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
Duration: 2 days
Teaching method: Classroom training
Participation fee: 1.370,00€ p.P.
Training dates 2024:
- 12.06. - 13.06.2024 (München)
- 16.10. - 17.10.2024 (München)