DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
RTCA DO-254 / EUROCAE ED-80 design assurance guidance for airborne electronic hardware, built in full from the held complete text.
DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware is a compliance framework from International (RTCA, United States; EUROCAE, Europe); recognised by FAA AC 20-152A (7 October 2022) and the EASA equivalent with 13 domains and 88 controls that map to 3 other frameworks. The largest domains are Section 10: Hardware design life cycle data – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware (21 controls), Section 11: Additional considerations – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware (12 controls), Section 5: Hardware design processes – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware (12 controls). Every control below carries what it requires and what an assessor expects to see.
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Framework Domains (13)
Appendix A: Life cycle data by design assurance level – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
| Code | Title |
|---|---|
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::A | Appendix A Modulation of life cycle data by design assurance level, and verification independence |
Appendix B: Design assurance for Level A and B functions – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
Section 10: Hardware design life cycle data – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
Section 11: Additional considerations – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
Section 1: Complexity and alternative methods – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
| Code | Title |
|---|---|
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::1.6 | 1.6 Complexity considerations |
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::1.7 | 1.7 Alternative methods or processes |
Section 2: System aspects of hardware design assurance – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
| Code | Title |
|---|---|
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::2.1.1 | 2.1.1 Information flow from the system process to the hardware design life cycle |
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::2.1.2 | 2.1.2 Information flow from the hardware design life cycle to the system process |
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::2.1.3 | 2.1.3 Information flow between the hardware and software life cycles |
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::2.2 | 2.2 System safety assessment processes |
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::2.3.1 | 2.3.1 Hardware safety assessment considerations |
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::2.3.2 | 2.3.2 Quantitative assessment of random hardware faults |
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::2.3.3 | 2.3.3 Qualitative assessment of hardware design errors and upsets |
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::2.3.4 | 2.3.4 Design assurance considerations for hardware failure condition classification |
Section 3: Hardware design life cycle – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
| Code | Title |
|---|---|
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::3.2 | 3.2 Transition criteria |
Section 4: Planning process – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
| Code | Title |
|---|---|
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::4.1 | 4.1 Planning process objectives |
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::4.2 | 4.2 Planning process activities |
Section 5: Hardware design processes – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
Section 6: Validation and verification process – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
Section 7: Configuration management process – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
Section 8: Process assurance – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
| Code | Title |
|---|---|
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::8.1 | 8.1 Process assurance objectives |
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::8.2 | 8.2 Process assurance activities |
Section 9: Certification liaison process – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
| Code | Title |
|---|---|
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::9.1 | 9.1 Means of compliance and planning |
| do-254-ed-80-design-assurance-guidance-for-airborne-electronic-hardware::9.2 | 9.2 Compliance substantiation |
Your Compliance Coverage
If you comply with DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware, you already cover:
SAE ARP4754B / ED-79B - Guidelines for Development of Civil Aircraft and Systems
42%
37 controls mapped
Compare →DO-178C / ED-12C - Software Considerations in Airborne Systems
33%
29 controls mapped
Compare →FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware
22%
19 controls mapped
Compare →Maps to 3 other frameworks
Coverage is not the same as your position
This page shows what DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware overlaps with in general. Where your organisation actually stands, against the standard you are going for and the certifications you already hold, is a different question. Same graph and the same recorded refutations, scoped to you rather than to a pair.
The Compliance Position Diagnostic, $5,000 fixed, ten business daysWhat is DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware and who does it apply to?
DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware is a compliance framework from International (RTCA, United States; EUROCAE, Europe); recognised by FAA AC 20-152A (7 October 2022) and the EASA equivalent with 13 domains and 88 controls. RTCA DO-254 / EUROCAE ED-80 design assurance guidance for airborne electronic hardware, built in full from the held complete text. It is used by organisations to establish and maintain compliance with industry standards and regulatory requirements.
What does DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware actually require?
DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware has 88 controls organised across 13 domains. The largest domains are Section 10: Hardware design life cycle data – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware (21 controls), Section 11: Additional considerations – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware (12 controls), Section 5: Hardware design processes – DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware (12 controls). Each control defines specific requirements that organisations must implement to achieve compliance.
If I already comply with another framework, how much of DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware do I already cover?
DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware maps to 3 other compliance frameworks. The top mapping partners are SAE ARP4754B / ED-79B - Guidelines for Development of Civil Aircraft and Systems (42% coverage), DO-178C / ED-12C - Software Considerations in Airborne Systems (33% coverage), FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware (22% coverage). Use our comparison tool to explore control-level mappings between frameworks.
How do I implement DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware?
Start your DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware compliance journey by running a self-assessment on our platform to identify your current compliance posture. Our AI advisory can answer specific questions about DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware requirements, and cross-framework mapping helps you leverage existing controls from other frameworks you may already comply with. Create a free account to access all 88 controls and track your progress.
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