Patent ID: 9688406
Date: 2017-06-27
CPC Classifications: B64D

Claim:
1. An interior component for an interior room of an aircraft, comprising: a body having a first surface and a second surface; and a multitude of functional modules forming a passenger service unit; wherein the second surface is arranged opposite the first surface; wherein the second surface comprises a continuous recess in a longitudinal direction along the entire length of the interior component; wherein the multitude of functional modules are arranged one after another in the recess in the longitudinal direction of the interior component, such that a first front surface of the functional module arranged frontally in the longitudinal direction closes flush with a first front surface of the body, and wherein the recess and the functional modules are configured such that the functional modules are pushable along the recess from the first front surface of the body to a second front surface of the body; wherein the multitude of functional modules comprise an identical extension in the longitudinal direction; and wherein a length of the body corresponds to an integral multiple of the length of a functional module.