A turbine engine assembly, comprising: a turbine engine case; a gearbox; and a plurality of mounts connecting the gearbox to the case, each of the mounts comprising: a linkage (162, 164, 178, 180, 182, 184) extending towards the case substantially in a first direction; and a fuse joint configured to substantially prevent movement between the gearbox and the case when the fuse joint is subject to loading less than a threshold, and to permit a constrained movement between the gearbox and the case when the loading is greater than the threshold; wherein the fuse joint of a first of the mounts has a different configuration than the fuse joint of a second of the mounts; characterised in that said turbine engine assembly further comprises: a bracket comprising a first aperture and a second aperture, wherein the linkage (162, 164, 178, 180, 182, 184) of the first of the mounts comprises a third aperture and a fourth aperture; the fuse joint of the first of the mounts comprises a first fastener and a second fastener; the first fastener extends into the first and the third apertures, and has a diameter that is substantially equal to diameters of the first and the third apertures; and the second fastener extends into the second and the fourth apertures, and has a diameter that is less than at least one of a diameter of the second aperture and a diameter of the fourth aperture. a turbine engine case; a gearbox; and a plurality of mounts connecting the gearbox to the case, each of the mounts comprising: a linkage (162, 164, 178, 180, 182, 184) extending towards the case substantially in a first direction; and a fuse joint configured to substantially prevent movement between the gearbox and the case when the fuse joint is subject to loading less than a threshold, and to permit a constrained movement between the gearbox and the case when the loading is greater than the threshold; wherein the fuse joint of a first of the mounts has a different configuration than the fuse joint of a second of the mounts; characterised in that said turbine engine assembly further comprises: a bracket comprising a first aperture and a second aperture, wherein the linkage (162, 164, 178, 180, 182, 184) of the first of the mounts comprises a third aperture and a fourth aperture; the fuse joint of the first of the mounts comprises a first fastener and a second fastener; the first fastener extends into the first and the third apertures, and has a diameter that is substantially equal to diameters of the first and the third apertures; and the second fastener extends into the second and the fourth apertures, and has a diameter that is less than at least one of a diameter of the second aperture and a diameter of the fourth aperture. a linkage (162, 164, 178, 180, 182, 184) extending towards the case substantially in a first direction; and a fuse joint configured to substantially prevent movement between the gearbox and the case when the fuse joint is subject to loading less than a threshold, and to permit a constrained movement between the gearbox and the case when the loading is greater than the threshold; wherein the fuse joint of a first of the mounts has a different configuration than the fuse joint of a second of the mounts; characterised in that said turbine engine assembly further comprises: a bracket comprising a first aperture and a second aperture, wherein the linkage (162, 164, 178, 180, 182, 184) of the first of the mounts comprises a third aperture and a fourth aperture; the fuse joint of the first of the mounts comprises a first fastener and a second fastener; the first fastener extends into the first and the third apertures, and has a diameter that is substantially equal to diameters of the first and the third apertures; and the second fastener extends into the second and the fourth apertures, and has a diameter that is less than at least one of a diameter of the second aperture and a diameter of the fourth aperture. a bracket comprising a first aperture and a second aperture, wherein the linkage (162, 164, 178, 180, 182, 184) of the first of the mounts comprises a third aperture and a fourth aperture; the fuse joint of the first of the mounts comprises a first fastener and a second fastener; the first fastener extends into the first and the third apertures, and has a diameter that is substantially equal to diameters of the first and the third apertures; and the second fastener extends into the second and the fourth apertures, and has a diameter that is less than at least one of a diameter of the second aperture and a diameter of the fourth aperture.