An assembly for connecting an engine to an aircraft, comprising: a first support configured to be structurally connected to the engine; a second support configured to be structurally connected to the aircraft; and a thrust link including: a load transferring member having opposed ends each connected to a respective one of the first and second supports (102, 105) for transferring engine thrust loads from the engine to the aircraft along a longitudinal axis of the load transferring member, the opposed ends having a fixed position relative to each other, and a tuned absorber coupled to the load transferring member intermediate the opposed ends, the tuned absorber tuned to absorb engine noise of at least one predetermined frequency; characterised in that: the tuned absorber has a damping member operatively coupled to the load transferring member and movable relative to the load transferring member at least along the longitudinal axis; and the damping member is disposed within a hollow portion of the load transferring member; wherein either: the hollow portion is filled with a viscous fluid operatively coupling the damping member to an inner surface of the load transferring member; or the tuned absorber further comprises a viscoelastic layer (118, 120) interconnecting the damping member and the load transferring member. a first support configured to be structurally connected to the engine; a second support configured to be structurally connected to the aircraft; and a thrust link including: a load transferring member having opposed ends each connected to a respective one of the first and second supports (102, 105) for transferring engine thrust loads from the engine to the aircraft along a longitudinal axis of the load transferring member, the opposed ends having a fixed position relative to each other, and a tuned absorber coupled to the load transferring member intermediate the opposed ends, the tuned absorber tuned to absorb engine noise of at least one predetermined frequency; characterised in that: the tuned absorber has a damping member operatively coupled to the load transferring member and movable relative to the load transferring member at least along the longitudinal axis; and the damping member is disposed within a hollow portion of the load transferring member; wherein either: the hollow portion is filled with a viscous fluid operatively coupling the damping member to an inner surface of the load transferring member; or the tuned absorber further comprises a viscoelastic layer (118, 120) interconnecting the damping member and the load transferring member. a load transferring member having opposed ends each connected to a respective one of the first and second supports (102, 105) for transferring engine thrust loads from the engine to the aircraft along a longitudinal axis of the load transferring member, the opposed ends having a fixed position relative to each other, and a tuned absorber coupled to the load transferring member intermediate the opposed ends, the tuned absorber tuned to absorb engine noise of at least one predetermined frequency; the tuned absorber has a damping member operatively coupled to the load transferring member and movable relative to the load transferring member at least along the longitudinal axis; and the damping member is disposed within a hollow portion of the load transferring member; wherein either: the hollow portion is filled with a viscous fluid operatively coupling the damping member to an inner surface of the load transferring member; or the tuned absorber further comprises a viscoelastic layer (118, 120) interconnecting the damping member and the load transferring member. the hollow portion is filled with a viscous fluid operatively coupling the damping member to an inner surface of the load transferring member; or the tuned absorber further comprises a viscoelastic layer (118, 120) interconnecting the damping member and the load transferring member.