A reinforced door for an aircraft includes a frame and a network of harnesses. The frame includes components. The network of harnesses links a majority of the components and reinforces the frame. The harnesses are laid out onto the frame and linked to one another to form a webbing.

 
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< Local backup hydraulic actuator for aircraft control systems

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> Pivoted flap mechanism for adjusting an aerodynamic pivoted flap associated with a wing
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