Loads interface, particularly loads interface of an aircraft structure and application of said loads interface

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

• a grid-like structure preferably made from fiber reinforced plastics said grid-like structure comprising at least one edge member and one beam with said edge member being adapted to said beam and
• a loads transferring flange adapted and mounted to said edge member,
• wherein:
• said loads transferring flange is provided with an angled upper transfer plane and an angled lower transfer plane to transmit transverse forces and bending moments resulting from transferring said transverse forces in said loads transferring flange and/or 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 edge member is provided with at least one angled edge member's lower and/or upper transfer plane, said at least one angled edge member's lower and/or upper transfer plane being essentially parallel to one of the angled upper transfer plane or the angled lower transfer plane of said flange with said angled upper transfer plane and said angled lower transfer plane being respectively oriented to each other with an angle of approximately 90° and said grid-like structure comprising the at least one beam being oriented to said edge member with an angle of preferably 90°.