Electronic centralised aircraft monitor

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Upper ECAM on an Airbus A320 ECAM Airbus.tif
Upper ECAM on an Airbus A320
An ECAM display on an A340-300. ECAM.jpg
An ECAM display on an A340-300.
Airbus A350 Warning Display A350 ecam.png
Airbus A350 Warning Display

An electronic centralised aircraft monitoring (ECAM) or electronic centralized aircraft monitoring is a system that monitors aircraft functions and relays them to the pilots. It also produces messages detailing failures and in certain cases, lists procedures to undertake to correct the problem. [1]

Contents

History

ECAM is similar to other systems, known as Engine Indicating and Crew Alerting System (EICAS), used by Boeing, Bombardier, Dornier, Embraer and Saab, Centralized Fault Detection System (CFDS) on McDonnell Douglas, or Engine Warning Display (EWD) on ATR, which display data concerning aircraft systems and also failures. Airbus developed ECAM, such that it not only provided the features of EICAS, but also displayed corrective action to be taken by the pilot, as well as system limitations after the failures. Using a colour-coded scheme the pilots can instantly assess the situation and decide on the actions to be taken. It was designed to ease pilot stress in abnormal and emergency situations, by designing a paperless cockpit in which all the procedures are instantly available.

System design

ECAM is a series of systems designed to work in unison to display information to the pilots in a quick and effective manner. Sensors placed throughout the aircraft, monitoring key parameters, feed their data into two System Data Acquisition Concentrator (SDACs) which in turn process the data and feed it to two Flight Warning Computers (FWCs). The FWCs check for discrepancies in the data and then display the data on the ECAM displays through the three Display Management Computers (DMCs). In the event of a fault the FWCs generate the appropriate warning messages and sounds. More vital systems are routed directly through the FWCs such that failures in them can still be detected even with the loss of both SDACs. The whole system can continue to operate even with a failure of one SDAC and one FWC.

Failures are classed by importance ranging from level 1 failures to level 3 failures. In the event of simultaneous failures the most critical failure is displayed first. The warning hierarchy is as follows:

In addition to the three failure levels are following status messages:

Alternative systems

Some alternatives are:

Presence

Airbus-developed jetliners have ECAM since the A300-600 and A310.

The Airbus A220 has EICAS, as it was originally a Bombardier product.

Limitations

The Qantas Flight 32 engine failure generated more than 80 ECAM alerts, whose treatment took over an hour to complete. [2]

The A350 and A380 are the only Airbus-developed jetliners with fully integrated checklists.

See also

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References

  1. "Airbus A320 ECAM: What is it and how does it help pilots?". BAA Ground Handling. 2017-09-11. Retrieved 2020-06-30.
  2. https://ntrs.nasa.gov/api/citations/20180003389/downloads/20180003389.pdf