Senior FEA Structural Engineer (Nastran/Patran) – Hybrid, Unlimited PTO

Panasonic Corporation of North America; Lake Forest (CA); Hybrid; USD 119.000 - 200.000; Vollzeit

Benefits dieser Stelle

Flexible-hybrid work opportunities

Unlimited PTO

Competitive benefits

Zusammenfassung

Panasonic Avionics Corporation is seeking an experienced engineer to support certification and installation of In-Flight Entertainment systems. You will manage certification-related issues, prepare technical documentation, and coordinate testing across multiple departments.

Responsibilities include FEM analysis, stress/interface loads reporting, and ensuring compliance with FAA/EASA and OEM requirements. Occasional travel up to 15% is expected as part of cross-functional collaboration.

Qualifikationen

• BS in Mechanical Engineering, Aerospace Engineering, Electrical Engineering, Industrial Engineering, System Engineering, Civil, Physics, Materials Science or equivalent degree.
• Masters preferred.
• 8+ years of experience in certification process.
• 9 years in In-Flight Entertainment related field.

Aufgaben

• Create a Finite Element Model in PATRAN/NASTRAN for aerospace components and run standard analyses.
• Prepare Stress/Interface Loads/StaticVibration reports and validate FEM results.
• Coordinate with Electrical, Mechanical, and Manufacturing teams to ensure FAA/EASA/ OEM compliance.
• Support certification and installation of IFE systems by managing issues and documenting test results.

Kenntnisse

FEM modeling

Structural analysis

Technical communication

Certification experience

Boeing/Airbus/Bombardier certs

Ausbildung

BS in Mechanical/Aerospace/EE/Industrial or related

Masters preferred

Tools

PATRAN

NASTRAN

Jobbeschreibung

Panasonic Avionics Corporation is seeking an experienced engineer to support certification and installation of In-Flight Entertainment systems. You will manage certification-related issues, prepare technical documentation, and coordinate testing across multiple departments.

Responsibilities include FEM analysis, stress/interface loads reporting, and ensuring compliance with FAA/EASA and OEM requirements. Occasional travel up to 15% is expected as part of cross-functional collaboration.