FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely to aircraft engine suspension assembly. Proposed suspension assembly (6) to be mounted between engine (2) and attachment bar (4) comprises coupling (20) jointed to first attachment device (34) that includes fork support (36) furnished with two eyes (36a, 36b), and pin (44) passing through said coupling (20) and both eyes (36a, 36b). Each eye comprises hole (48a, 48b) furnished with first sleeve (50) and second sleeve (60) receiving said pin, respectively. Second sleeve (50) comprises bottom (54) forming trust element for first end (44a) of said pin (44), while first attachment device (34) comprises additionally appliances (64) to inhibit translation of the pin that interact with second end (44b) of pin (44).
EFFECT: simplified mounting.
20 cl, 5 dwg
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