5-16
P/N 11934-003
Section 5
Cirrus Design
Performance Data
SR20
Figure 5-7
Stall Speeds
• Note •
• Altitude loss during wings level stall may be 250 feet or more.
• KIAS values may not be accurate at stall.
Conditions:
Example:
• Weight .................................. 3000 LB
Flaps ..................................... Up (0%)
• C.G. .......................................... Noted
Bank Angle.................................... 15°
• Power............................................ Idle
• Bank Angle ............................... Noted
Stall Speed.......... 66 KIAS | 68 KCAS
Weight
LB
Bank
Angle
Deg
STALL SPEEDS
Flaps 0%Full Up
Flaps 50%
Flaps 100%Full
Down
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
3000
Most
FWD
C.G.
0
65
67
61
63
56
59
15
66
68
62
64
57
60
30
70
72
65
68
61
63
45
78
80
72
75
67
70
60
92
95
86
89
80
83
3000
Most
AFT
C.G.
0
64
66
59
62
54
57
15
65
67
60
63
55
58
30
69
71
64
66
58
61
45
76
78
71
73
64
68
60
90
93
84
87
76
81
Reissue A
Summary of Contents for SR20
Page 10: ...1 2 P N 11934 003 Section 1 Cirrus Design General SR20 Intentionally Left Blank Revision A3 ...
Page 22: ...2 2 P N 11934 003 Section 2 Cirrus Design Limitations SR20 Placards 2 21 Revision A6 ...
Page 308: ...9 2 P N 11934 003 Section 9 Cirrus Design Supplements SR20 Intentionally Left Blank Reissue A ...