Importance

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Abstract

A latch and keeper combination is utilized for securing a radome to an aircraft fuselage. The keeper has a keeper housing and an eyebolt member which extends toward the latch from the keeper housing. The latch has a pivoting handle member pivotally attached to a latch housing. A hook member depends from the handle member. Once the hook member is generally placed about the eye bolt, depressing the handle member further causes the hook to rotate within the latch housing. As the handle member is completely depressed, the hook member fully engages the eye bolt, while at the same time members axially extend from the latch to engage the keeper which provides a resistance to shear between the latch and keeper. The apparatus may also have a safety which prevents the handle from fully closing until the eye bolt is fully engaged by the hook member, thereby providing visual confirmation that the latch has completely engaged the keeper.

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First Claim