Conjunto de panel carenado ala a cuerpo de un avión y método para la fabricación del mismo

Un conjunto de panel carenado de ala a cuerpo (30) de avión (10) para unir a un elemento de marco estructural (46) del avión (10), donde el conjunto (100) comprende: un primer elemento del panel (102a) que tiene al menos un primer borde no lineal de panel (122a); y, un segundo elemento del panel (102b) que tiene al menos un segundo borde no lineal de panel (122b), donde el segundo borde no lineal de panel (122b) se diseña para entrelazarse con el primer borde no lineal de panel (122a) para formar un conjunto de panel con cantos del panel entrelazados (108a, 108b) para unirse a una estructura (115). An access door assembly for joining to a structure. The access door assembly has an access door with at least one access door nonlinear edge, a support structure with at least one support structure nonlinear edge, and a doubler element attached to an interior side of the support structure. The support structure nonlinear edge is designed to interlace with the access door nonlinear edge to form an access door assembly for joining to a structure, the access door assembly having an interlaced nonlinear edge interface. A diameter of the doubler element of the access door assembly is preferably reduced as compared to a diameter of a doubler element of an access door assembly having a linear or circular edge, such that the reduced diameter preferably results in an overall reduced weight of the access door assembly and the structure to which the access door assembly is joined.