Specifications

5-16 Information Manual
Section 5 Cirrus Design
Performance Data SR20
Figure 5-7
Stall Speeds
• Note •
• Altitude loss during wings level stall may be 250 feet or more.
• KIAS values may not be accurate at stall.
Conditions: Example:
• Weight .................................. 3000 LB Flaps ..................................... Up (0%)
• C.G. .......................................... Noted Bank Angle....................................15°
• Power............................................Idle
• Bank Angle ............................... Noted Stall Speed.......... 66 KIAS | 68 KCAS
Weight
LB
Bank
Angle
Deg
STALL SPEEDS
Flaps 0%Full Up Flaps 50%
Flaps 100%Full
Down
KIAS KCAS KIAS KCAS KIAS KCAS
3000
Most
FWD
C.G.
0 65 67 61 63 56 59
15 66 68 62 64 57 60
30 70 72 65 68 61 63
45 78 80 72 75 67 70
60 92 95 86 89 80 83
3000
Most
AFT
C.G.
0 64 66 59 62 54 57
15 65 67 60 63 55 58
30 69 71 64 66 58 61
45 76 78 71 73 64 68
60 90 93 84 87 76 81
March 2010