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S-TEC System 55X - Section 3 - Emergency Procedures; Autopilot Malfunction

S-TEC System 55X
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6 of 24 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

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