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

FAA AC 20-152A - Development Assurance for Airborne Electronic Hardware COTS-6: COTS-6 Failure modes and common modes fed to the safety assessment

The failure modes of the device's used functions and their possible common modes are identified and returned to the system safety assessment.

Maintained by Gerard Blokdyk

What else in your programme already covers this

This control maps to 1 controls across 1 other frameworks. If you already hold one of them, the evidence you collected for it is the starting point here rather than new work.

DO-254 / ED-80 - Design Assurance Guidance for Airborne Electronic Hardware · 1 control

  • 2.1.2 2.1.2 Information flow from the hardware design life cycle to the system process

Every mapping shown was judged rather than inferred from wording similarity, and the ones that failed review are published too. See the coverage reports and what was rejected.

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

Query this from an agent

The graph holds this control, the 1 it maps to, and the evidence behind each claim, over MCP and REST.

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