Provided is an aircraft lavatory unit installation method and an aircraft that are advantageous in increasing the number of seats. A body frame 28 of a lavatory unit 18 includes a front wall having an entrance 32 opened and closed off by a door 30, side walls on both sides, and a floor surface 2810. The outer surface of the side wall positioned closer to the front constitutes a wall 2802 facing backrests 2402 of a rear seat row 26 and extending in a latitudinal direction. The lavatory unit 18 is capable of being disposed at a front position P1 in which the wall 2802 is disposed behind and near the backrests 2402 of the seats 24 of the rear seat rows 26 with the backrests being in an upright position, and at a rear position P2 in which the wall 2802 is disposed behind and near the backrests 2402 of the rear seat rows 26 of the seats 24 with the backrests being in a reclining position.


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    Title :

    INSTALLATION METHOD FOR AIRPLANE LAVATORY UNIT, AND AIRPLANE


    Additional title:

    INSTALLATIONSVERFAHREN FÜR EINE FLUGZEUGTOILETTENEINHEIT UND ENTSPRECHENDES FLUGZEUG
    PROCÉDÉ D'INSTALLATION D'UNITÉ DE TOILETTES D'AVION ET AVION


    Contributors:

    Publication date :

    2020-05-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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