A latch indication assembly includes a latch (120) and an indicator assembly (130). The latch (120) is movable between a locked position and an unlocked position, and is configured to secure a fan cowl (102) of an aircraft. The indicator assembly (130) is operably coupled to the latch (120), and includes an indicator (132) movable between an open position (134) and a closed position responsive to movement of the latch. The indicator extends from an exterior of the fan cowl when in the open position, and is visible from an exterior position proximate at least one of a side or an underside of the aircraft when in the open position. The indicator assembly extends to the open position when the latch is in the unlocked position, and is configured to be retractable to the closed position when the latch is in the locked position.


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    Title :

    APPARATUSES AND METHODS FOR COWL LATCH INDICATION


    Additional title:

    VORRICHTUNGEN UND VERFAHREN ZUR HAUBENEINRASTANZEIGE
    APPAREILS ET PROCÉDÉS D'INDICATION DE VERROUILLAGE DE CAPOT



    Publication date :

    2019-09-25


    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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