| CPC B64D 29/06 (2013.01) [F16B 5/06 (2013.01)] | 19 Claims |

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1. An apparatus for an aircraft, comprising:
a latch including a handle, a hook structure and a linkage system operatively coupling the handle to the hook structure, the linkage system including a mounting link, a handle link, a handle pivot member and an inter-link pivot member; and
a latch mount pivot member received within a link aperture in the mounting link;
the hook structure including a hook, a structure aperture and a structure slot located longitudinally between the hook and the structure aperture;
the handle link pivotally connected to the handle;
the handle pivot member received within the structure aperture, and the handle pivot member pivotally connecting the handle to the hook structure;
the inter-link pivot member received within the structure slot, and the inter-link pivot member pivotally connecting the mounting link and the handle link to the hook structure;
the latch mount pivot member extending laterally across a channel in the hook structure when the latch is in a latched position; and
the latch mount pivot member disposed outside of the channel in the hook structure when the latch is in an unlatched position.
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