Patent ID: 11873072
Assignee: THE BOEING COMPANY
Field: Control (Instruments)
Classification: CPC B  G | IPC B  G

Claim 5:
6. The method of claim 5, further comprising steps of:
based at least in part on a virtual overlay of the first three-dimensional profile of the aft pressure bulkhead and the second three-dimensional profile of the plurality of splice angles, determining an outline and a third surface profile for a shim to be positioned between the first interface surface of the aft pressure bulkhead and the second interface surface of a corresponding one of the plurality of splice angles;
determining third locations of a plurality of third holes to be drilled in the shim, wherein the plurality of third holes correspond to a portion of the plurality of first holes in the aft pressure bulkhead and the plurality of second holes in the corresponding one of the plurality of splice angles; and
drilling the plurality of third holes in the shim at the third locations.