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đŤA monocoque structure uses its outer shell to support stresses and loads applied to it, whereas a semi-monocoque structure has an internal "skeleton" of supports and braces to keep its shape rigid and strong.
đŤThe vast majority of pressurized aircraft are semimonocoque to help distribute stresses equally along the fuselage during flight.
đŤHowever, some helicopters use monocoque structure to maximize internal space in the flight compartment.
đŤMonocoque fuselage has its skin holding the skeleton structure together while the semi-monocoque has both the skin and the skeleton holding together.
đŤSemi-monocoque also has "stringers" running horizontally down the plane to help hold the frame together.
đŤThe monocoque fuselage also cannot be used for airframes after a certain size (small aircraft with single engine), but the semi-monocoque has been used from single piston engines to commercial airliners.
đŤA monocoque design would also have a safety risk involved if the skin was damaged because it is the load-bearing structure.
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