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Questions and Answers

What is DATAC?

  • A technology for a single global data bus developed by ARINC
  • A technology for a single global data bus developed by Airbus.
  • A technology for a single global data bus developed by NASA
  • A technology for a single global data bus developed by Boeing. (correct)

What type of cable does DATAC use to carry information between components of an aircraft system?

  • Coaxial cable
  • Fiber optic cable
  • Ethernet cable
  • Twisted pair of wires (correct)

What is the purpose of coding each component's data in DATAC?

  • To prevent jumbling (correct)
  • To increase the transmission rate
  • To reduce maintenance needs
  • To allow for bidirectional communication

What was the benefit of using DATAC in aircraft systems?

<p>Greater number of integrated components (A)</p> Signup and view all the answers

What is ARINC 629?

<p>A new industry data bus standard developed by ARINC (C)</p> Signup and view all the answers

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Study Notes

  • DATAC is a technology for a single global data bus developed by Boeing.
  • It uses a single twisted pair of wires to carry information between components of an aircraft system.
  • Each component's data is coded and broadcasted in a synchronized order to prevent jumbling.
  • DATAC allowed a greater number of components to be integrated into aircraft systems and reduced maintenance needs.
  • DATAC was installed and tested on a NASA 737 before being incorporated into Boeing's B777.
  • ARINC used DATAC as the basis for a new industry data bus standard called ARINC 629.
  • ARINC 629 is a bidirectional, distributed control bus that can support up to 120 users at a transmission rate of 2 Mbps.
  • Terminals listen to the bus and wait for a quiet period before transmitting, and only one terminal can transmit at a time.
  • The ARINC 629 terminal controller and Serial Interface Module (SIM) are installed on a circuit board within each Line Replacement Unit (LRU).
  • The SIM interfaces with the stub cable via a connector on the LRU, which is then coupled to the global data bus via a current mode coupler.

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