Cirrus SR22 Pilot Operating Handbook page 443

Cirrus Design
SR22
Conditions:
• Weight ...................................3400 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
3400
15
Most
30
FWD
C.G.
45
60
0
3400
15
Most 30
AFT
45
C.G.
60
13772-130
Revision 03: 05-09-11
Stall Speeds
• Note •
Flaps 0%
Full Up
KIAS KCAS
73 70
74 71
76 75
83 83
99 99
72 69
73 70
76 74
82 82
98 98
Example:
Flaps......................................Up (0%)
Bank Angle ................................... 15°
C.G ........................................Forward
Stall Speed ..........74 KIAS | 71 KCAS
STALL SPEEDS
Flaps 50%
KIAS KCAS
66 64
67 65
71 69
77 76
90 90
65 63
66 64
69 67
76 75
89 89
Section 9
Supplements
Flaps 100%Full
Down
KIAS KCAS
62 60
64 61
66 64
72 71
84 84
60 58
61 59
63 62
69 69
82 82
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