A latch mechanism (120; 220) is disclosed. In various embodiments, the latch mechanism (120; 220) includes a T-bolt body (230) and a T-bolt (238) comprising a longitudinal rod (262) extending in a longitudinal direction from the T-bolt body (230) and a transverse rod (264) disposed at an end of the longitudinal rod (262). A safety keeper (240; 340) defining a load slot (260) may be configured to receive the transverse rod (264) whereby the T-bolt (238) is configured to secure the T-bolt body (230) with respect to the safety keeper (240; 340).


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    Title :

    AIRCRAFT SAFETY KEEPER FOR LATCH UTILIZATION


    Additional title:

    FLUGZEUGSICHERHEITSHALTER ZUR VERRIEGELUNGSVERWENDUNG
    DISPOSITIF DE MAINTIEN DE SÉCURITÉ D'AÉRONEF POUR L'UTILISATION DE VERROU


    Contributors:

    Publication date :

    2023-11-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / E05C Riegel oder Feststellvorrichtungen für Flügel, insbesondere für Türen oder Fenster , BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS



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