Cirrus DESIGN SR20 User Manual

5-10 P/N 11934-004
Section 5 Cirrus Design
Performance Data SR20
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 ........................................................................................................3050 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
3050
Most
FWD
C.G.
0 69 67 66 63 61 59
15 70 68 67 65 62 60
30 74 72 70 68 64 63
45 81 80 76 75 70 70
60 95 95 89 90 83 83
3050
Most
AFT
C.G.
0 69 67 63 60 59 56
15 75 68 64 61 60 57
30 77 72 66 64 62 60
45 83 79 72 71 68 67
60 99 94 85 85 79 79
Original Issue

Cirrus DESIGN SR20 Specifications

General

Brand	Cirrus
Model	DESIGN SR20
Category	Aircrafts
Language	English