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The parameter data item file must be verified together with the executable object code, or else it must be tested for all possible ranges of the parameter data items. DO-330 "Software Tool Qualification Considerations", a new "domain independent, external document", was developed to provide guidance for an acceptable tool qualification process.
The system safety assessments combined with methods such as SAE ARP 4754A determine the after mitigation DAL and may allow reduction of the DO-178B software level objectives to be satisfied if redundancy, design safety features and other architectural forms of hazard mitigation are in requirements driven by the safety analyses. Therefore, DO ...
For DAL D hardware, as long as the applicant follows DO-254, the applicant does not need to apply this advisory circular since the FAA does not expect to examine the life cycle data. [3] [5] However, if the applicant chooses to follow other design practices for DAL D hardware (as permitted by this AC) the FAA will review the data. [7]
EASA wrote a certification memoranda to require the use of DO-254 for all complex electronics within a system, stating that all equipment and CBA with a Design assurance classification of A, B, C or D should meet level D objectives for the equipment and CBA, regardless of the DAL of the system or aircraft function. FAA wrote a Final Report for ...
Harris Corporation Awarded $331 Million Contract by FAA for Data Communications Integrated Services Program Highlights: Program will provide highly reliable air/ground data communications services ...
D & D Aviation: DUSTY United States DNK D&K Aviation: DIRECT JET United States V5 VPA DanubeWings: VIP TAXI Slovakia Former names VIP Air and VIP Wings DHE DAP Helicopteros: HELIDAP Chile VLF DFS UK Limited: VOLANTE United Kingdom WD DSR DAS Air Cargo: DAIRAIR Uganda RKC DAS Airlines: DAS CONGO Democratic Republic of the Congo DX DTR DAT Danish ...
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, and the additional guidance and clarifications in advisory circular
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.