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Extra info for SAE ARP 4754: Certification Considerations for Highly-Integrated or Complex Aircraft Systems
2 Design Related Assumptions: Design related assumptions are grouped into crew interface, system interface, and reliability. Accepting assumptions in this area may be accomplished by review against existing industry experience and practice. a. , response times, display interpretation, physical limitations), and crew interaction. , recognition of hardovers), decision making strategies, perceptual error rates, the discrimination accuracy on the basis of physical shape, visual form, color, or dynamic performance.
B. 4). c. 5). 5). The inputs to the verification process include the set of documented requirements for the implemented system or item and a complete description of the system or item to be verified. More than one verification method may be necessary to substantiate compliance with the requirements. For example, an analysis may be required in conjunction with a physical test to assure that worst case issues have been covered. During the process of verifying intended functions any anomalies recognized (such as an unintended function or incorrect performance) should be reported so that they can be reviewed.
MODIFIED AIRCRAFT: Many of the processes in this document rely on product and process information obtained during aircraft and system development. Such data may not always be available for existing aircraft. In such cases, alternative means may be necessary to satisfy the certification requirements. The objective of this section is to describe how the material in this document could be applied when modifying an aircraft or system that was not developed in accordance with these guidelines. 1 Certification Basis: The certification basis defines the applicable regulations to be met by the applicant and includes any special conditions required to supplement the published regulations.