Becker Avionics GmbH BXT6513 Manual De Usuario
Installation
Unit Configuration
46
BXT6513-(0XX)
DV15104.03 Issue 03 November 2016
2.6.2. ARINC 429 Output Labels
Parameter
Label
XPDR control
016 or 031
Flight ID
233…237
Mode S address
275, 276
Maintenance
350, 353, 354
GA equipment identification
371
Equipment identification
377
2.7.
Unit Configuration
The figure "General Architecture (example)", page 47 shows an example of a single unit installation
including:
including:
• Power supply without separate switch,
• Configuration from internal memory,
• Single ADC conformant to ARINC 706,
• FMC,
• ADLP,
• GNSS sensor conformant to ARINC 743A,
• Weight-on-wheels switch, active low,
• Indicators for system status and transponder reply,
• Standby switch,
• Dual antenna (Diversity).
• Service Connector (optional).
• Configuration from internal memory,
• Single ADC conformant to ARINC 706,
• FMC,
• ADLP,
• GNSS sensor conformant to ARINC 743A,
• Weight-on-wheels switch, active low,
• Indicators for system status and transponder reply,
• Standby switch,
• Dual antenna (Diversity).
• Service Connector (optional).
Relevant configuration settings:
Configuration
Set to
Air Data Source Configuration
Single
Air Data Format and Resolution
ARINC 429
Air Data Port A Selection
Dedicated port
Ground Sensor Enable
Enable, active low
XPDR Control Port A Selection
Dedicated port
TCAS Interface Enable
Disable
ADLP Interface Enable
Enable
FMC Input Selection
Dedicated port
GNSS Receiver Input Selection
Dedicated port
GNSS Data Format
ARINC 743A