Engineering Architect – Electrical Design
| Company | Airbus |
|---|---|
| Location | Grand Prairie, TX, USA |
| Salary | $Not Provided – $Not Provided |
| Type | Full-Time |
| Degrees | Bachelor’s |
| Experience Level | Senior |
Requirements
- Bachelor of Science in Electrical or Aeronautical Engineering (or equivalent technical degree and/or relevant experience)
- 7 (Seven) years in aircraft systems design, development, integration and/or certification
- Avionics and electrical system integration
- System Engineering understanding such as ARP 4754 and DO-160 requirements
- Airworthiness (identification of rules to be applied)
- Electrical Systems Integration (aircraft interfaces)
- Electrical harness design and manufacturing processes
- Electrical Wiring Diagram and wire-routing requirements understanding
- CAD design expertise and model-based design familiarity in alignment with industry standards and best methods (e.g. : CATIA-V5 and AutoCAD)
- High quality engineering drawing development capabilities based on industry standards
- Digital literacy
- Avionics environmental qualification requirements and limitations
- Avionics systems layout requirements and considerations
- Antenna location and installation requirements
- Understanding of integration and interface requirements of externally mounted equipment such has lighting, cameras, floats, hoists, cargo hooks, etc.
- US Person under ITAR definition (U.S. Citizen, green card holder or person covered under our existing ITAR license
- Ability to communicate effectively in verbal and written form in English
Responsibilities
- Design, develop, and review technical documents and engineering models and drawings needed to integrate avionics and electrical equipment, and their associated interfaces
- Present and communicate modifications and aircraft configuration(s) during design reviews and other required presentations
- Develop Electrical (wiring and routing) drawings and wiring requirements (including considerations of EMI/EMC requirements, antenna location, separation requirements, maintainability, etc.)
- Produce substantiation reports such as Electrical Load Analysis, and others as assigned
- Create and/or review Installation Instructions and Instructions for Continued Airworthiness
- Develop and coordinate Technical Publications
- Provide liaison support as required for support of aircraft integration and conformity efforts (suppliers, planning, industry, quality, etc.)
- Define System/Integration layout in accordance with requirements as elaborated during offer or architecture phases to meet customer, airworthiness, general engineering standards, and company requirements
- Design layout of aircraft modifications, zonal allocations, and weight & CG impact in relevant completions and STC projects
- Design, integrate and substantiate the defined solutions
- Validate design solutions by implementing simulation, 3D modeling, predictive tools, etc.
- Support the development of certification packages including certification plans, compliance checklists, and conformity inspection plans
- Coordinate with FAA DERs and ODA Unit Members in support of certification requirements
Preferred Qualifications
-
No preferred qualifications provided.