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___ 11934-S31 R1 Avidyne EMax™ Engine Instrumentation 12-15-07
___ 11934-S32 R1 Avidyne CMax™ Electronic Approach Charts 12-15-07
___ 11934-S33 R1 XM Satellite Weather System 12-15-07
___ 11934-S34 R2 Avidyne Flight Director 12-15-07
___ 11934-S36 R1 Artex ME406 406 MHz ELT System 12-18-08
___ 11934-S37 R1 SR20 Airplanes Equipped with the “G3 Wing” 08-26-09
___ 11934-S38 R1 Garmin 400W-Series GPS Navigator 11-11-07
___ 11934-S44 Part 135 Operations: Electrical Loading Shedding 06-13-09
___ 11934-S45 SR20 Airplanes Registered in Argentina 08-26-09
March 2010
9-4 Information Manual
Section 9 Cirrus Design
Supplements SR20
FAA Approved POH Supplements must be in the airplane for flight operations when the
subject optional equipment is installed or the special operations are to be performed.
This Log of Supplements shows all Cirrus Design Supplements available for the aircraft
at the corresponding date of the revision level shown in the lower left corner. A mark (x)
in the Part Number column indicates that the supplement is installed in the POH.
March 2010
P/N 11934-S01 1 of 10
Cirrus Design Section 9
SR20 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
Garmin GMA 340 Audio System
Includes Optional XM Radio System
When the Garmin GMA 340 Audio Panel and the optional XM Radio
System are installed in the Cirrus Design SR20, this Supplement is
applicable and must be inserted in the Supplements Section (Section
9) of the Cirrus Design SR20 Pilot’s Operating Handbook (Handbook).
Information in this supplement either adds to, supersedes, or deletes
information in the basic Handbook.
• Note •
This POH Supplement Revision dated Revision 02: 07-18-05
supersedes and replaces Revision 01 of this supplement
dated 07-03-04. This revision adds required data for the
optional XM Radio System available for the Garmin GMA 340.
Revision 02: 07-18-05
2 of 10 P/N 11934-S01
Section 9 Cirrus Design
Supplements SR20
Figure - 1
Section 1 - General
This supplement provides detailed operating instructions for the
Garmin GMA 340 Audio Selector Panel/Intercom System with internal
Marker Beacon. This supplement covers the basic operating areas of
the Audio Control Panel.
• Power On / Fail-safe Operation
• Audio / Transceiver Selection
• Speaker Output
• Public Address (PA) Function
• Personal Music Inputs
• Intercom (ICS)
• Marker Beacon
1. Marker Beacon Annunciators
2. Marker Audio Select Button / LED
3. Marker Sensitivity Select Button
a. HI Sensitivity LED
b. LO Sensitivity LED
4. Pilot Intercom Squelch (outer knob)
5. Power / Intercom Volume (inner knob)
6. Transceiver Audio Select Buttons/
LEDs
7. Photocell
8. Receiver Audio Select Buttons / LEDs
9. Transceiver Audio/Transmit Select
Buttons / LEDs
10. Split COM Button / LED
11. Cabin Audio Select Buttons / LEDs
a. SPKR, Cabin Speaker
b. PA, Public Address
12. Intercom Isolation Buttons / LEDs
a. PILOT Intercom Mode
b. CREW Intercom Mode
13. Copilot / Passenger Intercom
Squelch (outer knob)
14. Copilot (IN) / Passenger (OUT)
Intercom Volume (inner knob)
15. Indicator Test Button
5 4 3 9 10 11 12 13 14
1 2 6 7 8 15
SR20_FM09_1108
Audio Control Panel
Revision 02: 07-18-05
P/N 11934-S01 3 of 10
Cirrus Design Section 9
SR20 Supplements
Section 2 - Limitations
Use of auxiliary AUDIO IN entertainment input and the optionally
installed XM Radio System is prohibited during takeoff and landing.
Section 3 - Emergency Procedures
In the event of an audio panel power failure, the audio system will
revert to COM 1 for the pilot’s mic and headphones and the pilot will
have transmit and receive capability.
Section 4 - Normal Procedures
Refer to Section 7 - System Description in this supplement for a
complete description and operation of the Audio Control Panel.
Section 5 - Performance
No change from basic Handbook.
Section 6 - Weight & Balance
Garmin GMA 340 Audio System: No change from basic Handbook.
Installation of the optional XM Radio System adds the following
optional (Sym = O) equipment at the weight and arm shown in the
following table.
Section 7 - System Description
Power On and Fail-safe Operation
The Audio Control Panel is powered ‘OFF’ when the left inner knob
(PILOT) is at the full CCW (counter-clockwise) position. Rotating the
　
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