Cirrus DESIGN SR22 Pilot Operating Handbook page 424

Section 9
Supplements
Section 1 - General
This airplane is equipped with an S-TEC System Fifty Five X Autopilot
and, if installed, an integrated Flight Director System.
Refer to S-Tec System Fifty Five X Pilot's Operating Handbook for full
operational procedures and description of implemented modes.
Refer to the Perspective Integrated Avionics System Pilot's Guide for a
detailed description of the avionics system and it's operating modes.
Section 2 - Limitations
1. The appropriate revision of the S-Tec System Fifty Five X, Pilot's
Operating Handbook for Perspective Equipped Cirrus Aircraft, (p/n
87277) must be immediately available to the pilot during flight.
2. Autopilot operation is prohibited above 185 KIAS.
3. The autopilot must not be engaged for takeoff or landing.
4. The autopilot must be disengaged for missed approach, go-
around, and balked landing.
5. Flaps must be set to 50% for autopilot operation in Altitude Hold at
airspeeds below 95 KIAS.
6. Flap deflection is limited to 50% during autopilot operations.
7. The autopilot must be disconnected in moderate or severe
turbulence.
8. Minimum engage height for the autopilot is 400 ft AGL.
9. Minimum speed with the autopilot engaged is 1.2V
configuration.
10. For VOR/GPS and ILS glideslope and localizer intercept, capture,
and tracking, the following limitations apply:
a. The autopilot must be disengaged no later than 100 feet below
the Minimum Descent Altitude.
b. The autopilot must be disconnect during approach if course
deviation exceeds 50%. The approach should only be
continued by "hand-flying" the airplane.
c. The autopilot must be disengaged at the Decision Height.
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Cirrus Design
SR22 / SR22T
for the given
s
P/N 13772-140
Revision 02: 09-20-12