Integration of airframe structure & system per FAA requirements:

• Engineering review of 3D model of all structure & system design for integration criteria including system separation, clash analysis etc.
• Lead the offboard workflow meeting to review design & coordinate with Manufacturing, Quality, M&P and Stress.
• Responsible for issue creation in GBMS against released design, which will turn into CR for change management team.
• Checking & approving design workflows (PDR & CDR) for all system and structure with consideration of FAA requirements.
• Define the system to system & system to structure interface during the CDR phase.