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ETTC'2003 - SEE

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BACK<br />

1 Introduction<br />

AIRBUS AIRCRAFT 0<br />

C.AUBERT<br />

AIRBUS INTEGRATION TEST CENTRE<br />

The aim of this document is a presentation of AIRCRAFT 0 concept which is a general system<br />

integration of parts and equipment of a new aircraft on ground. An overview of the general<br />

development context and a general architecture are explained.<br />

In 1995, the A400M System Test Policy was initially defined and proposed by AIRBUS . This policy<br />

was based on the introduction of the “Aircraft –1” and “Aircraft 0” concepts which have been proven<br />

to be the most efficient ways to integrate systems in an aircraft program.<br />

These concepts proposed, at different phases of Aircraft design, an extension at aircraft level of system<br />

integration principles already applied by AEROSPATIALE with regards to the perimeter of its<br />

worksharing in A320 and A340 programs.<br />

For A380 an early integration was retained as a major way to improve the efficiency of the<br />

development considering the novelties of A380 systems and the important interactions intersystems<br />

which are generated by the AFDX communication network and the new interactive cockpit dialog<br />

with systems.<br />

The industrial context AIRBUS where all the ancient partners are integrated into the same entity<br />

privilege also the integration.<br />

Finally ,it was agreed between the different actors that these concepts will be applied firstly for A380<br />

program.

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