The invention provides an aircraft rear structure (10) comprising a substantially flat rear pressure bulkhead (11), with a first side and a second side, opposite to the first side. It also comprises a horizontal stabilizer (21) and a vertical stabilizer (1) which in turn comprises a first spar (2) and a second spar (3). The first spar (2) is attached to a first attachment zone (41) of the second side of the rear pressure bulkhead (11) by means of first attaching means (5, 6), and the second spar (3) is attached to a second attachment zone (42) of the second side of the rear pressure bulkhead (11) by means of second attaching means (7, 8). The second attachment zone (42) being different from the first attachment zone (41).


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    Titel :

    AIRCRAFT REAR STRUCTURE


    Weitere Titelangaben:

    FLUGZEUGHECKAUFBAU
    STRUCTURE ARRIÈRE D'AVION



    Erscheinungsdatum :

    2018-02-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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