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Aircraft Modification – Structural Substantiation
Storage Pillar Installation
Static strength substantiation of dual storage pillars, shelf loads, and aircraft seat-track attachment systems
Aircraft
DHC-8-100
Installation
Interior
Analysis
Linear Static FEA; Principal Stress; Fastener Analysis; Rigid Body Analysis; Margin of Safety
Solver
Simcenter Nastran SOL 101 (SESTATIC)
Skills Demonstrated
FEM Idealization; Weight & CoG Estimation; Comparative Substantiation; Mesh Refinement; Fastener Modeling; FEA Verification
Engineering Tools
FEMAP; Simcenter Nastran; 3D-RBA
Certification Basis
FAR Part 25; FAR 25.321–25.351; FAR 25.341; FAR 25.561
Project Category
Aircraft Modification – Structural Substantiation