Cirrus DESIGN SR20 - Altitude Correction - Normal Static Source

5-6 P/N 11934-004
Section 5 Cirrus Design
Performance Data SR20
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 101-126
5000 10-1166
10000 37 45 48 50 56
Original Issue