FIELD: process engineering.
SUBSTANCE: invention relates to aircraft engineering, particularly, to assembly of aircraft fuselage. Fuselage sections are arranged so that their openings face each other. Connector with coordinate locking holes is secured to one of said sections to drill set of bores in fuselage section skin and/or said connector using drilling template and said coordinate locking holes.
EFFECT: simplified and shorter procedure.
7 cl, 1 dwg
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