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  2. DO-178C - Wikipedia

    en.wikipedia.org/wiki/DO-178C

    The flexible nature of DO-178C's processes and entry/exit criteria make it difficult to implement the first time, because these aspects are abstract and there is no "base set" of activities from which to work. The intention of DO-178C was not to be prescriptive. There are many possible and acceptable ways for a real project to define these aspects.

  3. Modified condition/decision coverage - Wikipedia

    en.wikipedia.org/wiki/Modified_condition/...

    MC/DC is used in avionics software development guidance DO-178B and DO-178C to ensure adequate testing of the most critical (Level A) software, which is defined as that software which could provide (or prevent failure of) continued safe flight and landing of an aircraft.

  4. AC 20-115 - Wikipedia

    en.wikipedia.org/wiki/AC_20-115

    The Advisory Circular AC 20-115( ), Airborne Software Development Assurance Using EUROCAE ED-12( ) and RTCA DO-178( ) (previously Airborne Software Assurance), recognizes [1] the RTCA published standard DO-178 as defining a suitable means for demonstrating compliance for the use of software within aircraft systems.

  5. Automotive Safety Integrity Level - Wikipedia

    en.wikipedia.org/wiki/Automotive_Safety...

    DO-178C and DO-254 define the design assurance objectives that must be accomplished for given DAL. Unlike SIL, it is the case that both ASIL and DAL are statements measuring degree of hazard. DAL E is the ARP4754 equivalent of QM; in both classifications hazards are negligible and safety management is not required.

  6. DO-254 - Wikipedia

    en.wikipedia.org/wiki/DO-254

    The DO-254/ED-80 standard is the counterpart to the well-established software standard RTCA DO-178C/EUROCAE ED-12C. With DO-254/ED-80, the certification authorities have indicated that avionics equipment contains both hardware and software, and each is critical to safe operation of aircraft.

  7. ARP4754 - Wikipedia

    en.wikipedia.org/wiki/ARP4754

    ARP4754 is intended to be used in conjunction with the safety assessment process defined in SAE ARP4761 (updated to Revision A in December 2023) and is supported by other aviation standards such as RTCA DO-178C/DO-178B and DO-254. This guideline addresses Functional Safety and design assurance processes.

  8. Category:RTCA standards - Wikipedia

    en.wikipedia.org/wiki/Category:RTCA_standards

    Download as PDF; Printable version; In other projects ... Pages in category "RTCA standards" ... DO-178C; DO-212; DO-219; DO-232; DO-242A; DO-248C;

  9. Certification Authorities Software Team - Wikipedia

    en.wikipedia.org/wiki/Certification_Authorities...

    With application of DO-178B, it was discovered that many projects were not complying with DO-178B, but there was also wide variations in how various certification authorities conducted project assessments. In response, the CAST developed a standard software compliance assessment approach.

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