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This POH Supplement Revision dated Revision 1: 12-15-07
supersedes and replaces the original release of this
supplement dated Original: 10-12-05.
Revision 1: 12-15-07
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
Revision 1: 12-15-07
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
Revision 1: 12-15-07
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 for a more
complete description of EMax Engine Instruments, its operating
modes, and additional detailed operating procedures.
Revision 1: 12-15-07
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
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.
• Note •
This POH Supplement Revision dated Revision 1: 12-15-07
supersedes and replaces the original release of this
supplement dated Original: 10-12-05.
Revision 1: 12-15-07
2 of 4 P/N 13772-125
Section 9 Cirrus Design
Supplements SR22
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 1: 12-15-07
P/N 13772-125 3 of 4
Cirrus Design Section 9
SR22 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
　
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