An apparatus is provided for an aircraft. This apparatus includes a latch. The latch includes a handle, a hook structure and a linkage system operatively coupling the handle to the hook structure. The linkage system includes a back link, a center link, a back link pivot member and a center link pivot member. The hook structure includes a hook, a structure aperture and a structure slot located longitudinally between the hook and the structure aperture. The back link is pivotally coupled to the center link. The back link pivot member is received within the structure aperture and pivotally couples the back link to the hook structure. The center link pivot member is received within the structure slot and pivotally couples the handle and the center link together and to the hook structure.


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    Title :

    LONG THROW LATCH FOR AIRCRAFT SYSTEM


    Contributors:

    Publication date :

    2024-10-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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