| 摘要 |
The invention concerns a method to mount an aircraft engine on a rigid structure of an engine mount, comprising a securing step, on the structure, to secure an attachment body ( 46 ) for an engine attachment, this attachment body being intended to lie against a contact surface of the rigid structure oriented forwardly, and secured to this structure by at least one shear pin ( 68 ) passing through a first and a second primary orifice, the securing step of the body ( 46 ) comprising the following operations: pre-positioning the engine relative to the engine mount for the purpose of placing the first orifice opposite the second orifice; and inserting a pin fitted with a convex centering head through the two orifices, so that this pin forms the shear pin.
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