A method for installing a preassembled internal fitting component of an aircraft, at least one luggage compartment being attached in an articulated manner to a fixing means and beside a ceiling lining and, optionally, a service unit being attached in an articulated manner to the luggage compartment and, likewise optionally, a covering element being attached in an articulated manner to the service unit. Following transport of the preassembled internal fitting component into a final mounting position, the individual elements of the internal fitting component can be mounted in the aircraft one after another by folding out and mounting. Also, a corresponding internal fitting component and to a system for mounting internal fitting components with a mobile mounting device.
METHOD FOR INSTALLING AN INTERIOR FITTING COMPONENT OF AN AIRCRAFT, INTERIOR FITTING COMPONENT FOR AN AIRCRAFT AND SYSTEM FOR MOUNTING INTERIOR FITTING COMPONENTS
2020-03-05
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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