Loads interface, particularly a loads interface for a plug type aircraft door

A loads interface, particularly a loads interface of an aircraft door, comprising:

• a background structure particularly a stiffened shell-like background structure, comprising a beam, an edge-frame component and a shell-like outer skin, preferably made from fiber reinforced plastics, said edge frame being adapted to and connected with said beam and said outer skin and
• a loads transferring flange adapted and mounted to at least said beam,
• wherein:
• said loads transferring flange is designed to transmit transverse forces and bending moments resulting from transferring said transverse forces in said loads transferring flange and/or designed to transmit circumferential and/or longitudinal forces and torsional/bending moments resulting from transferring said circumferential and/or longitudinal forces in said loads transferring flange,
• said loads transferring flange is provided with at least three angled flanges,
• said edge frame is provided with an edge frame transfer section interacting with an edge frame flange of said three flanges of said loads transferring flange,
• said beam is provided with at least one beam web transfer section interacting with at least one beam web flange of said three flanges of said loads transferring flange, and
• said outer skin is provided with an outer skin transfer section interacting with an outer skin flange of said three flanges of said loads transferring flange.