FIELD: process engineering.
SUBSTANCE: set of invention relates to production of aircraft components. Drilling device 7, 15 may be encoded in drilling aircraft components. Proposed method comprises: locating drilling template with at least on drilled hole on component to be machined, locating drill bush 1 and fitting drilling device 7, 15 in template drilled hole. Drill bush 1 comprises coding device made up of bush 2 while drilling device incorporates coding coupling. Said coding coupling gets into engagement with said coding device.
EFFECT: higher precision.
4 cl, 3 dwg
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