Airborne Electronic Hardware Design Assurance: A by Randall Fulton

By Randall Fulton

Written through a Federal Aviation management (FAA) advisor distinctive engineering consultant (DER) and an electronics layout engineer who jointly taught the DO-254 type on the Radio Technical fee for Aeronautics, Inc. (RTCA) in Washington, District of Columbia, united states, Airborne digital layout insurance: A Practitioner's consultant to RTCA/DO-254 is a sworn statement to the teachings realized and knowledge received from decades of first-hand event within the layout, verification, and approval of airborne digital hardware.

This useful consultant to using RTCA/DO-254 within the improvement of airborne digital for security serious airborne applications:

  • Describes how one can optimize engineering techniques and practices to harmonize with DO-254
  • Addresses the only so much complicated element of engineering and compliance to DO-254—poorly written requirements
  • Includes an academic on tips on how to write standards that may reduce the price and energy of digital layout and verification
  • Discusses the typical pitfalls encountered via practitioners of DO-254, besides how these pitfalls ensue and what should be performed approximately them
  • Settles the continued debate and misconceptions concerning the real definition of a derived requirement
  • Promotes embracing DO-254 because the top skill to accomplish compliance to it, in addition to the simplest route to high quality digital hardware

Airborne digital layout coverage: A Practitioner's advisor to RTCA/DO-254 deals real-world perception into RTCA/DO-254 and the way its targets will be happy. It offers engineers with precious info that may be utilized to any venture to make compliance to DO-254 as effortless and problem-free as possible.

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Extra info for Airborne Electronic Hardware Design Assurance: A Practitioner's Guide to RTCA/DO-254

Sample text

While DO-254 has a broad scope, AC 20-152 limits the scope to complex custom micro-­coded components. The guidance in DO-254 represents industry consensus on design assurance for airborne electronic hardware. DO-254 also incorporates best practices for design assurance identified by the aviation and electronics industry. Guidance in DO-254 covers a variety of topics including: • Hardware standards • Hardware design life cycle data • Additional design assurance techniques for design assurance (IDAL) A and B functions • Previously developed hardware • Tool assessment and qualification • Use of COTS components • Product service experience • Hardware safety assessment • Design assurance strategy, including consideration for design assurance (IDAL) A and B functions • Planning process • Requirements capture • Conceptual design • Detailed design • Implementation • Production transition • Validation process 26 Airborne Electronic Hardware Design Assurance Code of Federal Regulations Title 1 Title 2 Title 50 Title 14 Title 14 Aeronautics and Space Vol.

13093 Federal Aviation Regulations have an amendment level to identify the date and identification of the most recent change to the regulation. In general, aircraft certification programs for new aircraft or changes to existing aircraft use the most recent amendment level of the regulations applicable to the program. In some instances 19 Regulatory Background Title 1 Title 2 Title 3 Title 4 Title 48 Title 49 Title 50 Title 14 Title 14 Aeronautics and Space Vol. 1 Vol. 2 Vol. 3 Chapter I Part 1–59 Part 60–109 Part 110–199 Vol.

The document identifier should use the project specific designation. When DO-254 is used at the system level, the data should be more similar to what is shown in DO-254. In other words, the Top-­Level Drawing would actually be used and not replaced with the PLD equivalent document. The additional considerations section of the PHAC includes a description of any previously developed hardware, usage of COTS components, product service experience, and an assessment of the development and verification tools used in the hardware life cycle.

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