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Air data module

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Illustration of the airspeed indication and detection system on fly-by-wire aircraft

Air Data Module is a component of the navigation system on fly-by-wire aircraft, such as Airbus A320 or later Airbus.[1] Each unit converts pneumatic (air pressure) information from a Pitot tube or a static port in to numerical information which is sent on the ARINC 429 data bus.[2] This pressure information is received and processed by the Air Data Reference (ADR) component of the Air Data Inertial Reference Unit (ADIRU)[1]. This processed information is then sent to a display management computer(s) that present information on the cockpit's primary flight display.[3] Airspeed information is also sent to the flight computers and other electronics.[4] Airspeed information is also sent to the autoflight subsystem (.e.g flight management and guidance system).[5]

References

  1. ^ a b "SmartCockpit - Airline training guides, Aviation, Operations, Safety".
  2. ^ "Erroneous flight instruments". Boeing Aero Magazine, Issue 08. Retrieved 2008-07-14.
  3. ^ "SmartCockpit - - A330 - Systems - Indicating and Recording".
  4. ^ "SmartCockpit - - A330 - Control systems".
  5. ^ "SmartCockpit -A330 - Autoflight systems".

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