FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware
Section 5: Custom device development (CD objectives) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware

FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware CD-8: CD-8 Robustness: abnormal and boundary conditions as requirements

For hardware at DAL A or B, abnormal and boundary conditions of inputs and internal states, and the design's expected behaviour in them, are defined as requirements (often derived requirements where not allocated from above), since DO-254 names robustness defects without addressing robustness explicitly.

Maintained by Gerard Blokdyk

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