Abstract: An assembly for an aircraft. The assembly comprises a frame, an instrument panel fixed to the frame, a support system with an arm bearing a tray in which the arm positions the tray behind the instrument panel, and in which the tray comprises a first attachment arrangement, and a support comprising a second attachment arrangement which cooperates with the first attachment arrangement to removably fix the support onto the tray. The support also comprises a fixing system which ensures the removable fixing of a touch tablet onto the support. With such an assembly, the touch tablet is held without the aid of the pilot and it is positioned in front of him or her for easy access.

Abstract: An aircraft fuselage portion extending in a general longitudinal direction and comprising a fuselage structure comprising annular frames and a flat floor. The fuselage portion also comprises struts perpendicular to the floor in a nominal position and extending from the floor to a frame. Each strut comprises, in the vicinity of at least one of the ends thereof, a detachable link so that the strut can be moved relative to the fuselage structure or separated from the fuselage structure to temporarily grant access to a triangle area located between the frames, the floor and the struts in the nominal position. This allows access to be granted to the area in which the ducts must be installed in the aircraft, in particular, in the form of sets of ducts assembled prior to their installation in the fuselage.

Abstract: An aircraft duct assembly comprising at least two ducts extending along a general direction of rectilinear extent, each duct being an electrical, hydraulic or aeraulic duct connected to a duct support. The duct support comprises a first slideway element configured to cooperate with a second slideway element to form a slideway in the general direction of extent of the ducts. The duct assembly can thus be inserted, after mounting, by translation along the direction of the slideway into an aircraft fuselage portion. The mounting of the duct assembly and installation thereof in a fuselage are simplified, and the duct assembly is more reliable.

Abstract: An assembly for an aircraft. The assembly comprises a frame, an instrument panel fixed to the frame, a support system with an arm bearing a tray in which the arm positions the tray behind the instrument panel, and in which the tray comprises a first attachment arrangement, and a support comprising a second attachment arrangement which cooperates with the first attachment arrangement to removably fix the support onto the tray. The support also comprises a fixing system which ensures the removable fixing of a touch tablet onto the support. With such an assembly, the touch tablet is held without the aid of the pilot and it is positioned in front of him or her for easy access.

Abstract: An aircraft fuselage portion extending in a general longitudinal direction and comprising a fuselage structure comprising annular frames and a flat floor. The fuselage portion also comprises struts perpendicular to the floor in a nominal position and extending from the floor to a frame. Each strut comprises, in the vicinity of at least one of the ends thereof, a detachable link so that the strut can be moved relative to the fuselage structure or separated from the fuselage structure to temporarily grant access to a triangle area located between the frames, the floor and the struts in the nominal position. This allows access to be granted to the area in which the ducts must be installed in the aircraft, in particular, in the form of sets of ducts assembled prior to their installation in the fuselage.

Abstract: An aircraft duct assembly comprising at least two ducts extending along a general direction of rectilinear extent, each duct being an electrical, hydraulic or aeraulic duct connected to a duct support. The duct support comprises a first slideway element configured to cooperate with a second slideway element to form a slideway in the general direction of extent of the ducts. The duct assembly can thus be inserted, after mounting, by translation along the direction of the slideway into an aircraft fuselage portion. The mounting of the duct assembly and installation thereof in a fuselage are simplified, and the duct assembly is more reliable.