An aircraft wing configured to be fixed to and extend from an aircraft fuselage, the wing having a leading edge and a trailing edge; an aerodynamic control device attached to the trailing edge, and an input controller, wherein movement of the control device is subject to the input controller; a moveable aerodynamic hinge panel proximal to the aerodynamic control device, the hinge panel separately attached to the trailing edge; a bell crank mechanism configured to link movement of the moveable aerodynamic hinge panel directly to movement of the aerodynamic control device and including a center link, having opposed ends, pivotally connected to, but translationally fixed to, the trailing edge, for supporting only pivotal movement of the center link relative to the trailing edge, and a flap link connected to the aerodynamic control device, and a hinge panel link directly connetced to the moveable aerodynamic hinge panel, wherein the opposed ends of the center link are each pivotally coupled to one end of the flap and hinge panel links (166, 182) respectively via separate pivot couplings, and wherein the center link has three connecting joints (168, 172, 176) including a center pivot coupling positioned intermediately between the opposed ends of the center link, the center pivot coupling being fixed to the trailing edge for permitting the pivotal movement of the center link relative to the trailing edge, said links being serially coupled together, each link having a pivot coupling at each end configured to join each link to an adjacent link via one of the pivot couplings. an aerodynamic control device attached to the trailing edge, and an input controller, wherein movement of the control device is subject to the input controller; a moveable aerodynamic hinge panel proximal to the aerodynamic control device, the hinge panel separately attached to the trailing edge; a bell crank mechanism configured to link movement of the moveable aerodynamic hinge panel directly to movement of the aerodynamic control device and including a center link, having opposed ends, pivotally connected to, but translationally fixed to, the trailing edge, for supporting only pivotal movement of the center link relative to the trailing edge, and a flap link connected to the aerodynamic control device, and a hinge panel link directly connetced to the moveable aerodynamic hinge panel, wherein the opposed ends of the center link are each pivotally coupled to one end of the flap and hinge panel links (166, 182) respectively via separate pivot couplings, and wherein the center link has three connecting joints (168, 172, 176) including a center pivot coupling positioned intermediately between the opposed ends of the center link, the center pivot coupling being fixed to the trailing edge for permitting the pivotal movement of the center link relative to the trailing edge, said links being serially coupled together, each link having a pivot coupling at each end configured to join each link to an adjacent link via one of the pivot couplings. a center link, having opposed ends, pivotally connected to, but translationally fixed to, the trailing edge, for supporting only pivotal movement of the center link relative to the trailing edge, and a flap link connected to the aerodynamic control device, and a hinge panel link directly connetced to the moveable aerodynamic hinge panel, wherein the opposed ends of the center link are each pivotally coupled to one end of the flap and hinge panel links (166, 182) respectively via separate pivot couplings, and wherein the center link has three connecting joints (168, 172, 176) including a center pivot coupling positioned intermediately between the opposed ends of the center link, the center pivot coupling being fixed to the trailing edge for permitting the pivotal movement of the center link relative to the trailing edge, said links being serially coupled together, each link having a pivot coupling at each end configured to join each link to an adjacent link via one of the pivot couplings.