| 摘要 |
The present invention relates to a method for coding a drilling device for an aircraft. The method comprises: placing a drilling template with at least a drilling hole on a work piece; placing a drilling bushing in the drilling hole of the drilling template; placing the drilling device in the drilling hole of the drilling template; wherein the drilling bushing comprises a coding master device, in particular a bushing edge; wherein the drilling device comprises a coding sleeve device and wherein the coding sleeve device is adapted for engaging with the coding master device.
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