CAA NZ AME Aeroplanes 1 (Subject 4) Practice Questions - CAA NZ AME Licence Exam - Aeroplanes 1 (Subject 4, New Zealand) Exam

What is the primary function of a sandwich panel honeycomb core in composite aircraft structures?

To provide high shear strength and keep the outer face sheets at a fixed distance while keeping weight low To absorb fuel in wet-wing storage compartments To conduct electrical grounding currents across composite panels To eliminate the need for surface resin priming prior to painting

Correct Answer:

To provide high shear strength and keep the outer face sheets at a fixed distance while keeping weight low

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