Cirrus DESIGN SR20 Information Manual page 322

Section 9
Supplements
Section 3 - Emergency Procedures
Autopilot Malfunction
Refer to Electric Trim/Autopilot Failure procedure in the SR20 POH. Do
not reengage the autopilot until the malfunction has been identified
and corrected. The autopilot may be disconnected by:
1. Pressing the A/P DISC/Trim switch on the control yoke handle.
2. Pulling the AUTOPILOT circuit breaker on Essential Bus.
Altitude lost during a roll axis autopilot malfunction and recovery:
Flight Phase
Climb
Cruise
Descent
Maneuvering
Approach
Altitude lost during a pitch axis autopilot malfunction and recovery:
Flight Phase
Cruise
ILS
6 of 16
Bank Angle
30°
55°
55°
10°
0°
Altitude Loss
200 ft
Cirrus Design
Altitude Loss
None
100 ft
120 ft
None
20 ft
25 ft
P/N 11934-S13
Revision 04: 08-15-07
SR20