ACCESS DOOR ASSEMBLY FOR AN AIRCRAFT
    1.
    发明公开

    公开(公告)号:US20240262486A1

    公开(公告)日:2024-08-08

    申请号:US18428366

    申请日:2024-01-31

    CPC classification number: B64C1/1461

    Abstract: An access door assembly for a fuselage having a structure delimiting an access hatch, an upper part and a lower part of an access door, hinges fastened between the structure and the upper part in the vicinity of an upper edge, a guiding system between the lower part and the structure and guiding the lower part in translation, upper locks between the upper part and the lower part and/or the structure and lower locks between the lower part and the structure.

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