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Aircraft Modification – Structural Substantiation
Inertial Navigation and Surveying System Installation
Static strength substantiation of an inertial navigation system, mounting tray, support beams, and aircraft structural attachments
Aircraft
DHC-8-100
Installation
Exterior
Analysis
Classical Stress Analysis; Rigid Body Analysis; Beam Bending; Combined Stress; Fastener Analysis; Plastic Bending
Solver
N/A (Analytical)
Skills Demonstrated
Weight & CoG Estimation; Load Path Assessment; Rigid Body Analysis; Beam Analysis; Fastener Analysis; Margin of Safety
Engineering Tools
FEMAP; Excel
Certification Basis
FAR Part 25; FAR 25.321–25.351; FAR 25.341
Project Category
Aircraft Modification – Structural Substantiation