Patent ID: 8087608

Claim:
An arrangement configured to connect an evener bar of a thrust mount device, transferring thrust loads generated by an aircraft engine, onto a rigid structure of an engine mount, the arrangement comprising: a bracket configured to be fixedly mounted on the rigid structure and through which a first pin system passageway passes extending along a first longitudinal axis; and a pin system passing through the first pin system passageway, wherein the pin system is slidingly mounted in the first passageway so that the pin system can be moved along the first longitudinal axis in a first direction from a normal extended position in which the pin system projects sufficiently with respect to the bracket so that the pin system can cooperate with the evener bar, to a retracted position in which the pin system is retracted within the same bracket, and conversely in a second direction from the retracted position to the normal extended position; and wherein the arrangement further comprises a pin extending member carried internally by the pin system and configured to be moved parallel to the first longitudinal axis, in the second direction from a normal retracted position in which the pin extending member is retracted within the pin system, to an extended position in which the pin extending member is joined to the pin system and projects beyond the pin system, and conversely in the first direction from the extended position to the normal retracted position.