Abstract: An adapting part is designed to be held on a casing of a turbo-engine, partially covering the casing. The adapting part includes, in the extension of one of its axial ends, a first connector to engage with a first complementary connector associated with the casing to form a sliding connection. The adapting part also includes, at its other axial end, a second connector to be secured to a second complementary connector associated with the casing to form a rigid connection.

Abstract: A method for mounting an aircraft engine on a pylon includes positioning at least a first shear pin either in a first opening provided in a front engine fastener which is previously attached to the engine using connecting rods, or in a first bore provided in a front surface of the pylon; prepositioning the assembly including the engine and the front engine fastener relative to the pylon by placing the first shear pin opposite a receiving cavity, the receiving cavity being either the first bore, if the first shear pin has been positioned in the first opening, or the first opening, if the first shear pin has been positioned in the first bore; and inserting the first shear pin into the receiving cavity.

Abstract: Ball joint device for suspending a turbine engine from a pylon or suspending equipment on the body of the turbine engine, comprising a connecting rod, one end of which bears a ball and which is inserted between the two lugs of a clevis, the ball having a boring for the passage of a spindle having an axial boring for mounting a screw for clamping and axial locking the ball, the ball being axially locked by clamping between a bushing and a ring which carries removable means for axially retaining the ring with respect to the clevis during an operation of dismantling the device.

Abstract: Ball joint device for suspending a turbine engine from a pylon or suspending equipment on the body of the turbine engine, comprising a connecting rod, one end of which bears a ball and which is inserted between the two lugs of a clevis, the ball having a boring for the passage of a spindle having an axial boring for mounting a screw for clamping and axial locking the ball, the ball being axially locked by clamping between a bushing and a ring which carries removable means for axially retaining the ring with respect to the clevis during an operation of dismantling the device.

Abstract: An adapting part is designed to be held on a casing of a turbo-engine, partially covering the casing. The adapting part includes, in the extension of one of its axial ends, a first connector to engage with a first complementary connector associated with the casing to form a sliding connection. The adapting part also includes, at its other axial end, a second connector to be secured to a second complementary connector associated with the casing to form a rigid connection.

Abstract: A method for mounting an aircraft engine on a pylon includes positioning at least a first shear pin either in a first opening provided in a front engine fastener which is previously attached to the engine using connecting rods, or in a first bore provided in a front surface of the pylon; prepositioning the assembly including the engine and the front engine fastener relative to the pylon by placing the first shear pin opposite a receiving cavity, the receiving cavity being either the first bore, if the first shear pin has been positioned in the first opening, or the first opening, if the first shear pin has been positioned in the first bore; and inserting the first shear pin into the receiving cavity.