Cirrus System 55X Autopilot User Manual

5-12 P/N 13772-005
Section 5 Cirrus Design
Performance Data SR22T
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........................................................................................................3600 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
3600
Most
FWD
CG
0 74 73 70 67 64 61
15 76 74 71 68 64 62
30 80 78 74 72 67 65
45 87 87 79 79 73 72
60 103 103 92 94 85 86
3600
Most
AFT
CG
0 72 70 69 66 63 60
15 73 71 70 67 64 61
30 77 75 73 71 66 65
45 84 83 79 78 72 72
60 99 99 91 93 85 85
Original Issue

Cirrus System 55X Autopilot Specifications

General

Brand	Cirrus
Model	System 55X Autopilot
Category	Aircrafts
Language	English