Stall Speeds - Cirrus DESIGN SR20 Pilot's Operating Handbook And Flight Manual

Section 5
Performance Data

Stall Speeds

Conditions:
• Weight ........................................................................................................ 3050 LB
• CG ..................................................................................................................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
3050
15
Most
30
FWD
C.G.
45
60
0
3050
15
Most 30
AFT
45
C.G.
60
5-10
• Note •
Flaps 0%
Full Up
KIAS KCAS
69 67
70 68
74 72
81 80
95 95
69 67
75 68
77 72
83 79
99 94
STALL SPEEDS
Flaps 50%
KIAS KCAS
66 63
67 65
70 68
76 75
89 90
63 60
64 61
66 64
72 71
85 85
Cirrus Design
SR20
Flaps 100%Full
Down
KIAS KCAS
61 59
62 60
64 63
70 70
83 83
59 56
60 57
62 60
68 67
79 79
P/N 11934-004
Original Issue