FIELD: technological processes.
SUBSTANCE: invention refers to the method for connecting of aircraft structural units and concerns the connection of the fuselage casing to the fuselage bearing structure. In order to connect the parts between themselves, it is necessary to place and temporarily clamp the parts and drill a number of guide holes through the temporarily clamped parts. Then the temporary locks are mounted into the number of guide holes. In this case, the temporary locks are removed by means of drilling and subsequent installation of permanent locks into them.
EFFECT: time of connecting the parts together is shortened.
8 cl, 3 dwg
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