SAE ARP4754B / ED-79B - Guidelines for Development of Civil Aircraft and Systems
Section 4: Aircraft and system development process – SAE ARP4754B / ED-79B - Guidelines for Development of Civil Aircraft and Systems

SAE ARP4754B / ED-79B - Guidelines for Development of Civil Aircraft and Systems 4.6.3: 4.6.3 Item integration and verification

The first integration of an item can be done on breadboards or prototypes, in computer emulation, or on test articles for the laboratory or flight; detailed procedures are used to confirm that integration is complete and every item requirement is met, and interface documents may be developed so integrated items work together (for example correct electronic hardware initialization, memory maps). What comes out are configuration-controlled items accompanied by their assurance records and life cycle data.

Maintained by Gerard Blokdyk

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  • A-5.7 Integration outputs checked as complete and correct

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Other controls in Section 4: Aircraft and system development process – SAE ARP4754B / ED-79B - Guidelines for Development of Civil Aircraft and Systems

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