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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
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-S33
Section 9 Cirrus Design
Supplements SR20
Figure - 1
Section 1 - General
The XM Satellite Weather System enhances situational awareness by
providing the pilot with real time, graphical weather information
depicted on the MAP page of the EX5000C MFD display.
XM Satellite Weather Overlay
Revision 01: 12-15-07
P/N 11934-S33 3 of 4
Cirrus Design Section 9
SR20 Supplements
Section 2 - Limitations
1. Do not use the XM Satellite Weather System for navigation of the
aircraft. The XM Satellite Weather System is intended to serve as
a situational awareness tool only.
Section 3 - Emergency Procedures
No Change.
Section 4 - Normal Procedures
No Change.
Section 5 - Performance
No Change.
Section 6 - Weight & Balance
Installation of the XM Satellite Weather System adds the following
optional (Sym = O) equipment at the weight and arm shown in the
following table.
Section 7 - System Description
The XM Satellite Weather System enhances situational awareness by
providing the pilot with real time, graphical weather information. The
XM antenna, integrated with the COM1 antenna, receives weather
information from dual-redundancy satellites. This signal is sent to the
XM receiver, installed in the co-pilot side of the instrument console,
which interprets and overlays the weather data on the MAP page of
the EX5000C MFD.
Once activated, the XM Satellite Weather System will overlay the
following weather data on the EX5000C MFD:
• NEXRAD Radar
ATA /
Item
Description Sym Qty Part Number
Unit
Wt
Arm
34-07 XM Receiver O 1 16665-001 1.7 114.0
Revision 01: 12-15-07
4 of 4 P/N 11934-S33
Section 9 Cirrus Design
Supplements SR20
• METARs
• SIGMETs
• AIRMETs
• TFRs
• Lightning Strikes
The XM Satellite Weather System is powered by 28 VDC supplied
through the 3-amp Weather/Stormscope breaker on the Non-Essential
Bus.
Refer to Avidyne FlightMax EX5000C Pilot’s Guide for a more
complete description of XM Satellite Weather System, its operating
modes, and additional detailed operating procedures.
Revision 01: 12-15-07
P/N 11934-S34 1 of 4
Cirrus Design Section 9
SR20 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
Avidyne Flight Director
When the Avidyne Flight Director 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 02: 12-15-07
supersedes and replaces the original release of this
supplement dated Revision 01: 08-15-07.
Revision 02: 12-15-07
2 of 4 P/N 11934-S34
Section 9 Cirrus Design
Supplements SR20
Avidyne Primary Flight Display with Flight Director
Section 1 - General
The Flight Director system enhances situational awareness by
reducing cockpit workload through providing a visual cue for the pilot
to follow as indicated by the PFD’s Flight Director Steering Command
Bar. Through turning or pitching the airplane as “directed” by the
Steering Command Bar, the pilot will follow the necessary course to
　
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