Cirrus SR22 - Altitude Correction Alternate Static Source: Primary Flight Display

5-8 P/N 13772-004
Section 5 Cirrus Design
Performance Data SR22
Altitude Correction
Alternate 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.
• Heater, Defroster, & Vents ..................................................................................ON
Flaps Density
Alt
CORRECTION TO BE ADDED - FEET
Alternate Static Source - KIAS
60 70 80 90 100 120 140 160 180 200
0%
S.L
4 8 14 21 40 64 94 127 164
5000
4 1016254775109148191
10000
5 1119295587127172222
15000
6 13233464102149202261
50%
S.L
-10 -4 4 11 29 50 80
5000 -12 -4 4 13 33 58 93
10000 -14 -5 5 15 39 68 108
100%
S.L -2 -9 -2 6 15 39
5000 -2 -11 -2 7 17 45
10000 -3 -13 -3 8 20 53
Original Issue