Design Assurance Guidance according to ED80/DO-254

for Airborne Electronic Hardware

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ED-80/DO-254 application is meanwhile required as an important qualification for the certification in civil aviation. This seminar deals with all aspects of applicability and contains a widespread overview of required activities and documents.

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Content

•  Overview regulations and standards​

  • Overview Safety Assessment according to ARP4754A

  • EASA CS 25 § 1309

  • EASA/FAA Electronic Hardware Development Assurance Requirements

• Failure Conditions - Design Assurance Level (HW DAL Level Definition)

• Status, overview and applicability of DO-254, and impact on implementation through EASA Certification Memoranda, EASA AMC20-152A and FAA AC20-152A.

• Hardware Design Life Cycle Processes

  • Hardware Planning Process  

  • Hardware Design Processes  

  • Supporting Processes

    • Validation and Verification Process

    • Configuration Management Process

    • Process Assurance Process  

    • Certification Liaison Process

• Additional Considerations

  • PLDs, FPGA, ASICs Development 

  • COTS and Complex Hardware (Microcontroller Classification and Selection) 

  • Product Service Experience 

  • Tool Assessment and Qualification​

• Design Assurance Considerations for Level A and B 

 

Interest group

• Hardware Engineers

• Projectmanager

• Quality assurance with experience on hardware-development

 

Fields

• Aviation (civil, military)

 

Information
Duration: 2 Days
Time: 08:30 - 17:00 h
Language: German, English
Participants: 3-12
Price: 1.370,00 €*
Early Bird: 1.250,00 €*

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* excl. VAT; Early Bird until 4 weeks before start of seminar, our general terms and conditions for seminars apply

 

Speakers

• Roger Plieske