Cirrus DESIGN SR22 User Manual

5-12 P/N 13772-002
Section 5 Cirrus Design
Performance Data SR22
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 ........................................................................................................3400 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
3400
Most
FWD
CG
0 73 70 66 64 62 60
15 74 71 67 65 64 61
30 76 75 71 69 66 64
45 83 83 77 76 72 71
60 99 99 90 90 84 84
3400
Most
AFT
CG
0 72 69 65 63 60 58
15 73 70 66 64 61 59
30 76 74 69 67 63 62
45 82 82 76 75 69 69
60 98 98 89 89 82 82
Reissue A

Cirrus DESIGN SR22 Specifications

General

Brand	Cirrus
Model	DESIGN SR22
Category	Aircrafts
Language	English