Specifications

24 of 56 11934-S37
Section 9 Cirrus Design
Supplements SR20
Altitude Correction
Alternate 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.
• Heater, Defroster, & Vents ..................................................................................ON
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 28 43 57 82 104 126 148 172
5000
16 35 54 71 104 136 168 203 242
10000
20 43 66 87 128 169 211 258 311
15000
23 51 78 103 152 200 251 308 373
50%
S.L
43 65 87 108 148
5000 21 32 39 42 26
10000 36 54 70 82 88
100%
S.L 42 56 67 80 95
5000 37 45 48 50 56
10000 61 81 99 119 148
Revision 01: 08-26-09