normal Static Source
• 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 Press
Alt
CORRECTION TO BE ADDED - FEET
Normal Static Source - KIAS
60 70 80 90 100 120 140 160 180 200
0%
S.L
12 9 5 0 -11 -23 -36 -49 -59
5000
13 10 5 0 -13 -27 -42 -56 -69
10000
16 12 6 0 -15 -32 -49 -66 -80
15000
18 14 7 0 -17 -37 -58 -77 -94
50%
S.L
9 2 -4 -10 -16
5000 11 3 -5 -12 -18
10000 12 3 -6 -14 -22
100%
S.L 101-12 6
5000 10-1166
10000 37 45 48 50 56
Revision 01: 08-26-09