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compass) inoperative. Refer to Kinds of Operation Equipment List.
• Note •
The Avidyne PFD software version is displayed on the PFD
during system startup.
4. Serials 0002 and subsequent before installation of PFD software
version 530-00123-XXX-REV05 (where X can be any digit from 0
to 9): Backcourse approaches are prohibited.
When the PFD is coupled with Autopilot System, the
following Limitations apply:
5. Autopilot operation is prohibited above 185 KIAS.
6. The autopilot must not be engaged for takeoff or landing.
7. The autopilot must be disengaged for missed approach, goaround,
and balked landing.
8. Flaps must be set to 50% for autopilot operation in Altitude Hold at
airspeeds below 95 KIAS.
9. Flap deflection is limited to 50% during autopilot operations.
Revision A8
2-18 P/N 13772-001
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.
Revision A5
P/N 13772-001 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 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 on-board
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. Serials with ARNAV MFD installed; The ARNAV ICDS 2000 Pilot’s
Operation Handbook, P/N 572-0550 dated May 1998 or later
revision, must be available to the pilot during all flight operations
8. Serials with Avidyne MFD installed: 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.
Revision A8
2-20 P/N 13772-001
Section 2 Cirrus Design
Limitations SR22
Oxygen System
Whenever the operating rules require the use of supplemental oxygen,
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CIRRUS DESIGN SR22西锐22飞行员操作手册和飞机飞行手册(13)
