| 摘要 |
PROBLEM TO BE SOLVED: To provide an aircraft capable of reducing an effect to a load transmission system of a primary structure related to a main wing regarding the support of a fairing to the main wing of the aircraft.SOLUTION: An aircraft is provided with a center fairing 22 with which at least a lower surface of a center part of a main wing is covered. A seal 29 is inserted between both edges 28 in a lateral direction of the fairing 22 and a lower surface 14A of an outer wing 14. An outermost broadside fitting 27located on the outermost broadside and an outer wing fitting 17disposed on the outer wing 14, of fittings 27 disposed on the fairing 22 are combined via pins P1, P2 along the longitudinal direction and the outer wing fitting 17is combined with the outer wing 14 on the inner broadside than the edge 28 and besides a position of a splice plate 16 which joins the center wing 13 to the outer wing 14.SELECTED DRAWING: Figure 5 |
