Patent ID: 7934753

Claim:
An aircraft comprising: a supply chamber; and a cabin chamber, at least one first conduit element positioned in the supply chamber and at least one second conduit element positioned in the cabin chamber, a separation element separating the supply chamber and the cabin chamber from each other; a connection element at the separation element and connecting the at least one first conduit element to the at least one second conduit element, wherein the connection element comprises a connection part which comprises a fastening element fastening together the first and second conduit elements, the fastening element is a plug-type lock and/or a snap lock configured for fastening the second conduit at the fastening element, wherein at least the fastening element is configured for fastening the at least one second conduit element of the cabin chamber within the connection part and wherein the connection element at the separation element is configured to not protrude from the separation element into the cabin chamber.