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时间:2010-10-20 20:31来源:蓝天飞行翻译 作者:admin
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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
Revision 01: 12-15-07
4 of 4 P/N 11934-S31
Section 9 Cirrus Design
Supplements SR20
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 for a more
complete description of EMax Engine Instruments, its operating
modes, and additional detailed operating procedures.
Revision 01: 12-15-07
P/N 11934-S32 1 of 4
Cirrus Design Section 9
SR20 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 SR20, this POH Supplement is
applicable and must be inserted in the Supplements Section (Section
9) of the Cirrus Design SR20 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 SR20 Pilot’s Operating Handbook.
• Note •
This POH Supplement Revision dated Revision 01: 12-15-07
supersedes and replaces the original release of this
supplement dated Original: 10-12-05.
Revision 01: 12-15-07
2 of 4 P/N 11934-S32
Section 9 Cirrus Design
Supplements SR20
Figure - 1
Section 1 - General
Avidyne CMax™ Electronic Approach Charts allows the pilot to view
terminal procedure chart data on the EX5000C MFD. If the chart is
geo-referenced, an ownship symbol and flight plan legs can be
overlaid on the chart to further enhance the pilot’s situational
awareness. Most approach charts and airport diagrams are georeferenced;
most arrival, departure, and miscellaneous charts are not.
Avidyne CMax™ Electronic Approach Charts
Revision 01: 12-15-07
P/N 11934-S32 3 of 4
Cirrus Design Section 9
SR20 Supplements
Section 2 - Limitations
1. Do not use the CMax Approach Charts function for navigation of
the aircraft. The CMax Approach Charts function is intended to
serve as a situational awareness tool only.
2. 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.
Section 3 - Emergency Procedures
Loss of CMax™ Electronic Approach Charts
• In the event CMax Approach Charts cannot be displayed on the
MFD, refer to back-up approach data such as paper copies or a
laptop containing the JeppView software and data.
• If no back-up data is available contact Air Traffic Control for
approach information.
Section 4 - Normal Procedures
• Note •
Back-up approach charts for CMax are not required. However,
back-up approach data for departure, destination, and
alternate field is recommended. Reference CMax Description
in this supplement.
Section 7 - System Description
The CMax installation is entirely software dependant. No additional
hardware is required.
• Note •
Back-up approach charts for CMax are not required. However,
back-up approach data for departure, destination, and
alternate field is recommended. Back-up approach data could
be printed copies of published approach charts, a laptop
containing the JeppView software and data, or notes providing
the approach vertical data (the Garmin 430 can display lateral
approach information).
Revision 01: 12-15-07
4 of 4 P/N 11934-S32
Section 9 Cirrus Design
Supplements SR20
Refer to Avidyne FlightMax EX5000C Pilot’s Guide, for a more
complete description of CMax Approach Charts, its operating modes,
and additional detailed operating procedures.
Revision 01: 12-15-07
P/N 11934-S33 1 of 4
Cirrus Design Section 9
SR20 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
XM Satellite Weather System
When the XM Satellite Weather System system is installed in the
Cirrus Design SR20, this POH Supplement is applicable and must be
inserted in the Supplements Section (Section 9) of the Cirrus Design
SR20 Pilot’s Operating Handbook. This document must be carried in
 
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