NCAA CPL Aircraft General Knowledge Practice Questions - NCAA CPL Aircraft General Knowledge (Nigeria) Exam

In a semi-monocoque fuselage design, which structural components primary absorb the longitudinal bending loads?

Longerons and stringers combined with the skin Formers and bulkheads only Skin panels exclusively Internal drag wires and tubular struts

Correct Answer:

Longerons and stringers combined with the skin

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