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June 2007
2-18 Information Manual
Section 2 Cirrus Design
Limitations SR22
10. The autopilot must be disconnected in moderate or severe
turbulence.
11. Minimum engage height for the autopilot is 400 ft AGL.
• WARNING •
Autopilot may not be able to maintain all selectable vertical
speeds. Selecting a vertical speed that exceeds the aircraft’s
available performance may cause the aircraft to stall.
12. Minimum speed with the autopilot engaged is 1.2Vs for the given
configuration.
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 disconnected 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.
d. 12 knot maximum crosswind component between the missed
approach point and outer marker.
e. The intercept of the localizer shall occur at least 5 miles
outside of the outer marker.
f. If the crosswind component is greater than 12 knots and less
than 17 knots, the intercept shall occur at least 10 miles
outside of the outer marker.
g. The intercept angle shall be no greater than a 45-degree
intercept.
h. The ILS is flown at normal approach speeds, and within any
STC or TC speed constraints and as defined in this flight
manual.
i. The flaps should be extended in the approach configuration
prior to the Outer Marker. No further changes in the flap
configuration should be made throughout the autopilotcoupled
approach.
June 2007
Information Manual 2-19
Cirrus Design Section 2
SR22 Limitations
j. The glideslope is approached in such a manner to allow
automatic arming of the glideslope, or if the glideslope is
manually armed no more than 15% above the glideslope.
Multi-Function Display
1. The moving map display must not be used as the primary
navigation instrument. The moving map display provides visual
advisory of the airplane’s GPS position against a moving map.
The information supplements CDI course deviation and
information provided on the GPS navigator.
2. Use of Map page during IFR flight requires an IFR approved GPS
receiver installation operated in accordance with applicable
limitations.
3. Under no circumstances should the Map page terrain
representations be used as a basis for terrain avoidance.
4. The Avidyne electronic checklists display supplements the Pilot
Operating Handbook checklists and is advisory only. The
electronic checklists must not be used as the primary set of onboard
airplane checklists.
5. The MFD interfaces with separately approved sensor installations.
Adherence to limitations in the appropriate sensor installation
POH Supplements is mandatory.
6. Traffic information shown on the Map page display is provided to
the pilot as an aid to visually acquire traffic. Pilots should
maneuver their aircraft based only on ATC guidance or positive
visual acquisition of the conflicting traffic. Maneuver should be
consistent with ATC instructions. No maneuvers should be made
based solely on a traffic advisory.
7. The Avidyne FlightMax EX5000C Pilot’s Guide, P/N 600-00108-
000, Revision 03 or later, must be available to the pilot during all
flight operations
June 2007
2-20 Information Manual
Section 2 Cirrus Design
Limitations SR22
Oxygen System
Whenever the operating rules require the use of supplemental oxygen,
the pilot must:
• Use an oxygen system approved by Cirrus Design and listed in
the Oxygen System AFM Supplement Part Number 13772-109.
• Secure the oxygen bottle in the right front seat as described in
the AFM Supplement noted above.
Inflatable Restraint System
Serials 0002 thru 1499, 1501 thru 1519 after SB 2X-25-14 and serials
1500, 1520 and subsequent; Use of a child safety seat with the
inflatable restraint system is prohibited.
Flap Limitations
Serials 0002 through 0227 before accomplishment of Service Bulletin
SB 22-27-02: Simultaneous Flap operation and COM transmission is
prohibited.
Approved Takeoff Settings...........................................UP (0%) or 50%
Approved Landing Settings ............................. Up (0%), 50%, or 100%
Paint
To ensure that the temperature of the composite structure does not
exceed 150° F (66° C), the outer surface of the airplane must be
painted with an approved white paint, except for areas of registration
　
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