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Cirrus SR20 - Section 3 - Emergency Procedures; Autopilot Malfunction

Cirrus SR20
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4 of 32 P/N 11934-S41
Section 9 Cirrus Design
Supplements SR20
Section 3 - Emergency Procedures
Autopilot Malfunction
Refer to Electric Trim/Autopilot Failure abnormal procedure in the
basic 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 on the control yoke.
or
2. Pulling the AP SERVOS circuit breaker on MAIN BUS 1.
Altitude lost during a roll or pitch axis Autopilot malfunction and
recovery:
Flight Phase Bank Angle Altitude Loss
Climb 45° 300 ft
Cruise 45° 300 ft
Maneuvering 45° 300 ft
Descent 45° 300 ft
Approach 45° 70 ft
Revision 03: 09-08-14

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