Garmin GNS 530W, Installation Manual

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500W Series Installation Manual Page 5-5
190-00357-02 Rev. D
5.3.2 MAIN RS-232 CONFIG Page
Select the MAIN RS-232 CONFIG page (see Figure 5-2).
Change the selectable RS-232 inputs and/or outputs to
match that of the equipment installed in the aircraft.
NOTE
Interfacing systems listed in the following tables are provided for reference only. Refer
to Appendix G to determine if the interface to a particular system is approved under the
400W/500W Series AML STC.
CHANNEL INPUTS
Selection Description
Off
No unit(s) connected to input of this channel.
Arnav/ei-fuel Serial fuel flow information from the following units:
ARNAV FC-10, FT-10
Electronics International FP-5L
Crossfill
Serial transfer of flight plans and user waypoints between two 400W/500W
Series units
GDL 69
Serial data input for in-flight access to weather and messaging from the
following units:
Garmin GDL 69/69A
Icarus-alt
Serial altitude data from the following units:
Icarus Instruments 3000
Sandia SAE5-35
Garmin GTX 327 Transponder
Trans-Cal Industries IA-RS232-X, SSD120
ACK Technologies A-30 (Mod 8 and above)
Ryan TCAD
Traffic information from a Ryan TCAD 9900B or 9900BX Series system.
Shadin-adc Serial air data information from the following units:
Shadin ADC 200, 200+, 2000
Shadin-alt
Serial altitude data from the following units:
Shadin 8800T, 9000T, 9200T
Shadin-fadc
Serial air data and fuel flow information from the following units:
Shadin 9628XX-X Fuel/Air Data Computer
INSIGHT TAS 1000 Air Data Computer
Shadin-fuel Serial fuel flow information from the following units:
Shadin 91053XM Digital Fuel Management System
Shadin 91204XM Digital Fuel Management System
JP Instruments EDM-700 or EDM-760 Engine Monitor
WX-500
Lightning strike information from an L3 Communications WX-500
Stormscope.
Figure 5-2. MAIN RS-232 CONFIG
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