Stall Speeds - Cirrus SR22 Pilot Operating Handbook

Section 5
Performance Data

Stall Speeds

Conditions:
• Weight ........................................................................................................ 3600 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
3600
15
Most
30
FWD
CG
45
60
0
3600
15
Most 30
AFT
45
CG
60
5-12
• Note •
Flaps 0%
Full Up
KIAS KCAS
74 73
76 74
80 78
87 87
103 103
72 70
73 71
77 75
84 83
99 99
STALL SPEEDS
Flaps 50%
KIAS KCAS
70 67
71 68
74 72
79 79
92 94
69 66
70 67
73 71
79 78
91 93
Cirrus Design
SR22
Flaps 100%
Full Down
KIAS KCAS
64 61
64 62
67 65
73 72
85 86
63 60
64 61
66 65
72 72
85 85
P/N 13772-004
Original Issue