A mounting structure 300 for mounting a plinth fairing (400,fig.5) to a fuselage (100,fig.1) of an aircraft, the mounting structure comprising a plurality of lateral frames 310 comprising at least one pair of adjacent frames comprising a first lateral frame 311, and a second lateral frame 312; a plurality of intercostal ribs 320 comprising at least a first intercostal rib 321; wherein the at least one pair of adjacent lateral frames is configured to be attachable to the fuselage of the aircraft; and wherein the first intercostal rib is configured to be selectively removably attachable to the first lateral frame and the second lateral frame. Also disclosed is a kit including the mounting structure and plinth fairing as well as a method off attachment and reconfiguration.


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    Title :

    Customisable plinth for an aircraft



    Publication date :

    2025-05-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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