P/N 11934-S41 3 of 16
Cirrus Design Section 9
SR20 Supplements
7. The autopilot and flight director will not command pitch or roll
beyond the Command Limits.
8. Use of VNAV is not supported during an approach with a teardrop
course reversal. VNAV will be disabled at the beginning of the
teardrop.
Section 3 - Emergency Procedures
Autopilot Malfunction
Refer to Electric Trim/Autopilot Failure procedure in the basic Pilot’s
Operating Handbook. 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:
Axis Autopilot Command Limit
FD Pitch Command Limits +20°, -15°
FD Roll Command Limits ± 25°
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 01: 08-26-09
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