Patent ID: 9056685
Filing Date: 2015-06-16
Classification: B64D,B64F,Y10T

Abstract:
1. A method for mounting interior components in an aircraft, comprising: preassembling a first interior component, preassembling a second interior component, fastening at least one of the first and the second interior component to an assembly apparatus and connecting the first and the second interior component together to form an individual module, connecting together a plurality of individual modules fastened to the assembly apparatus to form a large module fastened to the assembly apparatus, connecting together a plurality of large modules fastened to the assembly apparatus to form a cabin structure fastened to the assembly apparatus, testing at least one of the cabin structure fastened to the assembly apparatus, one or more of the plurality of individual modules fastened to the assembly apparatus, and one or more of the plurality of large modules fastened to the assembly apparatus, after the testing, separating from one another each of the plurality of large modules that form the cabin structure, and individually, for each of the separated plurality of large modules,