6 of 16
P/N 11934-S27
Section 9
Cirrus Design
Supplements
SR20
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:
Altitude lost during a pitch axis autopilot malfunction and recovery:
Flight Phase
Bank Angle
Altitude Loss
Climb
30°
None
Cruise
55°
100 ft
Descent
55°
120 ft
Maneuvering
10°
None
Approach
0°
20 ft
Flight Phase
Altitude Loss
Cruise
200 ft
Revision 2: 07-18-05
Summary of Contents for SR20
Page 10: ...1 2 P N 11934 003 Section 1 Cirrus Design General SR20 Intentionally Left Blank Revision A3 ...
Page 22: ...2 2 P N 11934 003 Section 2 Cirrus Design Limitations SR20 Placards 2 21 Revision A6 ...
Page 308: ...9 2 P N 11934 003 Section 9 Cirrus Design Supplements SR20 Intentionally Left Blank Reissue A ...