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 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 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 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 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 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 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 interconnecting the damping member and the load transferring member . <EOS>