The invention relates to a cabin system for an aircraft fuselage, having one or more lining components for interior lining, and optionally one or more cabin equipment components, wherein the lining component can be installed either separately or in combination with a further lining component and/or a cabin equipment component under tension in the aircraft fuselage such that a cabin that is under tension in the circumferential direction and attaches to the aircraft fuselage is defined. In this manner a passenger cabin configured as a closed safety cell is created in a fuselage, which is of particular advantage in an aircraft fuselage made of a fiber composite material because no splinters or the like can penetrate the self-supporting passenger cabin in case of damage to the same.
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