Design Assurance Guidance nach ED80/DO-254

For Airborne Electronic Hardware

The application of ED80/DO-254 is now required as an important requirement for certification in civil aviation. This seminar highlights all aspects of applicability and contains a comprehensive overview of the required activities and documents.

Training category: Aviation

Target group: The training is aimed at hardware engineers, project managers and quality assurance staff with experience in hardware development.

Content:

Overview of regulations and standards
- Overview of 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 by 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 (classification and selection of microcontrollers)
- Product service experience
- Tool evaluation and qualification
Design assurance considerations for Level A and B