SAE ARP4754B / ED-79B - Guidelines for Development of Civil Aircraft and Systems
Sections 5.1 and 5.2: Safety assessment and development assurance level assignment – SAE ARP4754B / ED-79B - Guidelines for Development of Civil Aircraft and Systems

SAE ARP4754B / ED-79B - Guidelines for Development of Civil Aircraft and Systems 5.1.4: 5.1.4 Preliminary system safety assessment

The PSSA systematically evaluates a proposed system architecture against the SFHA failure conditions and the requirements allocated from the PASA, proposing system-level safety requirements and assumptions, and identifying safety requirements for systems, subsystems and items (including safety, reliability, independence and separation) and the FDAL and IDAL assignments. It shows where protection is needed, for example redundancy, monitors, partitioning, higher development assurance rigor, built-in test, or maintenance tasks and intervals that safety depends on, takes common cause into account and accounts for latent failures and their exposure times. It starts early, iterates with the design, allocates system safety requirements down to subsystems and items, and hands over to the SSA as designs mature.

Maintained by Gerard Blokdyk

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  • 2.3.1 2.3.1 Hardware safety assessment considerations

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Other controls in Sections 5.1 and 5.2: Safety assessment and development assurance level assignment – SAE ARP4754B / ED-79B - Guidelines for Development of Civil Aircraft and Systems

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