RTCA DO-254 / EUROCAE ED-80 — Design Assurance Guidance for Airborne Electronic Hardware

DO-254

Section 07: The Big Standards Map

Definition

The primary guidance document for design assurance of airborne electronic hardware, including complex programmable hardware devices such as FPGAs, ASICs, PLDs, and complex COTS components. DO-254 defines a hardware design lifecycle similar in structure to DO-178C's software lifecycle, including planning, requirements capture, conceptual design, detailed design, implementation (synthesis, place-and-route), verification, configuration management, and process assurance. The objectives scale based on the hardware Design Assurance Level (DAL A through E). DO-254 applies specifically to complex electronic hardware; simple hardware items may be addressed through conventional quality assurance processes.

Where This Shows Up

As avionics increasingly implement safety-critical functions in programmable hardware (FPGAs, ASICs), DO-254 provides the framework for ensuring these devices meet certification requirements. Unlike software which is deterministic (the same input always produces the same output), hardware can experience timing-related issues, metastability, and technology-specific failure modes. DO-254 addresses these concerns through requirements-based design and verification, combined with process assurance. The EUROCAE equivalent is ED-80.

Primary Sources

RTCA DO-254 (2000) — Design Assurance Guidance for Airborne Electronic Hardware

The primary document defining hardware design assurance objectives and processes.

FAA AC 20-152A — RTCA, Inc. Document RTCA/DO-254, Design Assurance Guidance for Airborne Electronic HardwareFAA

FAA Advisory Circular recognizing DO-254 as an acceptable means for airborne electronic hardware design assurance.

EASA AMC 20-152AEASA

EASA acceptable means of compliance referencing DO-254 / ED-80 for hardware design assurance.

Across Jurisdictions

FAA (United States)

AC 20-152A

FAA recognizes DO-254 for design assurance of complex airborne electronic hardware. Applicability is based on hardware complexity and DAL.

EASA (Europe)ED-80

AMC 20-152A

EASA recognizes ED-80 (the EUROCAE equivalent of DO-254) through AMC 20-152A. DO-254 and ED-80 are technically identical.

No technical differences. EASA references ED-80 as the primary designation.

Related Terms

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