Cirrus SR22 Pilot Operating Handbook page 351

Aircraft serials 22-3915 & subsequent 3600 pound takeoff weight
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Cirrus Design
SR22 / SR22T
6. The Autopilot may not be engaged beyond the Engagement
Limits. If the Autopilot is engaged beyond the command limits (up
to engagement limits), it will be rolled or pitched to within the
command limits and an altitude loss of 1000 feet or more can be
expected while attitude is established in the selected mode.
Axis
Pitch
Roll
7. The Autopilot and Flight Director will not command pitch or roll
beyond the Command Limits.
FD Pitch Command Limits
FD Roll 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.
9. For aircraft with optional USP or optional Discrete-Triggered Low
Speed ESP, if Stall Warning is inoperative, Autopilot Underspeed
Protection will not be provided in Altitude Critical Modes (ALT, GS,
GP, TO and GA), and Low Speed ESP will not be available.
P/N 13772-135
Revision 04: 09-08-14
Autopilot Engagement Limit
Axis
± 30°
± 75°
Autopilot Command Limit
+20°, -15°
± 25°
Section 9
Supplements
3 of 32

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