C
IRRUS
D
ESIGN
S
ECTION
5: P
ERFORMANCE
D
ATA
SR20
S
TANDARD
C
HARTS
P/N 11934-005
5-15
Alternate Static Source: Primary Flight Display
Conditions:
•
Power for level flight or maximum continuous, whichever is less.
•
Heater, Defroster & Vents..................................................................... ON
• N
OTE
•
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
CORRECTION TO BE ADDED (ft)
Alternate Static Source - KIAS
60
70
80
90 100 120 140 160 180 200
0%
S.L.
-2
15
33
52
92
131 170 209 253
5000
-3
17
39
61
107 152 197 243 294
10000
-3
20
45
71
125 178 230 283 343
15000
-4
23
53
83
146 209 270 332 403
50%
S.L.
12
29
47
65
96
114 109
5000
14
34
55
75
112 133 127
10000
17
40
64
88
130 155 148
100%
S.L.
43
29
42
54
66
114
5000
49
34
49
62
77
132
10000
58
40
57
72
90
154
Reissue A
Содержание 2220
Страница 12: ...SECTION 1 GENERAL CIRRUS DESIGN SR20 1 2 P N 11934 005 Reissue A Intentionally Left Blank ...
Страница 120: ...SECTION 4 NORMAL PROCEDURES CIRRUS DESIGN SR20 4 2 P N 11934 005 Reissue A Intentionally Left Blank ...
Страница 188: ...SECTION 6 WEIGHT AND BALANCE CIRRUS DESIGN SR20 6 2 P N 11934 005 Reissue A Intentionally Left Blank ...
Страница 198: ...SECTION 7 AIRPLANE AND SYSTEMS CIRRUS DESIGN SR20 7 4 P N 11934 005 Reissue A Intentionally Left Blank ...
Страница 326: ...SECTION 10 SAFETY INFORMATION CIRRUS DESIGN SR20 10 2 P N 11934 005 Reissue A Intentionally Left Blank ...