5-12
P/N 13772-005
Section 5
Cirrus Design
Performance Data
SR22T
Stall Speeds
• Note •
Altitude loss during wings level stall may be 250 feet or more.
KIAS values may not be accurate at stall.
Conditions:
• Weight ........................................................................................................3600 LB
• CG ..................................................................................................................Noted
• Power................................................................................................................. Idle
• Bank Angle .....................................................................................................Noted
Weight
LB
Bank
Angle
Deg
STALL SPEEDS
Flaps 0%
Full Up
Flaps 50%
Flaps 100%
Full Down
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
3600
Most
FWD
CG
0
74
73
70
67
64
61
15
76
74
71
68
64
62
30
80
78
74
72
67
65
45
87
87
79
79
73
72
60
103
103
92
94
85
86
3600
Most
AFT
CG
0
72
70
69
66
63
60
15
73
71
70
67
64
61
30
77
75
73
71
66
65
45
84
83
79
78
72
72
60
99
99
91
93
85
85
Original Issue
