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FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware

United States (FAA Aircraft Certification Service); EASA counterpart AMC 20-152A
vAC 20-152A, 7 October 2022 (cancels AC 20-152, 30 June 2005); current at 2026-10-01
4 domains
29 controls

FAA AC 20-152A objectives supplementing DO-254 for custom devices, COTS IP, COTS devices and circuit board assemblies.

Verified

FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware is a compliance framework from United States (FAA Aircraft Certification Service); EASA counterpart AMC 20-152A with 4 domains and 29 controls that map to 1 other frameworks. The largest domains are Section 5: Custom device development (CD objectives) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware (13 controls), Section 6: Use of COTS devices (COTS objectives) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware (8 controls), Section 5.11: COTS IP in custom devices (IP objectives) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware (7 controls). Every control below carries what it requires and what an assessor expects to see.

Maintained by Gerard Blokdyk

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Framework Domains (4)

Section 5.11: COTS IP in custom devices (IP objectives) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware

7 controls
Controls in the Section 5.11: COTS IP in custom devices (IP objectives) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware domain of FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware — 7 controls
CodeTitle
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::IP-1IP-1 Selection of COTS IP
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::IP-2IP-2 Assessment of the COTS IP provider and data
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::IP-3IP-3 Complementary development assurance for COTS IP
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::IP-4IP-4 Verification strategy for COTS IP
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::IP-5IP-5 Planning the COTS IP development assurance approach
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::IP-6IP-6 Requirements for COTS IP functions
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::IP-7IP-7 DO-254 Appendix B for COTS IP at DAL A and B

Section 5: Custom device development (CD objectives) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware

13 controls
Controls in the Section 5: Custom device development (CD objectives) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware domain of FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware — 13 controls
CodeTitle
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::5.105.10 Clarifications to DO-254 Appendix A life cycle data
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::CD-1CD-1 Custom device DAL and simple or complex classification
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::CD-10CD-10 Independent assessment of tool output
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::CD-11CD-11 Relevant tool history
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::CD-12CD-12 Reuse of previously developed hardware
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::CD-2CD-2 Development process for simple custom devices
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::CD-3CD-3 Validation of all custom device requirements
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::CD-4CD-4 Detailed design review and design-to-requirement traceability
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::CD-5CD-5 Review of design tool reports
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::CD-6CD-6 Review of verification cases and procedures
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::CD-7CD-7 Verification of implementation timing performance
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::CD-8CD-8 Robustness: abnormal and boundary conditions as requirements
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::CD-9CD-9 HDL code coverage criteria for elemental analysis

Section 6: Use of COTS devices (COTS objectives) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware

8 controls
Controls in the Section 6: Use of COTS devices (COTS objectives) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware domain of FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware — 8 controls
CodeTitle
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::COTS-1COTS-1 COTS device complexity assessment
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::COTS-2COTS-2 Electronic component management process
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::COTS-3COTS-3 Use outside manufacturer specification
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::COTS-4COTS-4 Embedded microcode
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::COTS-5COTS-5 Errata assessment and mitigation
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::COTS-6COTS-6 Failure modes and common modes fed to the safety assessment
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::COTS-7COTS-7 Definition and verification of COTS device usage
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::COTS-8COTS-8 Critical configuration settings

Section 7: Circuit board assemblies (CBA objective) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware

1 controls
Controls in the Section 7: Circuit board assemblies (CBA objective) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware domain of FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware — 1 controls
CodeTitle
faa-ac-20-152a-development-assurance-for-airborne-electronic-hardware::CBA-1CBA-1 Circuit board assembly development process

Maps to 1 other framework

29 total controls
DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware
27 source controls mapped|19 target controls covered
93%

Coverage is not the same as your position

This page shows what FAA AC 20-152A - Development Assurance 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.

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What is FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware and who does it apply to?

FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware is a compliance framework from United States (FAA Aircraft Certification Service); EASA counterpart AMC 20-152A with 4 domains and 29 controls. FAA AC 20-152A objectives supplementing DO-254 for custom devices, COTS IP, COTS devices and circuit board assemblies. It is used by organisations to establish and maintain compliance with industry standards and regulatory requirements.

What does FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware actually require?

FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware has 29 controls organised across 4 domains. The largest domains are Section 5: Custom device development (CD objectives) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware (13 controls), Section 6: Use of COTS devices (COTS objectives) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware (8 controls), Section 5.11: COTS IP in custom devices (IP objectives) – FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware (7 controls). Each control defines specific requirements that organisations must implement to achieve compliance.

If I already comply with another framework, how much of FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware do I already cover?

FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware maps to 1 other compliance frameworks. The top mapping partners are DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware (93% coverage). Use our comparison tool to explore control-level mappings between frameworks.

How do I implement FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware?

Start your FAA AC 20-152A - Development Assurance 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 FAA AC 20-152A - Development Assurance 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 29 controls and track your progress.

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