Abstract: The invention relates to a device for connecting parts of an aircraft engine. The connection device comprises connectors suitable for connecting a first and a second part so as to establish a physical transfer link between these parts and means which enable it to monitor the state of the connection in particular by means of an impedance measurement carried out in a circuit formed by components integrated into said connectors.

Abstract: The invention relates to an assembly for the removal, transportation and maintenance of an aircraft turbine engine (10) on a maintenance trolley (34), comprising a turbine engine (10) comprising an upper means (14) for attaching the housing (16) of the turbine engine (10) to the aircraft and a first lower means (20) dedicated to transportation for attaching the housing (16) of the turbine engine (10), a maintenance trolley (34), and a member (32) comprising a means for attaching said member (34) to the housing (16) and at least one means for support and articulation of said member (32) and of the turbine engine (10) on the trolley (34), allowing the turbine engine (10) to pivot to the vertical; characterised in that the member comprises a first attachment means designed to engage with the upper means (14), a second attachment means designed to engage with the first lower means (20), and a pivot means forming the support and articulation means engaging with a complementary receiving means (44) of the trolley (

Abstract: The invention relates to an assembly for the removal, transportation and maintenance of an aircraft turbine engine (10) on a maintenance trolley (34), comprising a turbine engine (10) comprising an upper means (14) for attaching the housing (16) of the turbine engine (10) to the aircraft and a first lower means (20) dedicated to transportation for attaching the housing (16) of the turbine engine (10), a maintenance trolley (34), and a member (32) comprising a means for attaching said member (34) to the housing (16) and at least one means for support and articulation of said member (32) and of the turbine engine (10) on the trolley (34), allowing the turbine engine (10) to pivot to the vertical; characterised in that the member comprises a first attachment means designed to engage with the upper means (14), a second attachment means designed to engage with the first lower means (20), and a pivot means forming the support and articulation means engaging with a complementary receiving means (44) of the trolle