Cirrus DESIGN SR22 - Page 145

Cirrus Design Section 5
SR22 Performance Data
P/N 13772-002 5-7P/N 13772-002 5-7
Altitude Correction
Normal Static Source: Standby Altimeter
• 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.
• 3400 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
12 9 5 0 -11 -24 -37 -50 -60
5000
14 11 6 0 -13 -28 -43 -57 -69
10000
17 12 7 0 -15 -33 -50 -67 -81
15000
20 15 8 0 -18 -38 -59 -79 -95
50%
S.L
11 3 -5 -11 -14
5000 13 3 -6 -13 -17
10000 15 4 -7 -15 -20
100%
S.L 151-14 6
5000 171-15 7
10000 201-16 8
Reissue A