Abstract: A fastening system for suspended installation of stowage compartments, in particular in aircraft, includes a first fastening element, which fastens on a supporting structure, a second fastening element, which fastens on a stowage compartment, and a connecting arrangement, configured for surface-area fastening on the first fastening element. The connecting arrangement and the second fastening element each include a supporting eyelet for accommodating a fastening bolt, to fasten the connecting arrangement on the second fastening element.

Abstract: A fastening system for suspended installation of stowage compartments, in particular in aircraft, includes a first fastening element, which fastens on a supporting structure, a second fastening element, which fastens on a stowage compartment, and a connecting arrangement, configured for surface-area fastening on the first fastening element. The connecting arrangement and the second fastening element each include a supporting eyelet for accommodating a fastening bolt, to fasten the connecting arrangement on the second fastening element.

Abstract: A device for fixing cabin side wall and cabin light paneling to a structural component of an aircraft and spacecraft includes: a structure holding component; and a cabin side wall holding component. The structure holding component has a surface for fixing the holding component to the structural component, and an adjustable surface for fixing the side wall holding component. The side wall holding component has an intermediate bracket and a side wall receiver for fixing cabin side wall paneling. The intermediate bracket is arranged between the adjustable fixing surface and the side wall receiver. The intermediate bracket has an intermediate guide element which guides the intermediate bracket, and the side wall receiver has a receiver guide element which guides the side wall receiver. The intermediate bracket has a fixing element for locking the intermediate bracket, and the side wall receiver has a fixing element for locking the side wall receiver.

Abstract: A device for fixing cabin side wall and cabin light paneling to a structural component of an aircraft and spacecraft includes: a structure holding component; and a cabin side wall holding component. The structure holding component has a surface for fixing the holding component to the structural component, and an adjustable surface for fixing the side wall holding component. The side wall holding component has an intermediate bracket and a side wall receiver for fixing cabin side wall paneling. The intermediate bracket is arranged between the adjustable fixing surface and the side wall receiver. The intermediate bracket has an intermediate guide element which guides the intermediate bracket, and the side wall receiver has a receiver guide element which guides the side wall receiver. The intermediate bracket has a fixing element for locking the intermediate bracket, and the side wall receiver has a fixing element for locking the side wall receiver.