FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly to aircraft engine stub design. Proposed stub comprises engine suspension rear assembly 8 comprising rear suspension housing 54 and first safety pin arranged to transfer forces acting in crosswise direction (Y) of the stub. Note here that said first safety pin 66 pass through lower spar 20 and includes lower end 70 that enters rear suspension assembly housing 54. Lower end 70 of the first safety pin has bore 76 for first cotter 74 to pass through. Said cotter passes also through rear suspension housing 54.
EFFECT: simplified design reduced weight.
11 cl, 6 dwg
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