FIELD: transport.
SUBSTANCE: proposed method comprises attaching main part 46 of engine attachment 6 on rigid pylon. Note here that said engine attachment 6 is preliminary mounted on the engine, main part of attachment being arranged nearby contact surface 72 of rigid structure and oriented forward and secured to said rigid stricture 10 with the help of shear pin 68 that passes through first primary bore 56 and second primary bore 58. Said bores are made in the attachment main part 46 and rigid structure 19, respectively. Attachment of main part 46 on rigid structure comprises the following stages. First, engine 2 is arranged relative to engine support 4 so that first primary bore 46 stays opposite second primary bore 58. Then pin 80 with convex centering head 82 is fitted in two primary bores 56, 58 so that said pin 80 fitted in two primary bores 56, 58, makes aforesaid shear pin.
EFFECT: simplified mounting of aircraft engine.
12 cl, 12 dwg
