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DO-254 Training | Design Assurance of Airborne Electronic Hardware

DO-254 Training | Design Assurance of Airborne Electronic Hardware

DO-254 Training:

DO-254 Training covers principals, objectives, and guidance for design assurance of airborne electronic hardware based on RTCA DO-254/Eurocae ED-80 standards. Do-254 Training covers all aspects of airborne electronic hardware from conception through initial certification and subsequent post-certification product improvements to ensure continued airworthiness. Getting familiar with DO-254 defines objectives that must be met by avionics equipment manufacturers according to EASA and FAA guidelines.<>

DO-254 is a two-day training class providing a good overview and application of DO-254 as defined by current FAA and EUROCAE ED-12C / ED-109A guidance. Students will learn current FAA and EASA guidance on the application of DO-254 in airborne systems. DO-254 training also covers the objectives of RTCA DO-254’s five levels of criticality from level A (highest) to level E (lowest). These design assurance levels are required for all civil airborne electronic hardware. Learn also how military airborne applications such as A400M are now requiring DO-254 compliance.

Learn about DO-254, Design Assurance Guidance for Airborne Electronic Hardware

DO-254 Training is intended to help aircraft manufacturers and suppliers of aircraft electronic systems techniques on how to assure that electronic airborne equipment safely performs its intended function. The DO-254 training clarifies design life cycle processes for hardware that includes line replaceable units, circuit board assemblies, application-specific integrated circuits (ASICs), programmable logic devices, etc. It also characterizes the objective of the design life cycle processes and offers a means of complying with DO-254 certification requirements.

Learn about:

  • DO-254 Requirements Capture
  • DO-254 Conceptual Design
  • DO-254 Detailed Design
  • DO-254 Implementation and Production Transition
  • DO-254 Verification and Validation

Your Registration Includes?

  • 2 days of DO-254 Training with an expert instructor
  • DO-254 Training Electronic Course Guide
  • 100% Satisfaction Guarantee
  • Certificate of Completion

Resources:

Related Courses

Customize It:

  • If you are familiar with some aspects of the DO-254 Training course, we can omit or shorten their discussion.
  • We can adjust the emphasis placed on the various topics or build the DO-254 Training course around the mix of technologies of interest to you (including technologies other than those included in this outline).
  • If your background is nontechnical, we can exclude the more technical topics, include the topics that may be of special interest to you (e.g., as a manager or policy-maker), and present the DO-254 Training course in a manner understandable to lay audiences.

Audience / Target Group:

The target audience for this DO-254 Training course:

  • Program managers, Project managers, process managers, hardware engineers and designers, verification, and quality assurance engineers working on projects requiring DO-254 certification.

Objectives:

Upon completing this DO-254 Training course, learners will be able to meet these objectives:

  • How to write, organize and optimize requirements for verification.
  • How FAA Avionic certification works
  • Navigate and understand the RTCA/DO-254 document
  • Create Hardware Management Plans and Standards
  • Plan for Hardware Aspects of Certification
  • Understand DO-254 Hardware Requirements Apply the DO-254 lifecycle and supporting processes
  • Understand system safety assessments and the DAL
  • How DO-254 Compliance Works
  • How to work with DO-254 Design Assurance Level (DAL)
  • How to use PLDs in Avionics
  • Regulatory background and use of design assurance
  • CAST Papers
  • Understand Order 8110.105 & Job Aid
  • Set up a project correctly through proper planning
  • Follow the current guidance for DO-254 projects
  • Identify and avoid common pitfalls in DO-254 projects
  • Review and use the FAA AEH Job Aid
  • How to make verification less difficult, less expensive, and less time-consuming.
  • The difference between requirements and design.
  • How to perform Elemental Analysis according to RTCA/DO-254
  • The definition of a functional element.
  • How to express functions
  • Plan for Hardware Aspects of Certification (PHAC)
  • Appendix B for Levels A and B hardware

DO-254 Training – Course Syllabus:

Introduction to DO-254

  • DO-254 Hardware Design Lifecycle objectives and Data
  • Design Assurance of Airborne Electronic Hardware
  • System Safety and DAL
  • Application of DO-254 by EASA and FAA
  • Additional documents defining application of DO-254
  • CRIs and Issue papers
  • Simple Vs. Complex Device
  • How to use the DO-254 Document
  • Integral/supporting Processes
  • Validation and Verification
  • Configuration Management
  • Process Assurance
  • Certification Liaison
  • Additional Considerations
  • Tool Qualification
  • Previously Developed HW
  • COTs Cores and IPs
  • Single Event Upset and SRAM parts
  • Functional Failure Path (FFP)
  • Elemental analysis
  • Advanced Verification techniques
  • COTS & IP cores
  • Classic Design Process
  • RTCA/DO-254 Design Process Considerations
  • Design Assurance Through Design Practice
  • Serial Line Data Receiver
  • Verification and Validation Considerations
  • Test Cases
  • Considerations for Application of RTCA/DO-254 to complex electronic circuits
  • Elemental Analysis LRU Example
  • System Safety and DAL
  • Application of DO-254 by EASA and FAA
  • Additional documents defining application of DO-254
  • CRIs and Issue papers
  • Simple Vs. Complex Device
  • How to use the DO-254 Document
  • Planning Process
  • PHAC, HDP, HVP, HCMP, HQAP
  • Requirements, design and Code Standards
  • Hardware Design Process

System Aspects of Hardware Design Assurance 

  • System Development Process
  • Hardware Design Life Cycle Process
  • Information Flow from Hardware Design Life Cycle Process to System Development Process
  • Information Flow between Hardware Design Life Cycle Process and Software Life Cycle Process
  • System Safety Assessment Processes
  • Hardware Safety Assessment
  • Hardware Design Life Cycle Processes
  • Transition Criteria

FPGA design lifecycle and DO-254 

  • Principals
  • Traceability
  • Transition Criteria
  • Requirements
  • Conceptual Design
  • Detailed Design
  • Implementation
  • Production Transition
  • Integral/supporting Processes
  • Validation and Verification
  • Configuration Management and Process Assurance
  • Design Assurance Guidance for Airborne Electronic Hardware
  • what is DO-254 Compliance?
  • System Safety
  • Design Assurance Level (DAL)
  • Application of DO-254 by EASA and FAA
  • DO-254 Hardware Design Lifecycle objectives and Data
  • Tool Qualification
  • COTs Cores and IPs
  • Single Event Upset and SRAM parts
  • Functional Failure Path (FFP)
  • Elemental analysis
  • Advanced Verification techniques
  • Plan for Hardware Aspects of Certification (PHAC)
  • Requirements Capture
  • Conceptual Design
  • Detailed Design
  • Implementation and Production Transition
  • Verification and Validation

DO-254 Planning Processes

  • Planning Process Objectives
  • Planning Process Activities

 DO-254 Hardware Design Process

  • Requirements Capture Process
  • Conceptual Design Process
  • Detailed Design Process
  • Implementation Process
  • Production Transition Process
  • Acceptance Test
  • Series Production

DO-254 Hardware Design Lifecycle objectives and Data

  • Integral/supporting Processes
  • Validation and Verification
  • Configuration Management
  • Process Assurance
  • Certification Liaison

DO-254 V&V and CM Methods

  • Validation process
  • Verification Process
  • Validation and Verification Methods
  • Configuration Management
  • Configuration Management Activities
  • Data Control Categories
  • Process Assurance

DO-254 Hardware Design Life Cycle Data

  • Hardware Plans
  • Hardware Design Standards and Guidance
  • Validation and Verification Data
  • Hardware Acceptance Test Criteria
  • Problem Reports
  • Hardware Configuration Management Records
  • Hardware Process Assurance Records
  • Hardware Accomplishment Summary
  • Use of Previously Developed Hardware
  • Commercial-Off-The-Shelf (COTS) Components Usage
  • Product Service Experience
  • Tool Assessment and Qualification

Additional Considerations

  • Tool Qualification
  • Previously Developed HW
  • COTs Cores and IPs
  • Single Event Upset and SRAM parts
  • Functional Failure Path (FFP)
  • Elemental analysis
  • Advanced Verification techniques

DO-254 Data Items and Templates

  • Plan for Hardware Aspects of Certification (PHAC)
  • Hardware Design Plan
  • Hardware Validation Plan
  • Hardware Verification Plan (HVP)
  • Hardware Configuration Management Plan
  • Hardware Process Assurance Plan
  • Hardware Design Standards
  • Requirements Standards
  • Validation and Verification Standards
  • Hardware Archive Standards
  • Hardware Requirements
  • Conceptual Design Data
  • Detailed Design Data
  • Top-Level Drawing
  • Assembly Drawings
  • Installation Control Drawings
  • Hardware/Software Interface Data
  • Hardware Traceability Data
  • Hardware Review and Analysis Procedures
  • Hardware Review and Analysis Results
  • Hardware Test Procedures
  • Hardware Test Results
  • Hardware Acceptance Test Criteria
  • Problem Reports
  • Hardware Configuration Management Records
  • Hardware Process Assurance Records
  • Hardware Accomplishment Summary (HAS)

Wrap-up – DO-254 Training

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