Patent ID: 11958610
Assignee: SAFRAN CABIN INC.
Field: Transport (Mechanical engineering)
Classification: CPC B  Y | IPC B

Claim 5:
6. A method comprising the steps of:
removing a first galley monument assembly from an aircraft interior, the first galley monument assembly including a first outer wall and at least first and second standard insert spaces, wherein the first standard insert space is defined between a first vertical divider and a second vertical divider, wherein the second standard insert space is defined between the second vertical divider and a third vertical divider, wherein the first standard insert space defines a first width, and wherein the second standard insert space defines a second width, wherein each of the first and the second standard insert space satisfy size requirements mentioned in ARINC standards,
replacing the first galley monument assembly with a second galley monument assembly that includes a second outer wall and at least a first non-standard insert space, wherein the first outer wall and the second outer wall have the same dimensions, wherein the first non-standard insert space is defined in the second galley monument in the same location as the first and second standard insert spaces in the first galley monument, and
inserting a first non-standard insert into the first non-standard insert space,
wherein the first standard insert space includes a first standard insert electrical connector that connects to a first monument electrical connector,
wherein the second standard insert space includes a second standard insert electrical connector that connects to a second monument electrical connector,
wherein the first non-standard insert space includes a first non-standard insert electrical connector that connects to one of the first or second monument electrical connectors.