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• Mode C Transponder with Altitude Encoder (Garmin GTX 327)
• Horizontal Situation Indicator
• Course Deviation Indicator
Avionics Configuration 2.2 - Serials 1268 through 1336:
• Moving Map Display (Avidyne MFD)
• Two-Axis Autopilot (S-Tec System 55X)
• Integrated Audio System with Intercom (Garmin GMA 340)
• Marker Beacon Receiver (Garmin GMA 340)
• Two IFR Approach-Certified GPS (Garmin GNS 430)
• Two VHF Communications Transceivers (Garmin GNS 430)
• Two Navigation (VOR/LOC/GS) Receiver (GNS 430)
• Mode C Transponder with Altitude Encoder (Garmin GTX 327)
• Electronic Navigation Display (Sandel SN3308)
• Course Deviation Indicator
Avionics Configuration PFD - Serials 1337 and subsequent:
• Moving Map Display (Avidyne MFD)
• Primary Flight Display (Avidyne PFD)
• Two-Axis Autopilot (S-Tec System 55SR)
• Integrated Audio System with Intercom (Garmin GMA 340)
• Marker Beacon Receiver (Garmin GMA 340)
• One IFR Approach-Certified GPS (Garmin GNS 430) and One
VFR GPS (Garmin GNC 250XL)
• Two VHF Communications (Garmin GNS 430 and Garmin GNC
250XL)
• Single Navigation (VOR/LOC/GS) Receiver (GNS 430)
• Mode C Transponder with Altitude Encoder (Garmin GTX 327)
Avionics Configuration SRV - Serials 1337 and subsequent:
• Primary Flight Display (Avidyne PFD)
• Moving Map Display (Avidyne MFD)
March 2010
Information Manual 7-89
Cirrus Design Section 7
SR20 Airplane Description
• Integrated Audio System with Intercom (Garmin GMA 340)
• Marker Beacon Receiver (Garmin GMA 340)
• One IFR Certified GPS (Garmin GNC 420)
• One VHF Communications (Garmin GNC 420)
• Mode C Transponder with Altitude Encoder (Garmin GTX 327)
Multi-Function Display
This airplane is equipped with an Avidyne FlightMax EX5000C 700-
00004-XXX-() Multi-Function Flight Display (MFD). The MFD is a 10.4-
inch landscape-oriented display mounted in the instrument panel. The
MFD provides supplemental display of situational and navigation
information to the pilot. This is accomplished by showing an icon
representing the airplane against a moving map. The MFD accepts
data from a variety of sources, including the GPS sensors, the WX-
500 Stormscope, and the SkyWatch Traffic Advisory System. The unit
is organized around logical grouping of information presented on
“Pages.”
The Avidyne FlightMax EX-Series MFD is 10.4-inch diagonal color
Active Matrix Liquid Crystal Display (AMLCD) integrated into a Control
Display Unit (CDU), which displays the airplane current position and
track against a moving map. The EX-Series MFD can perform the
following functions:
• Generate and display a moving map based on GPS position
data with obstacle and terrain data.
• Display Stormscope lightning strike bearing and distance.
• Display Skywatch traffic advisory information. (EX5000C
only)
• Display a GPS flight plan based on pilot inputs.
• Display Normal and Emergency checklists as well as
performance data.
• Display navigation data, such as groundspeed and track.
The pilot can configure the moving map display. Some of its
configuration features are:
• Select Track-up or North-up modes.
• Select map scale.
March 2010
7-90 Information Manual
Section 7 Cirrus Design
Airplane Description SR20
• Select terrain features, such as airports and special use
airspace and select color enhanced terrain.
• Select and view trip data from GPS.
Power for the MCU is 28 VDC supplied through the 5-amp MFD circuit
breaker on the Avionics Non-Essential Bus.
• Note •
Serials 1005 through 1472 before MFD software version 530-
00162-000 Revision 02; Do not use the Garmin 420 or 430
Navigators to display Stormscope lightning data when the
Avidyne MFD’s Lightning mode is set to either DATALINK or
OFF. For the Garmin 420 or 430 Navigators to accurately
display lightning strikes, the Lightning mode selected on the
MFD’s MAP Page, must be set to either STRIKE or CELL.
Refer to Avidyne FlightMax EX5000C Pilot’s Guide, for a more
complete description of the MFD, its operating modes, and additional
detailed operating procedures.
Autopilot
Avionics Configuration 2.0:
The standard SR20 is equipped with an S-TEC System Twenty
Autopilot. This single-axis autopilot system is a rate-based system,
deriving roll axis control inputs from its electric turn coordinator. The
　
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