Rapid attachment for a movable flap module of an aircraft wing

A method for manufacturing a connecting part between a wing box and a leading edge module, the method comprising the steps:

• performing a three-dimensional scan of a first representative part of the wing box to obtain a first computer model,
• performing a three-dimensional scan of a second representative part of the leading edge module in order to obtain a second computer model,
• the first part comprising a first reference region and a first connecting region, the second part comprising a second reference region and a second connecting region,
• defining a relative position of the first reference region with respect to the second reference region,
• from the first and second computer model, configuring the connecting part to provide a connection between the first and the second connecting region such that the first and the second reference region are located in said relative position,
• manufacturing the connecting part,
• the connecting part comprising an eccentric guide ring and
• the step of configuring the connecting part to provide a connection between the first and the second connecting region comprises adjusting at least one eccentricity of the ring to coincide an exterior of the ring with a first aperture and an interior of the ring with a second aperture, the first and second aperture being located in the connecting region.