A control lever assembly (10) for controlling an aircraft system, comprising: a housing (30) having an outer side (33) and an aperture (35) defined by a rim (36); and a control lever (20) extending through the aperture (35) and movable in the aperture (35); the control lever (20) having an outer cover member (61) arranged to slide over the outer side (33) of the housing (30) and cover the rim (36) throughout the range of movement of the control lever (20).


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    Title :

    CONTROL LEVER ASSEMBLY FOR CONTROLLING AN AIRCRAFT SYSTEM


    Additional title:

    ASSEMBLAGE DE LEVIER DE COMMANDE POUR CONTROLER UN SYSTEME DE BORD D'AERONEF


    Contributors:

    Publication date :

    2023-03-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16J Kolben , PISTONS / B64C AEROPLANES , Flugzeuge



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