FIELD: transport.
SUBSTANCE: proposed assembly 1, 100, 300 fastening turbojet 2 to aircraft stationary structure by fastening strut 5 comprises solid box covering turbojet blower case 3 on both sides of its lengthwise axis and equipped means 201 for attachment to the strut and engine attachment means 4 arranged at said box on both sides of turbojet lengthwise axis and designed for jointing with turbojet part intended for taking up forced acting thereat.
EFFECT: easier mounting and dismantling, better distribution of forced over box edges.
18 cl, 15 dwg
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