- TCAS II Transmitter/Receiver.
- DO-185A (Change 7.0) software.
- Greater target location accuracy.
- ARINC 735A interfaces.
- Processor and memory to accommodate potential future “Free Flight” CNS/ATM requirements.
- 115 Vac/28 Vdc common power supply.
- Growth space for two additional modules in 6 MCU package, or optional 4 MCU size available.
- Top/Bottom Antenna switching circuitry.
- Can operate with no forced air cooling or internal cooling fans at reduced reliability levels.
- Advisories can be displayed on various dedicated indicators depending on aircraft configuration requirements.
- Combine proven advanced technology components, high density circuit designs and comprehensive self-test circuitry to provide exceptionally reliable operation.