Applying DO-254 for Avionics Hardware Development and Certification
The avionics hardware industry world-wide is now commonly required to follow DO-254 Design Assurance Guidance for Airborne Electronic Hardware for literally all phases of development: Safety, Requirements, Design, Logic Implementation, V&V, Quality Assurance, etc. The DO-254 standard is a companion to the software DO-178B standard; however, there are many differences between hardware and software which must be understood. This basic course introduces the intent of the DO-254 standard for commercial avionics hardware development. The content will cover many aspects of avionic hardware including: aircraft safety; systems; hardware planning, requirements, design, implementation and testing. Attendees will learn industry-best practices for real-world hardware development, common DO-254 mistakes and how to prevent them, and how to minimize risks and costs while maximizing hardware quality. The avionics hardware development process will be summarized including DO-254C"s relationship to other standards including ARP-4761 for Safety and ARP-4754A for Systems Development.