Stall Speeds - Cirrus SR22 Pilot Operating Handbook

C D
IRRUS ESIGN
SR22

Stall Speeds

Conditions:
• Weight.............................................................................................. 3600 LB
• CG........................................................................................................ Noted
• Power........................................................................................................Idle
• Bank Angle ......................................................................................... Noted
Altitude loss during wings level stall may be 250 ft or more.
Bank Angle
Deg
3600 lb - Most FWD C.G.
0
15
30
45
60
3600 lb - Most AFT C.G.
0
15
30
45
60
P/N 13772-006
Reissue A
• N
KIAS values may not be accurate at stall.
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
S
ECTION
•
OTE
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
5: P
ERFORMANCE
S C
TANDARD HARTS
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
D
ATA
5-17