| CPC B64C 25/16 (2013.01) [B64C 1/18 (2013.01); B64C 25/04 (2013.01); B64C 25/14 (2013.01)] | 7 Claims |

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1. A structural assembly for an aircraft having a longitudinal direction and a median plane, the structural assembly comprising:
a plurality of pairs of main gantries, wherein, for a pair, the main gantries face one another with respect to the median plane and wherein the pairs are distributed in the longitudinal direction;
two transverse panels that are perpendicular to the longitudinal direction and are fixed to a front and a rear of the plurality of pairs of main gantries to together define a compartment for a landing gear of the aircraft;
at least one pair of secondary gantries which extend parallel to the longitudinal direction between the main gantries and ends of which are fixed to the transverse panels;
at least one crossmember which extends parallel to the transverse panels and is disposed straddling at least one secondary gantry; and
for each secondary gantry and each crossmember straddling the secondary gantry, a connecting rod mounted to be able to freely rotate, via a first end, on a lower part of the crossmember and, via a second end, on an outer lateral part of the secondary gantry;
wherein at least one of the connecting rods is inclined at a non-zero angle relative to a vertical direction.
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