摘要 |
The tool has a support body (7) having an inverted U-shape and defining a horizontal beam (70) and two vertical branches (71, 72). Two fixing arms (81, 82) are attached to a high pressure module of a turbojet of an aircraft, where the fixing arms are connected to the vertical branches of the support body by a pivot joint (9), so as to allow rotation of the high pressure module about a horizontal rotation axis (V) between the branches of the support body. The socket body includes a fixing ring (73) for connection to a traction chain. |