FAA Order 8110.105
American regulatory order / From Wikipedia, the free encyclopedia
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FAA Order 8110.105B, Airborne Electronic Hardware Approval Guidelines is an explanation of how Federal Aviation Administration (FAA) personnel can use and apply the publication
- DO-254, Design Assurance Guidance for Airborne Electronic Hardware, RTCA,
Abbreviation | FAA Order 8110.105 |
---|---|
Year started | 2008[1] |
Latest version | B 2024 (2024) |
Organization | Federal Aviation Administration |
Domain | Avionics, type certification |
Website | faa.gov |
and the additional guidance and clarifications in advisory circular
- AC 20-152A, Development Assurance for Airborne Electronic Hardware, FAA.
The order additionally identifies
- AC 00-72, Best Practices for Airborne Electronic Hardware Design Assurance Using EUROCAE ED80() and RTCA DO 254(), FAA.
This revision cancels 8110.105A and 8110.105, Simple and Complex Electronic Hardware Approval Guidance, which had remarkably different intent and content. These cancelled revisions supplemented RTCA DO-254() by explaining to private users of that standard how FAA aircraft certification staff could use that document "when working on type certification projects".[1] They covered "specific topics of interest to the FAA that may go above and beyond content specific to DO-254."[1] As such, these revisions were recommended for reference by developers applying under DO-254() for certification of electronic hardware designs,[2] including those implemented in "custom micro-coded components" (ie., ASICs, PLDs, or FPGAs).
The order now only gives limited instructions on the Airborne Electronic Hardware Review Process to FAA staff and designees. The previous content was removed "to eliminate duplication or conflict with AC 20-152A or AC 00-72," which were released in 2022.