Designer Senior - Electrical System Design

SOGECLAIR•Wichita, KS

12d

About The Position

Lead the integration of mission systems on Bombardier aircraft, developing solutions that meet the specific requirements of Bombardier Defense customers. Identify deliverables, risks, and challenges during the bid and proposal phase, and create technical deliverables during active programs. Support design, integration, verification, certification, change management, and resolution of aircraft build or test issues in coordination with suppliers and internal customers. Demonstrate compliance with 14 CFR Part 25 FAA, TCCA, and EASA certification requirements.

Requirements

Bachelor of Science in Electrical or Aerospace Engineering, or equivalent.
Minimum of 5 years’ experience in electrical system design or a related field.
Working knowledge of FAA, TCCA, and EASA Part 25 certification requirements.
Working knowledge of system safety processes.
Familiarity with RTCA DO-160, DO-178, and DO-254 standards.
Proficiency with MS Office, including Word, Excel, PowerPoint, and Access.
Excellent written and verbal communication skills.
Interpersonal skills to establish and maintain effective working relationships with coworkers, employees, management, and suppliers.
Self-motivated, with the ability to coordinate multiple activities and manage time effectively.
Must be authorized to work in the US.

Nice To Haves

Experience with AutoCAD.

Responsibilities

Identify deliverables, risks, and challenges for proposed solutions during the bid and proposal phase.
Create active-program deliverables, including system schematics, supplier requirement documents, system descriptions, interface control documents, wiring diagrams, electrical load analyses, functional test requirements or test plans, qualification test plans, test reports, and design compliance reports.
Review installation drawings and qualification test data and reports.
Decompose internal or external customer statements of work into detailed requirements.
Analyze ground and flight test data to verify system performance and functionality.
Research component specifications to support component selection.
Support change management through research, concepts, design reviews, trade studies, impact analysis, and implementation.
Work with suppliers and internal customers to investigate, troubleshoot, and resolve aircraft build or test issues.
Support internal and external design reviews and program governance sessions.
Show compliance with 14 CFR Part 25 FAA, TCCA, and EASA certification requirements.