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- Q3011402 subject Q6401172.
- Q3011402 subject Q7216224.
- Q3011402 subject Q8281295.
- Q3011402 subject Q8617370.
- Q3011402 abstract "RTCA/DO-254, Design Assurance Guidance For Airborne Electronic Hardware is a document providing guidance for the development of airborne electronic hardware, published by RTCA, Incorporated.The DO-254 standard was formally recognized by the FAA in 2005 via AC 20-152 as a means of compliance for the design of complex electronic hardware in airborne systems. Complex electronic hardware includes devices like Field Programmable Gate Arrays (FPGAs), Programmable Logic Devices (PLDs), and Application Specific Integrated Circuits (ASICs). The DO-254 standard is the counterpart to the well-established software standard RTCA DO-178B/EUROCAE ED-12B. With DO-254, the FAA has indicated that avionics equipment contains both hardware and software, and each is critical to safe operation of aircraft. There are five levels of compliance, A through E, which depend on the effect a failure of the hardware will have on the operation of the aircraft. Level A is the most stringent, defined as "catastrophic" (e.g. loss of the aircraft), while a failure of Level E hardware will not affect the safety of the aircraft. Meeting Level A compliance for complex electronic hardware requires a much higher level of verification and validation than Level E compliance.".
- Q3011402 wikiPageExternalLink AC25.1309-1A.pdf.
- Q3011402 wikiPageExternalLink AC%2020-152.pdf.
- Q3011402 wikiPageExternalLink whitepapers.
- Q3011402 wikiPageExternalLink www.do254.com.
- Q3011402 wikiPageExternalLink TAEsdaT2-052496.pdf.
- Q3011402 wikiPageExternalLink techpubs.cfm.
- Q3011402 wikiPageExternalLink www.rtca.org.
- Q3011402 wikiPageWikiLink Q10566551.
- Q3011402 wikiPageWikiLink Q1063837.
- Q3011402 wikiPageWikiLink Q1115443.
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- Q3011402 wikiPageWikiLink Q217302.
- Q3011402 wikiPageWikiLink Q221329.
- Q3011402 wikiPageWikiLink Q276255.
- Q3011402 wikiPageWikiLink Q2919644.
- Q3011402 wikiPageWikiLink Q335357.
- Q3011402 wikiPageWikiLink Q3614972.
- Q3011402 wikiPageWikiLink Q464490.
- Q3011402 wikiPageWikiLink Q4653885.
- Q3011402 wikiPageWikiLink Q4653886.
- Q3011402 wikiPageWikiLink Q502522.
- Q3011402 wikiPageWikiLink Q5205827.
- Q3011402 wikiPageWikiLink Q5491415.
- Q3011402 wikiPageWikiLink Q626741.
- Q3011402 wikiPageWikiLink Q6401172.
- Q3011402 wikiPageWikiLink Q6496962.
- Q3011402 wikiPageWikiLink Q7216224.
- Q3011402 wikiPageWikiLink Q751137.
- Q3011402 wikiPageWikiLink Q7921330.
- Q3011402 wikiPageWikiLink Q80831.
- Q3011402 wikiPageWikiLink Q8281295.
- Q3011402 wikiPageWikiLink Q837992.
- Q3011402 wikiPageWikiLink Q8617370.
- Q3011402 wikiPageWikiLink Q906182.
- Q3011402 comment "RTCA/DO-254, Design Assurance Guidance For Airborne Electronic Hardware is a document providing guidance for the development of airborne electronic hardware, published by RTCA, Incorporated.The DO-254 standard was formally recognized by the FAA in 2005 via AC 20-152 as a means of compliance for the design of complex electronic hardware in airborne systems.".
- Q3011402 label "DO-254".