Cirrus DESIGN SR22T Pilot Operating Handbook page 162

Section 5
Performance Data
Altitude Correction
Alternate Static Source: Primary Flight Display
Conditions:
• Power for level flight or maximum continuous, whichever is less.
• Heater, Defroster, & Vents .................................................................................. ON
Add correction to desired altitude to obtain indicated altitude to fly.
Indicated airspeed values assume zero instrument error.
KIAS: Knots Indicated Airspeed.
Flaps Density
Alt
S.L
5000
10000
0%
15000
20000
25000
S.L
50% 5000
10000
S.L
100% 5000
10000
5-8
• Note •
CORRECTION TO BE ADDED - FEET
Alternate Static Source - KIAS
60 70 80
-3 16
-3 18
-3 21
-4 25
-5 29
-6 35
13 31
15 36
17 42
14 30 44
16 35 51
18 40 60
90 100 120
35 56 98
41 65 114
48 76 133
56 89 156
67 105 184
79 125 218
50 69 102
58 80 119
68 94 139
57 71
66 82
77 96
Cirrus Design
SR22T
140 160 180
139 178 218
161 207 253
188 241 296
220 283 347
260 334 410
309 397 487
P/N 13772-003
Original Issue
200
265
307
358
420
497
590