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A method of joining a wing to an aircraft fuselage by forming a series of pinned lug joints between a fuselage side and a wing side of a wing box structure. The joint forming process includes providing a single row of lugs on one side of the joint to be formed, and providing a respective double row

A method of joining a wing to an aircraft fuselage by forming a series of pinned lug joints between a fuselage side and a wing side of a wing box structure. The joint forming process includes providing a single row of lugs on one side of the joint to be formed, and providing a respective double row of lugs on the other side of the joint to be formed. A gap between opposing lugs of the double row varies along the row. The wing side and the fuselage side of the wing box structure are brought together such that the lugs of the single row are located within the respective gaps between opposing lugs of the double row, and the lugs are pinned to form the series of pinned lug joints. Also, a joint formed by the method.

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1. An aircraft wing-fuselage joint, comprising a series of pinned lug joints between a fuselage side and a wing side of a wing box structure, wherein a single row of lugs is provided on one side of the joint, and a respective double row of lugs is provided on the other side of the joint, and wherein

1. An aircraft wing-fuselage joint, comprising a series of pinned lug joints between a fuselage side and a wing side of a wing box structure, wherein a single row of lugs is provided on one side of the joint, and a respective double row of lugs is provided on the other side of the joint, and wherein a gap between opposing lugs of the double row varies along the row. 2. A joint according to claim 1, wherein the gap is varied along the row in dependence on the local wing geometry. 3. A joint according to claim 1, wherein the double row of lugs is provided on the fuselage side and the single row of lugs is provided on the wing side. 4. A joint according to claim 1, wherein the double row of lugs is of metal and the single row of lugs is of composite material. 5. A joint according to claim 1, wherein the lugs on the wing side are integrally formed with upper and/or lower wing covers of the wing. 6. A joint according to claim 1, wherein at least some of the lugs include eccentric bushes. 7. A joint according to claim 1, further comprising one or more tie rods between a wing rib and a wing cover or spar adjacent the pinned lug joints. 8. A method of joining a wing to an aircraft fuselage by forming a series of pinned lug joints between a fuselage side and a wing side of a wing box structure, the joint forming process including: providing a single row of lugs on one side of the joint to be formed, and providing a respective double row of lugs on the other side of the joint to be formed, wherein a gap between opposing lugs of the double row varies along the row;bringing the wing side and the fuselage side of the wing box structure together such that the lugs of the single row are located within the respective gaps between opposing lugs of the double row; andpinning the lugs to form the series of pinned lug joints. 9. A method according to claim 8, wherein the gap is varied along the row in dependence on the local wing geometry. 10. A method according to claim 8, wherein the double row of lugs is provided on the fuselage side and the single row of lugs is provided on the wing side. 11. A method according to claim 8, wherein the wing side and the fuselage side of the wing box structure are brought together by relative movement along a predetermined insertion vector. 12. A method according to claim 8, wherein around the circumference of the wing box structure on the other side of the joint to be formed, the double row of lugs is provided around a portion of the circumference and a first single row of lugs is provided around the remainder of the circumference. 13. A method according to claim 12, wherein after the step of bringing the wing side and the fuselage side of the wing box structure together, the method further comprises attaching a lug plate having a second single row of lugs adjacent the first single row of lugs such that the first and second single rows form a double row of lugs on the other side of the joint to be formed. 14. A method according to claim 8, wherein at least some of lugs include eccentric bushes, and the method further comprises rotating the eccentric bushes, where necessary, to align the lugs on each side of the joint prior to pinning. 15. A method according to claim 8, wherein the step of pinning the lugs comprises forming the series of pinned lug joints around the entire circumference of the wing box structure. 16. A method according to claim 8, further comprising connecting one or more tie rods between a wing rib and a wing cover or spar adjacent the pinned lug joints.