5-8 P/N 13772-003
Section 5 Cirrus Design
Performance Data SR22T
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
-3 16 35 56 98 139 178 218 265
5000
-3 18 41 65 114 161 207 253 307
10000
-3 21 48 76 133 188 241 296 358
15000
-4 25 56 89 156 220 283 347 420
20000
-5 29 67 105 184 260 334 410 497
25000
-6 35 79 125 218 309 397 487 590
50%
S.L
13 31 50 69 102
5000 15 36 58 80 119
10000 17 42 68 94 139
100%
S.L 14 30 44 57 71
5000 16 35 51 66 82
10000 18 40 60 77 96
Original Issue
To Next Page
Loading...
