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P/N 13772-108
Section 9
Cirrus Design
Supplements
SR22
Section 3 - Emergency Procedures
Autopilot Malfunction
Refer to Electric Trim/Autopilot Failure
procedure in the SR22 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 or pitch axis autopilot malfunction and
recovery:
Flight Phase
Bank Angle
Altitude Loss
Climb
40°
200 ft
Cruise
45°
300 ft
Descent
40°
350 ft
Maneuvering
10°
60 ft
Approach
10°
80 ft
Revision 5: 08-15-07