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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.
Called attention to RTCA DO-178. [6] AC 20-115A 1986 Called attention to RTCA DO-178A. [6] [7] AC 20-115B 1993 Called attention to RTCA DO-178B. [8] AC 20-115C 2013 Calls attention to RTCA DO-178C [3] w/guidance for Rev B to Rev C change. [9] AC 20-115D 2017 Minor updates largely to harmonize with EASA guidance. [10] [4] [11]
RTCA, Inc. (formerly known as Radio Technical Commission for Aeronautics) is a United States non-profit organization that develops technical guidance for use by government regulatory authorities and by industry. It was founded in 1935 and was re-incorporated in 1991 as a private not-for-profit corporation.
Airborne Software Development Assurance Using EUROCAE ED-12( ) and RTCA DO-178( ) ED-12C/DO-178C ED-215/DO-330 ED-218/DO-331 ED-217/DO-332 ED-216/DO-333: AC 20-136: Aircraft Electrical and Electronic System Lightning Protection: RTCA DO-160 §22: AC 20-148: Reusable Software Components: AC 20-152A Design Assurance Guidance for Airborne ...
DO-248C, Supporting Information for DO-178C and DO-278A, published by RTCA, Incorporated, is a collection of Frequently Asked Questions and Discussion Papers addressing applications of DO-178C and DO-278A [1] in the safety assurance of software for aircraft and software for CNS/ATM systems, respectively.
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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 .
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