曝光台 注意防骗
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the pilot is expected to actuate the flight controls as required to track
the bars.
The following describes push-button annunciation and related
Autopilot and Flight Director status:
The Flight Director system is powered by 28 VDC through the 5-amp
AUTOPILOT circuit breaker on the Essential Bus.
Refer to Avidyne FlightMax Entegra-Series PFD Pilot’s Guide, P/N
600-00081-000, Rev 08 or later for a more complete description of the
Flight Director, its operating modes, and additional detailed operating
procedures.
No
Annunciation
• Autopilot off.
or
• Autopilot not active in either roll or pitch control.
Green
AP ON
Annunciation
• Autopilot active in roll and/or pitch control.
• If Autopilot active in roll and pitch control, “AP”
annunciation appears on top edge of PFD, and
Flight Director Steering Command Bars
MAGENTA.
Amber
AP OFF
FD ON
Annunciation
• Autopilot uncoupled.
• If Autopilot active in roll and pitch control, Flight
Director ON, “FD” annunciation appears on top
edge of PFD, and Flight Director Steering
Command Bars GREEN.
Original: 10-12-05:
P/N 13772-124 1 of 4
Cirrus Design Section 9
SR22 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
Avidyne EMax™ Engine
Instrumentation
When the Avidyne EMax™ Engine Instrumentation system is installed
in the Cirrus Design SR22, this POH Supplement is applicable and
must be inserted in the Supplements Section (Section 9) of the Cirrus
Design SR22 Pilot’s Operating Handbook. This document must be
carried in the airplane at all times. Information in this supplement adds
to, supersedes, or deletes information in the basic SR22 Pilot’s
Operating Handbook.
Original: 10-12-05
2 of 4 P/N 13772-124
Section 9 Cirrus Design
Supplements SR22
Figure - 1
Section 1 - General
EMax™ Engine Instrumentation provides the pilot with engine
parameters depicted on simulated gauges and electrical system
parameters located in a dedicated region within in the EX5000C MFD
display.
Avidyne EMax™ Engine Instrumentation
Original: 10-12-05
P/N 13772-124 3 of 4
Cirrus Design Section 9
SR22 Supplements
Section 2 - Limitations
No Change.
Section 3 - Emergency Procedures
No Change.
Section 4 - Normal Procedures
No Change.
Section 5 - Performance
No Change.
Section 6 - Weight & Balance
Installation of the Avidyne Engine Instruments adds the following
optional (Sym = O) equipment at the weight and arm shown in the
following table.
Section 7 - System Description
An Engine Sensor Unit interfaces (SIU) with engine-mounted sensors,
some of which are shared with the standard airplane gauges, and
provide data to the MFD for display.
Airplanes equipped with EMax™ Engine Instrumentation display all
engine settings and parameters on a dedicated MFD engine monitor
page. The MFD also displays engine and fuel data in data blocks on
the full-screen moving map display. In the event of an exceedence,
each out-of-limit parameter is highlighted on the screen for immediate
attention. The engine monitor also includes data capture capability,
ATA /
Item
Description Sym Qty Part Number
Unit
Wt
Arm
34-03 Engine Sensors O 11 - 1.0 75.0
34-04 Engine Sensor Unit O 1 14843-001 1.1 118.0
34-05 Engine Sensor Harness O 1 15030-001 0.9 92.0
34-06 Engine Sensor Cabin Harness O 1 15032-001 2.1 108.0
Original: 10-12-05
4 of 4 P/N 13772-124
Section 9 Cirrus Design
Supplements SR22
providing full-time recording of critical engine performance
parameters.
The Engine Instruments system is powered by 28 VDC supplied
through the 5-amp Engine Instruments breaker on the Main Bus 1.
Refer to Avidyne FlightMax EX5000C Pilot’s Guide, P/N 600-00108-
000, Revision 03 or later for a more complete description of EMax
Engine Instruments, its operating modes, and additional detailed
operating procedures.
Original: 10-12-05
P/N 13772-125 1 of 4
Cirrus Design Section 9
SR22 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
Avidyne CMax™ Electronic
Approach Charts
When the Avidyne CMax™ Electronic Approach Charts system is
installed in the Cirrus Design SR22, this POH Supplement is
applicable and must be inserted in the Supplements Section (Section
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(132)
