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

Claim 19:
20. The method of claim 18, further comprising:
mating the second interface surface of each one of the plurality of splice angles on a corresponding portion of the first interface surface of the aft pressure bulkhead such that the plurality of second holes in each one of the plurality of splice angles is aligned with the plurality of first holes in the aft pressure bulkhead;
positioning the shim between the second interface surface of a corresponding one of the plurality of splice angles and the first interface surface of the aft pressure bulkhead such that the plurality of third holes in the shim are aligned with 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
installing fasteners through the plurality of first holes in the aft pressure bulkhead, the plurality of third holes in the shim and the plurality of second holes in the corresponding one of the plurality of splice angles to secure the shim and the corresponding one of the plurality of splice angles to the aft pressure bulkhead.