Stall Speeds - Cirrus DESIGN SR20 Information Manual

Section 5
Performance Data
Conditions:
• Weight .................................. 3000 LB
• C.G. .......................................... Noted
• Power............................................Idle
• Bank Angle ............................... Noted
• Altitude loss during wings level stall may be 250 feet or more.
• KIAS values may not be accurate at stall.
Weight Bank
Angle
LB Deg
0
3000
15
Most
30
FWD
C.G.
45
60
0
3000
15
Most 30
AFT
45
C.G.
60
5-16

Stall Speeds

• Note •
Flaps 0%Full Up
KIAS KCAS
65 67
66 68
70 72
78 80
92 95
64 66
65 67
69 71
76 78
90 93
Figure 5-7
Example:
Flaps ..................................... Up (0%)
Bank Angle....................................15°
Stall Speed.......... 66 KIAS | 68 KCAS
STALL SPEEDS
Flaps 50%
KIAS KCAS
61 63
62 64
65 68
72 75
86 89
59 62
60 63
64 66
71 73
84 87
P/N 13999-002 Info Manual
Cirrus Design
SR20
Flaps 100%Full
Down
KIAS KCAS
56 59
57 60
61 63
67 70
80 83
54 57
55 58
58 61
64 68
76 81
September 2011