DO-254

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DO-254 / ED-80
Design Assurance Guidance for Airborne Electronic Hardware
Latest Revision	April 2000
Prepared by	RTCA SC-190 EUROCAE WG-46

DO-254, Design Assurance Guidance for Airborne Electronic Hardware is a standard for complex electronic hardware development published by RTCA, Incorporated.

Contents 1 Outline of contents 2 Resources 3 Certification in Europe 4 See also 5 External links

[edit] Outline of contents

1. Introduction
2. System Aspects of Hardware Design Assurance
3. Hardware Design Life Cycle
4. Planning Process
5. Validation and Verification Processes
6. CM Process
7. Process (Quality) Assurance
8. Certification Liaison
9. Hardware Design Life Cycle Data
10. Additional Considerations

• App A. Modulation of Data Based on Level
• App B. Design Assurance for Levels A and B
• App C. Glossary
• App D. Acronyms

[edit] Resources

• FAR Part 23/25 §1301/§1309
• FAR Part 27/29
• AC 23/25.1309
• RTCA DO-254

[edit] Certification in Europe

• Replace FAA with EASA, JAA or CAA
• Replace FAR with JAR
• Replace AC with AMJ

[edit] See also

• avionics
• hazard analysis
• DO-178B (similar to DO-254, but for software)
• ARP4761
• ARP4754

[edit] External links

• AC 25.1309-1A

• Simulink, Stateflow and HDL Coder from The MathWorks